| Entries |
| Document | Title | Date |
|---|
| 20080201952 | METHOD OF MANUFACTURING A VEHICLE - A method of manufacturing a vehicle. A set of vehicle body structure components is assembled with interlocking mating features. | 08-28-2008 |
| 20080244907 | METHOD OF MANUFACTURING A MOUNTING FRAME FOR A VEHICLE WIND DEFLECTOR - The present invention provides a method of mounting a fairing to a roof of a vehicle and a method of manufacturing a mounting frame for mounting a fairing to a roof of a vehicle. The mounting frame has a lower portion for mounting to the roof of the vehicle and an upper portion for securing the fairing. The mounting frame is formed by determining a contour of the mounting surface, creating a mould for moulding the lower portion of the mounting frame having a bottom edge configured generally complementary to the contour of at least a portion of the mounting surface, and moulding an upper portion affixed to the lower portion and having an outer face configured generally complementary to an interior surface of the fairing. | 10-09-2008 |
| 20080295334 | APPARATUS AND METHODS FOR SECURING A FIRST STRUCTURAL MEMBER AND A SECOND STRUCTURAL MEMBER TO ONE ANOTHER - Apparatus and methods for securing a first structural member and a second structural member to one another. In one embodiment a two-piece fitting is provided. The fitting includes a variable gap between attachment surfaces, enabling the fitting to accommodate structural members of variable thickness. The fitting also includes overlapping sections that provide increased resistance to pull-off loads and impact loads. The configuration of the fitting advantageously simplifies the assembly process and preserves the integrity of the adhesive to form a strong joint. | 12-04-2008 |
| 20080295335 | VEHICLE FRAMING SYSTEM FOR PLURALITY OF VEHICLE BODY STYLES - A method for randomly interchanging up to four pairs of side framing gates at a framing station of a vehicle for randomly interchanging up to four pairs of side framing gates at a framing station of a vehicle assembly line while maintaining a predetermined build cycle time interval of the assembly line. The method includes positioning first and second carousels on opposite sides of the assembly line upstream of the framing station and third and fourth carousels on opposite sides of the production line downstream of the framing station. The method further includes providing a first linear track structure extending from the first carousel to a first side of the framing station, a second linear track structure extending from the second carousel to a second, opposite side of the framing station, a third linear track structure extending from the third carousel to the first side of the framing station, a third linear track structure extending from the third carousel to the first side of the framing station, and a fourth linear track structure extending from the fourth carousel to the second side of the framing station. The carousel are provided with at least two sides, possibly three sides, four sides or more, each side capable of receiving a framing gate. The method includes randomly interchanging framing gates positioned at the framing station by a combination of rotary movements of the carousels and linear movements of framing gates along the linear track structures. | 12-04-2008 |
| 20080307652 | Method For Manufacturing Bicycle Crank - A method for manufacturing a bicycle crank, comprises the steps of: blowing air into a blowing opening at a lower end of a backbone so as to fixing the backbone; wherein the backbone has a first embedding portion; using a cutter to cut the backbone; and then form a second embedding portion in the end of the backbone having the blowing opening; winding an unidirectional carbon-fiber cloth around the backbone; adhering carbon-fiber adhesive sheet upon an outer side of the backbone; and heating the backbone so as to firmly secure the carbon-fiber adhesive sheet to the backbone. Furthermore before the blowing step, the method further comprises a step of forming a first embedding portion at one end of the backbone; and embedding a metal first tube into the first embedding portion. | 12-18-2008 |
| 20090038156 | METHOD OF MAKING A TUBULAR SUPPORT BAR FOR A DASHBOARD SUPPORT - In a method of making a tubular support bar for a dashboard support, a sheet metal blank is placed in a first forming tool and pressed in a first shaping step by a ram into a U-shaped cavity of a first bottom die to form a U-shaped member. While remaining in the first bottom die, the U-shaped member is provided with connecting elements in the form of weld nuts by a automated placement device. Subsequently, the U-shaped member is transferred to a second forming tool and undergoes a second shaping step between a top die and a second bottom die to form a slotted tube. The longitudinal edges of the slotted tube are then joined together to form the support bar. | 02-12-2009 |
| 20090064502 | METHOD FOR FORMING A BUMPER BEAM FOR A MOTOR VEHICLE - A method for forming a bumper beam includes providing an elongated piece of sheet metal having opposing end portions and an intermediate portion, bending the end portions with respect to the intermediate portion until the end portions are substantially perpendicular to the intermediate portion, bending a central section of the intermediate portion to form a protruding bulge in the intermediate portion after the bending the end portions, and bending side sections of the intermediate portion to move ends of the end portions adjacent to one another and adjacent to the protruding bulge after the bending the central section to from the bumper beam. The end portions form front walls of the bumper beam, the protruding bulge forms inner side walls and a web portion of the bumper beam, and the side sections form outer side walls and rear walls of the bumper beam. | 03-12-2009 |
| 20090133261 | CONFORMAL VACUUM CUP APPARATUS AND METHOD - During the manufacture an aircraft, a tool-carrying rail is removably attached to a rail-side surface of the aircraft with a vacuum cup. The tool-carrying rail includes a longitudinal axis to mount a tool. The vacuum cup is stiffened along a first axis transverse to the longitudinal axis of the tool-carrying rail and the vacuum cup is stiffened along a second axis parallel to the rail-side surface of the aircraft. To removably attach the tool-carrying rail, a perimeter of the vacuum cup is removably sealed to the rail-side surface of the aircraft against vacuum loss and a point on the rail is rigidly positioned with respect to a point on the rail-side surface of the aircraft. In addition, a vacuum source is coupled to a spatial volume occupying all of a space between the vacuum cup and the rail-side surface of the aircraft and the tool is slidably positioned along the longitudinal axis of the tool-carrying rail. | 05-28-2009 |
| 20090139091 | FIELD INSTALLATION OF A VEHICLE PROTECTION SYSTEM - A method for armoring a vehicle by placing ballistic material inside a part of the vehicle and adding a foam material on the ballistic material that adheres to, and stabilizes, the ballistic material to form a lightweight armor, where the ballistic material and the foam material can absorb energy associated with projectile impact. | 06-04-2009 |
| 20090217529 | TUBULAR COMPONENTS FOR AERONAUTICAL FUSELAGES AND PROCESSES AND JIGS FOR ITS MANUFACTURING - The present invention relates to a tubular-shaped component ( | 09-03-2009 |
| 20090217530 | METHOD FOR MOUNTING A SEAT PROVIDED WITH WEIGHT SENSORS ON A MOTORCAR FRAME - A method for mounting a seat including weight sensors on a motorcar frame. The method includes the rigid connection to the motorcar frame of a number of weight sensors, each of which rests on a flat resting area of the motorcar frame and is rigidly connected to the motorcar frame by a number of bolts fastened in threaded holes obtained through the motorcar frame itself. The motorcar frame is completed by leaving the resting areas rough, and after completing the construction of the motorcar frame, each rough resting area is subjected to precision machining by a machine tool, which includes a flattening by milling and subsequently a drilling and a threading to make the holes. | 09-03-2009 |
| 20090235527 | METHOD OF MANUFACTURING HANDGUARDS - An improved method for manufacturing hand guards, utilizing this method multiple sheets can be stacked and then clamped to a XY cutting table to cut multiple patterns therein, subsequently a forming tool or die is used to form complex 3 dimensional shapes in any XY, XZ, YZ or XYZ planes in a single operation. | 09-24-2009 |
| 20090235528 | METHOD FOR FORMING A FLEXIBLE SINGLE RAIL DRILLING SYSTEM - A method for manufacturing a mobile platform component that may involve attaching only a single rail to the mobile platform component, and positioning a carriage system having a main carriage and a secondary carriage on the rail. The main carriage may be positioned along a first axis of movement on the rail. The secondary carriage may be positioned along a second axis of movement perpendicular to the first axis of movement on the main carriage. The main carriage may be releasably secured to the secondary carriage, and the carriage system may be releasably secured to the mobile platform component. | 09-24-2009 |
| 20090277010 | Method for Production of a Link Rod with U-Shaped Cross Section from Sheet Metal for a Car Multi-Link Axle - A link rod with a U-shaped profile made from a one-piece sheet metal shell including two part shells and a back connecting said part shells. Bearing eyes are formed from a pair of aligned holes in the part shells. To obtain outer collars having inner bearing support surfaces for the bearing eyes with a slim-shaped construction of the link rod, the forming is performed stepwise by firstly producing the holes and bending the edges thereof to form the collars on one of the part shells which have not yet been brought parallel to each other by bending. Only then is what is to become the second part shell bent such as to be parallel to the first part shell. The holing and the bending of the edges of the holes on the second part shell is then carried out through the holes of the first part shell. | 11-12-2009 |
| 20090277011 | RIB FOR AIRCRAFT WING AND METHODS FOR THE MANUFACTURE THEREOF - There is provided a method of manufacturing a rib for an aircraft wing, the method comprising providing a billet of material for forming the rib, machining away material from all sides of the billet to form a rib for use in an aircraft, the rib including a web that extends between first and second flanged portions, each flanged portion having a flange that facilitates fixing of the rib to another component of the aircraft, wherein the material that forms the web extends diagonally across the billet, the web having a first face on a first side and a second face on a second side opposite to the first side of the web, and the first flanged portion extends more to the first side of the web than to the second side and the second flanged portion extends more to the second side of the web than to the first side. | 11-12-2009 |
