45th week of 2017 patent applcation highlights part 19 |
Patent application number | Title | Published |
20170320549 | HEAT-INSULATION SYSTEM FOR LIQUEFIED NATURAL GAS CARGO HOLD - Disclosed is a heat-insulation system for a liquefied natural gas cargo hold, which comprises a primary sealing wall, a secondary sealing wall, and a secondary heat-insulating layer, and is applied to a liquefied natural gas cargo hold. The heat-insulation system for a liquefied natural gas cargo hold comprises a collar stud installed on a line on the upper surface of the secondary heat-insulating layer where an anchor strip is installed. | 2017-11-09 |
20170320550 | VESSEL WITH UNITARY BOW DOOR AND MULTI-FOLD RAMP - A powered water vessel includes a unitary section of the bow that is pivotably rotatable about a horizontal axis thereby permitting a closed-bow configuration and an opened-bow configuration. The closed-bow configuration is generally amenable to regular boat operations, while the opened-bow configuration is generally amenable to loading and unloading passengers, vehicles and/or cargo. A folding ramp assembly is extendable through the open-bowed configuration for loading and unloading, with track extensions providing additional extension distance. | 2017-11-09 |
20170320551 | CUSHIONS FOR USE IN SEATING FOR BOATS AND METHODS OF USING SAID CUSHIONS - Cushions for use in seating for boats and methods of using the same. According to one embodiment, the cushion is designed for use with a bucket-type boat seat and includes an insert and a casing. The insert has a J-shape and is made up of three foam pads joined to one another, with a first of the foam pads designed to be positioned over the boat seat, with a second of the foam pads designed to be positioned in front of the boat seat, and with a third of the foam pads designed to be positioned under the boat seat. The casing preferably conforms substantially to the shape of the insert and is designed to permit the insert to be inserted into and/or removed from the casing. The cushion additionally includes a fastener coupled to the casing for use in securing the casing to the boat seat. | 2017-11-09 |
20170320552 | BOAT APPARATUS FOR PRODUCING A SURF WAKE - A boat propeller apparatus can be coupled to virtually any motor boat to cause the boat to safely and efficiently produce a surfable wake. The boat propeller apparatus can be configured to mount to the boat in a way that causes the apparatus to be positioned and secured behind but spaced from the propeller while the boat is moving forward. The apparatus will therefore be in the path of the propelled water and will function to divert the propelled water in such a way as to create a larger/taller wake than would otherwise be produced by the boat. The boat propeller apparatus can also function as a propeller shield and be used in conjunction with a propeller guard. | 2017-11-09 |
20170320553 | FLUID HINGES FOR TRIM TAB CONNECTIONS - A fluid hinge includes a first part of a two-part element including a planar surface of a trim tab and a second part of the two-part system having at least one bracket secured to the hull of a watercraft and the first and second parts of the two-part element are not physically coupled together. It also provides at least one bracket secured to the hull on which the planar surface of the trim tab may rest and the at least one bracket not taking any load from the planar surface except at rest to keep the planar surface from descending below the horizon of the hull. | 2017-11-09 |
20170320554 | Combination of propulsion group and marine vessel, propulsion method of a marine vessel, and propulsion group for marine vessel - Combination of marine vessel and outboard motor, wherein at least one outboard motor is attached in a predetermined position to the transom of the marine vessel, the motor being mounted so as to translate according to a path with at least one motion component having an orientation parallel to the direction of the transverse axis of the hull and/or parallel to the transom of said hull and alternatively towards one or the other side of the hull. | 2017-11-09 |
20170320555 | SHIP EMERGENCY STOPING - The present application relates generally to a control arrangement for controlling at least two azimuthing propulsion units of a ship. The control arrangement comprises a crash stop activation member for activating a crash stop procedure, after which the crash stop procedure is executed in which the orientation and propulsion speed of the azimuthing propulsion units are controlled until the propagation speed of the ship has at least been reduced from the moment when the crash stop procedure was activated. | 2017-11-09 |
20170320556 | TRANSLUCENT PANEL SYSTEM - A translucent panel system comprising a panel ( | 2017-11-09 |
20170320557 | SYSTEM FOR MANUFACTURE OF FOAM SHEET RIGIDIZED WITH POLYMER INFILTRATION - A rigid polymer porous material sheet is produced by feeding a slurry of polymer mixture comprising ultrafine polyvinylchloride particle, non-phthalate plasticizer, foaming agent and thermal stabilizer, polymer chips, fillers and fire retardant chemicals into a heated mold and pressing the mixture with high applied pressure. The temperature of the mold is below 190° C. to soften the polymer mixture and decompose the foaming agent forming the closed cell polyvinylchloride foam with 10 to 40% density with closed air cells. The thermal resistance of the rigid polymer porous sheet and sound attenuation properties are significantly improved. The rigid polymer porous sheet can be bent at sharp angles without crack formation facilitating its use as wall boards. The sheets produced may be embossed or molded to produce decoration boards, advertising boards, cabinet doors and furniture with decorative features. They can also be used in aeronautical applications as acoustic thermal insulation systems. | 2017-11-09 |
20170320558 | FLIGHT VEHICLE GENERATING A LIFT FROM AN INTERIOR THEREOF - The invention discloses a flight vehicle generating a lift from an interior thereof. The fluid channel inside the flight vehicle communicates with the engine and the ports on the upper surface of the outer shell. With the powerful suction of the engine, the fluid on the upper surface of the outer shell is quickly sucked into the fluid channel via respective ports under conditions of long path, large area, high speed and low air pressure, which results in large lift from the interior of the flight vehicle. In the course of generating the lift, the fluid resistances of the fluid wall and the fluid hole are sucked into the fluid channel through the ports at the front and the surrounding area of the flight vehicle, then high-speed fluid is emitted from the rear port. This approach contributes greatly to the transformation of the existing flight vehicle. The present invention significantly improves the lift, the speed and the carrying capacity of the existing flight vehicle with lowered energy consumption. | 2017-11-09 |
20170320559 | SOLID-LIQUID COMPOSITE STRUCTURES - A pressurized, fluid-filled channel network embedded in an elastic structure, asymmetrically to the neutral plane, is used to create a deformation field within the structure by the pressurization of the embedded fluidic network, which can be applied in accordance with external forces acting on the structure. The deformation of the structure resulting from the liquid pressure and geometry of the network is related to a continuous deformation-field function. This enables the design of networks creating steady arbitrary deformation fields as well as to eliminate deformation created by external time varying forces, thus increasing the effective rigidity of the beam. By including the effects of the deformation created by the channel network on the beam inertia, the response of the beam to oscillating forces can be modified, enabling the design of channel networks which create pre-defined oscillating deformation patterns in response to external oscillating forces. | 2017-11-09 |
20170320560 | Mechanical Fastening System and Associated Structural Assembly and Method - A structural assembly including a first structural member defining a first partial bore and including a first protrusion extending from a periphery of the first partial bore on a first side and a second protrusion extending from the periphery of the first partial bore on a second side, a second structural member defining a second partial bore and including a first protrusion extending from a periphery of the second partial bore on a first side and a second protrusion extending from the periphery of the second partial bore on a second side, wherein the second partial bore is aligned with the first partial bore to define a through-bore, a first engagement member engaged with the first protrusions and a second engagement member engaged with the second protrusions, wherein the first and second structural members are clamped between the first and second engagement members. | 2017-11-09 |
