37th week of 2022 patent applcation highlights part 22 |
Patent application number | Title | Published |
20220289321 | TRACK SHOE WITH LARGE CAVITIES ON GROUND ENGAGING SURFACES HAVING A PROTRUDING SIDEWALL OR AN OVAL PERIMETER - A track pad includes a shoe member that has two bottom voids extending upwardly from the ground engaging surface of the shoe member, and which form a central support pillar having a serpentine surface laterally on side of the central support pillar, and another serpentine surface laterally on the other side of the central support pillar. The two bottom voids form oval perimeters at the ground engaging surface. | 2022-09-15 |
20220289322 | GROUND-ENGAGING TRACK SHOE HAVING RAISED-RELIEF FIXTURING SURFACES - A ground-engaging track shoe includes a shoe plate having link-side fixturing surfaces and ground-side fixturing surfaces. The link-side fixturing surfaces and the ground-side fixturing surfaces are raised in profile relative to a link-facing surface and a ground-facing surface, respectively. The fixturing surfaces enable a fixture to clamp the track shoe for support during processing, enabling improvements in maintaining portions of the track shoe flat and reducing part to part variation. | 2022-09-15 |
20220289323 | TRACTION MODULE FOR ROBOT WITH VARIABLE EXTENSION POSITIONS - A traction module for a robot system and a robot system using the traction module having, an outer frame and a rotating frame rotatably mounted within the outer frame. A drive system is operatively coupled to the rotating frame and configured to drive a traction drive component to propel the robot. An actuator is operatively connected to the rotating frame to controllably rotate the rotating frame. During a first portion of a rotating movement of the rotating frame, the drive system moves between a flat mode position relative to the outer frame and a clearance mode position in which the drive system extends outwardly from the outer frame to a greater extent than in the first position. During a second portion of the rotating movement of the rotating frame, the drive system may be positioned in a desired orientation to propel the robot. | 2022-09-15 |
20220289324 | MOBILE GOLF SIMULATION SYSTEM - Herein disclosed is a mobile golf simulation system, more particularly, a double-bayed golf simulator apparatus mounted to a wheeled trailer that may be readily transported and deployed to remote, particularly outdoor locations. The mobile golf simulation system of the present invention is uniquely designed to include a projection system installed beneath a floating floor that, along with right and left drop-down walls, allows for the creation of an open air platform from which a user may play a realistic form of virtual golf, hitting his ball into a built-in screen. | 2022-09-15 |
20220289325 | ADJUSTABLE SADDLE - An adjustable saddle may include a first saddle half that may be slidably adjustable to a front mounting assembly and slidably adjustable to a rear mounting assembly. An adjustable saddle may further include a second saddle half that may be slidably adjustable to a front mounting assembly and slidably adjustable to a rear mounting assembly. Additionally, the attachment features may be configured to be releasably securable to the mounting assemblies. The first saddle half and the second saddle half may be adjusted independently of each other to adapt to a given sit bone width and riding position to achieve maximum comfort. | 2022-09-15 |
20220289326 | Apparatuses and Methods for Crank-Based Lighting - The present disclosure describes various aspects of crank-based lighting, which may improve visibility of pedal-based vehicles or conveyances. In some aspects, a light generating apparatus includes a crank interface and lighting system. The crank interface may facilitate mounting of the apparatus to a crank (or crankarm) of a bicycle or other pedal-based vehicle. The lighting system may generate or emit light based on information indicating an angle, movement, and/or position of the crank, such as to cause light emission to emulate or project leg movement of a rider. | 2022-09-15 |
20220289327 | INFORMATION PROCESSING TERMINAL DEVICE COUPLING MECHANISM AND COUPLING METHOD - When an information terminal device having a GPS function, a communication function, and the like is coupled to a bicycle, a body, or another object to be fixed or supported, the degree of freedom of a coupling mechanism is enhanced to reduce design limitation, and user-friendliness and operability are improved. | 2022-09-15 |
20220289328 | HOLDING DEVICE FOR RELEASABLY HOLDING AN ENERGY STORE ON A FRAME - A holding device for releasably holding an energy store, in particular, a bicycle energy store, at a frame, in particular, at a bicycle frame. The holding device includes at least one carrier unit, which includes at least one carrier element, in particular, a guide bar for at least partially receiving and/or guiding the energy store, and including at least one support unit for securing the energy store in a form-fit manner at the carrier unit. The support unit includes at least one support element situated at the carrier element, which secures the energy store at the carrier element in a state in which the energy store is situated at the carrier element at least along a direction extending transversely to a longitudinal axis of the carrier element. | 2022-09-15 |
20220289329 | Bicycle Safety Accessory Device - A bicycle safety accessory device is provided which may comprise an outer body having an internal cavity and an electronic data communication module. The electronic data communication module may be stored within the internal cavity and the internal cavity may comprise a first structural configuration defining an enclosed state and a second structural configuration defining an exposed state. In the first structural configuration, the internal cavity may be physically sealed from fluid and particulates external thereto and, in the second structural configuration, the internal cavity may be accessible to a hand of an individual. The bicycle safety accessory device further comprises a coupling mechanism which retains the outer body adjacent a recreational object in a first mode while allowing the outer body to be removed from the recreational object in a second mode. | 2022-09-15 |
20220289330 | HANDS FREE BICYCLE - An electric bicycle includes a frame that has a concave or arc shape. The bicycle also includes two wheels—a front wheel and a rear wheel, with each wheel being connected with an end portion of the frame. A battery-powered electric motor may be connected with the rear wheel to drive the rear wheel and propel the bicycle forward. The battery may be rechargeable. The speed of the bicycle may be controlled by the operator moving a lever with one of their feet. A rotatable knob located on the frame may be used as a cruise control speed setting device. The electric bicycle may be steered by the operator using their feet resting on a pair of foot pegs that are attached to or connected with the front wheel. The electric bicycle may include a regenerative braking system or a friction braking system. | 2022-09-15 |
20220289331 | FRICTIONAL DRIVE UNIT - To provide a frictional drive unit that can arrange drive rollers with high density and facilitate an attachment operation of the drive rollers, a frictional drive unit | 2022-09-15 |
20220289332 | COMPOSITE STRUCTURES AND METHODS OF FORMING COMPOSITE STRUCTURES - Composite structures and methods of forming composite structures are provided. A composite structure as disclosed herein incorporates one or more composite structure components, such as composite panels and composite inserts. A composite panel is formed from one or more sheets of fiber reinforced thermoplastic material. Composite inserts can include one or more composite blocks or braided sleeves. A composite block can be formed as a stacked or molded structure from trimmings or waste produced during the formation of the composite structures. A braided sleeve can include a seamless, woven sleeve formed of reinforcing fibers and thermoplastic threads. In a completed composite structure, composite inserts are at least partially disposed within a volume defined by surfaces of composite panels. The various composite structures and inserts can be given a final shape and can be fused to one another in a molding and fusing step. | 2022-09-15 |
20220289333 | AUTOMATIC METHOD FOR CONTROLLING IN CURRENT-MODE A MOTOR FOR ASSISTING WITH PEDALLING ON AN ELECTRICALLY ASSISTED PEDAL CYCLE AND ELECTRICALLY ASSISTED PEDAL CYCLE INTENDED TO IMPLEMENT SUCH A METHOD - An automatic method for controlling in current-mode a motor for assisting with pedaling on an electrically assisted pedal cycle equipped with a sensor that measures a resultant force on its pedal and gear mechanism is provided, including injecting a control current into the motor to generate an assistance torque and computing the value of the assistance torque; computing a value of the longitudinal resultant of the assistance torque by applying a second coefficient of proportionality to the torque value computed in the preceding step; measuring a value of the longitudinal resultant of the total torque; computing a value of the longitudinal resultant of the torque exerted by the cyclist; computing an average value of the torque exerted by the cyclist over a fraction of a crank rotation; computing the value of the assistance torque to be generated in the motor; and deducing the value of the current to be injected. | 2022-09-15 |