| 20090300919 | METHOD OF MANUFACTURING A VEHICLE FRAME ASSEMBLY INCLUDING AN INTEGRATED HITCH HAVING A COATING - A method of manufacturing a vehicle frame assembly including an integrated hitch having a coating of a material provided thereon includes the initial step of providing a vehicle frame assembly including an integrated hitch. A coating of a first material is provided on the integrated hitch. The coating of the first material provided on the integrated hitch is dehydrated, and a coating of a second material is provided over the coating of the first material provided on the integrated hitch. Lastly, the coating of the first material and the coating of the second material provided on the integrated hitch are cured. | 12-10-2009 |
| 20090313830 | METHOD, APPARATUS AND PLANT FOR MANUFACTURING SHELL STRUCTURES - According to the invention, a shell handling carriage ( | 12-24-2009 |
| 20090320292 | METHOD AND APPARATUS FOR FORMING AND INSTALLING STRINGERS - A hands-free method and related apparatus are used to shape, place and compact a composite stringer on a composite skin of an aircraft. A composite charge is placed on a tool assembly that used to shape the charge into a preformed stringer. With the stringer held on the tool assembly, the tool assembly is used to move the preformed stringer into proximity with the skin and both place and compact the stringer against the skin. Following compaction of the stringer, the tool assembly is removed and the skin and the stringer are co-cured. | 12-31-2009 |
| 20100011580 | METHOD AND APPARATUS FOR LAYUP PLACEMENT - Method and apparatus for layup placement on a layup structure is provided. The method includes iteratively loading a layup for the layup structure on a support frame of a saddle module; aligning the saddle module with a pre-selected registration position corresponding to a predetermined application path on the layup structure; and impressing the layup into forced contact with the layup structure along the predetermined application path using a predetermined application force. The apparatus includes a plurality of saddle modules configured to operate in unison, wherein the plurality of saddle modules is configured to receive a pre-selected composite material layup. | 01-21-2010 |
| 20100011581 | METHOD OF MANUFACTURING A VEHICLE FRAME ASSEMBLY - A vehicular frame assembly is manufactured by initially providing a vehicular frame assembly that is formed from a plurality of structural members, each having an inherent torsional rigidity. Then, a desired inherent torsional rigidity can be determined for at least one of the plurality of structural members. Lastly, the at least one of the plurality of structural members can be deformed to achieve the desired inherent torsional rigidity. Alternatively, the vehicular frame assembly can be manufactured by initially providing a plurality of structural members, each having an inherent torsional rigidity. A desired inherent torsional rigidity can be determined for at least one of the plurality of structural members, and the at least one of the plurality of structural members is deformed to achieve the desired inherent torsional rigidity. Lastly, the plurality of structural members can be assembled to form the vehicular frame assembly. | 01-21-2010 |
| 20100031509 | Method for Producing a Fuselage Cell of an Aircraft - The invention relates to a method for producing at least one fuselage cell of an aircraft with the following steps: at least partial production of surface protection and thermal insulation in the region of the at least one shell part, at least partial introduction of technical outfitting systems | 02-11-2010 |
| 20100043231 | METHOD FOR MACHINING A STRUCTURAL MEMBER HAVING AND UNDULATING WEB - Machined structural members and methods for forming the same are disclosed. In one embodiment, a structural member includes a web portion that extends in a first direction that includes a non-planar portion, and a first flange portion coupled to the web portion that extends in the first direction. A second flange portion is coupled to the web portion that also extends in the first direction. The first flange portion and the second flange portion are spaced apart in a second direction that is approximately perpendicular to the first direction. The web portion and the first and second flange portions are integrally formed as a unitary, monoblock component. | 02-25-2010 |
| 20100083504 | METHODS OF MANUFACTURING STRUCTURAL PANELS - Structural panels for use in manufacturing aircraft fuselages and other structures are disclosed herein. In one embodiment, a structural panel configured in accordance with the invention includes a skin and at least first and second stiffeners. The first stiffener can have a first flange portion mated to the skin and a first raised portion projecting away from the skin. The second stiffener can have a second flange portion mated to the skin and a second raised portion projecting away from the skin. At least one of the first flange portion of the first stiffener and the second flange portion of the second stiffener can extend toward the other of the first flange portion and the second flange portion to form an at least approximately continuous support surface to which a frame can be attached. | 04-08-2010 |
| 20100088896 | MANUFACTURING PROCESS FOR A SECTION OF AIRCRAFT FUSELAGE IN COMPOSITE MATERIAL - The disclosed embodiments relate to a method for manufacturing an aircraft fuselage section of composite material that comprises the following operations manufacturing a one-piece section; cutting the section longitudinally; spreading apart two edges located on the two sides of the cut; reassembling the section and making a longitudinal joint with the two edges overlapping. The disclosed embodiments also relate to a section made in accordance with this method. | 04-15-2010 |
| 20100095527 | STEEL BEAM AND METHOD OF MANUFACTURE AND USE - The present invention generally relates to a beam suitable for providing support to, for example, an automobile body. More specifically, the present invention relates to a steel boxed I-beam structure having compound curves, formed without use of a dedicated fixture or jig. Typically, the steel boxed I-beam structure provides a strong support that can be manufactured with a minimum of effort, and without the use of heavier shop machinery. | 04-22-2010 |
| 20100101090 | Method of Making a Composite Component and Apparatus - A method of making a composite component and the composite component is disclosed. The composite component can comprise multiple portions with different materials. By configuring the composite component with different materials, the weight of the composite component can be reduced while maintaining the strength and support of the composite component for a cockpit assembly. Furthermore, the method provides for an increase in the efficiency of the die casting process used to create the composite component. | 04-29-2010 |
| 20100115773 | PREFORM, HYDROFORMING METHOD, AND HYDROFORMED PRODUCT - A preform having edges overlapped and jointed, two outer members for forming outer surfaces of a hydroformed product, and reinforcement members for forming reinforcement ribs that divide a hollow cross section of the hydroformed product, including a joint formed by, when more than three sheet materials for forming the outer members and the reinforcement members are overlapped together, welding a first sheet material on a surface of the overlapped sheet materials to a second sheet material positioned inside the first sheet material, and a space disposed and aligned with a joint plane between the second sheet material and a third sheet material located inside the second sheet material during the welding process. | 05-13-2010 |
| 20100162567 | MOUNTING DEVICE FOR AN AIRCRAFT - The invention relates to a mounting device in an aircraft. In one aspect of the invention, a method is disclosed for assembling a metal securement member of the mounting device. In another aspect of the invention, a mounting device is disclosed. In another aspect of the invention, a method is disclosed for installing and using a mounting device in an aircraft. | 07-01-2010 |
| 20100180443 | Method For Fabricating Structural Propellants - A vehicle includes at least one polyoxymethylene structural support member. The polyoxymethylene structural support member includes a polyoxymethylene component that is a propellant that provides thrust to the vehicle upon pyrolysis or combustion of the polyoxymethylene component of the product of pyrolysis of the polyoxymethylene component. The vehicle can be a satellite or other type of spacecraft. | 07-22-2010 |
| 20100180444 | CROSSMEMBER CENTER SECTION - A center section for a crossmember of a vehicle chassis comprises a driveshaft hoop, crossmember attachment areas extending generally from opposing sides thereof, and trailing arm mounts on either side of the driveshaft hoop for attachment of one or more trailing arms to the center section. The crossmember attachment areas have heights that allow attachment of crossmember portions to the center section at offset heights. A method of constructing a crossmember of a vehicle chassis comprises providing a center section having crossmember attachment areas of predetermined heights extending generally from opposite sides of a driveshaft hoop, and attaching crossmember portions within the crossmember attachment areas at heights that are offset from each other. | 07-22-2010 |
| 20100192376 | METHOD AND DEVICE FOR PRODUCING A FUSELAGE CELL OF AN AIRPLANE - The invention relates to a method for the economic production of entire fuselage cells of airplanes and to a site for carrying out the method. Differing from the conventional sectional assembly according to the invention separate shells (shell components) are attached to a substantially completed cockpit section and/or rear section. At this the half shell construction and the four shell construction as well as a combination hereof can be applied. Alternatively, the cockpit section and the rear section as well as the central wing box section can be aligned and positioned to each other in a site forming gaps in longitudinal direction. Subsequently, the shell components as well as the floor framework sections are adjusted circularly revolving between the sections and are ideally simultaneously connected to these by means of at least four cross-seams and a plurality of longitudinal seams. | 08-05-2010 |
| 20100192377 | METHOD FOR PRODUCING A FUSELAGE AIRFRAME OF AN AIRCRAFT - Disclosed is a method for producing a fuselage of an aircraft, wherein several fuselage sections that are arranged one behind another are joined together, comprises the following steps:
| 08-05-2010 |