20170320561 | AIRCRAFT EMPENNAGE - An aircraft aerodynamic surface ( | 2017-11-09 |
20170320562 | ROTOR OR PROPELLER BLADE WITH DYNAMICALLY VARIABLE GEOMETRY AND OTHER PROPERTIES - A blade is provided for the cycloidal marine propellers or cycloidal aerial rotors. Said blade is provided with the capabilities, in response to the control system commands to dynamically and in real time; flex itself along its chord in any required way, vary its relative pivot point position, change its planform by extending or retracting a trailing edge extension, differentially if needed on the right and left, turn the flap along the trailing edge in either direction or allow it to be turned by the flows. Said blade is also optionally provided with one or more elastic trailing edges whose stiffness is dynamically, and possibly differentially along the blade span, variable by the control system. For the reversal of the leading and trailing edges for operation in reverse airflow and other conditions the blades are provided with edges that can be made rigid when functioning as the leading edge and flexible if needed when functioning as the trailing edge. Also the blades are provided with the capability of varying their cross-sectional profile thickness and reshaping it. Finally the blades are given on command flow permeability along much of their surface. These capabilities will enable each control system controlled blade to continually optimally adjust to and make the best use of its immediate operating environment as it travels along its trajectory within each revolution. | 2017-11-09 |
20170320563 | AIRCRAFT PROVIDED WITH A BUOYANCY SYSTEM, AND A BUOYANCY METHOD - An aircraft having an airframe that extends longitudinally along an anteroposterior plane. A buoyancy system is provided with at least one pair of two floats arranged transversely on opposite sides of said anteroposterior plane. Each float is movable in elevation from a bottom position to a top position. For each float, the buoyancy system includes a blocking system for blocking each float by default in the bottom position, and for acting under a predetermined condition to block the floats present on one of the sides only of the aircraft in the top position. | 2017-11-09 |
20170320564 | AIR WHEEL ROTOR, A GYRO STABILIZED AIRCRAFT AND A WIND-DRIVEN POWER GENERATOR USING THE AIR WHEEL ROTOR, AND A STATIONARY LAUNCHING DEVICE - The ‘Air Wheel’ rotor is a rotor with blades of variable pitch and variable twist. The ‘Air Wheel’ rotor comprises one or more hubs connected to the closed axisymmetric wing via flexible blades. There is provided a wide range of combinations of the wing relative width and coning angle typical for a lifting rotor with a thin planar wing attached to the tips of long blades, for a shrouded fan in a wide annular wing, or an impeller in a rotating cylindrical wing is provided. | 2017-11-09 |
20170320565 | HINGE MECHANISM FOR A WEIGHT-SHIFTING COAXIAL HELICOPTER - A helicopter includes a gimbal assembly, a first rotor assembly, a second rotor assembly, a fuselage, and a controller. The first rotor assembly, the second rotor assembly, and the fuselage are mechanically coupled to the gimbal assembly. The first rotor assembly includes a first rotor and the second rotor assembly includes a second rotor, the first rotor including a plurality of first fixed-pitch blades and the second rotor including a plurality of second fixed-pitch blades. Each of the plurality of first and the second fixed-pitch blades are coupled to a hub of its respective rotor via a hinge mechanism that is configured to allow each of the fixed-pitch blades to pivot from a first position to a second position, the first position being substantially parallel to the fuselage and the second position being substantially perpendicular to the fuselage. | 2017-11-09 |
20170320566 | SYSTEM FOR DRIVING A SLAT DEVICE OF AN AIRCRAFT WING - Disclosed herein is an exemplary embodiment of a system for driving a slat of an aircraft. The system includes first and second hinge support elements of a wing structure, a first arm device, a second arm device, and a third arm device. Also disclosed is an aircraft having the system, an aircraft wing having the system, and a method for driving a slat of an aircraft. The system utilizes a particular configuration of connection junctions, which rotatably connect the arm devices and the hinge support elements. | 2017-11-09 |
20170320567 | Rotor Assembly with High Lock-Number Blades - An aircraft rotor assembly has a central hub and a plurality of rotor blades coupled to the hub for rotation with the hub about an axis, each blade having a Lock number of approximately 5 or greater. A lead-lag pivot for each blade is formed by a flexure coupling the associated blade to the hub. Each pivot is a radial distance from the axis and allows for in-plane lead-lag motion of the associated blade relative to the hub, each pivot allowing for in-plane motion from a neutral position of at least 1 degree in each of the lead and lag directions. Elastic deformation of the flexure produces a biasing force for biasing the associated blade toward the neutral position, and the biasing force is selected to achieve a first in-plane frequency of greater than 1/rev for each blade. | 2017-11-09 |
20170320568 | Aircraft - An electrically powered vertical takeoff and vertical landing (VTOL) aircraft, which comprises at least two main propellers, wherein the main propellers are adapted to generate at least 70% of the aircraft propulsion. The aircraft also comprises at least one adjustment propeller, which has its propeller slipstream adapted to produce a torque relative to a first axis or the first and second axes with respect to a fuselage of the aircraft for turning the aircraft relative to said first axis or said first and second axes. In addition, not less than 35%, but not more than 85%, of the aircraft's mass is adapted to lie, during takeoff and/or landing, on a rear side of a propeller line of said main propellers with respect to a nose of the aircraft. | 2017-11-09 |
20170320569 | ALERT SYSTEM FOR AN UNMANNED AERIAL VEHICLE - An unmanned aerial vehicle for aerial transportation of delivery items. The unmanned aerial vehicle includes an attachment device to fasten and unfasten one or more delivery items to the unmanned aerial vehicle, a motor to aerially transport the one or more delivery items along a delivery route, a sensor mounted on the unmanned aerial vehicle to detect at least one environmental variable during the delivery route, and an alert system to generate a status associated with the unmanned aerial vehicle along the delivery route to an observer when the environmental variable exceeds a predetermined threshold. | 2017-11-09 |
20170320570 | UNMANNED AERIAL VEHICLE (UAV) HAVING VERTICAL TAKEOFF AND LANDING (VTOL) CAPABILITY - An unmanned aerial vehicle (UAV), or drone, includes a fuselage, left and right airfoil-shaped wings connected to the fuselage to generate lift in forward flight, a left thrust-generating device supported by the left wing, and a right thrust-generating device supported by the right wing. The UAV further includes a vertical stabilizer, a top thrust-generating device mounted to a top portion of the vertical stabilizer, and a bottom thrust-generating device mounted to a bottom portion of the vertical stabilizer. An onboard power source is provided for powering the thrust-generating devices. The left, right, top and bottom thrust-generating devices provide forward thrust during forward flight and also provide vertical thrust to enable the unmanned aerial vehicle to take-off and land vertically when the fuselage is substantially vertical and further enabling the unmanned aerial vehicle to transition between forward flight and vertical take-off and landing. | 2017-11-09 |
20170320571 | ROTARY PROPELLER DRONE WITH INTEGRATED POWER STORAGE - A rotational power device including a blade having a core formed by battery material as a power source. | 2017-11-09 |
20170320572 | SYSTEMS AND METHODS FOR TRANSPORTING PRODUCTS VIA UNMANNED AERIAL VEHICLES - In some embodiments, methods and systems of facilitating movement of product-containing pallets include at least one forklift unit configured to lift and move the product-containing pallets, at least one motorized transport unit configured to mechanically engage and disengage a respective forklift unit, and a central computer system in communication with the at least one motorized transport unit. The central computer system is configured to transmit at least one signal to the at least one motorized transport unit. The signal is configured to cause the at least one motorized transport unit to control the at least one forklift unit to move at least one of the product-containing pallets. | 2017-11-09 |