20220289334 | METHOD FOR OPERATING A VEHICLE OPERABLE BY MOTOR POWER AND/OR PEDAL POWER, AND VEHICLE - A method for operating a vehicle operable by motor power and/or pedal power, in particular, an electric bicycle. The vehicle includes an electric drive, a crank mechanism, at least one torque sensor, which is configured to detect a torque applied by a rider onto the crank mechanism, in the form of a multitude of torque measuring signals, and a control unit, which is configured to generate a control signal for activating the electric drive as a function of at least one of the torque measuring signals. Upon detection of an error regarding the torque sensor, the control signal is generated in the form of a substitute control signal, based on at least one of the torque measuring signals, when this at least one torque measuring signal is recognized as plausible. A vehicle operable by motor power and/or pedal power, in particular, an electric bicycle, is also described. | 2022-09-15 |
20220289335 | APPARATUS FOR THE ELECTRIC PROPULSION OF A VEHICLE, IN PARTICULAR OF A HUMAN-POWERED VEHICLE - An apparatus for the electric propulsion of a vehicle, in particular of a human-powered vehicle, preferably in the form of a bicycle or the like, comprising a support body, electric propulsion means for the forwarding actuation of the vehicle, preferably in the form of an electric motor, in particular of the brushless type, having a corresponding rotatable shaft for outputting the power generated by the same electric actuation means, or motor, and means for outputting the power generated by the electric propulsion apparatus, in particular comprising means for engaging, or meshing, with said operative connection means of the transmission means of the vehicle, i.e., with an elongated and closed-loop member, or articulated link chain. Said means for transferring the power generated by said electric actuation means, or motor, to said means for outputting the power generated by the electric propulsion apparatus comprise a first and a second speed reducer stage. | 2022-09-15 |
20220289336 | HOLDING DEVICE FOR RELEASABLY HOLDING AN ACCUMULATOR AT A FRAME - A holding device for releasably holding an accumulator, in particular, a bicycle accumulator, at a frame, in particular, at a bicycle frame. The holding device includes at least one carrier unit for at least partially receiving and/or guiding the accumulator. The holding device also includes at least one locking unit situated at the carrier unit, in particular, at least mostly within the frame, for releasably, in particular, axially fixing the accumulator at the carrier unit on one side. | 2022-09-15 |
20220289337 | BICYCLE REAR DERAILLEUR - A bicycle rear derailleur comprises a base member, a linkage structure, a movable member, a first pulley assembly, and a second pulley assembly. The first pulley assembly includes a first pulley support and a first toothed pulley. The first pulley support is pivotally coupled to the movable member about a first pivot axis. The first toothed pulley is rotatably coupled to the first pulley support about a first pulley axis spaced apart from the first pivot axis. The second pulley assembly includes a second pulley support, a second toothed pulley, and a third toothed pulley. The second pulley support is pivotally coupled to the movable member about a second pivot axis. The second toothed pulley is rotatably coupled to the second pulley support about a second pulley axis. The third toothed pulley is rotatably coupled to the second pulley support about a third pulley axis. | 2022-09-15 |
20220289338 | GLOW-IN-THE-DARK WATERCRAFT MATTING AND OTHER GLOW-IN-THE-DARK ACCESSORIES - A watercraft matting is described that includes a bottom surface configured to come into contact with a watercraft surface, a top surface having a plurality of recessed portions disposed between a plurality of protruding portions, where the protruding portions being formed of a non-skid material, and a phosphorescent material positioned within the plurality of recessed portions. The phosphorescent material is adapted to glow-in-the-dark when exposed to an ultraviolet light. The plurality of protruding portions may be formed of a cross-linked-closed-cell (CLCC) foam material. | 2022-09-15 |
20220289339 | RETRACTABLE BOAT AWNING. - A retractable boat awning or “bimini cover” is provided. The present retractable boat awning may replace existing awnings on a boat or may be added to a boat which lacks an awning. The present retractable boat awning has a first folding locking bar and a second folding locking bar which are concealed within a slim securing container when the device is not in use. To use the awning, the first and the second locking bar are rotated outward from the interior of the securing container and secure a protective awning fabric cover. The awning may be fully assembled into the usable form or may be collapsed into the stored securing container in around a minute. | 2022-09-15 |
20220289340 | MOORING DEVICE AND A METHOD FOR OPERATING A MOORING DEVICE - A mooring device ( | 2022-09-15 |
20220289341 | Support system for outboard marine motors at the transom of a boat - A support system for outboard marine motors at the transom of a boat includes a support device having a first part that is integral with the transom and a second part that is integral with the outboard motor. The second part is translatable with respect to the first part, so that the second part moves according to an orientation in the distancing or approaching direction of the water line of the boat. A control unit is configured to set the position of the second part with respect to the first part and to generate control signals, so as to move the second part in the direction of immersion of the propeller of the outboard motor. | 2022-09-15 |
20220289342 | Subsea Anchorage Installation System - Various aspects include devices, systems, and methods for securing an anchoring element to a seafloor. The methods may use a subsea anchorage installation system that may include a subsea grout supply assembly. The subsea grout supply assembly may include a variable volume grout storage chamber, a paddle, and a subsea grout pump. The variable volume grout storage chamber may be configured to transport dry grout to a seafloor. The variable volume grout storage chamber may include a water injection port configured to receive water for mixing with the dry grout on the seafloor. The variable volume grout storage chamber may also be configured to expand from a collapsed configuration as water is injected. | 2022-09-15 |
20220289343 | FLOATING DOCKABLE LIQUEFIED NATURAL GAS SUPPLY STATION - A floating dockable liquefied natural gas supply station, comprising: a main hull, a bottom base and a positioning system. The bottom base comprises a base plate or at least two base plates. The base plate is securely connected to a lower lateral side of the main hull by means of a splicing securing system. Therefore, the main hull and the bottom base of the floating dockable liquefied natural gas supply station can be assembled in a modular manner. It is possible to individually construct the main hull and bottom base of the floating dockable liquefied natural gas supply station, and to then use a modular method for connecting and assembling same on the ocean or on land, thus being able to flexibly form various types and dimensions of supply station, allowing for docking transport vessels accommodating various loading capacities of liquefied natural gas (LNG), and reducing the construction cost thereof. | 2022-09-15 |
20220289344 | FLOATING ARRANGEMENT FOR SUPPORTING SOLAR PANELS - A floating arrangement may include at least one support-floatation-unit for supporting a solar panel, the at least one support-floatation-unit has a main body having a flat base and at least one connection portion; and at least one connecting-floatation-unit having a flat base and at least one connection portion. The respective corner-connection-portions may be coupled together to form a connection joint connecting the support-floatation-unit and the connecting-floatation-unit in a side-by-side arrangement. A height from the base of the support-floatation-unit to the connection joint may be larger than a height from the base of the connecting-floatation-unit to the connection joint such that the base of the support-floatation-unit may extend downwards from the base of the connecting-floatation-unit by a depth which defines an additional displacement volume of the support-floatation-unit configured to provide additional buoyancy to support the solar panel. | 2022-09-15 |
