17th week of 2022 patent applcation highlights part 21 |
Patent application number | Title | Published |
20220126961 | ACTIVE AND PASSIVE SAIL FOR IMPROVED COMMUNICATION NETWORKING AT SEA - Provided is a radar and communications enhanced sail for a sailboat, sail ship, or sail drone. The sail includes a first sail section comprising an active communication system, a second sail section comprising a passive communication system, or a combination thereof. The active communication system includes an antenna array (transceiver) and a software-defined radio (SDR), while the passive communication system comprises a reflective panel or sections and/or array of reflector panels or sections. The active system utilizes its SDR and transceiver to communicate back and forth with an onshore SDR and transceiver to provide information as necessary. The passive system receives a radar signal via the reflective material on the sail and reflects the signal back at the radar, which produces a radar cross section indicating that there is an object (in this case the sailboat) in the ocean. | 2022-04-28 |
20220126962 | Collapsible Blade Equipped Paddle Device - A collapsible blade equipped paddle device enabling an underwater return stroke includes a shaft, which has a blade engaged to a first end thereof. The blade comprises a frame having a panel engaged thereto and extending therebetween. The frame is selectively collapsible so that the blade assumes an open cupped configuration when a forward stroke is applied to the shaft and a collapsed configuration when an underwater return stroke is applied to the shaft. The blade provides thrust to a marine vessel during the forward stroke and minimal resistance during the underwater return stroke. | 2022-04-28 |
20220126963 | VESSEL OPERATION SYSTEM AND VESSEL - A vessel operation system includes an outboard motor or other propulsion apparatus disposed on a hull, a trolling motor mounted externally to the hull, a joystick or other first operator, and a controller. The joystick is operated by a vessel operator in order to indicate at least one of a magnitude and a direction of a thrust that the outboard motor is to apply to the hull. In a state in which the trolling motor is generating a first thrust, the controller controls the outboard motor so as to generate a second thrust in accordance with a command indicated by the joystick. Additionally, the controller controls the trolling motor so that the first thrust changes. | 2022-04-28 |
20220126964 | OUTBOARD MOTOR - An outboard motor includes a swivel bracket supporting a drive shaft housing such that the drive shaft housing is pivotable about an axis thereof and is movable in an axial direction thereof, a steering adjuster attached to the swivel bracket and configured to increase or reduce a rotational resistance force of the drive shaft housing against the swivel bracket, and at least one spacer mounted to the drive shaft housing at a position adjacent to at least one of both ends of the swivel bracket in the axial direction. In a state in which the spacer is mounted to the drive shaft housing, the drive shaft housing is restricted from moving in the axial direction with respect to the swivel bracket. A dimension from the swivel bracket to a rotation shaft of the propeller is changed by changing a mounting position of the spacer. | 2022-04-28 |
20220126965 | EXHAUST GAS PURIFICATION STRUCTURE AND OUTBOARD MOTOR - An exhaust gas purification structure of an outboard motor includes an exhaust gas pipe that has an exhaust gas passage through which exhaust gas of an engine can flow; and a catalyst that is provided in the exhaust gas passage and purifies the exhaust gas by allowing the exhaust gas to pass through the inside thereof. The exhaust gas pipe includes a coolant flow passage allowing a coolant that cools the exhaust gas to flow therethrough. An exhaust gas bypass passage allowing the exhaust gas to flow without passing through the catalyst is formed between the catalyst and an inner surface of the exhaust gas pipe forming the exhaust gas passage. | 2022-04-28 |
20220126966 | BOAT STEERING AND PROPULSION SYSTEM - Techniques are disclosed to enable a system for controlling the propulsion and steering of a boat by a boat operator. The boat has at least one propulsion and steering motor assembly connected to the boat with a propeller, and a propulsion motor. It also has left and right pivoting pedals to provide a signal that controls the angle of the propeller so that if the left pedal is pivoted in a first pivot direction by a first percentage and the right pedal is pivoted in a second pivot direction by a second percentage, the boat executes a turn, moves forward, or moves in reverse. | 2022-04-28 |