20170320573 | METHOD AND SYSTEM FOR DELIVERING BIODEGRADABLE SHELLED PORTIONS - A method of delivering over the air, shelled portions of fluids or granular substances containing effective ingredients, to a target, includes the following stages: selecting a type and a size of the shelled portions containing the required effective ingredients, based on mission parameters and physical data of a scene containing the target; conveying the shelled portions to a delivery point, based on the mission parameters and the physical data; and ballistically delivering the shelled portions towards the target, wherein the shelled portions comprise fluids or granular substances covered by shells that provide the shelled portions a ballistic coefficient that is significantly higher than a ballistic coefficient of similar portions without the shells. | 2017-11-09 |
20170320574 | METHODS AND SYSTEMS FOR PROVIDING A SAFETY APPARATUS TO DISTRESSED PERSONS - Various embodiments of the present invention comprise systems for providing a lifesaving apparatus to a distressed individual. Such systems may comprise an unmanned aerial vehicle (UAV) configured to selectably support a lifesaving apparatus. The UAV may comprise a release mechanism configured to release the lifesaving apparatus when proximate a distressed person. The system may additionally comprise a control device configured to wirelessly communicate with the UAV such that a user can pilot the UAV from a distance and deliver the lifesaving apparatus to a distressed person. Methods of using the same may comprise piloting the UAV proximate a distressed person, providing a signal to the UAV to release the lifesaving apparatus by operating the release mechanism, and then pulling the lifesaving apparatus and the distressed person to safety via a control line secured to the lifesaving apparatus. | 2017-11-09 |
20170320575 | FAUCET FOR WATER SUPPLY SYSTEM FOR AIRCRAFT - A faucet for a water supply system for an aircraft includes a body portion having a water passage formed therein, and an adapter removably mounted to a discharge portion of the body portion, wherein the adapter is configured so that a mounting member is received within a casing, and the mounting member includes an orifice, a negative pressure forming chamber through which water having passed through the orifice flows, and an air passage hole communicated with the negative pressure forming chamber and mixing air taken in from an exterior of the adapter. | 2017-11-09 |
20170320576 | GREY WATER INTERFACE VALVE LIQUID LEVEL SENSOR SYSTEM - Embodiments of the present disclosure generally provide a grey water interface valve liquid level sensor system. The liquid level sensor system may deliver information about the water level and the water movement that occurs in a water reservoir. A control unit may then activate a valve to open so that the water can be removed via vacuum. | 2017-11-09 |
20170320577 | SYSTEM AND METHOD FOR DISPOSING OF FLUID FROM A KITCHEN SINK - A fluid-disposing system for a galley sink includes: a galley sink for a galley cabin monument, a self-regulating valve, a control unit, a sensor, and a signal connection between the sensor and the control unit. The valve input is connected to a fluid line, connected to a drainage opening of the galley sink. The valve is arranged underneath the drainage opening, such that fluid from the galley sink can flow through the associated drainage opening into the fluid line. The valve output is designed to be couplable with a source of negative pressure. The valve is designed to automatically open at a predetermined amount M | 2017-11-09 |
20170320578 | Aircraft Passenger Seat Fixing Systems and Arrangements - An aircraft passenger seating system comprises an array of floor panels ( | 2017-11-09 |
20170320579 | SEATING SUSPENSION DIAPHRAGM HAVING INTEGRATED SLIDE-IN ATTACHMENT MEANS - A method of upholstering a seat having a seating frame, and a corresponding attachment assembly, comprises providing a diaphragm generally having a weave of warp and weft yarns with an attachment member for installation of the diaphragm to the seat. The attachment member comprises an adapter strip and a coil member. The coil member is adapted to be intertwined with the weave of the diaphragm and thereafter inserted into and held by the channel in the seating frame. The adapter strip may be connected to the coil member to facilitate feeding the assembly through the channel in the seating frame. Alternately, the adapter strip can replace the channel in the seating frame and instead provide a mounting structure to which the diaphragm can be attached through the coil member's engagement with the adapter strip. A retainer sheet may also be used to maintain a desired tension of the diaphragm during installation. | 2017-11-09 |
20170320580 | Expandable aircraft monument, and aircraft area having an expandable aircraft monument - An aircraft monument for installation in an aircraft cabin. The aircraft monument comprises a movable side wall that is configured for separating the aircraft monument from a passenger area of the aircraft cabin, and that is configured for being moved. The aircraft monument further comprises at least one seat that is fastened to the movable side wall. Also disclosed is an aircraft area having a main aisle that extends along a longitudinal axis of an aircraft cabin, and having an aircraft monument situated next to the main aisle. Also disclosed is an aircraft that includes at least one aircraft area. | 2017-11-09 |
20170320581 | DEPLOYABLE SEAT ASSEMBLY, SYSTEM, AND METHOD FOR AN INTERIOR CABIN OF A VEHICLE - A vehicle includes an interior cabin including a floor and a ceiling. A deployable seat assembly is moveably coupled to the ceiling. The deployable seat assembly is moveable between a stowed position in which at least a portion of the deployable seat assembly is stowed within a stowage space within the ceiling, and a deployed position in which the deployable seat assembly extends between the ceiling and the floor. | 2017-11-09 |
20170320582 | HUMAN FACTORS APPROACH TO CONTROL CONTAMINANT CONCENTRATIONS IN AIRCRAFT SUPPLY AIR FROM ENGINE AND APU BLEED AIR AND GROUND AIR SOURCES, AND IN RECIRCULATED AIR BEING DELIVERED TO AIRCRAFT CABINS FOR THE OPTIMIZATION OF USER EXPERIENCE AND ENERGY CONSUMPTION - An Environmental Control System includes a sensor, an air purification subsystem, and a controller in communication with the sensor and air purification subsystem. The sensor detects a contaminant in the air and generates a contaminant signal. The controller compares the contaminant signal to a predicted sensory response threshold. When the contaminant signal reaches the predicted sensory response threshold, the controller commands the air purification subsystem to alter a condition in the air. | 2017-11-09 |
20170320583 | SYSTEMS AND METHODS FOR RETAINING REMOVABLE PANEL WHEN DEPLOYING EVACUATION SYSTEM - Systems and methods for evacuation systems are provided. A evacuation system for an aircraft may include a packboard, an inflatable, a blow-out panel for the packboard, and a plurality of straps coupled to the blow-out panel. A first strap is coupled between an inner surface of the blow-out panel and the packboard and a second strap is coupled between the inner surface of the blow-out panel and the inflatable. The first strap is coupled to the blow-out panel in close proximity to a first edge of the blow-out panel and the second strap is coupled to the blow-out panel in close proximity to a second edge of the blow-out panel, the first edge being positioned opposite the second edge of the blow-out panel. The blow-out panel may be retained to the evacuation system after the inflatable is deployed. | 2017-11-09 |
20170320584 | HYBRID GAS-ELECTRIC TURBINE ENGINE - A hybrid gas-electric turbine engine for turboprop or turboshaft applications is disclosed together with associated methods. In various embodiments disclosed herein, the turbine engine comprises a turbine configured to be driven by a flow of combustion gas; a turbine shaft configured to be driven by the turbine and transfer power to a load coupled to the turbine engine and an electric motor configured to transfer power to the load coupled to the turbine engine. The rotor may have a rotor axis of rotation that is radially offset from a shaft axis of rotation of the turbine shaft. In some embodiments, the electric motor may be a multi-rotor electric motor. | 2017-11-09 |