20220289345 | AN OFFSHORE DRILLING VESSEL WITH AN EXTERNAL CABLE CONNECTION AND METHOD THEREFOR - An offshore drilling vessel includes a hull and at least one opening in the hull arranged to receive an end of at least one submersible cable. The offshore drilling vessel also comprises a cable capture mechanism configured to lift the end of the at least one submersible cable through the at least one opening from a submersed position to a raised position. A cable connector is configured to couple to the end of the at least one submersible cable when the end of the at least one submersible cable is in the raised position such that the offshore drilling vessel comprises an external data and/or power connection via the submersible cable. | 2022-09-15 |
20220289346 | Braking System for Gyroscopic Boat Roll Stabilizer - A gyroscopic boat roll stabilizer for a boat comprises a gimbal, having a gimbal axis, an enclosure mounted to the gimbal and configured to precess about a gimbal axis, a flywheel assembly rotatably mounted inside the enclosure for generating a torque that is applied to counter a rolling motion of the boat, and a braking system for controlling precession of the enclosure. The braking system is configured to enable precession in the first and second directions. | 2022-09-15 |
20220289347 | DEVICE AND METHOD FOR LAUNCHING AND RECOVERING AN UNMANNED UNDERWATER VEHICLE - Devices and methods for recovering an unmanned underwater vehicle. The device includes a gantry mounted on a recovery vehicle, a frame, and a shaft extending between the gantry and the frame and configured to vertically move the frame relative to the gantry. Attached to the frame are a plurality of rotatable arms movable between an opened position and a closed position. A first end of each arm is attached to the frame at a pivot. A flexible strap extends between each of the second ends of the arm and the frame. As the arms are moved to the closed position around the unmanned underwater vehicle, the straps will support the unmanned underwater vehicle. | 2022-09-15 |
20220289348 | IMPLANTABLE MICRO-SENSOR TO QUANTIFY DISSOLVED INERT GAS - Methods and devices including implantable micro-sensors used to detect tissue-dissolved inert gas and to detect microbubble formation to avoid Caisson disease are described. The disclosed methods and devices are based on measuring the refractive index changes in hydrophobic liquids after absorbing an inert gas such as nitrogen. The changes in the refractive index are based on implementing one of an interferometry, optical microcavity resonance shift, a photonic crystal resonance, a beam deflection, a resonance tuning or detuning, an amplitude change, or an intensity change method. | 2022-09-15 |
20220289349 | SUBSURFACE MULTI-MISSION DIVER TRANSPORT VEHICLE - A subsurface diver transport vehicle includes a vehicle body and at least one propulsion device. The vehicle body incorporates a number of individual mission modules mechanically assembled together to define a substantially continuous hull and deck of the vehicle. The mission modules include at least one battery module adapted for supplying electrical current to electrical subsystems of the vehicle. The propulsion device is attached to the vehicle body and capable of propelling the vehicle through a body of water. | 2022-09-15 |
20220289350 | KAYAK AND OTHER WATERCRAFT TYPE STORAGE SYSTEM - A watercraft storage system for storing and securing one or more watercraft and other equipment used in conjunction with the watercraft. Securing of the watercraft in a storage location of the watercraft storage system, and the other equipment in a compartment associated with the storage location, is achieved, at least in part, by a moveable, e.g., rotational, arm structure associated with the storage location being in a locked position and the size of at least one dimension of the watercraft exceeding the size of a corresponding dimension of the storage location including the moveable arm structure. | 2022-09-15 |
20220289351 | BUOYANCY ADJUSTMENT DEVICE - A buoyancy adjusting device for an underwater device is described the device comprising: a tube having first and second ends; a resilient mechanism located at the first end of the tube and extending towards the second end of the tube; an opening near the second end of the tube; a catch at the second end of the tube; 5 and at least one block insertable into from the first end of the tube to adjust the buoyancy. | 2022-09-15 |
20220289352 | A MARINE PROPELLER - A marine propeller having reduced noise characteristics, which has a hub having a central axis, one or more blades having blade length with a proximal end attached to the hub and a distal end extending radially outward from the hub, wherein the propeller has a diameter in between 360-400 mm, and wherein a combination of the diameter, pitch angle, skew angle, and number of blades of the propeller provides required thrust while generating low noise. | 2022-09-15 |
20220289353 | Paddle - The utility model provides a new type of paddle, which belongs to the technical field of rowing. The new type of paddle comprises a paddle blade, the left end of the paddle blade is fixed with a paddle handle, the left end of the paddle handle is provided with a connecting rod, the circumferential surface of the connecting rod is provided with elastic piece, and the left side of the connecting rod is connected with length adjusting rod through a locking mechanism. And the length adjusting rod is movably inserted into the connecting rod, the left end of the length adjusting rod is fixed with a handle, and the paddle handle, the connecting rod and the length adjusting rod are all made of new aluminum alloy materials. The entire paddle structure is reasonably set up and ingenious in concept. Through the modification of the paddle structure, not only the handle has a non-slip function during use, but also avoids the situation that the user sweats when holding the handle or can't hold the handle when it comes into contact with water during use. Meanwhile, the function diversity of the whole device can be improved by adjusting the length between the connecting rod and the length adjusting rod. | 2022-09-15 |
20220289354 | OUTBOARD MOTOR - The outboard motor includes a drive shaft | 2022-09-15 |
20220289355 | MARINE PROPULSION APPARATUS - In a marine propulsion apparatus that transmits power of at least one of an internal combustion engine (ICE) and a generator motor (GM) mounted on a ship to a propeller via a forward reverse switching mechanism, the marine propulsion apparatus can be downsized as a whole. The marine propulsion apparatus includes a connection switching mechanism capable of selectively connecting the GM to an upstream side and a downstream side of the power transmission from the ICE in the forward reverse switching mechanism. Then, the forward reverse switching mechanism is interposed between the ICE and the connection switching mechanism, and a large torque from the ICE is not directly transmitted to the connection switching mechanism. As a result, it is not necessary to increase the capacity of the connection switching mechanism, and the connection switching mechanism and thus the marine propulsion apparatus can be downsized. | 2022-09-15 |
20220289356 | System and Methods for Heat Treatment of Ballast Fluid - Heat treatment system and methods to decontaminate ballast fluid includes ballast tank(s) each having a temperature sensor. A heat source transfers heat to ballast fluid when circulated therethrough. Diverter valves provide selective direction of fluid flow to either the onboard heat source or external auxiliary heat source when connected. A pump moves ballast fluid between the ballast tank(s) and the heat source, recirculating ballast fluid for iterative heating. The temperature sensor provides ballast fluid temperature information in the ballast tank(s). Recirculation is stopped when ballast fluid meets predetermined ballast temperature conditions. A display provides decontamination status to an operator. A control unit monitors all sensors, valves and pumps to coordinate the performance of the heat treatment process and provide history report confirming decontamination. | 2022-09-15 |
20220289357 | REUSABLE BALLOON SYSTEM - An example reusable high-altitude balloon system includes a balloon with a first end supporting a payload and a second end with an aperture and an apex fitting that is positioned within the aperture. A clamp applies a pressure to a plurality of pleated folds formed in the perimeter of the aperture around the apex fitting to form an air-tight seal against the balloon at the perimeter of the aperture. The reusable high-altitude balloon system further includes control circuitry that controllably releases the apex fitting from the balloon to initiate a descent sequence. | 2022-09-15 |