20220126967 | VESSEL OPERATION SYSTEM AND VESSEL - A vessel operation system includes an outboard motor or other propulsion apparatus on a hull, an electrically-driven trolling motor mounted externally to the hull, and a controller configured or programmed to control the outboard motor and the trolling motor. The outboard motor generates a thrust and electric power with an engine. The trolling motor generates a thrust by being driven by electric power from a battery that is charged by the electric power generated by the outboard motor. In a state in which the trolling motor is generating the thrust, the controller is configured or programmed to control the outboard motor so as to generate an assist thrust that hastens a behavior of the hull by the thrust generated by the trolling motor. | 2022-04-28 |
20220126968 | SHIP PROPULSION SYSTEM - A ship propulsion system includes authentication devices that respectively stores different authentication codes. Each of the authentication devices corresponds to one or more ship propulsion devices. Two or more authentication devices among the plurality of authentication devices do not simultaneously correspond to one ship propulsion device. Each of the authentication devices operates as a master authentication device when an authentication code transmitted from a communication device matches an authentication code stored in the authentication devices. The master authentication device recognizes whether a malfunction occurs in the authentication devices; and to select a ship propulsion device disposed in a manner of being bilaterally symmetrical about the center of the ship in the left-right direction from ship propulsion devices corresponding to an authentication device in which no malfunction occurs. A control device brings the ship propulsion device selected by the master authentication device into an operable state. | 2022-04-28 |
20220126969 | Marine Diesel Power System - The embodiment of the invention provides a marine diesel power system comprising a diesel engine, a conformal heat exchanger with a first inlet and a first outlet thereof connected to the diesel engine and upper and lower sealing heads thereof as well as a second inlet and a second outlet for inflowing and discharging seawater, and a jet device at a second outlet of the conformal heat exchanger, wherein a first inlet, a second inlet and an outlet of the jet device are separately used for sucking seawater discharged from the second outlet, connecting to a diesel engine exhaust tube and discharging seawater and waste gas discharged from the diesel engine exhaust tube. By arranging the jet device at the second outlet, the heat exchange form of the conformal heat exchanger is changed into forced convection heat exchange, so that the heat exchange efficiency of the conformal heat exchanger is improved. | 2022-04-28 |
20220126970 | POWERTRAIN FOR AN AMPHIBIAN - A power train for an amphibian operable in land and marine modes includes a prime mover having an integral speed change transmission, at least a first land propulsion unit, at least a first marine propulsion unit, and a power transmission unit including a drive member configured to couple the prime mover to the at least first marine propulsion unit, wherein the prime mover is arranged to drive the at least first land propulsion unit through/via the integral speed change transmission in the land mode, and the prime mover is arranged to drive the at least first marine propulsion unit through/via the power transmission unit in both the marine mode and the land mode. | 2022-04-28 |
20220126971 | User Interface Apparatus For Controlling Marine Vessel - A user interface apparatus for controlling a marine vessel. The apparatus includes concentric positioned mechanical stick, block and ring for setting a control parameter, electric motors, and electric visual elements. The apparatus also includes one or more processors configured to operate the user interface apparatus in a plurality of operation modes, each operation mode with a distinct configuration, retrieve distinct settings for the tactile feedback and/or the visual feedback, and control the tactile feedback given by the one or more electric motors and/or the visual feedback given by the one or more electric visual elements based on the retrieved distinct settings during setting a selected control parameter mapped to the mechanical stick, block or ring. | 2022-04-28 |
20220126972 | Marine Vessel Brake Assist And Stabilization System - A vessel braking control system for a marine vessel that utilizes one or more of the vessel's features and effectors to increase the drag on the vessel both through increased drag on the features and effectors themselves and by creating a downward force on the vessel as a whole, increasing the wetted hull area and increasing hull drag thereby; the control system operates to place the features and effectors in a braking state through rotation relative to the vessel's direction of travel and relative to the water's surface, and may automatically return the features and effectors to their normal operating state upon the vessel's reaching a detected, predetermined speed. | 2022-04-28 |