| 20100205806 | Method To Produce Suspension Module And Frame That Reduces Need For Final Alignment - A method of assembling a frame and suspension module includes determining locations of first and second suspension member supports on the frame. Target positions of first and second connections between the frame and third and fourth suspension members are defined based on the locations of the first and second suspension member supports. Target positions of third and fourth connections between a fifth suspension member and the first and second suspension members are defined based on the locations and the target positions of the first and second connections. The first and second suspension members are connected to the frame at the locations. The third and fourth suspension members are connected to the frame at the first and second target positions. The fifth suspension member is connected to the first and second suspension members at the third and fourth target positions. | 08-19-2010 |
| 20100218375 | METHOD OF PRODUCING METAL CLOSED-SECTION MEMBER - The present invention provides a method capable of accurately producing a metal closed-section member in a relatively simple manner. The method of producing a metal closed-section member formed in a cross-sectionally closed shape, from a metal plate workpiece, comprises a first press-forming step of using a first forming die assembly to press-form the plate workpiece into a convex shape, and a second press-forming step of providing a second forming die assembly, and, after the first press-forming step, under a condition that the press-formed plate workpiece is positioned between a receiving die and a core die of the second forming die assembly, causing relative movement of the core die with respect to the receiving die to press-form the press-formed plate workpiece into a given shape so that two sidewalls of a convex-shaped portion of the press-formed plate workpiece formed on respective ones of both sides of a top wall of the convex-shaped portion of the press-formed plate workpiece during the first press-forming step are displaced toward an inward side of the press-formed plate workpiece and cross-sectionally closed together. | 09-02-2010 |
| 20100218376 | METHOD OF ASSEMBLING A DE-ICING MAT ON A PIECE OF WING STRUCTURE - A method of assembling a de-icing mat ( | 09-02-2010 |
| 20100242284 | MIXED METAL MAGNETIC PULSE IMPACT BEAM - An impact beam assembly includes a beam of high-strength steel, and a pair of end brackets constructed of a dissimilar material than the high-strength steel. The brackets are locally deformed onto the beam to thereby surround a portion of the beam. Once deformed, the brackets define a flat section suitable for welding to a vehicle door panel, as well as a section for retaining the beam. The beam can include a surface feature suitable for retaining the beam to the end brackets. A method of reinforcing a vehicle door assembly includes positioning the beam with respect to the end brackets such that the brackets surround a portion of the beam, and then activating a magnetic pulse coil (MPC) to deform an overlapping portion of the brackets onto the beam. The brackets are then attached to a surface of the door assembly to reinforce the door assembly. | 09-30-2010 |
| 20100257738 | REINFORCEMENTS, BAFFLES AND SEALS WITH MALLEABLE CARRIERS - There is disclosed a process of forming reinforcements, baffles and seals having malleable carriers. The process typically includes application of an activatable material to a malleable carrier and contouring of the activatable material the malleable carrier or both. | 10-14-2010 |
| 20100287776 | METHOD FOR ASSEMBLING A PART OF A METAL MATERIAL AND A PART OF A COMPOSITE MATERIAL USING A FASTENER - A method for assembling a part of a metal material and a part of a composite material, the junction of the two parts being achieved through a fastener having a substantially constant section and received in a first hole formed in the part of a metal material and a second hole formed in the part of a composite material. According to the disclosed embodiments and before assembling the aforementioned parts, the method includes: an expansion step for generating a field of compression stresses at the periphery of the first hole and locally in the material constituting the part of a metal material using an expansion tool; a single boring step for making the first hole and the second hole with a diameter Ø | 11-18-2010 |
| 20100287777 | Air Bag Deployment Chute and Method - An integrated air bag support structure that includes a support base for attachment to the rear side of a substrate. The support base is configured to surround a door support panel and both are configured for attachment to the rear side of a substrate in an area that is pre-weakened to define an air bag deployment door in a vehicle instrument panel or a steering wheel air bag module. The upper surfaces of the support base and door support panel are attached to the rear surface of the substrate, and a test tab extends from the base that is attached to the rear surface of the substrate in the same manner as the support base and the door support panel. The test tab has an unattached extension portion for the purpose of gripping and pulling to test the integrity of the attachment without affecting the attachment of the support panel. | 11-18-2010 |
| 20100313422 | PLATFORM TRAILER WITH EXTRUDED FLOOR PANEL CROSS MEMBERS - A platform trailer includes first and second aluminum beams. The first and second beams are defined with an arch. A platform is supported on the first and second beams. The platform includes a plurality of extruded aluminum panels that each extend from a left lateral end abutted with the left side rail to a right lateral end abutted with the right side rail. The extruded aluminum panels are abutted in series with the first end wall of one panel abutted with the second end wall of an adjacent abutted panel such that the respective upper walls of adjacent abutted panels of the platform together define an upper, cargo supporting surface of the platform. The platform is arched to correspond with the arch of the first and second beams. A method for constructing the platform trailer is also disclosed. | 12-16-2010 |
| 20110061237 | Tubular B-Pillar to Stamped Rocker Joint and Method of Assembling The Same - A pillar to rocker joint assembly comprising a tubular pillar having a pinched flange near a lower end of the pillar is joined to a rocker assembly including a side sill and rocker reinforcement. A method of making a pillar to rocker joint assembly that comprises a vehicle structural support is formed by welding a structural support pillar to an outer body panel through an access opening in the pillar and welding a rocker reinforcement to a side sill. The rocker reinforcement is welded to the pillar through an access opening in the side sill, an access hole in the body outer panel, and an access opening in the pillar that is vertically spaced relative to the first access opening. A bottom flange of the B-pillar is welded to a lower edge flange of the rocker reinforcement and a lower edge flange of the side sill. | 03-17-2011 |
| 20110119919 | Determinant Assembly System for Manufacturing Objects - A Method and apparatus may be present for processing parts. A first part may be positioned in a first position. A first number of features may be formed on the first part using a feature forming system at a number of points for attachment to a second part. The second part may be positioned in a second position relative to the first position for assembly of the first part with the second part. A second number of features may be formed on the second part at the number of points for attachment to the first part using the feature forming system. | 05-26-2011 |
| 20110119920 | TAPERED STABILIZER BAR HAVING CONTINUOUSLY CHANGING CROSS-SECTION AND METHOD FOR MANUFACTURING THE SAME - A method for manufacturing a stabilizer bar for a vehicle includes cutting a stabilizer bar material having a round bar-shaped configuration, heating both end portions of the cut stabilizer bar material to be formed as leg bars of the stabilizer bar, rolling both side surfaces of each of both heated end portions of the stabilizer bar material so that both side surfaces are tapered, rotating the stabilizer bar material about an axis thereof between rollers to taper both remaining non-rolled side surfaces of each of both end portions of the stabilizer bar material to be formed as the leg bars of the stabilizer bar, so that each or both end portions of the stabilizer bar material has an elliptical cross-section, forming eyes on distal ends of the stabilizer bar material, and bending the stabilizer bar material into the shape of the stabilizer bar. | 05-26-2011 |
| 20110258854 | METHOD AND APPARATUS FOR REINFORCING A SUBSTRATE OR A FABRIC IN A CORE STRUCTURE OF A COMPONENT, E.G. FOR AN AIRCRAFT OR SPACECRAFT, COMPONENT, E.G. FOR AN AIRCRAFT OR SPACECRAFT, AND AIRCRAFT OR SPACECRAFT - A method for reinforcing a substrate or textile of a core structure of a component with the following method steps: a continuous semi-finished product is fed, via a feed means, into a cartridge of a conveying means which comprises a plurality of cartridges; the continuous semi-finished product is cut to length using a cutting means in order to produce a cut, reinforcing semi-finished product which is received in the cartridge; the cartridge is conveyed to a machining means; the cut, reinforcing semi-finished product is sharpened using the machining means; the cartridge is conveyed to a textile or substrate to be reinforced of a core structure; and the sharpened semi-finished product is shot into the textile or substrate of a core structure by a stud-shooting means. | 10-27-2011 |
| 20110265330 | METHOD AND APPARATUS FOR MANUFACTURING AN AXLE FOR A VEHICLE - A datum is created in an axle housing. A finished brake flange is welded to the axle housing with reference to the datum to make an axle sub-assembly. The axle sub-assembly is fixed to a first part of a machine. A finished spindle is supplied to a second part of the machine. The spindle is welded to the axle sub-assembly with reference to the datum. A dial indexing table is rotated to a first position. An axle is placed on the dial indexing table with its longitudinal axis oriented vertically. The dial indexing table is rotated to a second position, wherein the axle aligned with a CNC machine. A machining operation is performed on the axle with the CNC machine. The dial indexing table is rotated to a third position. The axle is removed from the dial indexing table. An axle and an apparatus for manufacturing an axle are described. | 11-03-2011 |
| 20110302784 | AIRCRAFT STRUCTURE MANUFACTURING APPARATUS - A first lift stand is provided with a first supporting unit to support a first portion of a positioning object, and a first servo system to drive the first supporting unit in a vertical direction. A second lift stand is provided with a second supporting unit to support a second portion of the positioning object, and a second servo system to drive the second supporting unit in the vertical direction. A third lift stand is provided with a third supporting unit to support a third portion of the positioning object, and a third servo system to drive the third supporting unit in the vertical direction. A fourth lift stand is provided with a fourth supporting unit to support a fourth portion of the positioning object, and a fourth servo system to drive the fourth supporting unit in the vertical direction. | 12-15-2011 |