20220289358 | COMPOSITE STRUCTURES FOR AERODYNAMIC COMPONENTS - There is provided a composite structure for an aerodynamic component having an aerofoil-like cross-section and a leading edge, the composite structure being in the form of a torsion box arrangement made from composite materials and having a core, the torsion box having a forward wall, an aft wall, a top wall and a bottom wall, together defining the core, the front wall being formed as the leading edge of the aerodynamic component. Also provided is a load-bearing composite structure for use with an aerodynamic component and configured for supporting at least one external load, this composite structure being made from composite materials and configured for being joined to the external aerodynamic surface of the aerodynamic component such as to be in overlying abutting relationship with at least a contact surface portion of the external aerodynamic surface, including the leading edge, at least a forward portion of each of the suction surface and the pressure surface thereof. | 2022-09-15 |
20220289359 | AIRCRAFT FUSELAGE CONFIGURATIONS FOR UPWARD DEFLECTION OF ART FUSELAGE - A fixed-wing cargo aircraft having a kinked fuselage is disclosed. The fuselage contains a continuous interior cargo bay, and includes a forward portion, an aft portion, and a kinked portion forming a junction in the fuselage between the forward and aft portions. The kinked portion contains a transition region of the cargo bay and defines a bend between a forward centerline and an aft centerline. The kinked portion is formed with a forward transverse frame section, a separate aft transverse frame section, and a plurality of longitudinal frame elements extending between the forward and aft frame sections, the forward frame being coupled to an aft end of the forward portion and the aft frame section being coupled to a forward end of the aft portion such that the aft frame section is angled with respect to the forward frame section about a lateral axis of the cargo aircraft. | 2022-09-15 |
20220289360 | SYSTEM AND METHOD TO ACTIVELY MORPH AN AIRCRAFT WHILE IN FLIGHT FOR SONIC BOOM SUPPRESSION AND DRAG MINIMIZATION - A system that optimizes the shape or configuration of an aircraft to minimize ground overpressure shock strength while in supersonic flight over speed restricted terrain and to morph to an optimized configuration for drag minimization while over unrestricted terrain. | 2022-09-15 |
20220289361 | PROPELLER SAFETY DEVICE - A propeller safety device is provided. The propeller safety device is configured to insert a moving part of a propeller into a fixed part during a crash of an air mobility to allow a reduction in the total length of the propeller, thereby preventing the propeller from hitting the ground. Accordingly, a secondary accident due to fragments formed when the rotating propeller hits the ground is prevented. | 2022-09-15 |
20220289362 | TURBOMACHINE MODULE EQUIPPED WITH A SYSTEM FOR CHANGING THE PITCH OF THE BLADES OF A PROPELLER AND WITH A DEVICE FOR FEATHERING THE BLADES - The invention relates to a module of a turbomachine of longitudinal axis X, the module comprising: ⋅—a rotary casing ( | 2022-09-15 |
20220289363 | SYSTEM AND METHOD FOR FLIGHT CONTROL IN ELECTRIC AIRCRAFT - A system for flight control in electric aircraft includes a flight controller configured to provide an initial vehicle torque signal including a plurality of attitude commands. The system includes a mixer configured to receive the initial vehicle torque signal and a vehicle torque limit, receive prioritization data including a prioritization datum corresponding to each of the plurality of attitude command, determine a plurality of modified attitude commands as a function of the vehicle torque limit, the attitude commands, and the prioritization data, generate, as a function of modified attitude commands, an output torque command including the initial vehicle torque signal adjusted as a function of the vehicle torque limit, generate, as a function of the output torque command, a remaining vehicle torque. The system includes a display, wherein the display is configured to present, to a user, the remaining vehicle torque and the output torque command. | 2022-09-15 |
20220289364 | SYSTEM AND METHOD FOR FLIGHT CONTROL IN ELECTRIC AIRCRAFT - A system for flight control in electric aircraft includes a flight controller configured to provide an initial vehicle torque signal including a plurality of attitude commands. The system includes a mixer configured to receive the initial vehicle torque signal and a vehicle torque limit, receive prioritization data including a prioritization datum corresponding to each of the plurality of attitude command, determine a plurality of modified attitude commands as a function of the vehicle torque limit, the attitude commands, and the prioritization data, generate, as a function of modified attitude commands, an output torque command including the initial vehicle torque signal adjusted as a function of the vehicle torque limit, generate, as a function of the output torque command, a remaining vehicle torque. The system includes a display, wherein the display is configured to present, to a user, the remaining vehicle torque and the output torque command. | 2022-09-15 |
20220289365 | AIRCRAFT INCLUDING A REINFORCED MAIN LANDING GEAR BOX - An aircraft including two main landing gears and also a main landing gear bay configured to house, on either side of a vertical median plane, the two main landing gears in a retracted position, the main landing gear bay including a rear transverse wall, a front transverse wall and also an end wall that is approximately perpendicular to the rear and front transverse walls. The main landing gear bay includes at least one strut connecting the rear or front transverse wall and the end wall, approximately positioned in the vertical median plane. | 2022-09-15 |
20220289366 | SYSTEM FOR ROLLING LANDING GEAR - A system for rolling landing gear is illustrated. System includes a skid component attached to an aircraft and comprising at least a skid tube oriented laterally to a longitudinal axis of the aircraft. System also includes at least a wheel journaled on a rotational fulcrum and at least a biasing means attaching the rotational fulcrum to the skid tube, wherein the biasing means comprises at least a leaf spring and exerts a recoil force resisting upward displacement of the rotational fulcrum with respect to the skid tube. | 2022-09-15 |
20220289367 | ROTATING WING AIRCRAFT - A rotating wing aircraft | 2022-09-15 |
20220289368 | PRECISION BLADE PITCH ADJUSTMENT - A blade pitch adjustment mechanism includes a pitch cylinder having a first face and pitch slots extending longitudinally from the first face, a blade sleeve having a second face and a blade slot extending longitudinally from the second face, the blade sleeve is configured to be rotationally positioned in the pitch cylinder with the second face located with the first face, wherein the blade slot and the pitch slots are cooperative to form keyway, corresponding to a discrete blade pitch, when the blade slot is aligned with a pitch slot. | 2022-09-15 |
20220289369 | SWASHPLATE ASSEMBLY WITH INTEGRATED ELECTRIC MOTOR - A swashplate assembly, that includes an integrated electric motor. The present embodiments also relate to a multi-blade rotor for a rotary-wing aircraft with such a swashplate assembly and to a rotary-wing aircraft with such a multi-blade rotor. The swashplate assembly may include a rotating plate that is mounted to the rotor shaft and rotates in operation with the rotor shaft, a stationary plate that is coupled to the rotating plate by means of bearings, and an electric motor that generates torque for driving the rotor shaft. The electric motor comprises a stator that is mounted to one of the stationary or the rotating plates and a rotor that is mounted to the other one of the stationary or rotating plates. | 2022-09-15 |
20220289370 | DIFFERENTIAL THRUST VECTORING SYSTEM - A differential thrust vectoring system includes a first thruster, a second thruster, a main actuator, and a trim actuator. The system is configured such that actuation of the main actuator causes rotation of the thrusters together about an axis, whereas actuation of the trim actuator causes relative rotation of the first and second thrusters about the axis. | 2022-09-15 |
20220289371 | Line Replaceable Centerbody Assemblies for Ducted Propulsion - A ducted propulsion assembly for an aircraft includes a duct and a plurality of stators. The distal ends of the stators are coupled to the duct. The ducted propulsion assembly includes a line replaceable centerbody assembly isostatically coupled to the proximal ends of the stators. The line replaceable centerbody assembly includes one or more electric motors driving an output driveshaft. The ducted propulsion assembly also includes a proprotor assembly interchangeably coupled to and rotatable with the output driveshaft of the line replaceable centerbody assembly. The proprotor assembly is rotatable in a rotational plane to generate thrust. | 2022-09-15 |