20220126973 | SELF-CONTAINED MARINE AIR CONDITIONING UNIT, AIR-CONDITIONING SYSTEM, AND METHOD OF INSTALLATION - A do-it-yourself-friendly self-contained marine air conditioning unit, marine air conditioning system, and method for installation is disclosed. The unit includes a seawater cooling circuit, a refrigerant circuit, and a blower assembly. The refrigerant circuit includes a reverse valve connecting a compressor, an evaporator, and a refrigerant tube thermally engaged with a titanium condenser coil. The seawater cooling circuit includes the titanium condenser coil. The titanium condenser coil has a titanium condenser coil outflow and a titanium condenser coil inflow. The blower assembly is mounted in communication with the evaporator, wherein the blower assembly may pull air through the evaporator. This blower is capable of achieving up to 270-degrees of rotation about a single axis. The system also includes a universal controller to allow for optimal integration with existing systems. | 2022-04-28 |
20220126974 | AIRCRAFT DOOR HAVING A MECHANISM FOR CONDITIONAL OPENING ALONG TWO TRAJECTORIES - Aircraft door ( | 2022-04-28 |
20220126975 | EJECTION SYSTEM FOR AN EMERGENCY EXIT OF A VEHICLE - Ejection system for a vehicle emergency exit ejection system for a vehicle emergency exit, the emergency exit extending along a base surface and being designed to cooperate in a mounted position with a receiving frame of the vehicle, the ejection system including a retaining element and a locking mechanism designed to cooperate with the retaining element in a locking configuration in which a movable part of the locking mechanism prevents a relative movement of the retaining element and the locking mechanism in a direction of ejection of the emergency exit which is transversal to the base surface, the movable part being configured to be moved in a closing plane that extends transversally to the base surface and an ejection configuration in which the locking mechanism is capable of moving in the direction of ejection relative to the retaining element. | 2022-04-28 |
20220126976 | RADOME COVER SHELL AND OPENING KINEMATIC - An aircraft with an aircraft structure that comprises a radome cover opening kinematic and a radome cover shell that is adapted to enclose equipment in a nose region of the aircraft in a closed position. The radome cover opening kinematic may enable movements of the radome cover shell between the closed position and an opened position and vice versa. The radome cover opening kinematic may include a guiding rail that is attached to the radome cover shell, and at least three rollers that are attached to the aircraft structure, wherein a first and a second roller are arranged on opposing sides of the guiding rail, and wherein the second and a third roller are arranged on the same side of the guiding rail. | 2022-04-28 |
20220126977 | RADOME COVER SHELL AND OPENING KINEMATIC - An aircraft with an aircraft structure that comprises a radome cover opening kinematic and a radome cover shell that is adapted to enclose equipment in a nose region of the aircraft in a closed position. The radome cover opening kinematic may enable movements of the radome cover shell between the closed position and an opened position and vice versa. The radome cover opening kinematic may include a guiding rail that is attached to the radome cover shell, and at least three rollers that are attached to the aircraft structure, wherein a first and a second roller are arranged on opposing sides of the guiding rail, and wherein the second and a third roller are arranged on the same side of the guiding rail. The radome shell opening kinematic further comprises a radome cover shell rotation stopper that can stop movement of the radome cover shell at the completely opened position. | 2022-04-28 |
20220126978 | LEADING-EDGE COMPONENT FOR AN AIRCRAFT - A leading-edge component for an aircraft includes at least a part of a flow body having a front skin, a hollow space at least partially delimited by the front skin and at least one separate retention device. The at least one retention device comprises a flexible structure with a mesh, a web, a fabric or a plurality of strings. The retention device is arranged behind the front skin in a distance thereto and extends along a main extension direction of at least a section of the front skin. The retention device is configured to retain a front skin that deforms to move into the hollow space upon an impact of a foreign object. | 2022-04-28 |