20170320585 | OPTIONALLY HYBRID POWER SYSTEM - The disclosure is directed to an optionally hybrid power system that may operate either as a traditional power system, deriving power from a single power source, or as a hybrid power system, deriving power from multiple types of power sources. An example optionally hybrid power system may include a gas turbine engine and one or more electric motors. When configured as a traditional power system the optionally hybrid power system may derive all power from the gas turbine engine. However, when configured as a hybrid power system, the one or more motors may be coupled to the optionally hybrid power system to supplement the power produced by the gas turbine engine. Additionally, an operator interface that may control the optionally hybrid power system may select from a plurality of operating modes that depend on the configuration of the optionally hybrid power system. | 2017-11-09 |
20170320586 | ENGINE DEGREDATION MANAGEMENT VIA MULTI-ENGINE MECHANICAL POWER CONTROL - A multi-engine power system is described that includes at least a first engine and a second engine configured to jointly provided mechanical power to the multi-engine power system. The multi-engine power system further includes a controller configured to estimate a deterioration factor of the first engine. The controller is further configured to adjust, based on the deterioration factor of the first engine, a first amount of mechanical power being provided by the first engine to increase a service time of the first engine, and adjust, based on the first amount of mechanical power being provided by the first engine, a second amount of mechanical power being provided by the second engine to compensate for the adjustment to the first amount of mechanical power. | 2017-11-09 |
20170320587 | Method And System For The Circulation Of Fuel In An Aircraft - A method for the circulation of fuel in an aircraft uses at least one diaphragm pump having an undulating diaphragm that can undulate between two flanges, under the action of an actuator, for circulating the fuel between an admission line of the pump and an exhaust line of the pump. | 2017-11-09 |
20170320588 | FLEXIBLE FUEL TANK HAVING ELECTROSTATIC CHARGE DISSIPATING PROPERTIES - A flexible fuel tank ( | 2017-11-09 |
20170320589 | METHODS AND SYSTEMS FOR CONVEYING DESTINATION VIABILITY - Methods and systems are provided for facilitating analysis and selection of a destination for operating a vehicle. One exemplary method facilitating analysis of landing an aircraft at an airport involves displaying a map of the airport that includes a graphical representation of a runway at the airport, determining a runway viability parameter for the runway using current status information associated with one or more of the aircraft and the airport, and displaying indicia of the runway viability parameter on the map in graphical association with the graphical representation of the runway, thereby providing indication of the value or state of the runway viability parameter for that runway on the airport map. | 2017-11-09 |
20170320590 | Task-based Health Data Monitoring of Aircraft Components - Systems, methods and non-transitory computer readable storage medium are provided for task-based health data monitoring relating to aircraft components of aircraft within an aircraft fleet. One method includes establishing a review item with a first data review state to create a review task relating to health data of an aircraft component, generating images relating to the review item for display on a display device, retaining the review item for monitoring responsive to receiving user input changing the first data review state of the review item to a second data review state, receiving new health data relating to the aircraft component and automatically resetting the review item from the second data review state to the first data review state responsive to receiving the new health data to create a new review task. | 2017-11-09 |
20170320591 | SUPPORT FOR A RADIO EQUIPMENT OF AN AIRCRAFT, RADIO SYSTEM AND AIRCRAFT - A support device for a radio equipment of an aircraft, radio system and aircraft are provided. The support device includes a fastening structure ( | 2017-11-09 |
20170320592 | APPARATUS AND METHOD FOR LAUNCH AND RECOVERY OF AN UNMANNED AERIAL VEHICLE - An apparatus for launch and recovery of an Unmanned Aerial Vehicle (UAV), a method for launching a UAV, a method for recovering a UAV and a kit of parts for launch and recovery of a UAV. The apparatus comprises a boom having a center member for receiving the UAV, and first and second arm members extending outwardly and upwardly from the center member, wherein the boom is configured to be lifted to a predetermined height into the air from a reference point; and wherein the boom is movable in the air to an operating position forward of the reference point. | 2017-11-09 |
20170320593 | HELIPAD AND HELIPAD ILLUMINATION SYSTEM - Helipad and helipad illumination system The invention relates to a dynamic helipad illumination system ( | 2017-11-09 |
20170320594 | TOWING SYSTEM FOR A TRAVELLING MACHINE, IN PARTICULAR FOR A HELICOPTER - A towing system comprises a bar, a first attachment device arranged at a first end of the bar, the first attachment device being able to attach the towing system to a towing vehicle, a second attachment device arranged at a second end of the bar, the second attachment device being able to attach the towing system to a travelling machine to be towed, the second attachment device comprising a fork able to hold at least one wheel of the travelling machine, the fork having two longitudinal members between which at least one wheel of the travelling machine is able to be received, a separation device able to modify the spacing between the two longitudinal members and a holding device able to hold the wheel between the two longitudinal members. | 2017-11-09 |
20170320595 | AIRCRAFT WING REPAIR METHODS - A wing skin, which was secured to a wing structure by a plurality of fasteners extending through the wing skin, is removed from the wing and aligned with a template. Template holes are drilled through the template corresponding to each of the fastener holes of the wing skin. The template is then aligned with a new wing skin, and pilot holes are drilled through the new wing skin corresponding to each of the template holes. The new wing skin is then aligned with the wing structure such that the pilot holes permit access to corresponding fastener holes of the wing structure. A mill bit is then positioned through each pilot hole and aligned with the center of the corresponding consumable bushing in the fastener hole of the wing sub-structure, and the skin pilot holes are milled to form fastener holes in the new wing skin aligned with existing sub-structure. | 2017-11-09 |
20170320596 | CONSUMABLE BUSHING FOR USE WITH AIRCRAFT WING REPAIR SYSTEMS AND METHODS - A wing skin, which was secured to a wing structure by a plurality of fasteners extending through the wing skin, is removed from the wing and aligned with a template. Template holes are drilled through the template corresponding to each of the fastener holes of the wing skin. The template is then aligned with a new wing skin, and pilot holes are drilled through the new wing skin corresponding to each of the template holes. The new wing skin is then aligned with the wing structure such that the pilot holes permit access to corresponding fastener holes of the wing structure. A mill bit is then positioned through each pilot hole and aligned with the center of the corresponding consumable bushing in the fastener hole of the wing sub-structure, and the skin pilot holes are milled to form fastener holes in the new wing skin aligned with existing sub-structure. | 2017-11-09 |
20170320597 | MODULAR AND CONFIGURABLE SPACECRAFT ATTACHMENT AND DEPLOYMENT ASSEMBLIES - A configurable spacecraft attachment and deployment system and a method of constructing a configurable spacecraft attachment and deployment system are provided herein. In one embodiment, the configurable spacecraft attachment and deployment system includes: (1) a connecting structure configured to secure at least one spacecraft to a launch interface, (2) an actuating assembly configured to constrain the spacecraft to the connecting structure before deployment thereof and release the spacecraft from the connecting structure when deployed, and (3) a deploying mechanism coupled to the connecting structure and configured to eject the spacecraft from the attaching structure, wherein the connecting structure, the actuating assembly, and the deploying mechanism are modular components and the connecting structure and deploying mechanism are selected to form the system based on parameters of the spacecraft. | 2017-11-09 |