20220289372 | System and method for detecting and tracking non-stationary obstacles in an aerial movement volume - A system for navigating an aerial robotic device (ARD) from a first to a second location includes an object detection module for detecting and generating a first object record of a non-stationary object, an object tracking module for receiving second object records, and comparing the first object record with each second object record, which includes determining whether a distance between centers of bounding boxes of the first and second object records is less than a pre-defined threshold value, identifying the first object record to be a match with the second object record, and updating the second object record with details of the first object record, when the calculated distance is less than the pre-defined threshold, updating a prediction list of a second object record with predicted future locations of corresponding object,and navigating the ARD in the presence of a non-stationary object based on prediction list of corresponding second object record. | 2022-09-15 |
20220289373 | MANAGEMENT APP FOR DRONE WITH REMOTE ID - A global positioning satellite (GPS) receiver and a transmitter are at a base remote from a drone, and the transmitter sends GPS packets along with control packets to the drone. In turn, the drone also has a GPS receiver and a transmitter that transmits both the controller and drone GPS coordinates to the remote base. A management app for law enforcement is provided. | 2022-09-15 |
20220289374 | APPARATUS FOR ASSISTING FORMATION FLIGHT OF UNMANNED AERIAL VEHICLE - Provided is an apparatus for assisting formation flight. The apparatus comprises a formation maintaining member for maintaining formation of a plurality of unmanned aerial vehicles in flight and having connection points formed at points corresponding to positions of each unmanned aerial vehicle on the formation, and a plurality of fastening members, in which one end is connected to the connection points of the formation maintaining member and the other end is fastened to the unmanned aerial vehicle to connect the formation maintaining member and the plurality of unmanned aerial vehicles, wherein a movement permitting member for permitting a posture change of the unmanned aerial vehicle within a predetermined range is formed on the other end of the plurality of fastening members. | 2022-09-15 |
20220289375 | A METHOD FOR AUTONOMOUS IN-FLIGHT TRANSFER OF A LOAD FROM A FIRST AERIAL VEHICLE TO A SECOND AERIAL VEHICLE, SYSTEM COMPRISING A FIRST AERIAL VEHICLE AND A SECOND AERIAL VEHICLE, AND AERIAL VEHICLES - A method for autonomous in-flight transfer of a load from a first Aerial Vehicle, AV, to a second AV is provided. Each of the first AV and the second AV includes a frame with a vertical opening for receiving the load. A plurality of rotors are attached to the frame. The method comprising autonomously performing the following in-flight: fastening means of the first AV hold the load in the vertical opening of the first AV such that a bottom end of the load is accessible by the second AV; the second AV approaches the first AV from below in order to couple a fastening means of the second AV to the bottom end of the load; the fastening means of the first AV releases the load after the fastening means of the second AV couples to the bottom end of the load; and the fastening means of the second AV lower the load with respect to the frame of the second AV in order to move the load into a flight position. | 2022-09-15 |
20220289376 | FLYING BODY, CONTROL METHOD, AND PROGRAM - A flying body includes a control unit that acquires inclination information regarding inclination of a landing point and sets a horizontal speed according to the inclination information. | 2022-09-15 |
20220289377 | AUTONOMOUS PLACEMENT OF AN AERIALLY-MOUNTABLE ELECTRONIC DEVICE - An autonomous placement device for securing an electronic device to and/or removing an electronic device from an object (such as, for example, a utility pole or a streetlight luminaire optionally forming a part thereof) includes a repository and a remove-and-place system. The repository is arranged to store at least one electronic device. The remove-and-place system is operable, in one embodiment, to retrieve an electronic device from the repository and, after the autonomous placement device has been positioned proximate an aerial placement position, secure the electronic device to the object at the aerial placement position. The autonomous placement device may further include a guidance system operable to locate the aerial placement position prior to aerial positioning. The autonomous placement device may form part of a system, which also includes an unmanned aerial vehicle (UAV) and a payload coupling system that mechanically couples the autonomous placement device to the UAV. | 2022-09-15 |
20220289378 | ENCLOSED UNMANNED AERIAL VEHICLE - The present disclosure is directed to a propeller driven remote control flying device having an enclosed body. The motor and propellers of the device can be contained within the enclosed body. The enclosed body can include a plurality of pores through which air passes, with one side of the body generally functioning as an air intake, and the opposite side of the body functioning as an air outlet. The pores can be sufficiently small so as to prevent contact between persons, animals or articles and the motor driven propellers. | 2022-09-15 |
20220289379 | MOBILE EMERGENCY POWER GENERATION AND VEHICLE PROPULSION POWER SYSTEM - A mobile emergency power generation and vehicle propulsion power system, method, and apparatus for full-scale, clean fuel, electric-powered vehicles having a fuel cell module including a plurality of fuel cells working together to process oxidizers including gaseous oxygen from the atmosphere or local oxygen supply and fuels including gaseous hydrogen or gaseous hydrogen from liquid hydrogen, to collect electrons from the plurality of hydrogen fuel cells to supply voltage and current to and control an amount and distribution of electrical voltage and torque or current for use with power inverters and power outlets for exterior use, and for propulsion systems of the vehicle itself. | 2022-09-15 |
20220289380 | ELIMINATION OF AIR FLOW INTERFERENCE FOR MID-AIR PACKAGE TRANSFERS - A method for stabilizing drones performing a mid-air package transfer. One or more processors detecting the proximity of a second drone to a first drone. Interference of air pressure between rotors of the first drone and rotors of the second drone is detected by data from sensors included on the first and second drone. Positions of the rotors of the first drone are adjusted by moving rotor arms in a first direction and the rotors of the second drone are adjusted by moving rotor arms of the second drone in a second direction that increases separation between the rotors of the first drone and the second drone, and the amount of separation is based on reduced interference of air pressure between rotors of the first and second drone. Responsive to determining completion of a package transfer, the positions of the rotors are adjusted to original positions. | 2022-09-15 |
20220289381 | PAYLOAD DELIVERY AND DROP DEVICE FOR UNMANNED AERIAL VEHICLE FOR AUTOMATIC RELEASE UPON SURFACE CONTACT - Embodiments of a payload delivery and drop device for an unmanned aerial vehicle, and method of its use are described herein. In some embodiments, an apparatus includes a moveable collar defining a lumen having a centerline, and a rigid bar that has a first portion and a second portion different from the first portion. The first portion of the rigid bar has a centerline and the second portion of the rigid bar has a centerline different from the centerline of the first portion. The second portion of the rigid bar is disposed within the lumen of the collar when the rigid bar is in a first position. The centerline of the first portion of the rigid bar is substantially non-parallel to the centerline of the lumen of the moveable collar when the rigid bar is in the first position. The centerline of the second portion of the rigid bar is substantially non-parallel to the centerline of the lumen when the rigid bar is in the second position. | 2022-09-15 |
20220289382 | SYSTEMS AND METHODS FOR LOADING AND UNLOADING A CARGO AIRCRAFT UTILIZING A CURVED PATH - Systems, methods, and vehicles for loading and unloading cargo into or out of a large transport vehicle, such as an aircraft, utilizing a curved path are described. The systems and methods include one or more support structures disposed, either permanently or removably, within a cargo bay of the transport vehicle to form a curved path extending into an aft portion of the cargo bay. During loading, the payload can move in the aft direction while concurrently rotating about a center point of an arc. In some embodiments, the cargo bay can include a kinked portion disposed between a proximal and aft portions of the cargo bay, with the curved path extending at least through the kinked portion and into the aft portion. Methods, systems, and components thereof for assembling a cargo, unloading cargo from a large transport vehicle, and disassembling a cargo are also provided. | 2022-09-15 |