| 20120011721 | METHOD OF LIFTING A CAB ONTO A CHASSIS - A method of mounting a vehicle cab onto a vehicle chassis is provided. The method includes providing at least one structural anchor point on an upright wall of the vehicle cab, connecting a lifting device to the structural anchor point, and using the lifting device to lift the vehicle cab and mount it on the vehicle chassis. | 01-19-2012 |
| 20120017440 | METHOD OF REINFORCING A MOTORCYCLE FRAME DURING CONVERSION TO A MOTORIZED TRICYCLE - A method of reinforcing an L-shaped motorcycle frame during conversion to a motorized tricycle. The L-shaped motorcycle frame is an inverted L-shape with a horizontal portion and a vertical portion. A tricycle frame is provided having spaced apart side plates with a forwardly and downwardly extending portion which terminates in a mounting attachment. The side plates are fastened to opposed sides of the horizontal portion of the L-shaped motorcycle frame. The mounting attachment is secured to the vertical portion of the L-shaped motorcycle frame. This forms a triangular truss with the forwardly and downwardly extending portion of the side plates of the tricycle frame angled between the horizontal portion and the vertical portion to provide rigid support to the L-shaped motorcycle frame. | 01-26-2012 |
| 20120023748 | METHOD OF MAKING A SHAPED METAL PART FOR A MOTOR VEHICLE COMPONENT - In a method of making a shaped metal part for a motor vehicle component, a blank is made from a steel alloy containing, in weight percent: carbon (C) 0.18% to 0.3%, silicon (Si) 0.1% to 0.7%, manganese (Mn) 1.0% to 2.5%, phosphorus (P) maximal 0.025%, chromium (Cr) 0.1 to 0.8%, molybdenum (Mo) 0.1 to 0.5%, sulfur (S) maximal 0.01%, titanium (Ti) 0.02% to 0.05%, boron (B) 0.002% to 0.005%, aluminum (Al) 0.01% to 0.06%, balance iron and impurities resulting from smelting, The blank is heated to a temperature between 900° C. and 950° C., and formed in a press tool into a formed part which is quenched and tempered while still being in the press tool. At least one region of the formed part is then annealed to become soft by a heating operation within a time interval of less than 30 seconds to thereby provide the region with higher ductility. | 02-02-2012 |
| 20120066907 | INSTALLATION FOR MAKING A FUSELAGE PORTION OF AN AIRCRAFT - In the method of making an aircraft a mandrel is caused to pass through frames carried by a magazine; and as it passes through, the frames are transferred onto the mandrel. | 03-22-2012 |
| 20120073137 | AIRCRAFT RIB-SPAR JOINT - A method of forming a rib-spar joint during assembly of an aircraft wing, the method comprising: providing a spar with a fixedly attached rib post, the rib post having a first coordination feature; providing a rib having a web with a first tooling feature; providing a tooling component having a second tooling feature for cooperating with the first tooling feature, a second coordination feature for cooperating with the first coordination feature, and a plurality of drill bushings; fixedly attaching the tooling component to the rib web by aligning the first and second tooling features; aligning the rib with the spar by aligning the first and second coordination features; drilling fastener holes in the rib and the rib post off the drill bushings of the tooling component; removing the tooling component from the rib web; and fastening the rib to the rib post using the fastener holes to form a rib-spar joint. The method may be applied to form front and/or rear rib-spar joints. | 03-29-2012 |
| 20120102740 | HULL FLOOR SUPPORT SYSTEM - A method of making and installing a boat rib making a portion of a boat comprising the steps of: shearing a flat piece of metal to cut to a size; attaching the flat piece of metal to a moveable carriage; cutting apertures in the flat piece of metal; cut final outside dimensions in the flat piece of metal; bending said flat piece of metal to create a rib; and securing said rib to a floor. | 05-03-2012 |
| 20120110852 | Fuel tank fuel system - The present invention provides a fuel draw and return system including a plate, a first fuel tube secured to the plate, and a second fuel tube secured to the plate, wherein the first and second fuel tubes are secured to one another and to the plate to define a triangular shaped connection configuration. | 05-10-2012 |
| 20120124839 | CUT SHEET STOCK MYCELIUM AND METHOD - A method of making a vehicle part, including growing a live mycelium mat from interwoven hyphae. The mycelium mat is cured to terminate mycelium growth. The mycelium is cut into a single structural component without further processing for use in a vehicle. | 05-24-2012 |
| 20120174406 | METHOD AND PRODUCTION PLANT FOR MAKING COMPONENTS FOR A MOTOR VEHICLE - In a method of making a component for a motor vehicle, a metal part in the form of a plate, semifinished product, or a formed part, is heated in a fluidized bed of a fluidized bed furnace. The fluidized bed is being fluidized by a fluid, e.g. gas. Subsequently; the metal part is subjected to a forming, hardening or aging process. | 07-12-2012 |
| 20120174407 | Snowmobile ski and method - A runner for a snowmobile ski is fabricated from flat metal plate stock and incorporates mounting features for securing the runner to the ski and a wear strip of a relatively harder material provided on and projecting from a lower surface of the runner body. A quick release mounting system is provided for attaching the runner to the ski, including quick installation and release wedge mounting systems. The thin runner blade and wear strip are of the same thickness and are joined by a brazed joint. The invention contemplates a method of fabricating the runner and a method of mounting the runner. | 07-12-2012 |
| 20120192425 | METHOD FOR ATTENUATING DRIVELINE VIBRATIONS - A method for attenuating vibration in a driveline having a shaft assembly that transmits torque between first and second driveline components. The shaft assembly can have a hollow shaft member and at least one liner. The liner has a mass and a stiffness that are tuned such that the liner is a tuned resistive absorber for attenuating shell mode vibrations as well as at least one of a tuned reactive absorber for attenuating bending mode vibrations and a tuned reactive absorber for attenuating torsion mode vibrations. The tuned liner is inserted into the shaft member. | 08-02-2012 |
| 20120216405 | LIGHT-WEIGHT, ROLL-BONDED HEAVY DUTY TRUCK FRAME MEMBER - A frame member for a frame assembly of a vehicle includes a first outer steel layer, a second outer steel layer and an aluminum core layer between the first outer steel layer and the second outer steel layer. The first outer steel layer, the second outer steel layer and the aluminum core layer are metallurgically bonded together. | 08-30-2012 |
| 20120227264 | MOUNT FOR INLET CHECK VALVE - A fuel system includes a fuel tank filler neck associated with a fuel tank. The fuel tank filler neck includes a fill tube for receiving a fuel-dispensing pump nozzle and a fuel conductor interconnecting an interior region of the fuel tank and a passageway formed in the fill tube. | 09-13-2012 |
| 20120240407 | URETHANE ISOLATION MOUNT AND METHOD OF MOUNTING FOR VEHICLE DIFFERENTIALS - A urethane isolation mount secures a vehicle's differential while dampening or isolating noise, vibration, and movement between the differential and the remainder of the vehicle. The urethane isolation mount may comprise one or more resilient urethane materials. The urethane isolation mount may also have an opening to accept a support stem of the differential. The opening may have a wider bore and a narrower bore to provide a step to which a fastener may secure the support stem to the urethane isolation mount. The urethane isolation mount provides increased reliability and greatly reduces, if not eliminates, repair costs for replacement differential mounts when installed. | 09-27-2012 |
| 20120246938 | DEVICE AND METHOD FOR ALIGNING AND INSERTING A THREADED FASTENER - A device and method for aligning and inserting a threaded fastener into a threaded hole. The device contains a base and a rail extending up from the base. A gearbox may be attached to the rail such that the gearbox can travel along the rail between a fastener loading position, a fastener install position, and a fastener realigning position. A socket assembly is connected to or otherwise associated with the gearbox and includes a drive socket that is adapted to accept the threaded fastener and an input shaft which is adapted to translate rotational motion to the output socket. A spring mechanism is attached to the gearbox and contains a spring that will compress when the gearbox travels into the fastener realigning position. A compressible washer may be interposed between the output shaft and the drive socket of the socket assembly so that the central axes of these components may be misaligned without causing damage or disrupting the alignment process. | 10-04-2012 |
| 20120291285 | Aircraft Structure for High Capacity Pull Off - A method and apparatus comprising a composite elongate member, a channel, and a number of composite structures. The composite elongate member has a side configured for attachment to a structure. The channel is on the side of the composite elongate member and extends along a length of the composite elongate member. The number of composite structures is configured for placement in the channel and to attach a portion of the side of the composite elongate member to the structure. The number of composite structures is configured to increase a capacity of the composite elongate member to withstand forces that pull the composite elongate member away from the structure. | 11-22-2012 |
| 20130000123 | METAL BODIES CONTAINING MICROCAVITIES AND APPARATUS AND METHODS RELATING THERETO - Monolithic metal bodies (e.g., hard aluminum alloys) comprising a continuous microcavity contained within the body are disclosed. The ratio of the cross-sectional area of the metal body to the cross-sectional area of the microcavity may be not greater than 10. The produced metal bodies may be used in structural applications (e.g., aerospace vehicles) to monitor or test the integrity of the metal body. | 01-03-2013 |
| 20130036611 | MANUFACTURING A VIBRATION DAMPED LIGHT METAL ALLOY PART - A method of manufacturing a non-ferrous, light metal alloy vibration-damped part for a vehicle chassis includes introducing a polymer insert into a cavity formed in the part. The polymer insert may be introduced into the cavity by separately fabricating the polymer insert and then sliding or maneuvering the insert into the cavity or by injecting a liquid polymer material into the cavity and then solidifying and shrinking the liquid polymer material into the polymer insert. The vibration-damped light metal alloy part can damp vibrations that originate within or are imparted to the part when such vibrations effectuate relative contacting frictional movement between an exterior surface of the polymer insert and an interior surface of the cavity. | 02-14-2013 |