20220126979 | SUPPORTING STRUCTURE WITH PASSIVELY ADAPTABLE PROFILE - The invention relates to a supporting structure ( | 2022-04-28 |
20220126980 | WING FOR AN AIRCRAFT - A wing for an aircraft is disclosed having a fixed wing, a foldable wing tip portion and a flight latch device for latching the foldable wing tip portion in the extended position, wherein the flight latch device includes a housing, a latch bolt, and a motor for driving the latch bolt between the latched and unlatched positions. A flight latch device includes a threaded shaft rotationally driven by the motor, a nut engaging the shaft, so that the nut can rotate relative to the shaft, the nut is connected to the housing via a linear guide and is connected to the latch bolt for common linear movement with the latch bolt, and the flight latch device includes an offset compensation, providing that the shaft is supported pivotable relative to the housing and the latch bolt is coupled to the nut via a compensational bearing allowing angular play between the nut and the latch bolt. | 2022-04-28 |
20220126981 | PROPELLER FOLDING APPARATUS OF AIR MOBILITY VEHICLE - A propeller folding apparatus of an air mobility vehicle deploys or folds propeller blades depending on the flying state of the air mobility vehicle. The propeller blades are efficiently used depending on the flying state of the air mobility vehicle. The energy efficiency and the ferry range of the air mobility vehicle are increased. | 2022-04-28 |
20220126982 | ELECTROMECHANICAL ACTUATOR WITH NO-BACK SYSTEM - A compact, efficient, and reliable electromechanical actuator that is capable of driving heavy loads at a high rate of speed and also capable of resisting large back driving forces. The actuator resists tension and compression back driving forces in a static state as well as when the actuator extends and retracts. The back driving forces are resisted even if the electronics (e.g., motor) fail. | 2022-04-28 |
20220126983 | ACTUATION UNIT FOR ACTUATING A FOLDABLE WING TIP PORTION OF A WING FOR AN AIRCRAFT - An actuation unit for actuating a foldable wing tip portion of a wing for an aircraft is disclosed including a motor configured to be mounted to a fixed wing for an aircraft, a drive pinion driven rotationally by the motor, a first rack configured to be mounted to the fixed wing, a second rack configured to be mounted to the foldable wing tip portion, a third rack configured to be mounted to the fixed wing movably along a defined first movement path and drivingly engaged by the drive pinion, and a transfer pinion mounted to the third rack rotatably about an axis of rotation extending perpendicular to the first movement path, wherein the first rack engages the transfer pinion at a first side and the second rack engages the transfer pinion at an opposite second side of the transfer pinion, such that, when the drive pinion drives the third rack along the first movement path, the transfer pinion drives the second rack along a second movement path. | 2022-04-28 |
20220126984 | FLOW CONTROL DEVICE - A flow control device on a structure such that strain in the structure is at least partially transferred to the flow control device is disclosed having at least two states, or shapes, separated by an elastic instability region. The flow control device is arranged to rapidly transition, or snap through, from the first state to the second state when strain in the structure exceeds an activation threshold of the flow control device. A spoiler on an aerofoil may have a rest position where it is substantially flush with the low pressure surface and an activated position where it protrudes from the low pressure surface and modifies the airflow over that surface. The spoiler bends to move from the rest position to the activated position when the strain in the aerofoil crosses a threshold. The deployed spoiler reduces the lift on the aerofoil, acting to reduce the lift induced strain of the aerofoil to which the spoiler is attached. | 2022-04-28 |
20220126985 | COMPACT AIRCRAFT MAIN LANDING GEAR MODULE ALLOWING MODULAR MOUNTING - A module includes two main landing gears and a landing gear bay containing the landing gears. The bay has two lateral walls, a roof wall, a front wall and a rear wall. The roof wall, the front wall and the rear wall together form a pressurization barrier between the bay and a pressurized compartment. By virtue of the landing gear module, it is now possible to assemble and test the main landing gears and the one or more doors and the fairing before they are installed on the aircraft. | 2022-04-28 |
20220126986 | LANDING GEAR AND PIN LOCKED INDICATION - Apparatus to monitor the position of an aircraft landing gear. | 2022-04-28 |