20220289383 | REMOVABLE CARGO FLOOR SYSTEMS AND METHODS FOR CARGO AIRCRAFT - Systems and methods for removeably adding a cargo bay floor to the interior cargo bay of cargo aircraft bay are disclosed. The system includes a rail disposed in a cargo bay of a cargo aircraft with the rail extending longitudinally along both a length of a forward portion and an aft portion of the fuselage. The system includes a cargo floor segment configured to be removeably attached to the rail. When attached, the cargo floor segment can transform between a first arrangement with the cargo floor segment translatable along the rail, and a second arrangement with the cargo floor segment fixedly secured to a location along the rail. The cargo floor segment is configured to, when secured to the rail, define a section of a floor of the cargo bay of the cargo aircraft. Multiple floor segments can be used together to form a continuous floor for the aircraft. | 2022-09-15 |
20220289384 | SYSTEM AND APPARATUS FOR DETECTING RESTRAINED UNIT LOAD DEVICE USING FLOOR LATCH SENSOR - A unit load device (ULD) for aircraft cargo loading, the ULD including a container having a cargo portion and a ledge extending from the cargo portion. The ledge is configured to interface with a floor latch. A first latch sensor is disposed on the ledge. The first latch sensor is configured to detect a closed latch contact. A controller is electrically connected to the first sensor, and is configured to automatically perform an action in response to the first latch sensor detecting the closed latch contact. | 2022-09-15 |
20220289385 | METHODS AND SYSTEMS TO PROVIDE SERVICE LEVELS FOR AIRCRAFT IN-FLIGHT CONNECTIVITY COMMUNICATION SYSTEMS BASED UPON SSIDS - Methods and systems to provide service levels for aircraft in-flight connectivity network systems based on service set identifiers (SSIDs) are disclosed. A disclosed method includes providing a first wireless access point having a first SSID; providing a second wireless access point having a second, different SSID; segregating users by providing instructions regarding which of the first and second SSIDs to use to access services; tagging first data received via the first SSID with a first differentiated services code point (DSCP) value; tagging second data received via the second SSID with a second, different DSCP value; and handling the first and second data with different service levels based upon the first and second DSCP values. | 2022-09-15 |
20220289386 | Repair and Replacement Mechanism for Personal Control Units on Aircraft - An assembly for opening or accessing an electronic communication and entertainment device holder for repair or replacement of its contents, including a latch which can be released by the contraction of an attached muscle wire actuator in response to a low current pulse sent by an attached wireless receiver. | 2022-09-15 |
20220289387 | AIRCRAFT MONUMENT AND A SEAT ASSEMBLY - An aircraft monument for use in a cabin of an aircraft includes a monument assembly and a seat assembly. The monument assembly includes a frame having a plurality of walls defining a compartment. The plurality of walls include a first end wall having a forward section at a forward plane of the frame. The compartment is defined rearward of the forward section. The seat assembly is forward of the frame. The seat assembly has a shell configured to at least partially surround a passenger seat. The shell has a rear rearward of the forward plane of the frame. | 2022-09-15 |
20220289388 | SUPPLEMENTAL OXYGEN ASSEMBLIES - A supplemental oxygen assembly for a vehicle can include a container and a flow assembly attached to and/or configured to be contained within the container in a stowed position and to extend from the container in a deployed position. The flow assembly can be configured to be connected to an oxygen supply to supply oxygen to a person in the deployed position. The supplemental oxygen assembly can include an extension device connected to the flow assembly. The extension device can be configured to extend or allow extension of the flow assembly toward an aisle of the vehicle to aid the flow assembly in being reached from or moveable toward an aisle of the vehicle by a person in the aisle. | 2022-09-15 |
20220289389 | COCKPIT OF AN AIRPLANE AND METHOD OF OPERATING AN AIRPLANE - A cockpit for an airplane having, in a plan view, an aft direction, a central longitudinal axis parallel to the aft direction and a rear axis perpendicular to the central longitudinal axis. The cockpit as seen in the plan view comprises: a first seat having a first seating surface with a first seat rear edge passing through an intersection between the longitudinal and rear axes, the first seat being disposed within the cockpit and configured so as to allow a pilot sitting on the first seating surface to perform pre-determined primary pilot functions; and a second seat having a second seating surface with a second seat rear edge. The second seat has: an operational state, in which the second seat is disposed within the cockpit and configured so as to allow operational seating of a pilot on the second seating surface to perform pre-determined secondary pilot functions, the second seat rear edge being at an operational distance from the rear axis; and at least one non- operational state, in which the operational seating of the secondary pilot is disabled, the at least one non-operational state comprising a resting state in which the footprint of the second seat in plan view is longer in at least one dimension than the footprint of the second seat in the operational state, allowing a lying-down position of the secondary pilot. | 2022-09-15 |
20220289390 | SEAT RAIL ASSEMBLY FOR FASTENING A SEAT ASSEMBLY IN A VEHICLE, USE OF A SEAT RAIL ASSEMBLY OF THIS TYPE IN AN AIRCRAFT, AND METHOD FOR PRODUCING A SEAT RAIL ASSEMBLY - A seat rail assembly for fastening a seat assembly in a vehicle and a method for making such a seat rail assembly are described. The seat rail assembly includes a seat rail configured to fasten the seat assembly, the seat rail including a metal material. A fastening profile element of the seat rail assembly is configured to receive the seat rail, the fastening profile element being formed of a plastic material. The fastening profile element forms a receiving region, which is configured to receive the seat rail, and the seat rail includes a seat rail crown which is arranged in the receiving region of the fastening profile element such that a wall portion of the fastening profile element at least partly extends around the seat rail crown. The seat rail assembly may be used in an aircraft. | 2022-09-15 |
20220289391 | CABIN PRESSURE CONTROL SYSTEM WITH SELECTION OF RATE OF CHANGE - In some examples, a cabin pressure control and monitoring system includes an outflow valve and a manual control panel comprising a selector switch and configured to generate a signal, wherein a value encoded in the signal is dependent on a position of the selector switch. The cabin pressure control and monitoring system also includes a controller configured to receive the signal from the manual control panel, determine a target rate of change for a cabin pressure based on the value encoded in the signal, and control the outflow valve based on the target rate of change. | 2022-09-15 |
20220289392 | ICE PROTECTION COATING AND BONDING METHODS THEREOF - An airfoil is provided that includes an exterior substrate surface, and a coating layer adjacent to the exterior substrate surface. The coating layer has an icephobic coating composition that includes a first polymer, a second polymer that is a fluoropolymer, an isocyanate, and a curative. The coating layer is bonded to the airfoil via an intermediate adhesive layer. The coating layer has a bottom surface, and at least one of the exterior substrate surface and the bottom surface has an RMS surface roughness of at least about 1 micron or greater before the coating layer is bonded to the exterior substrate surface. | 2022-09-15 |
20220289393 | HYBRID PROPULSION SYSTEMS - An example hybrid aircraft propulsion system includes one or more power units configured to output electrical energy onto one or more electrical busses; a plurality of propulsors; and a plurality of electrical machines, each respective electrical machine configured to drive a respective propulsor of the plurality of propulsors using electrical energy received from at least one of the one or more electrical busses. | 2022-09-15 |