| 20130133202 | Fire Resistance For Optically Transparent Thermoplastics - A fire retardant, transparent panel and method of making the panel, that is especially well suited for use on mobile platforms, and particularly on aircrafts. The panel is a composite of a transparent matrix and a plurality of fire-retardant nanoparticles. The nanoparticles have a diameter less than the visible spectrum of light, and in one form between about 0.1 nm to about 400 nm in diameter. The nanoparticles may be arranged randomly or in predetermined patterns within the matrix during manufacturing of the panel. The panel is lightweight, transparent and yet highly fire retardant. | 05-30-2013 |
| 20130152397 | AUTOMATED ASSEMBLY OF PANELIZED AIRCRAFT FUSELAGES - A facility for assembling aircraft fuselages comprises a plurality of movable cradles. Each cradle is configured to support a fuselage keel structure and assemble a panelized fuselage in a single upright build position. | 06-20-2013 |
| 20130152398 | HOLE DEPTH MEASUREMENT DEVICE - A plastic hand-held measuring device, can measure the depth of a hole or bore or the length of a fixing, having particular application with composite aircraft components. A hook or tang, at the end of an elongate portion, can engage with the far end of the bore allowing the depth ascertained from a first measurement scale. A first formation can engage with a fixing, allowing measurement of the length of the fixing from a second measurement scale. A plastic slide can abut against a portion of the component to be measured and indicate the distance on the measurement scale that corresponds to the length of the dimension being measured. The slide may be arranged to engage with successive indexed formations along the length of the device, so that it is inclined to remain in a position corresponding to an indexed formation. | 06-20-2013 |
| 20130160295 | METHOD, APPARATUS AND COMPUTER PROGRAM PRODUCT FOR DETERMINING THE STRAIN INDUCED AT A SELECTED POINT IN A STIFFENED PANEL STRUCTURE IN RESPONSE TO A LOAD, TAKING INTO ACCOUNT ONE OR MORE OUT OF PLANE (OOP) EFFECTS - A method, apparatus and computer program product is disclosed for determining the strain induced at a selected point in a stiffened panel structure in response to a load, taking into account one or more out of plane (OOP) effects. | 06-27-2013 |
| 20130185941 | METHOD FOR MANUFACTURING VEHICLE BODY FRAME - A method of manufacturing a vehicle body frame of the present invention is a method of manufacturing a vehicle body frame including a roof structure, side structures that face each other, and a floor structure. The method includes a primary joining step of butt-joining only one set of face plates among the inner face plates and outer face plates of the plurality of panel boards that form the side structures, and manufacturing intermediate bodies of the side structures; a structure joining step of joining the roof structure, the floor structure, and the intermediate bodies; and a secondary joining step of joining, after the structure joining step, the other set of face plates among the inner face plates and the outer face plates of the plurality of panel boards that form the intermediate bodies to complete the side structures. | 07-25-2013 |
| 20130205591 | COMPOSITE STRUCTURAL ELEMENT, PARTICULARLY FOR A VEHICLE SUSPENSION, AND METHOD FOR MANUFACTURING THE SAME - A method for manufacturing a structural element comprises steps of providing separate first and second half-shells made of at least one layer of composite material including a fibre-reinforced polymeric matrix, providing a core made of ductile material Joking the core to the first half-shell such that at least one cavity is defined inside the structural element, and joining the second half-shell to the first half-shell. | 08-15-2013 |
| 20130212883 | Riveting device for aircraft fuselages - A head of a riveting device—for Hi-Lite type rivets—of at least two components of a structure for installing automatically collars on pins previously inserted in the structure. The head comprises: a collar installation tool; a collar supply to supply collars to the collar installation tool; a tool actuating device; a linear displacement device to linearly move the tool during the threading operation; a withdrawal device arranged to withdraw the second part of the collars; a control arrangement configured to automatically perform the installation of collars on pins and after this the withdrawal of the second part of the collars, using tools and collars appropriate for the pins. Also a robot having as end-effector the head and to a method of riveting two components of an aircraft fuselage are provided. | 08-22-2013 |
| 20130219720 | METHOD FOR PRODUCING A CHASSIS COMPONENT - A method of producing a chassis component. The method including the steps of coating an outside of a structural component, coating an outside of a joint cartridge which has been preassembled as a joint, and permanently and securely connecting the structural component to the joint cartridge using a material bonding or joining process. | 08-29-2013 |
| 20130239412 | METHOD OF MANUFACTURING AN AUTOMOBILE SUSPENSION PART - For manufacturing an aluminum alloy automobile suspension part, an ingot material is heat treated and forged, a through-hole is formed therein and it is subjected to thermal refining. A minimum length between a rib end on a side of the through-hole and a through-hole end is made 6 mm or larger. | 09-19-2013 |
| 20130276309 | METHOD FOR IMPROVED REINFORCEMENT BAFFLING AND SEALING - A method for reinforcing, baffling or sealing a vehicle structure, comprising the steps of providing one or more materials having a horizontal axis, at least one terminating edge, and an initial length, forming openings in the one or more materials, and applying the one or more materials to location requiring reinforcement, baffling, sealing or any combination thereof. | 10-24-2013 |
| 20130276310 | METHODS AND SYSTEMS FOR COMPOSITE STRUCTURAL TRUSS - Methods and structures for a composite truss structure are provided. The structure includes a web formed of a plurality of sheets of composite material, each sheet including a first face and an opposing second face and each face including a length and a width. Each of the plurality of sheets are coupled to at least one other of the plurality of sheets face to face such that the length and width of each face substantially match the length and width of a face of an adjacent sheet. The plurality of sheets are formed to include an upper chord member, a lower chord member, and a plurality of web members extending therebetween. The structure also includes at least a first flange plate coupled to the web proximate an outer periphery of the web. | 10-24-2013 |
| 20130283616 | METHOD FOR THE PRODUCTION OF A HOT FORMED AND PRESS HARDENED MOTOR VEHICLE BODY STRUCTURE, AND MOTOR VEHICLE BODY STRUCTURE - In a method of making a motor vehicle body structure, at least one region of a sheet metal plate of hardenable steel sheet is pierced using a blanking and/or cutting process. The at least one region of the sheet metal plate is preformed into a preform which is then hot formed in a hot forming tool and press hardened. | 10-31-2013 |
| 20130305536 | Wire Basket Attachment Spade and Spring Wire Trap - A length of a substantially linear wire is attached to a substantially linear portion of a wire basket rim wire at two spaced-apart locations. The spaced-apart connections allow the two wires to deflect or act as springs when a notched basket-to-frame attachment clip is driven into a hole or loop formed by a detent in one of the wires. A wire basket having the linear spring wire attached to a rim wire can be permanently attached to a frame portion without tools or welding. | 11-21-2013 |
| 20140026421 | RETRACTABLE ROOM ACTUATION ASSEMBLY FOR RECREATIONAL VEHICLE - A slide-out or retractable room for a mobile living quarters, such as a recreational vehicle, is provided with actuating assemblies mounted on opposite side walls of the slide-out room and the adjacent wall of the main living area. The actuating assemblies include a pair of parallel gear racks mounted on the side wall, which are engaged by pinions rotated by torque shafts mounted on the main living quarters. Each torque shaft is rotated by a separate motor. A roller engages a bearing surface on the lower portion of the gear racks. Accordingly, the slide-out room is extended and retracted by rotating the torque shafts to cause the gear racks and the attached slide-out room to extend and retract. The weight of the slide-out room is supported by the rollers, thereby supporting the slide-out room off of the floor of the main living quarters as it extends and retracts. A synchronizing control operates the motors. | 01-30-2014 |
| 20140033536 | BOTTOM CHASSIS, METHOD OF FABRICATING THE SAME, AND LIQUID CRYSTAL DISPLAY INCLUDING THE SAME - Provided are a bottom chassis, a method of fabricating the same, and a liquid crystal display (LCD) including the same. The bottom chassis is fabricated using an aluminum alloy plate including, by weight, 0.5 to 1.5% manganese, 0.8 to 1.5% magnesium, 0.01 to 0.03% titanium, less than 0.02% molybdenum, and 96% or more aluminum. | 02-06-2014 |
| 20140041231 | MECHANICALLY FASTENED LARGE PRESSURIZED VEHICLE STRUCTURE - A first part, a second part, and a seal ring are fastened together to form a pressure structure configured for a spacecraft structure of a spacecraft, wherein the first part and the second part are each formed from a single workpiece. | 02-13-2014 |
| 20140059859 | METHOD OF ASSEMBLING A FRONT END ASSEMBLY OF A VEHICLE - A method of assembling a front end assembly of a vehicle is provided. The method includes integrally forming a positioning and reinforcement structure having a relatively rectilinear configuration comprising a top support member, a bottom support member, a first side member and a second side member. The method also includes detachably coupling a first wing structure to the first side member. The method further includes operably mounting a first fender assembly to a first side flange of the first wing structure. The method yet further includes operably coupling a centering bracket proximate the top support member. The method also includes locating and centering the positioning and reinforcement structure to a hood with the centering bracket. The method further includes fixedly securing the positioning and reinforcement structure to a radiator support disposed rearwardly of the positioning and reinforcement structure. | 03-06-2014 |
| 20140059860 | Method of mating composite structures without the use of through-structure fasteners - A method is described of mating composite structures by means of straps, thus avoiding the use of through-structure fasteners and the need to drill holes through the composite structure. This method is applicable to any composite structures, but is particularly valuable for light weight composite aircraft wing-to-fuselage connections. The method described herein is for this particular application. | 03-06-2014 |