20220126987 | AIRCRAFT ELECTRIC TAXI SYSTEM DESIGN AND OPERATION - A method for designing and operating aircraft nose landing gear wheel-mounted electric taxi systems to move aircraft during ground travel. Electric taxi system components are engineered and sized to produce optimal ground travel torque to move aircraft during the majority of aircraft ground travel and are operated in conjunction with the aircraft steering to turn the nose wheels to an effective angle that moves the aircraft during pushback and in breakaway situations. The nose landing gear wheels are turned to an effective angle and the electric taxi systems are operated simultaneously to get the aircraft moving. After breaking away, the aircraft is driven with electric taxi systems at the optimal ground travel torque in a forward or reverse direction with the nose wheels parallel or in a desired ground travel direction with the nose wheels steered in the desired direction of ground travel. | 2022-04-28 |
20220126988 | AIRCRAFT LANDING GEAR SHOCK ABSORBER - A shock absorber for an aircraft landing gear is disclosed. The shock absorber includes a stop surface arranged to limit extension of the shock absorber and a crumple element configured to deform in the event that the extension load on the stop surface exceeds a predetermined threshold. The crumple element may form part of the out-stop tube of the shock absorber. Deformation of the crumple element may be identified by measuring the length of the fully extending landing gear, through non-destructive testing or by measuring the change in conductance of the crumple element. | 2022-04-28 |
20220126989 | VIBRATION ATTENUATOR - A vibration attenuator is configured for use on an aircraft rotor rotatable about a mast axis and has upper and lower weight assemblies, each comprising a weight with a center of gravity being a radial distance from the mast axis. The weight assemblies are configured for rotation together relative to the rotor at a selected angular rate about the mast axis, the weights being located on opposing sides of the mast axis. A first motor is configured for selective translation of one of the weight assemblies relative to the other weight assembly along the mast axis between a minimum-moment configuration, in which the centers of gravity of the weights revolve about the mast axis in the same plane, and a maximum-moment configuration, in which the centers of gravity of the weights revolve about the mast axis in different planes for producing a whirling moment about the mast axis. | 2022-04-28 |
20220126990 | DOUBLE-BLADE TANDEM HELICOPTER - A double-blade tandem helicopter comprising a fuselage ( | 2022-04-28 |
20220126991 | BIASED TENSION-TORSION STRAP - A rotor system includes a drive hub, a set of rotor blades extending radially from the drive hub, and a set of tension-torsion straps connecting the rotor blades to the drive hub. The drive hub has a rotor mast opening extending along a mast axis. The rotor system is configured to rotate about the mast axis. The drive hub further has a set of mounting slots for mounting the tension-torsion straps. The mounting slots are arranged along a circle around the drive hub, each mounting slot extending through the drive hub along a respective mounting axis. The mounting axis of each of the mounting slots is biased relative to the mast axis. The tension-torsion straps are mounted to the drive hub at their corresponding mounting slots. | 2022-04-28 |
20220126992 | DRIVE TUBE AND SWASHPLATE TRUNNION ASSEMBLY WITH CYLINDRICAL BEARINGS - In one embodiment of the present disclosure, there is provided a drive tube and swashplate trunnion assembly. The drive tube and swashplate trunnion assembly includes a drive tube having a plurality of grooves formed on an outer surface of the drive tube; a swashplate trunnion having a plurality of grooves formed on an inner surface of the swashplate trunnion, wherein individual grooves of the plurality of grooves on the swashplate trunnion mate with individual grooves of the plurality of grooves on the drive tube to form a plurality of channels; and a plurality of cylindrical bearings, wherein each of said cylindrical bearings is disposed within an individual channel of the plurality of channels. | 2022-04-28 |
20220126993 | PITCH HORN JOINT - A rotor assembly includes a pitch spider, rotor blade assemblies, and pitch horn joints. The pitch spider has a body and pitch spider legs extending from the body. Each blade rotor assembly includes a rotor blade, a pitch adapter joined to the rotor blade and connecting the rotor blade to the rotor hub, and a pitch horn. Each pitch horn joint joins one of the rotor blade assemblies to a corresponding pitch spider leg. Each pitch horn joint includes a pitch horn joint bolt extending from the pitch horn of the rotor blade assembly to the pitch spider leg along a pitch horn joint axis, the pitch horn joint bolt fixed to the pitch horn; a spherical bearing having an inner ring and an outer ring; and a slider sleeve coupled to the spherical bearing, the slider sleeve enabling the pitch horn to translate along the pitch horn joint axis. | 2022-04-28 |