20170320598 | ENERGY EFFICIENT SPHERICAL MOMENTUM CONTROL DEVICES - Embodiments of a spherical momentum control device are provided. In one embodiment, the spherical momentum control device includes a housing assembly bounding a cavity, a rotor support axle disposed within the cavity, and a spherical bearing interface formed between the rotor support axle and the housing assembly. The spherical bearing interface facilitates rotation of the rotor support axle within the cavity about three orthogonal axes transecting substantially at the cavity center point. A rotor is mounted to the rotor support axle (e.g., through precision bearings) for rotation about a spin axis. The spherical bearing interface can assume any form for facilitating rotation of the rotor support axle about the orthogonal axes including, for example, a low friction plane bearing interface. In one embodiment, the spherical bearing interface includes rolling element bearings embedded in the cavity walls or embedded in enlarged end caps forming part of the rotor support axle. | 2017-11-09 |
20170320599 | APPARATUS AND METHOD FOR CONTROLLING A SATELLITE - Provided is an apparatus for controlling an orbiting satellite by sensing a change in a yaw angle of the orbiting satellite and calculating a ground sample distance (GSD) based on the yaw angle. The apparatus may include a sensor configured to sense a yaw angle corresponding to yaw steering of the orbiting satellite, and a processor configured to calculate, based on the yaw angle, a GSD corresponding to a length of a pixel projected onto a planetary surface scanned by the orbiting satellite. | 2017-11-09 |
20170320600 | Solar Panel and Flexible Radiator for a Spacecraft - A spacecraft ( | 2017-11-09 |
20170320601 | Method of Space Travel Using a High Acceleration Thrust Vehicle in Combination with a Plurality of Low Acceleration Thrust Vehicles - A method of space travel using a high acceleration thrust vehicle in combination with a plurality of low acceleration thrust vehicles. A primary spacecraft has a kinetic launcher that is utilized to discharge a plurality of subsidiary spacecraft in order to navigate the primary spacecraft along a flight path. Each of the plurality of subsidiary spacecraft has a propulsion system, allowing each of the plurality of subsidiary spacecraft to navigate to a refueling point. The refueling point for each of the plurality of subsidiary spacecraft may be a central location or a unique position along a subsequent flight path. Each of the plurality of subsequent spacecraft is then reloaded onto the primary spacecraft or loaded onto a subsequent spacecraft for another voyage. The kinetic launcher can be repositioned in order to control the direction of the acceleration experienced by the primary spacecraft. | 2017-11-09 |
20170320602 | LOCKING DEVICE FOR A WHEELED LOAD - A locking device associable to a wrapping machine for locking in a defined locked position a wheeled load to be wrapped with a plastics film, the locking device including a first element elongated along a first direction and arranged to rest on, and be fixed to, a supporting plane of the wrapping machine, and a second element connected to the first element. The second element is provided with a seat open on the supporting plane and includes an inlet opening for allowing a first wheel of the wheeled load be inserted into, or disengaged from, the seat along an insertion direction, and a recess arranged to be engaged by the first wheel in the locked position so as to prevent the first wheel from moving along the first direction and along a second direction, which is substantially orthogonal to the first direction, and from disengaging from the seat. | 2017-11-09 |
20170320603 | DEVICE, METHOD AND PACKAGING MACHINE FOR PROCESSING A PACKAGING CONTAINER - The invention relates to a device for processing at least one packaging container, in particular for stretching out at least one stretching element of the packaging container, comprising at least one pivoting-arm pair, which comprises a first pivoting arm and a second pivoting arm, which is arranged in a mirror-symmetric manner in relation to the first pivoting arm with respect to an axis of symmetry perpendicular to the at least one linear axis, wherein the first pivoting arm is supported in such a way that the first pivoting arm can be rotated about a first pivoting-arm axis of rotation perpendicular to the axis of symmetry in a first rotational motion and can be displaced in the direction of the at least one linear axis in a first displacement motion and the second pivoting arm is supported in such a way that the second pivoting arm can be rotated about a second pivoting-arm axis of rotation perpendicular to the axis of symmetry in a second rotational motion and can be displaced in the direction of the at least one linear axis in a second displacement motion, and comprising a coupling transmission, which is designed to produce the first rotational motion and the first displacement motion of the first pivoting arm and the second rotational motion and the second displacement motion of the second pivoting arm from at least one first driving motion and one second driving motion, and wherein the first rotational motion and the second rotational motion are synchronous to each other and in opposite directions and the first displacement motion and the second displacement motion are synchronous to each other and in opposite directions. | 2017-11-09 |
20170320604 | Wire Release Mechanism - A wire release mechanism for securing an end of a wire during a wire tying cycle is provided. The wire release mechanism may secure a first end of a wire around a bale of recycled material during knotting of the wire. The wire release mechanism may include a wire release portion having an engaging surface and the wire release portion may be movable between an open and closed position. The wire release mechanism may further include a gripping arm movable between a first position and a second position and having a retractable surface. The engaging surface may disengage the wire based on movement from the closed position to the open position. Further, the retractable surface may engage against the first end of the wire based on movement from the first position to the second position. | 2017-11-09 |
20170320605 | MACHINE FOR WRAPPING GROUPS OF PRODUCTS IN A ROLL AND PACKAGING PROCESS - Described is a machine for wrapping groups ( | 2017-11-09 |
20170320606 | Apparatus for Delivering Product Carriers and Apparatus for Pivoting a Cover Section of a Product Carrier - An apparatus for delivering product carriers, in particular L boards, to a conveying line for food products comprises a store for the product carriers and a conveying device for conveying the product carriers, in particular isolated product carriers, along a conveying direction to the conveying line, wherein each product carrier has at least one base section and at least one cover section connected to the base section; and wherein the apparatus comprises a pre-treatment device for the product carriers that is configured to pre-treat the cover section of a product carrier with respect to its base section. | 2017-11-09 |
20170320607 | OPTICAL DEVICE FOR CHECKING A FACE OF A BLANK | 2017-11-09 |
20170320608 | METHOD AND MACHINE FOR FORMING A BOX BY PLACEMENT ON A V-SHAPED SUPPORT - A method and a machine for forming a box from a blank, in which the blank is removed from a storage magazine by suction, the blank is fed horizontally above a support having an upper edge with a V-shaped cross section and faces that correspond to the main walls and are inclined with respect to the horizontal by a given angle a, such that the central folding line, known as the reference folding line, is next to the edge, the blank is placed on the support, the blank is then pressed against a polygonal mandrel, the upper edge of which coincides with and/or is in line with the upper edge of the support, said mandrel having a shape complementary to that of the box, so as to form a tubular box body at an angle to the horizontal, the bottom of the box is formed by folding and pressing together flaps after application of glue, and the inclined box thus formed is ejected, is positioned upright and then is transferred to a filling station. | 2017-11-09 |