| 20140068945 | Method Of Producing Tailored Tubes - A method of manufacturing a hollow structural frame rail includes rotating a tube relative to a tool to reduce an outside diameter of the tube at predetermined positions along the length of the tube. An elastomeric insert is positioned within the tube. The tube is bent at a location containing the insert. The bent tube is hydroformed to define a finished shape of the frame rail. | 03-13-2014 |
| 20140090252 | SYSTEM AND METHOD FOR MANUFACTURING A WING PANEL - A system and method are provided to automate the assembly of a wing panel, such as utilized by commercial aircraft. In the context of a system, a tacking cell is provided that is configured to tack one or more stringers to a skin plank. The system also includes a riveting cell configured to receive a tacked plank from the tacking cell and to rivet the one or more stringers to the skin plank. The system also includes a splicing cell configured to receive a plurality of riveted planks from the riveting cell and to attach one or more splice stringers to the plurality of riveted planks. Further, the system includes a side of body cell configured to receive a spliced panel from the splicing cell and to attach a side of body chord thereto to produce a wing panel. | 04-03-2014 |
| 20140115894 | DUAL FUNCTION MOVEMENT COMPONENT FOR AUTOMATED ASSEMBLY SYSTEMS - A pneumatic device may be configured and used to provide multiple movement related functions, such as in an automated assembly system. The pneumatic device may comprise a chamber; a sealing element configurable to contact a surface, to enable creating a seal around the chamber by application of pneumatic suction into the chamber; a biasing element configurable to push the sealing element away from the surface; and a pneumatic cushion configurable to expand by application of pneumatic inflow, thus urging the pneumatic device away from the surface. | 05-01-2014 |
| 20140115895 | Method for Producing a Component or a Component Composite Consisting of a Plurality of Components, Using a Camera for Detecting the Position of a Component - A method produces a component, particularly a body component for a vehicle, or a component composite consisting of several components. The steps include forming a metal plate in a forming tool, particularly in a deep-drawing die, producing a reference marking at a predefined location of the metal plate, rough positioning of the formed metal plate by a positioning device such that the reference marking is situated in a predefined space area, identifying the reference marking of a position recognition device, such as a camera system, the position recognition device generating position data corresponding to the position of the reference marking, positioning of a first fixing element at the location of the reference marking based on the position data by an electronically controlled positioning device, and connecting the first fixing element with the formed metal plate, particularly by welding. | 05-01-2014 |
| 20140115896 | Circumferential Movement Device - The invention relates to circumferential movement field, including all circumferential movement devices such as transport vehicle, toy vehicle, space vehicle, blender etc, especially for energy-saving vehicles utilizing force of gravity. The energy-saving vehicle utilizes force of gravity as driving force, the vehicle body connects with the wheel by swing structure method or eccentric swing structure to utilize force of gravity more efficiently. The invention also provides solutions about two-wheel gravitational vehicle and multi-wheel vehicle and train connected by integrated vehicles or two-wheel vehicles. | 05-01-2014 |
| 20140123495 | BONDING OF ROOF PANELS - A method for attaching a roof panel to a roof rail of a vehicle bodyside frame, wherein the roof rail prohibiting access to an underside of an area at which the roof panel attaches to the roof panel, can include applying a single-component adhesive to a roof rail or to a portion of a roof panel that rests on the roof rail, placing the roof panel onto the roof rail, attaching the roof panel to the roof rail using single-sided spot welds, and heating the roof panel and vehicle bodyside frame to a temperature that cures the single-component adhesive. | 05-08-2014 |
| 20140137412 | METHOD OF PRODUCING DOOR FRAME - A method of producing a door frame, which includes a tubular portion which is positioned on a vehicle interior side and has a closed cross-sectional shape, a design portion which is positioned on a vehicle exterior side, and a connecting portion which connects the tubular portion and the design portion; the method includes forming a frame body having a uniform cross section by roll-forming a metal sheet, the frame body including the tubular portion, the design portion and the connecting portion; and varying a width of the tubular portion by press-deforming a section of the tubular portion toward the vehicle interior side. | 05-22-2014 |
| 20140144023 | Method and Apparatus for Drive Shaft Extension - A method and apparatus are provided for extending the length of a vehicle without the need to rebalance the original drive assembly. The method includes disconnecting the front drive shaft segment from the vehicle transmission, extending the length of the vehicle frame, and inserting a drive shaft extension segment which includes: a rigid tubular shaft rotatable about a longitudinal axis; a universal joint mounted at the tubular shaft front end and having a front flange configured for mounting to the transmission; and a bearing assembly mounted to the tubular shaft. The extension segment rear end includes a rearward facing flange configured for mounting to a forward facing flange of the front drive shaft segment that was disconnected from the vehicle transmission. The extension segment is installed in the vehicle between the vehicle transmission and the front drive shaft segment without the need to rebalance the original drive assembly. | 05-29-2014 |
| 20140144024 | Method Of Welding Work Pieces Together - A method of welding two sheet-like work pieces, such as a web and a belt of a vehicle suspension control arm, is provided. The method includes the step of positioning one of the sheet-like work pieces against and at an angle relative to the other work piece such that the first and second work pieces are in contact with one another by a generally flat contact surface. The method continues with the step of melting with a single welding process material of the first and second work pieces across the entire width of the contact surface. | 05-29-2014 |
| 20140157602 | VEHICLE DOOR FRAME STRUCTURE AND METHOD OF PRODUCING VEHICLE DOOR FRAME - A door frame, a frame body which includes a glass opposing portion, a design portion positioned on one side of the glass opposing portion on the vehicle exterior side, a tubular portion positioned on the other side of the glass opposing portion on the vehicle interior side, and a glass guide portion having a concave cross section surrounding the edge of the door glass, is structured as a single member which is continuous from an upper sash portion to a side sash portion by having a uniform cross section from the upper to side sash portions, and by a bending process performed on the corner portion. The width of the design portion of the frame varies at at least one area along the length thereof and the design portion of the frame body is covered with an exterior member. | 06-12-2014 |
| 20140157603 | METHOD OF ASSEMBLING SUB-FRAME AND FRONT SIDE END IN VEHICLE - A method of assembling a sub-frame of a vehicle with the front side member of the vehicle includes integrally forming a supporting end of a mounting nut that protrudes in a radial direction in a center of an external circumference of the mounting nut, forming a through hole in a lower surface of the front side member, forming a seat as a groove in an internal surface of the through hole, inserting a lower end of the mounting nut into the through hole so that the supporting end is supported by a circumference of the through hole, settling a head of the mounting nut in the seat, and welding the supporting end and the head along the circumference of the through hole and a side of the seat to assemble the sub-frame to the front side member. | 06-12-2014 |
| 20140165405 | Fastenable Member for Sealing, Baffling or Reinforcing and Method of Forming Same - There is disclosed a member for sealing, baffling and/or reinforcing components of an automotive vehicle. The assembly generally includes a carrier, an expandable material and at least one fastener. | 06-19-2014 |
| 20140182133 | THREE PIECE LIFT ARM APPARATUS AND METHOD - A method of assembling a weldment for a refuse truck loading arm includes providing a left-handed C-section and a right-handed C-section and at least one buttress, welding a first buttress into a concave end portion of the left-handed or right-handed C-section, welding a first edge of the left-handed C-section to a matching edge of the right-handed C-section, welding another matching edge of the left-handed C-section to a matching edge of the right-handed C-section, the edge welding steps defining a slot between the edges, said slot being at an end portion of said weldment, and welding a joint section into the slot, with the joint section having an inner face, bolt holes and a key recess. | 07-03-2014 |
| 20140196289 | Method And System For Identifying Fastener Placement Zones - Certain embodiments of the disclosure provide one or more methods and/or systems to provide for determination of valid fastener zones that meet certain design rules. A method may include selecting at least one fastener having a preselected size and providing a first structural member and second structural member each having preselected sizes and shapes. The method may include determining a first fastener placement zone in said first structural member and determining a second fastener placement zone in said second structural member, where the respective first and second fastener placement zones are determined as a function of said structural design rules. The method may include determining a final fastener zone by identifying an overlap of the first and second fastener zones. | 07-17-2014 |
| 20140196290 | Electromagnetic Crawler Assembly System - A method and apparatus for performing operations on a workpiece. A first frame in a frame system may be held on the workpiece by applying a vacuum to the first frame. A second frame in the frame system may be detached from the workpiece by applying a pressure to the second frame. The second frame may be moved to a location on the workpiece. The second frame may be attached to the workpiece by applying the vacuum to the second frame. An operation may be performed on the workpiece. | 07-17-2014 |