20220289394 | EMBEDDED ELECTRIC MACHINE - A gas turbine engine includes a compressor section and a turbine section together defining a core air flowpath. Additionally, a rotary component is rotatable with at least a portion of the compressor section and at least a portion of the turbine section. An electric machine is mounted coaxially with the rotary component and positioned at least partially inward of the core air flowpath along a radial direction of the gas turbine engine. A cavity wall defines at least in part a buffer cavity surrounding at least a portion of the electric machine to thermally insulate the electric machine, e.g., from the relatively high temperatures within the core air flowpath. | 2022-09-15 |
20220289395 | PROPULSION SYSTEM FOR AIRCRAFT AND METHOD OF MANUFACTURING AIRCRAFT - In a propulsion system for an aircraft, when a flight state of the aircraft is a first state in which the aircraft is cruising, power is supplied to an electric motor from only a high-capacity storage battery. When the flight state of the aircraft is a second state in which the aircraft is taking off or landing, power is supplied to the electric motor from only an output type storage battery when a charge amount of the output type storage battery is equal to or greater than a first threshold, and power is supplied to the electric motor from the output type storage battery and the high-capacity storage battery when the charge amount of the output type storage battery is smaller than the first threshold. | 2022-09-15 |
20220289396 | AIRCRAFT PYLON COMPRISING A TUBULAR PRIMARY STRUCTURE INCLUDING AT LEAST ONE TWIN-WALLED PIPE, AND AIRCRAFT COMPRISING AT LEAST ONE SUCH PYLON - An aircraft pylon comprising a primary structure and a pipe segment having an internal duct positioned inside at least one structural tube primary structure. This solution makes it possible to reduce the crowding outside the structural tubes of the primary structure, makes it easier to integrate other equipment inside the pylon, and may help to improve the aerodynamic performance of the pylon by reducing its cross section. | 2022-09-15 |
20220289397 | FUEL CELL POWERED AIRCRAFT WITH A CATHODE CONVERTIBLE BETWEEN OXYGEN AND AIR AND METHOD FOR USE THEREOF - An aircraft that includes a fuselage, an electric motor driven propulsion system, and a fuel cell system configured to provide electricity to the electric motor. The fuel cell system includes a fuel cell, a hydrogen tank, an oxygen tank, an air channel, and a cathode switch. The cathode switch being configured to convert between an air mode, wherein the fuel cell operates utilizing air from the air channel, and an oxygen mode, wherein the fuel cell operates utilizing oxygen from the oxygen tank. | 2022-09-15 |
20220289398 | TURBOSHAFT ENGINE CLUTCH CONFIGURATION - Gas turbine engines and methods of their operation are provided. For example, a method of operating a gas turbine engine comprises selectively engaging and disengaging an engine clutch disposed between a low speed spool and a rotor assembly of the engine. Engagement or disengagement of the engine clutch is selected based on an operating condition of an aircraft comprising the engine. Further, an inter-spool clutch disposed between the low speed spool and a high speed spool of the engine transitions between engaged and disengaged, disengaging when the high speed spool reaches a speed greater than an operational speed of the low speed spool. Similarly, a gas turbine engine comprises an engine clutch configured to selectively position a low speed spool in operative communication with a rotor assembly and an inter-spool clutch configured to position the low speed spool in operative communication with a high speed spool. | 2022-09-15 |
20220289399 | HEALTH BASED ACTUATOR ALLOCATION - Commands, including a first and second command associated with a first and second rotor module, are determined based at least in part on a set of desired forces or moments and a plurality of health metrics, including by determining a plurality of differences between the plurality of health metrics and a threshold and assigning a lower thrust value to the first command based at least in part on the first difference and a higher thrust value to the second command based at least in part on the second difference, where the first difference indicates a higher degree of wear on the first rotor module than the second difference indicates for the second rotor module. The commands are sent to the rotor modules and after the commands are performed, updated health metrics are determined. | 2022-09-15 |
20220289400 | Method of Adjusting Directional Movement Ability in a Multi-Rotor Aircraft - A method of adjusting a directional movement ability in an aircraft having two or more rotors includes receiving a desired thrust demand for each rotor of the two or more rotors, comparing the desired thrust demands to determine a maximum thrust demand, determining whether the maximum thrust demand exceeds a maximum thrust limit of the two or more rotors, and adjusting each desired thrust demand based on whether the maximum thrust demand exceeds the maximum thrust limit to provide an adjusted thrust demand for each rotor of the two or more rotors. Each rotor can be operated based on a respective adjusted thrust demand. | 2022-09-15 |
20220289401 | FLOW BODY FOR AN AIRCRAFT WITH INTEGRATED GAS TANK - A flow body for an aircraft includes a torsion box with spars and/or ribs and at least two skin portions for enveloping the spars and/or ribs, wherein at least one inner cell is formed in the torsion box. It is provided that a gas tank with a gas tank shell is arranged in the at least one inner cell, and that the gas tank includes fastening elements coupled to retaining elements in the relevant inner cell in order to hold the gas tank such that the gas tank shell is supported at a distance from the spars and/or ribs and the skin portions and is supported in three spatial directions. | 2022-09-15 |
20220289402 | PASSENGER BOARDING BRIDGE - Provided is a passenger boarding bridge that includes: a rotunda connected to a terminal building and supported in a horizontally rotatable manner; a tunnel unit whose proximal end is connected to the rotunda, the tunnel unit being extendable and retractable; a travel device that supports the tunnel unit and includes travel wheels, the travel device being configured such that a travel direction of forward travel of the travel wheels and a travel direction of backward travel of the travel wheels are changeable; a cab provided at a distal end of the tunnel unit, the cab being configured to be docked with an aircraft; and a determiner configured to, at a time before undocking the cab docked with the aircraft from the aircraft, perform determination whether or not the travel direction of the backward travel of the travel wheels at the time is a direction within a smooth undocking range. | 2022-09-15 |
20220289403 | SYSTEM AND METHOD FOR AUTOMATED SURFACE ANOMALY DETECTION - A system for automated surface anomaly detection includes at least one processor which is configured to retrieve from non-volatile memory a 3D control image; capture a 3D target image depicting at least the portion of the exterior of a target object; generate 2D target planar images of the target object based on the 3D target image, using a first plurality of virtual cameras; generate 2D control planar images of the control object based on the 3D control image using a second plurality of virtual cameras, the 2D control planar images corresponding to the 2D target planar images of the target object; detect at least one difference between the 2D target planar images and the 2D control planar images; and generate and cause to be displayed an output image comprising a depiction of the target object with the at least one difference indicated. | 2022-09-15 |
20220289404 | ORBITAL MECHANICS OF IMPULSIVE LAUNCH - Methods of launching a vehicle using impulsive force are disclosed. In one instance, a vehicle is launched easterly with impulsive force in a plane corresponding to the vehicle's elliptical orbital path. In another instance, a method of closing a timing difference is disclosed. The vehicle undergoes a series of forces after impulsive launch. The first force establishes an orbit having a period significantly different from the orbital period of a satellite or desired vehicle location, closing the difference in an integer number of orbits. The second force establishes the vehicle in circular orbit with the satellite or desired vehicle location. In another instance, the vehicle launched impulsively from a first celestial body travels a first path, and the vehicle experiences a second force along a hyperbolic path about the second celestial body and enters circular orbit about the second celestial body. | 2022-09-15 |