20170320609 | A MACHINE AND METHOD FOR ITS OPERATION - A labelling machine comprises a supply spool support for supporting a supply spool comprising label stock; a take-up spool support adapted to take up a portion of the label stock; a motive device configured to propel the label stock along a web path from the supply spool support towards the take up spool support; a first arrangement configured to produce a first signal indicative of a speed at which label stock is removed from the supply spool by the motive device; a controller configured to receive the first signal and output a brake assembly control signal based upon the first signal; and a brake assembly configured to apply a braking force to the supply spool support based upon the brake assembly control signal, the braking force resisting rotation of the supply spool support. The controller is configured to output the brake assembly control signal based upon a target supply spool speed. | 2017-11-09 |
20170320610 | A THERMOPLASTIC PREFORM FOR A WIDE-MOUTH CONTAINER - An innovative neck ( | 2017-11-09 |
20170320611 | HELICALLY COLLAPSIBLE BEVERAGE BOTTLE - A cylindrical bottle which collapses along helical groove, ridge and connecting rings along its sidewall. When inward force is applied along the bottle's vertical axis, the helical groove rings and connecting rings fold under the ridge rings and remain substantially “locked” under the ridge rings, thereby causing the sidewall to collapse and remain collapsed until sufficient outward force is applied. When sufficient outward force is applied along its vertical axis, the bottle extends as the distance between its helical groove rings and ridge rings lengthens. Due to the diamond-shaped cross-section of the connecting rings, in conjunction with the silicone composition of the bottle's body, the collapsing and extension of the bottle occur in sequential segments, creating a unique, playful sound and an amusing worm-like movement. | 2017-11-09 |
20170320612 | PACKAGING CONTAINER - The invention includes a packaging container comprising a generally pyramid-shaped body with a top and a base and including a waistband which fits over the top and into a position in which it abuts the sides of the body, wherein the waistband can be separated from the body and the body inverted and placed thereon so that the waistband forms a pedestal for supporting the body in an inverted fashion. The invention further includes methods for displaying foodstuffs and transporting foodstuffs with the packaging container described. | 2017-11-09 |
20170320613 | POUR TRAY - A liquid pour tray provides a plurality of liquid retaining receptacles each having a proximal portion and a distal portion defining an open end, the distal portion having a width narrowing in a direction opposite the proximal portion toward the open end. A plurality of partitions are interposed between the plurality of liquid retaining receptacles and an overflow reservoir is in fluid communication with the plurality of liquid retaining receptacles. | 2017-11-09 |
20170320614 | Layout and Box Folded from the Layout Suitable for Waste - The invention relates to a layout for a box, having a bottom wall, four sidewalls and a cover, wherein the sidewalls each share a crease line with the bottom wall; wherein adjacent sidewalls share a connecting surface, which connecting surface shares a crease line with each of the two adjacent sidewalls; wherein the connecting surfaces are provided with at least one diagonal crease line; wherein the at least one diagonal crease line of the connecting surface coincides in one point with both crease lines between each of the adjacent sides and the bottom wall. | 2017-11-09 |
20170320615 | Collapsible portable reusable container - A collapsible portable reusable container having a plurality of sides, gussets and opposing tension folds, as a tension hinge, optionl brackets as needed, with each gusset having a first section and a second section. One section of the gusset is foldably connected to a panel having an opposing tension fold, preferably on an adjacent connected panel, creating a tension hinge. The above gusset and opposing tension fold placements, allow a user to transform the container from a folded, collapsed position to a freestanding, open position in one simple move with no need for a securing mechanism to keep the container in an open position. | 2017-11-09 |
20170320616 | PIZZA CONTAINER - A container for pizza comprises a base, four edges, and a lid provided on one of said edges. The container is characterized in that it comprises a first support element and a second support element projecting respectively from a first edge and a second edge. The support elements have ends comprising connection means designed to allow temporary joining together of the two ends. | 2017-11-09 |
20170320617 | Procedure for Manufacturing a Laminated Package for Solid Products in Powder or Grain Form, as Well as a Package Obtained by This Procedure - A laminated package for solid products in powder or grain form, includes a set of stiffening notches, a dispensing mouth with a seal, valves for loading inert gas, in which the lateral folds of the upper face are folded inwards under the front and rear flaps, and the lateral folds of the lower face are folded outward and folded and stuck on the lower face over the front and rear flaps, and a method for forming the package. | 2017-11-09 |
20170320618 | ODOR-PROOF CONTAINER FOR PERSONAL ITEMS - A portable, personal container is formed from an inner container formed by a first tube and a second tube which slidably engage to form a sealed inner container, which fits within an outer container formed by a first tube and a second tube which slidably engage to form a sealed outer container. A spring allows a pumping action which creates a slight negative pressure in the inner container and creates a plenum within the outer container, keeping odors and freshness in. | 2017-11-09 |
20170320619 | VENTED CONTAINER END CLOSURE - A metallic container end closure is provided that generally comprises a dispensing opening and a vent opening. The vent opening improves pourability through the dispensing opening and provides an alternative option for consuming the contents of the container. The end closure may include features to ease opening of the vent opening, such as stiffeners and/or vent form features. | 2017-11-09 |
20170320620 | QUARTER PALLET WITH PRODUCT TAB RECEIVING AREAS FOR PRODUCTS CARRIED THEREON - A pallet includes a top including a product support surface and an opposing underside, with outer sides extending between the product support surface and the underside. Four feet each extend away from the underside of the top, and each foot has a first opening facing out through the product supporting surface of the top. The feet thus allow stacking of such pallets with the feet of a first such pallet extending into the first openings of a second such pallet. Product tab receiving areas are for receiving respective product tabs, with each product tab receiving area having a slot within the top adjacent a respective outer side of the top. The slot has a pair of spaced apart opposing long sidewalls and a pair of spaced apart opposing short sidewalls adjacent to the pair of long sidewalls, with one of the long sidewalls including a laterally extending tongue for engaging an opening in one of the product tabs. | 2017-11-09 |
20170320621 | STORAGE SYSTEM - A storage system includes at least two modular containers, at least two anchor members, and at least one coupler. Each of the modular containers includes a bottom wall and a surrounding wall unit with two opposite walls. Each of the two opposite walls has two lateral regions and an elongated depressed region which extends inwardly to form an elongated groove. Each of the anchor members includes a fitted end fitted slidably in a corresponding elongated groove, an enlarged head, and a neck disposed between the fitted end and the enlarged head. The coupler couples the enlarged heads of the at least two anchor members together so as to permit the at least two modular containers to be disposed in their respective orientations. | 2017-11-09 |
20170320622 | STACKABLE CONTAINER HAVING OVERHANGING CAP - A stackable container, including a body and a cap threadingly engageable with a neck portion of the body and having a vaulted interior and a top portion formed with a frustro-conical depression for snap-registered engagement with a base portion of a counterpart of the body, the cap further including handle projections and a skirt. Opposite stop structures prevent rotation of the cap relative to the body beyond predetermined threaded engagement; a decent releasably captures the body in the predetermined threaded engagement. A base portion of the body having inclined side walls facilitates rotation of the body with respect to the cap. The skirt guides the body into alignment with the cap. The base can have four of the side walls forming a square, the containers of a stack having any of four relative orientations. A consumable product such as a cosmetic can extend into the cap from the body. | 2017-11-09 |