| 20140208592 | Method and Apparatus for Automated Multi-Drilling and Multi-Rivet Machine - Method and apparatus for assembling, with fasteners, components of a structure having an outboard side, an inboard side, and a supporting frame. The components are placed together on the frame. An electromagnet having a core with multiple openings is positioned on the outboard side. A magnetically attractive member is placed against the inboard side opposite and aligned with the electromagnet. When activated, the electromagnet is attracted towards the magnetically attractive member and the two hold the components together. Multiple drill members pass through the openings in the core of the electromagnet and multiple openings are drilled simultaneously through the components. Subsequently, multiple rivets or huck bolts are simultaneously inserted into the drilled openings. Finally, fasteners are hammered through the drilled openings and rivets are secured by bucking bars provided on the magnetically attractive member. Alternatively, openings are provided in the magnetically attractive member for manually securing huck bolts to the components. | 07-31-2014 |
| 20140283386 | SYSTEM FOR ADJUSTING THE PROFILES OF AERONAUTICAL STRUCTURES - Interface fitting for supporting a component of a structure to be assembled on an assembly jig, comprising a component-side part, adapted to be attached to the component, and a jig-side part, configured to bear in an orientable way on the assembly jig. The support block further comprises a spacer member interposed between the component-side part and the jig-side part, which can be operated to adjust the distance between the component-side part and the jig-side part. | 09-25-2014 |
| 20140290064 | METHOD OF JOINING ALUMINIUM ALLOY SHEETS OF THE AA7000-SERIES - A method for producing a joint in at least two overlapping metal work pieces using a joining tool to obtain a mechanical joint between the overlapping work pieces, in particular joining by mechanical folding or pressure joining At least one of the first work piece and second work piece is a sheet material made of an aluminum alloy of the AA7000-series. A heat-treatment is applied to at least the work piece of 7000-series sheet material within 120 minutes prior to the production of the joint and/or for at least part of the time during production of the joint to temporarily reduce the tensile strength in the joining area of at least the work piece of said 7000-series sheet material. | 10-02-2014 |
| 20140317931 | MANUFACTURING METHOD FOR SEAT FRAME STRUCTURE - A predetermined component such as a recliner is attached to a long member in advance, and thereafter by bending the long member, a pair of side frames and an upper frame are integrally formed. Therefore, the recliner can be attached to the long member not bent yet and thus in a substantially flat state, and in addition, the pair of side frames and the upper frame can be integrally formed, which does not require labor and contributes to a reduction in manufacturing cost. Moreover, by adjusting a position where the bending is performed, it is possible to manufacture seat frame structures different in dimension even if the long members not bent yet have the same length, and from this viewpoint as well, it is possible to reduce labor and manufacturing cost. | 10-30-2014 |
| 20140366377 | JOINT GUARANTEE SYSTEM FOR VEHICLE ASSEMBLY AND CONTROL METHOD OF THE SAME - Disclosed is a joint guarantee system for vehicle assembly. The disclosed joint guarantee system for vehicle assembly manages a joining history of a joined component joined to a plurality of join points of a joining target, and includes: i) a tool detecting unit installed at a joining tool for joining the joined component to the joining target, and configured to detect movement displacements and angles of the joining tool for the join points based on a zero point of the joining tool; ii) a tool controller configured to receive a joining completion signal of the joining tool for each join point, and transmit a movement displacement value, an angle value, and a joint value for each join point of the joining tool detected by the tool detecting unit; and iii) a main controller configured to determine joining operation patterns for the join points based on the movement displacement value of the joining tool obtained from the tool controller. | 12-18-2014 |
| 20140373358 | METHOD OF MANUFACTURING TRAILER FROM METAL SHEETS - A method of manufacturing a trailer including a frame supporting a trailer bed and having rotatable wheels and a tongue for pivotal attachment to a land vehicle hitch. The method includes forming a plurality of structural members. Each structural member is made by cutting desired shapes having a desired perimeter edge outline and fastener holes from a metal sheet having galvanized protective coatings on both sides thereof, and bending the shapes for thereby forming into structural members. The structural members are secured together with rivets extending through the fastener holes thereby forming the trailer frame. The galvanized coatings are preferably one of zinc, aluminum or zinc and aluminum. The desired shapes are preferably cut by laser. | 12-25-2014 |
| 20140373359 | CONNECTING ARRANGEMENT AND ALSO A METHOD - A connecting arrangement for joining at least two components to form a structural assembly, near a wing of an aircraft, wherein at least one component is formed from a fibre composite plastic and at least one further component is formed from either a metal or a fibre composite plastic. A bushing is secured in a hole through the components. The bushing includes a first end with a collar which faces towards a lower face of the structural assembly and a second end. A zone of an upper face of the structural assembly radially surrounds the second end and includes a depression. A connecting element is installed in the bushing. This provides a smooth, aerodynamically beneficial configuration of the upper face, which can be coated, and which ensures a reliable electrical contact between the connecting element and a conductive surface of the first component. | 12-25-2014 |
| 20150007436 | TRAILER AND METHOD OF MANUFACTURING SAME - A trailer and method of manufacturing a trailer are provided. The trailer has a storage vessel which may include hoppers and which is partially formed from a plurality of top wall segments having peaks. The peaks or other components may be angled relative to one another to provide improved aerodynamics. A jig is provided to facilitate the manufacturing process. | 01-08-2015 |
| 20150013162 | Apparatus and Method for Moving a Structure in a Manufacturing Environment - A mobile fixture configured to move a structure in a manufacturing environment may include a motorized base configured to move on a surface and a support system connected to the motorized base, the support system being configured to support the structure, the support system being configured to position the structure along at least one of an X-axis, a Y-axis, and a Z-axis, the support system being configured to position the structure about the Z-axis, and the support system being configured to provide free rotation of the structure about at least one of the X-axis and the Y-axis. | 01-15-2015 |
| 20150020388 | UNIFRAME AND METHOD OF MAKING THE SAME - On variation may include using a plurality of node structures to assemble a uniframe. | 01-22-2015 |
| 20150047197 | DEVICE FOR ATTACHING AN APPARATUS ONTO A PANEL - The invention relates to a device ( | 02-19-2015 |
| 20150052756 | VEHICULAR BODY ASSEMBLY LOCKING APPARATUS AND METHOD - A vehicle body positioning and locking devices for use in assembling a vehicle body positioned on a movable vehicle support positioned at a vehicle build station. The locking device includes a remote vehicle locking device for selectively securing and locking a vehicle body to a support pallet. The support pallet is accurately and precisely positioned at a build station through alignment and inserting engagement of locating pads in at least one four-way and at least one two way receiver mounted to a build station foundation. A compliant body clamp design is included to provide a desired clamping force between the pallet and a vehicle body across a range of motion of the body clamp to accommodate vehicle build variances. | 02-26-2015 |
| 20150068042 | PIERCING TOOL AND PROCESS FOR FORMING AIRBAG TEAR SEAMS - A non-visible tear seam can be formed in a vehicle interior panel in a mechanical piercing process with a piercing tool that radially supports a needle during the process. The radial support enables the use of higher gauge needles and the formation of non-visible microholes through a visible surface of the panel. The piercing tool is capable of forming each of the microholes of the tear seam individually and may be disposable and/or may be configured with a replaceable needle. | 03-12-2015 |
| 20150082636 | Method and Device for Producing Shaped Sheet Metal Parts at a Low Temperature - The invention relates to a method for producing a shaped sheet-metal part from a panel or a semifinished part made of a material consisting of steel with at least 60 wt. % Fe and a residual austenite content of at least 5%, in which the panel or the semifinished part is at least partially cooled to a temperature below −20° C. before the shaping and is shaped at a temperature below −20° C. in a forming tool. The object of providing a method for producing load-compliantly configured components, which on the one hand permits industrial-scale use of low-temperature forming and is configured particularly simply, is achieved by reducing the material temperature of the panel or semifinished part to below −20° C. is carried out in a thermally regulated cooling apparatus. | 03-26-2015 |
| 20150101193 | LIGHTWEIGHT STEEL DOOR FOR VEHICLE AND METHOD FOR MANUFACTURING THE SAME - A vehicle door assembly comprises an inner panel integrally formed by upper and lower horizontal beams interconnected by front and rear upright beams, and an outer panel bonded to the inner panel. The frame portion comprises opposite front and rear U-shaped side frame members non-detachably attached to each other by upper and lower intermediate frame members so as to form a continuous perimeter. The side frame members are made of a first steel material and the intermediate frame members made of a second steel material, which is different from the first steel material. A method for manufacturing the inner panel comprises the steps: providing U-shaped sheets of the first steel material, providing top and bottom sheets of the second steel material, non-detachably connecting the U-shaped sheets to the top and bottom sheets so as to form a blank, and stamping the blank into the frame portion. | 04-16-2015 |
| 20150107113 | SYSTEM FOR ASSEMBLY OF A COMPONENT ON A MOTOR-VEHICLE BODY STRUCTURE - In a method for assembling a component on a motor-vehicle body structure, a device is set with a manipulator into a condition of connection with a component placed in a pick-up position, according to a predetermined mutual positioning; the component is gripped with the device to connect the component thereto; the device connected to the component is carried with the manipulator to a motor-vehicle body structure that is located in a position, on a conveying line, upstream of a centre for welding or fixing the component on the body structure; the component is constrained with the device to the body structure according to a mutual positioning whereby the component comes to occupy the proper position of assembly; the device is supported with the body structure; and with the device supported by the body structure, the body structure is conveyed with the conveying line to the centre. | 04-23-2015 |