20220126994 | Autonomous Multi-Purpose Heavy-Lift VTOL - An air transport vehicle that capitalizes on the strengths and complexities of a fixed and rotary winged aircraft. The air transport vehicle comprises a body aerodynamically designed to avoid substantial drag. The vehicle has a plurality of rotors configured to generate vertical thrust with a rear rotor configured to generate forward thrust. Additionally, each of the rotors are connected to the fixed wing elements and the fixed wing is positioned about the center of mass of the fuselage. Furthermore, each of the rotors are positioned at a fixed tilt angle such that the stability of the vehicle is maintained in a number of different flight configurations. | 2022-04-28 |
20220126995 | COAXIAL TILT-ROTOR UNMANNED AERIAL VEHICLE AND CONTROL METHOD THEREOF - A coaxial tilt-rotor unmanned aerial vehicle (CTRUAV) and a control method thereof. CTRUAV comprises three rotor modules, five rotors with motors respectively and a control system. Three rotor modules are in an inverted triangle layout. The left and right coaxial tiltable rotor modules in the front of the CTRUAV can rotate around the plane of a fuselage. A rear rotor is installed on the rear fixed-axis rotor module. Two pairs of coaxial rotors are respectively installed on the left and right coaxial tiltable rotor modules. Namely, the left and right coaxial tiltable rotor modules consists of an upper rotor and a lower rotor respectively; the upper rotor and the lower rotor have opposite rotation directions and the same rotation speed during the flight. Moreover, in the two pairs of coaxial rotors, the rotors on same layers have opposite rotation directions, and therotors on different layers have the same rotation directions. | 2022-04-28 |
20220126996 | VTOL AIRCRAFT FAN TILTING MECHANISMS AND ARRANGEMENTS - Disclosed is an electric aircraft, which includes a fuselage and at least one wing coupled to the fuselage. The electric aircraft includes a plurality of tilting fans coupled to the at least one wing, the plurality of tilting fans being configured to move between a vertical lift position and a forward flight position. The electric aircraft includes a plurality of tilting mechanisms coupled with at least one tilting fan. The electric aircraft includes a first actuator coupled to a first subset of the plurality of tilting mechanisms. The first subset of tilting mechanisms are identified among the plurality of tilting mechanisms according to a coupling scheme. The first actuator tilts a first group of tilting fans coupled to the first subset of the plurality of tilting mechanisms simultaneously. | 2022-04-28 |
20220126997 | PYLON MOUNTED TILT ROTOR - A pylon portion includes a first surface that attaches to an upper surface of a spar in a wing, where the pylon portion and a rotor portion protrude aft of the wing. A second surface attaches to a lower surface of the spar in the wing. The pylon portion also includes an intake air vent; a horizontal mounting surface; a rotor controller that is coupled to the horizontal mounting surface; and a heat sink that couples to the horizontal mounting surface and dissipates heat from at least the rotor controller. The rotor portion is moveably coupled to the pylon portion such that one or more rotor blades included in the rotor portion are able to move between: (1) a first position below the wing that is associated with a vertical flight mode and (2) a second position aft of the wing that is associated with a forward flight mode. | 2022-04-28 |
20220126998 | APPARATUS FOR GENERATING THRUST FOR AIR TRANSPORT - An apparatus for generating thrust for air transport includes a main thrust device, and an auxiliary thrust device configured to generate auxiliary thrust so as to enable an aircraft to vertically take off and land. The apparatus further includes: wings fixed to left and right sides of a fuselage of the aircraft, rotors installed on the wings and configured to generate thrust. In particular, the main thrust device provides driving force to the rotors using motors and an engine, and the auxiliary thrust device is installed in the fuselage and has a center of gravity configured to coincide with a center of gravity of the aircraft. | 2022-04-28 |