20170320623 | BEVERAGE CAN COUPLINGS - A coupling for assembling at least two beverage cans together, comprising at least a pair of collar portions, each to slidably receive a corresponding end region of one of the beverage cans, the collar portions being configured to engage the beverage cans for associated games and/or other amusement activities. | 2017-11-09 |
20170320624 | STACKABLE CONTAINER HAVING OVERHANGING CAP - A stackable container, including a body and a cap threadingly engageable with a neck portion of the body and having a vaulted interior and a top portion formed with a frustrum-shaped depression for snap-registered engagement with a base portion of a counterpart of the body, the cap further including handle projections and a skirt. Opposite stop structures prevent rotation of the cap relative to the body beyond predetermined threaded engagement; a detent releasably captures the body in the predetermined threaded engagement. A base portion of the body having inclined side walls facilitates rotation of the body with respect to the cap. The skirt guides the body into alignment with the cap. The base can have four of the side walls forming a square, the containers of a stack having any of four relative orientations. A consumable product such as a cosmetic can extend into the cap from the body. | 2017-11-09 |
20170320625 | CONTAINER SYSTEM - Engineered handheld bin system constructed of modular components creating custom heights and increased interior volume greater than known handheld plastic containers. | 2017-11-09 |
20170320626 | PACKAGE FOR VERTICAL RECEIVING - The present invention relates to a package for vertical receiving, which, when receiving various kinds of objects to be received, such as clothes, in a drawer, etc., packages and receives the objects to be received such that the objects to be received are stood using the same standard, thereby maximizing the receiving efficiency, easily identifying an object to be received even when searching for the object to be received in order to use the object to be received, and not dispersing the objects to be received, which are received uniformly. The package for vertical receiving comprises: a rear part ( | 2017-11-09 |
20170320627 | COLLAPSIBLE BOX - A collapsible box has a bottom with a plurality of foldable walls, each of which is hinged to the bottom. Each wall is displaceable between a collapsed state and an erected state, in which the walls are connected by locking means. The bottom and the walls in the erected state define a space. The bottom includes a guiding element configured to receive at least a part of an upper rim of another collapsible box stacked underneath. | 2017-11-09 |
20170320628 | FOOD SEPARATORS - Various embodiments of food separators are provided. Preferably, the food separator will have a first member which has a length and width, a second member which has a length and width, and a separation member which is built of a first substantially upright member which has a first base and a second base and a second substantially upright member which has a third base and a fourth base. The first base is connected to the third base at an angle, the first member is connected to the second base, and the second member is connected to the fourth base. | 2017-11-09 |
20170320629 | A Coating Composition Comprising a High MN Polyester and a Low MN Polyester - A coating composition comprising: (a) a first polyester material having a number-average molecular weight (Mn) of 500 to 5,500 Daltons, and (b) a second polyester material having a number-average molecular weight (Mn) of 6,000 to 100,000 Daltons. The coating composition is useful for, among other things, coating food and/or beverage containers. | 2017-11-09 |
20170320630 | LOCKING AND FOLDING ASSEMBLY FOR ATTACHMENT TO A BUCKET OR OTHER CONTAINER - A leg assembly capable of easy attachment to a container, having an elongated leg and a bracket, where the bracket contains a mounting pocket, two slots, substantially parallel to one another, and wherein at one end of the bracket there is disposed an L-shaped flange, and wherein the elongated leg contains a pin on each side of an end of the leg, and mounted so that the leg may rotate in the mounting pocket of the bracket, and wherein the leg has an outward protruding pin sized and shaped to fit into the two parallel recesses, and wherein the pin is formed on a flexible arm on the leg capable of being depressed to move the pin inward. | 2017-11-09 |
20170320631 | CLOSURE - A package includes a container and a closure cap for mounting on the container. The closure cap is coupled to a neck of the container to block selectively removal of product stored within the container at the selection of a user. | 2017-11-09 |
20170320632 | METHODS OF MAKING GUSSETED FLEXIBLE PACKAGE WITH SHAPED SIDES - A flexible side-gusseted package and methods of making the same are disclosed. The package has a central longitudinal axis, a front panel, a back panel, and a pair of gusseted side panels. The front panel is secured to the gusseted side panels along a pair of side seal lines. The back panel is secured to the gusseted side panels along a pair of side seal lines. Each of the seal lines includes a pair of end portions and an intermediate portion. The intermediate portion, e.g., a concave recessed portion, of each side seal line is located closer to the central longitudinal axis than the end portions of the side seal lines to provide a package which is somewhat necked-down at its middle, to facilitate grasping of the package by users. | 2017-11-09 |
20170320633 | Humidity Control Package - A humidity controlled package that uses a humidity sensitive valve that opens and closes an opening to control a humidity in the package. The package has a package holding area inside the package. The humidity level in the package controls the valve to open to allow air flow between an inside of the valve and an outside of the valve, and close to prevent air flow between the inside and outside of the valve. At least part of the valve is in the package. In one embodiment, the package is vented when the humidity value gets higher than a setpoint. In another embodiment, a sachet of dessicant is opened by the humidity level. | 2017-11-09 |
20170320634 | DRAW TAPE BAG - The bag may include a draw tape that may be used to cinch closed the opening of the bag. The draw tape has at least one stretched elastomeric strip attached to the draw tape in an extended condition. The draw tape may be smaller in size than the bag sidewalls. The draw tape may include an elastic characteristic, such as patterned ribs. In one embodiment, the roll of bag is kept under tension to maintain the elastomeric strips in a stretched condition. | 2017-11-09 |
20170320635 | DOUBLE CONTAINER FOR HIGH-VISCOSITY LIQUID - Provided is a double container which comprises a relatively rigid outer container and a flexible inner container disposed inside the outer container and capacity-variable in response to an amount of a content thereof The double container is configured to contain, particularly, a high-viscosity liquid, e.g., a liquid having a viscosity of 1000 to 100,000 mPa/s, and to be easily produced by a forming technique having no significant difference from conventional techniques, wherein the double container for a high-viscosity liquid is capable of containing the content without causing oxidation thereof, while maintaining the outer container in its original shape or dimensions, and discharging the content by squeezing the outer container, irrespective of a level of a remaining amount of the content. | 2017-11-09 |
20170320636 | METHOD AND APPARATUS FOR ENCLOSING - Presented are an apparatus and method for enclosing. An exemplary apparatus includes a bag having at least a first opening and a second opening, the bag comprising a first sheet coupled to a second sheet along a periphery of the first sheet and the second sheet, and a first closing device coupled to the first opening, the first closing device able to repeatedly open and seal the first opening. The apparatus further includes a second closing device coupled to the second opening, the second closing device able to repeatedly open and seal the second opening. | 2017-11-09 |
20170320637 | SYSTEM AND METHOD FOR SCREW ON TAMPER EVIDENT CLOSURES - A method for securing a tamper evident closure to a container includes providing a prethreaded closure that is defined by a top portion and a skirt portion that extends from the top portion. The skirt portion defines an inner closure thread surface and an opposed outer closure thread surface of at least one closure thread. The skirt portion also includes a tamper evident band. The prethreaded closure is rotated to engage the at least one closure thread with at least one container thread of a container. The inner closure thread surface contacts a surface of the at least one container thread. The tamper evident band of the prethreaded closure is rolled to secure the tamper evident band to the container. | 2017-11-09 |