| 20150291113 | ADJUSTABLE FRONT FASCIA FOR VEHICLES - An adjustable front fascia for vehicles includes a second vehicle structure that is fixed to a first vehicle structure at a location that is predefined relative to a hood of the vehicle. During assembly, the front fascia is movably supported on the second vehicle structure utilizing a temporary retaining mechanism that prevents unintended fore-aft movement of the front fascia unless a force exceeding a predefined release force is applied to the fascia. The front fascia can be fixed at a location providing a predefined gap relative to a front edge of the hood. The vertical position of the fascia relative to the hood can also be adjusted during assembly. | 10-15-2015 |
| 20150307181 | PANEL MEMBER, AIRCRAFT MAIN WING, AND METHOD FOR FORMING PANEL MEMBER - There is provided a panel member capable of restraining an increase in weight of a wing panel while restraining wasteful work in the manufacturing process, an aircraft main wing, and a method for forming the panel member. A wing panel | 10-29-2015 |
| 20150307211 | AUTOMATED ASSEMBLY OF PANELIZED AIRCRAFT FUSELAGES - A facility for assembling aircraft fuselages comprises a plurality of movable cradles. Each cradle is configured to support a fuselage keel structure and assemble a panelized fuselage from the keel structure to obtain a full fuselage contour in a single upright build position. | 10-29-2015 |
| 20150336157 | METHODS OF FORMING HOLLOW EXTRUDED VEHICLE FRAME COMPONENT FOR SUBASSEMBLY ATTACHMENT - A frame component of a vehicle, such as a header beam that couples between the A-pillars of a vehicle frame, includes an extruded hollow member having top and bottom exterior walls and side walls that together enclose an elongated internal volume of the hollow member. A pair of interior walls extends along the internal volume separating outer load sections adjacent to the side walls from a central attachment section. The outer load sections are void of apertures for supporting continuous load paths. A formation on the bottom exterior wall protrudes into the internal volume in the central attachment section. The formation includes an inset surface angled, located, and otherwise configured for attaching a subassembly to the frame component. | 11-26-2015 |
| 20150367930 | AUTOMATED SYSTEM FOR JOINING PORTIONS OF A CHASSIS AND METHOD THEREOF - An automated system for joining at least two portions of a chassis includes an actuation device ( | 12-24-2015 |
| 20160009415 | EXPANDED AIRLINER CONFIGURED SYMMETRICALLY REAR TO FRONT OR REAR TO REAR | 01-14-2016 |
| 20160009416 | Mobile Platforms for Performing Operations Inside a Fuselage Assembly | 01-14-2016 |
| 20160009419 | Towers for Accessing an Interior of a Fuselage Assembly | 01-14-2016 |
| 20160009420 | Assembly Fixture for Supporting a Fuselage Assembly | 01-14-2016 |
| 20160016622 | METHOD FOR IMPROVED REINFORCEMENT BAFFLING AND SEALING - A method for reinforcing, baffling or sealing a vehicle structure, comprising the steps of providing one or more materials having a horizontal axis, at least one terminating edge, and an initial length, forming openings in the one or more materials, and applying the one or more materials to a location requiring reinforcement, baffling, sealing or any combination thereof. | 01-21-2016 |
| 20160023690 | METHOD FOR PRODUCING A FASTENING ARRANGEMENT, AND SUCH FASTENING ARRANGEMENT - A method of producing a fastening arrangement for the position-correct fastening of a component to a structural part of a motor vehicle comprises the steps: providing of the structural part; providing of a first tolerance compensation element and a second tolerance compensation element; positioning of the first tolerance compensation element, while holding the structural part firmly, relative to the structural part in a nominal position for the later position-correct fastening of the component to be fastened, and holding of the first tolerance compensation element in the nominal position, the first tolerance compensation element being positioned with a gap relative to the structural part; inserting of the second tolerance compensation element between the first tolerance compensation element and the structural part, so that the gap between the first tolerance compensation element and the structural part is bridged over; joining of the second tolerance compensation element to the first tolerance compensation element and to the structural part. | 01-28-2016 |
| 20160023779 | Composite Panel Tool - A method and apparatus for holding a panel. A rigid frame is secured on an aircraft on a rework area on the aircraft. A carrier is attached to the rigid frame. The panel is held on the carrier and the carrier moves the panel about a plurality of axes. The panel moves with the carrier such that the panel has a desired position relative to a rework opening in the rework area. The panel is attached to the aircraft while the panel is held in the desired position relative to the rework opening. | 01-28-2016 |
| 20160067764 | Apparatus For And Method Of Forming A Metal Strut - The aspects of the present disclosure provide an apparatus for forming a metal strut mount having a C-shape cross-section and a pair of flanges extending therefrom and a method of forming a metal strut mount utilizing a rolling machine. | 03-10-2016 |
| 20160074977 | METHODS AND APPARATUS FOR STRUCTURAL REINFORCEMENT OF VEHICLE SUSPENSION MEMBERS - A method and apparatus for assembling a suspension. In one embodiment, a method includes altering a temperature of a first suspension component and then pressing the first suspension component and a second suspension component into engagement while the temperature remains substantially altered. | 03-17-2016 |
| 20160090136 | METHOD OF MANUFACTURING SUPPORT STRUCTURE FOR A PICKUP TRUCK BED - A vehicle includes a pair of longitudinal frame rails and a bed above the frame rails. A plurality of roll-formed aluminum cross-members contact the bed and are disposed between the bed and the frame rails for additional support of the bed. Extruded aluminum spacers are disposed between and in contact with the one of the cross members and one of the frame rails. A crush tube is spin-welded to the spacer and contacts the underside of the bed for additional support to inhibit downward relative movement of the bed. The crush tube is formed with a longitudinal hole extending therethough to receive a fastener that extends from above the truck bed, through the crush tube hole, through the cross-member and spacer, and into the frame rail. | 03-31-2016 |
| 20160114374 | SYSTEM AND METHOD FOR ASSEMBLING VEHICLE COMPONENTS WITH REINFORCED MOLDABLE RIVET - A system for assembling vehicle components includes a die assembly securing first and second vehicle components having first and second apertures, respectively. The die assembly positions the first and second vehicle components with the first and second apertures overlapping, and at least one of the first and second vehicle components including a polymeric material. The system further includes a joining component extending through the first and second apertures. The die assembly supports the joining component, and the joining component including a support shank and a moldable body at least partially encasing the support shank. The system also includes a punch member selectively engaging and deforming the moldable body of the joining component. The die assembly guides the moldable body into engagement with the first and second vehicle components, and the die assembly locates the support shank within at least one of the first and second apertures. | 04-28-2016 |
| 20160121949 | METHOD FOR COUPLING A SUNROOF GLASS APPARATUS TO A VEHICLE BODY - A method for coupling a sunroof glass apparatus includes the following steps: (a) moving a fixture toward a roof portion of a vehicle body in order to insert a plurality of pins of the fixture into locating holes formed in the vehicle body; (b) coupling net plates to the arms of an actuating mechanism of the sunroof assembly; (c) decoupling the fixture from the net plates while maintaining the net plates coupled to the arms of the actuating mechanism; and (d) coupling the flanges of the sunroof glass apparatus to arms of the actuating mechanism via the net plates in order to movably couple the sunroof glass apparatus to the vehicle body. In another embodiment, the presently disclosed method may additionally include coupling the net plates to the fixture before moving the fixture toward the roof portion of the vehicle body. | 05-05-2016 |
| 20160137283 | Method And Apparatus For Wing-To-Fuselage Integration - A method for wing-to-fuselage integration is disclosed. The method includes attaching a fitting to a wing box assembly of an aircraft at an early stage of integration and then attaching the fitting to a stub beam attached to a fuselage panel of the aircraft at a later stage of integration. The fitting eliminates the need to attach the stub beam directly to the wing box assembly. | 05-19-2016 |
| 20160137314 | CONSTRUCTION METHOD FOR A LEVER KINEMATICS AND USES THEREOF - To simplify the construction of lever kinematics under difficult installation and boundary conditions, a construction method for constructing a lever kinematics comprises a main lever and at least one connecting strut. The main lever can be rotated about a main lever axis by a predetermined angle, and the connecting strut connects a force application point to a hinge point on the main lever. A first position of the force application point is predetermined at the beginning of the rotational angle and a second position of the force application point is predetermined at the end of the rotational angle. The method includes representing a line of the possible hinge points for the given rotational angle, the main axis and the first and second positions of the force application point, and selecting the hinge point on the line. | 05-19-2016 |
| 20160250950 | METHOD FOR ASSEMBLING VEHICLE SEAT WITH CUSHION PLATE | 09-01-2016 |
| 20160251045 | Production System and Methods for Producing Different Shell Assembly Variants | 09-01-2016 |
| 20160375989 | METHOD OF PRELOADING AN AIRCRAFT ASSEMBLY, A PRELOADING TOOL AND AN AIRCRAFT ASSEMBLY - A method of preloading an aircraft assembly involving a step of operating an extendible preloading tool to move a landing gear strut to decrease the distance between first and second link attachment joints for attachment of a preloading linkage. A tool and aircraft assembly are also provided. | 12-29-2016 |
| 20170232596 | SPRING COMPRESSOR AND METHOD OF USE THEREOF | 08-17-2017 |
| 20180022326 | VEHICLE JACK POSITIONING DEVICE AND METHODS OF MAKING AND USING THE SAME | 01-25-2018 |
| 20190145487 | METHOD OF MANUFACTURING LIQUID-SEALED ANTIVIBRATION DEVICE AND MANUFACTURING APPARATUS OF LIQUID-SEALED ANTIVIBRATION DEVICE | 05-16-2019 |