20220289405 | MULTI-PURPOSE PLANET ROVER - A multi-purpose planet planetary exploration rover is provided in this invention, which relates to the field of planet exploration. The multi-purpose planetary exploration rover includes a case body, mounted with a first wheel at left and right sides respectively; and a cantilever, having a front end connected to the case body, a rear end of the cantilever being mounted with a second wheel; wherein the cantilever is rotated or fixed relative to the case body, the second wheel is steered relative to the cantilever, and the first wheel and the second wheel are used to drive the multi-purpose planetary exploration rover. Compared with the prior art, the multi-purpose planetary exploration rover of this invention can effectively explore special geographic locations such as cliffs, volcanic craters, craters and lava caves on alien planets. | 2022-09-15 |
20220289406 | DEPLOYABLE STRUCTURES - The present disclosure relates to deployable structures, to methods and apparatus for deployment of deployable structures, and to associated manufacturing methods. Such deployable structures suitably comprise components for space structures, such supports for solar arrays, antennas or other similar systems. The deployable structure ( | 2022-09-15 |
20220289407 | Multifunctional Structures for Attitude Control - A structure for changing the attitude of a spacecraft is provided including an elongated member and a plurality of actuators coupled to the elongated member. The elongated member is coupled to the spacecraft. The elongated member has a length and an angular position relative to an axis. The plurality of actuators are configured to deflect the angular position of the elongated member relative to the axis and to alter the length of the elongated member. | 2022-09-15 |
20220289408 | OBSERVATION CONTROL DEVICE, OBSERVATION SYSTEM, SPACECRAFT, OBSERVATION CONTROL METHOD, AND OBSERVATION CONTROL PROGRAM - The purpose of the present invention is to provide an observation control device, an observation system, a spacecraft, an observation control method, and an observation control program which enable stable observation. An observation control device | 2022-09-15 |
20220289409 | APPARATUS FOR FILLING FOOD CONTAINERS AND CORRESPONDING METHOD - Described is an apparatus for filling food containers, including:
| 2022-09-15 |
20220289410 | APPARATUS AND METHOD FOR IMPORTING FLUID, METHOD FOR TEARING FILM, AND AIR EXTRACTING DEVICE - An apparatus and a method for importing fluid, and a method for tearing film are provided. The apparatus imports fluid into a product and tears a breathable film covered on the product, the product defines a vent in a surface, the breathable film covers on the vent. The apparatus includes a transfer assembly and a controller. The breathable film is connected to the transfer assembly. The controller is coupled to the transfer assembly and configured to control the transfer assembly to vertically move relative to the surface of the product to tear the breathable film from the vent. | 2022-09-15 |
20220289411 | BAGMAKING AND PACKAGING DEVICE AND TUBE MEMBER FOR BAGMAKING AND PACKAGING DEVICE - A bagmaking and packaging device includes a transverse sealing unit, a first tube member, and a gas flow path member. The first tube member is disposed above the transverse sealing unit and extends in an up and down direction. The first tube member allows a packaging material to become wrapped around it to thereby form the packaging material into a tubular shape. At least part of the gas flow path member is disposed inside the first tube member. The gas flow path member delivers nitrogen into the packaging material formed into the tubular shape. The first tube member includes a cutout portion that extends in the up and down direction. The cutout portion is formed so that the nitrogen can move between a space between the packaging material formed into the tubular shape and the first tube member and the inside space of the first tube member. | 2022-09-15 |
20220289412 | TAPING APPARATUS AND TAPING METHOD - Disclosed is a taping apparatus including: a tray storage device supplying a designated one of plural kinds of trays on which respective different kinds of parts are scattered; a carrier tape feed device intermittently moving a designated one of plural kinds of carrier tapes which correspond to the respective different kinds of parts; a first camera capturing an image of the scattered parts on the designated tray; a first image recognizing device recognizing respective centers of the scattered parts; a rotary head individually sucking the scattered parts to rotatable suction nozzles; a second camera capturing an image of the parts sucked to the suction nozzles; a second image recognizing device recognizing respective orientations of the sucked parts; and a part inserting device adjusting the orientations of the sucked parts to orientations insertable into part storage recesses defined in the designated carrier tape and then inserting the parts into the part storage recesses, respectively. | 2022-09-15 |
20220289413 | PACKAGING MACHINE FOR MAKING FILTER BAGS WITH INFUSION PRODUCTIONS - A packaging machine for making filter bags with infusion products includes a plurality of processing stations defining a processing path for making filter bags with infusion products and an extraction station situated immediately downstream of the processing path. The extraction station comprises a stacking unit having a guide channel to allow the ordered and continuous feeding of the filter bags and a transfer device for transferring the filter bags coming from the processing path to the stacking unit. The stacking unit includes a connecting element positioned downstream of the processing stations and upstream of the guide channel for receiving as input from the transfer device the filter bags coming from the processing path. The connecting element is connected at the outlet with the guide channel and includes a chute surface having a curved stretch shaped to allow feeding of the filter bags along a feed direction. | 2022-09-15 |
20220289414 | TRIPLE CENTER SEALING DEVICE IN PILLOW PACKAGING MACHINE - The present invention relates to a triple center sealing device in a pillow packaging machine. To this end, the present invention comprises: a plurality of film supply rollers ( | 2022-09-15 |
20220289415 | METHOD AND APPARATUS FOR PACKAGING OBJECTS OF DIFFERENT TYPES - A method comprises the steps of:
| 2022-09-15 |
20220289416 | A METHOD AND AN APPARATUS FOR FILLING CONTAINERS WITH FOOD ITEMS - A system is provided for placing food items into containers such that the containers fulfil at least one criterion. The system has handling devices arranged along a conveyor belt of a conveyor system and a control unit connected to a position tracker for controlling the handling devices using position data from the position tracker. | 2022-09-15 |
20220289417 | Method and Device for Attaching Carrying Handles to Packaging Means or Groups of Packaging Means - A handle applicator includes controller that receives signals concerning marks on an endless band. The controller controls a contact body to be between a release position, in which a handle applicator is freely driven and a drawing position, in which the contact body contacts the endless band of material prior to its being cut to form the handle. The contact body moves along a continuum of positions between the release position and the drawing position based on actual position data indicative of actual positions of position markings on the handle. | 2022-09-15 |
20220289418 | CUP SEALING APPARATUS - A cup sealing apparatus with a shaft, a heating element, an alignment plate, and a spring biasing the alignment plate into engagement with the alignment cone. The shaft extends has an alignment cone at an end thereof, the alignment cone having a modified cone taper surface centered about a longitudinal axis. The heating element includes a heating surface operable to adhere a seal to a cup presented to the heating surface. The alignment plate is spaced from the opposite axial surface, and has a profile corresponding with the taper surface so that the profile and the taper surface form a non-circular interface between the alignment cone and the alignment plate. With deflection of the spring, the alignment plate and the heating element are free to deviate from a prescribed orientation and out of coaxial alignment to match a cup axis of a cup presented to the heating surface. | 2022-09-15 |
20220289419 | SYSTEM FOR MANUFACTURING CARDBOARD BOX WITH ELECTRONIC TAG AND METHOD THEREFOR - A system of manufacturing a corrugated cardboard box to which an electronic tag is attached. The system includes: a corrugated cardboard sheet forming part that forms a corrugated cardboard sheet | 2022-09-15 |
20220289420 | LABELER WITH PUSHER ASSEMBLY - A labeler comprises at least one pusher assembly for pressing labels onto an article web, the pusher assembly being mounted to be adjustable in height. The pusher assembly comprises a base plate, at least one pin cartridge connected to the base plate, and several press-on pins that are received by the pin cartridge and that are mounted at the pin cartridge in a slidable manner between a respective extended position and a retracted position. The press-on pins are each formed as integrally manufactured injection molded parts. | 2022-09-15 |