20170320638 | Lid-to-Container Locking Combinations and Methods - A lid-to-container locking combination maximizes lid-to-container retention and includes a container and a container lid. The container includes an upper container rim and a container wall. The container wall includes a radially outwardly extending indentation or groove located in inferior adjacency to the upper container rim at an inner surface thereof. The container lid includes a rim-receiving groove, a lid wall, and a wall-to-groove resilient portion. The resilient portion traverses a structural distance between the lid wall and the rim-receiving groove and is resiliently actuable intermediate a relaxed configuration and an actuated configuration. The resilient portion includes a radially outer indentation-engaging portion. The rim-receiving groove receives the upper container rim, and the indentation-engaging portion engages the radially outwardly extending indentation when in the actuated configuration. The rim-receiving groove and radially outer the indentation-engaging portion together lock the container lid to the liquid container for cooperatively maximizing lid-to-container retention. | 2017-11-09 |
20170320639 | CONTAINER - A container is provided. A main body has a barrel body and a cover body, the cover body is normally in a first position and optionally movable to a second position. An electronic processing unit is arranged on the main body. A sensing device, a power connecting device and a driving device are arranged on the main body and electrically connected to the electronic processing unit. When the cover body is in the first position, the cover body covers the placement opening, the cover body and the barrel body are in a fixed relative position; and when the cover body is in the second position, the cover body is remote from the placement opening. When the cover body receives an external force to move away from the barrel body, the driving device actuates the cover body to move from the first position to the second position. | 2017-11-09 |
20170320640 | PORTABLE BEVERAGE CONTAINER - A portable beverage container is provided. The portable beverage container may include a glass vessel having a neck; a metal outer shell configured to surround a first portion of the glass vessel; a cap configured to engage with the metal outer shell to surround a second portion of the glass vessel; and an amorphous thermoplastic spout having a neck configured to be inserted through an opening in the cap and into the neck of the glass vessel. The spout may be configured to securely engage with the cap. The cap may include a lid with an elastomeric sealing member having a knob configured to extend into a recess in the spout and a recess configured to wrap around and over a lip of the spout. The spout may be removable from the cap while the cap is engaged with the outer shell. | 2017-11-09 |
20170320641 | TUBE WITH THROTTLE INSERT | 2017-11-09 |
20170320642 | Coffee Bag Vent - A laser formed vent in packaging material, formed by an interior breach and an exterior breach, which are connected to one another by a channel. The next interior breach an exterior breach are laterally offset from one another, the channel is formed by vaporizing a bubble in an interior layer, for example a foil layer. In one embodiment, the bubble can be crushed, but returns to its original configuration. | 2017-11-09 |
20170320643 | EASILY CLEANABLE DRINKING ASSEMBLY - An easily cleanable drinking assembly having a receptacle, a lid, and a coating with hydrophobic, oleophobic, and antimicrobial properties. The receptacle has an inner curved surface having a geometry with no edges, corners, or distinctly angled connections between sections, preventing any fluid or particles from remaining in these areas. The receptacle further has a wider opening and narrower end, allowing for ease of cleaning, so that a cleaning instrument can easily be inserted and easily reach all parts of the interior of the receptacle. Both the interior of the receptacle and the lid are coated with a coating with hydrophobic, oleophobic, and antimicrobial properties, repelling common fluids and particles, maintaining the cleanliness of the interior surfaces and improving the ease of cleaning. | 2017-11-09 |
20170320644 | RECEPTACLE COMPRISING A SAFETY LOCKING MECHANISM FOR A VEHICLE - A receptacle including a safety locking mechanism in a motor vehicle. A lever is providing including a mass, which is held by a snap-fit device releasably in a non-deflected basic position or in a deflected locking position. In the deflected locking position, the lever, by way of a head, holds a closing element of a lock in a closed position. The lock can be opened in a non-deflected position of the lever. During opening, the lock restores the lever to the basic position, whereby the receptacle can be opened after an accident. The lever is deflected by accelerations that occur in the event of an accident. | 2017-11-09 |
20170320645 | BEVERAGE CONTAINER - A plastic beverage container includes a body, a closure, and a dry granular consumable. The body has a closed base portion and an open top end. The closure includes a top member, a bottom member, a pull tab, and an adhesive. The adhesive is disposed between a perimeter of each of the top and bottom members of the closure to form a sealed pouch container having a pull tab with a perforation. The top and bottom members are formed from one of a metal foil and polymer film. The dry granular consumable is disposed in the sealed pouch container. The adhesive is also disposed between the perimeter of the closure and a sealing surface of the top end of the body to form a liquid-tight seal between the closure and the top end of the body. | 2017-11-09 |
20170320646 | COMPACT CONTAINER PROVIDED WITH AIRTIGHT PACKING HAVING UPPER AND LOWER SEALING RUBBERS AND COUPLING TENSION PROTRUSION - The present invention relates to a compact container provided with an airtight packing having upper and lower sealing rubbers, and a coupling tension protrusion, in which the airtight packing is coupled on top of a refill container, wherein the upper sealing rubber is brought into close contact with a refill container cover and the lower sealing rubber is brought into close contact with the refill container, so as to render airtight a cosmetic material accommodating space, thereby preventing cosmetic material from evaporating or becoming volatile to allow the cosmetic material to function properly for a long time. Also, the cosmetic material accommodation space in the refill container is maximized by removing an existing middle container and directly coupling the refill container to a container main body, thereby enabling effective filling of more cosmetic material to minimize frequent refilling of the cosmetic material. | 2017-11-09 |
20170320647 | SECURITY COVER FOR BEVERAGE CANS AND OTHER CONTAINERS - A security cover system and apparatus for beverage cans and other containers. The system includes a security cap that is installed upon the top of an unopened container for containing an adult beverage or the like. The cap is adapted for secure installation upon the top of a container having a top with a circumferential rim, such as an aluminum beverage can. The cap has catches engagable with the rim of the container. The system includes an opener tool with a specially shaped key portion thereon. The opener engages with a complementary slot in the cap to permit an authorized person, using the opener tool, to remove the cap from the container. | 2017-11-09 |
20170320648 | Carton For Articles - A carton for containing a plurality of containers includes a plurality of panels and a plurality of end flaps. The plurality of end flaps is foldably connected to respective panels of the plurality of panels and at least partially closes an end of the carton. The plurality of end flaps includes a first end flap foldably connected to one of a top panel and a bottom panel at a first fold line, a second end flap foldably connected to the one of the top panel and the bottom panel at a second fold line that is oblique to the first fold line, and a third end flap foldably connected to the at least one side panel at a third fold line. The third end flap has at least one notch overlapping at least a portion of one of the first end flap and the second end flap. | 2017-11-09 |