20220126999 | METHOD AND APPARATUS FOR UTILIZING AN UNMANNED AIR VEHICLE TO DEFINE OR PROVIDE GUIDANCE ALONG A ROUTE - An apparatus, method and system utilize an unmanned air vehicle (UAV) in order to support the definition and use of routes by bicyclists, pedestrians or scooters. With respect to defining a bicycle route a map database is accessed that represents roads segments in a geographic area. The map database contains map data that indicates attributes of the road segments. The bicycle route is then defined from an origin to a destination based upon the map data indicative of attributes of the road segments. In this regard, the bicycle route is defined to include one or more road segments that allow bicycle traffic unaccompanied by a UAV and one or more road segments for which bicycle traffic is unauthorized unless accompanied by a UAV. The bicycle route is subsequently caused to be provided to the bicyclist or a device accessible to the bicyclist. | 2022-04-28 |
20220127000 | UNMANNED AERIAL VEHICLE - An unmanned aerial vehicle (UAV) for application of an active ingredient to agricultural crops comprises at least one liquid reservoir, at least one liquid application unit, a processing unit, at least one set of rotor blades, and a plurality of legs. The at least one liquid application unit is configured to receive at least one input from the processing unit. The at least one input is useable to activate the at least one liquid application unit. The UAV is configured to fly within an environment using the at least one set of rotor blades, land within the environment, and walk on the plurality of legs to a location to apply liquid from the liquid reservoir to at least one plant. A location to apply the liquid is determined based on image analysis of one or more image of at least one image of the environment. | 2022-04-28 |
20220127001 | RETENTION SYSTEMS FOR MULTI-CART BAYS - A cart retention system for a multi-cart bay can include a first retainer configured to retain a front cart in the multi-cart bay and a second retainer configured to retain a rear cart in the multi-cart bay such that the rear cart is held spaced from the front cart. The system can also include a third retainer configured to retain both the front cart and the rear cart in the multi-cart bay separate from each other. | 2022-04-28 |
20220127002 | AIRCRAFT SEAT DEVICE - An aircraft seat device with at least one shell element, with at least one table unit, with at least one support device that is configured to obliquely connect the at least one table unit to the shell element at least in a stowage position, the support device comprising at least one rotational bearing unit, which is configured for pivoting the table unit between the stowage position and at least one intermediate position that is situated substantially in a horizontal plane, the support device comprising at least one linear bearing unit, which is configured for traversing the table unit between the intermediate position and at least one completely deployed usage position that is close to a seat. | 2022-04-28 |
20220127003 | Aircraft Tray Table Retention Assembly - An aircraft tray table retention assembly may include a seat magnetic component installed within a rear bezel of an aircraft seat, and a tray table magnetic component installed within an aircraft tray table. The aircraft tray table may be coupled to the aircraft seat via at least one of one or more hinges or a set of rails, and may be configured to actuate between a stowed position and a deployed position via the at least one of one or more hinges or a set of rails. The tray table magnetic component may be configured to engage the seat magnetic component when the aircraft tray table is in the stowed position. The aircraft tray table retention assembly may include a tray magnetic component configured to engage the tray table magnetic component when the aircraft tray table is in the deployed position. | 2022-04-28 |
20220127004 | SEATBACK FOR A VEHICLE SEAT - Examples of the disclosure provide a seatback for a vehicle seat, in particular an aircraft seat, comprising a seatback structure that includes a rear side having a partially circumferential outer edge and a recess which is partially surrounded by the outer edge. The recess is configured to retain a panel at least partially arranged within the recess and at least partially covered by the outer edge. The panel is detachable retained to and/or in the recess and is configured as an interchangeable and customized part. | 2022-04-28 |
20220127005 | PRESSURE REGULATING VALVE ASSEMBLY - A pressure regulating valve assembly includes: a valve having an upstream side receiving an input flow and a downstream side providing an output flow, an actuator for opening and closing the valve, including partially opening the valve, and a regulator controlling the actuator to open, close or partially open the valve. The regulator includes a sense pressure port, wherein pressure at the port is maintained constant by the regulator. A chamber has a first entry orifice, a second entry orifice and an exit orifice. The first entry orifice is connected to the upstream side, the second entry orifice is connected to the downstream side, and the exit orifice is connected to the port. The exit orifice provides that the pressure at the exit orifice lies between the pressure at the first entry orifice and the pressure at the second entry orifice. | 2022-04-28 |
20220127006 | PARACHUTE DEVICE, FLIGHT DEVICE, AND FLYING BODY EJECTION MECHANISM - To provide a parachute device capable of quickly and reliably opening a parachute even when an airflow effect during flying or falling of a flight device cannot be immediately obtained. A parachute device ( | 2022-04-28 |
20220127007 | SYSTEMS FOR AIRCRAFT LANDING AFTER EJECTION - A system for controlling an aircraft in response to deployment of an ejection seat may comprise a seat controller located on the ejection seat and configured to output a signal in response to initiation of an ejection sequence. An aircraft controller may be configured to receive the signal from the seat controller. A tangible, non-transitory memory may be configured to communicate with the aircraft controller. The tangible, non-transitory memory may have instructions stored thereon that, in response to execution by the aircraft controller, cause the aircraft controller to perform operations, which may comprise receiving the signal from the seat controller, receiving data signals from an operational data source, and sending command signals configured to control a component of the aircraft | 2022-04-28 |
20220127008 | SMART SYSTEMS AND METHODS FOR AUTOMATIC DEPLOYMENT OF AN EJECTION SYSTEM - An ejection system may comprise an ejection seat and a smart deployment system configured to initiate a deployment of the ejection seat. The smart deployment system may comprise a pilot health monitoring system including a plurality of sensors configured to detect a plurality of physiological conditions, and a controller configured to make ejection system decisions based on a pilot health signal received from the pilot health monitoring system and an aircraft health signal output from an aircraft health monitoring system. | 2022-04-28 |
20220127009 | AIRCRAFT POWER PLANT WITH SUPERCRITICAL CO2 HEAT ENGINE - Aircraft power plants including combustion engines, and associated methods for recuperating waste heat from such aircraft power plants are described. A method includes transferring the heat rejected by the internal combustion engine to supercritical CO | 2022-04-28 |
20220127010 | BRACED-PYLON ARCHITECTURE FOR MOUNTING AN ENGINE TO AN AIRCRAFT - An engine mounting pylon for suspending a turbofan beneath an aircraft wing, including a primary structure, a fastening device for fastening to the turbofan, and a fastening device for fastening to the wing. The engine mounting pylon furthermore comprises multiple rigid braces that mechanically connect the primary structure to the wing of the aircraft, a first brace-attachment device that mechanically connects a first end of each brace to the wing, and a second brace-attachment device that mechanically connects a second end of each brace to the primary structure. This braced-pylon architecture makes it possible to reduce the dimensions of the primary structure and the various elements that constitute the first and second attachment devices. | 2022-04-28 |
20220127011 | POWER DISTRIBUTION CIRCUITS FOR ELECTRICALLY POWERED AIRCRAFT - A power distribution circuit for an electrically powered aircraft includes a plurality of batteries and a plurality of electric propulsion systems. A plurality of isolated power distribution circuits each couple a battery of the plurality of batteries to two or more electric propulsion systems. The plurality of electric propulsion systems are positioned on the aircraft to apply balanced forces to the aircraft such that in the event of a failure, the aircraft remains stable and only experiences a loss in altitude or speed. | 2022-04-28 |
20220127012 | GEAR SHROUDING WITH INTEGRAL LUBRICATING FEATURES - In one embodiment of the present disclosure, there is provided an aircraft gearbox including a gear and a gear shrouding for providing lubrication to the gear. The gear shrouding is disposed around the gear, has an inner surface facing the gear and an opposing outer surface facing away from the gear, and includes a channel formed along at least a portion of the gear shrouding between the inner surface and the outer surface of the gear shrouding, an input orifice extending to the channel, wherein the input orifice is at a first position on the channel, and an output orifice extending to the channel, wherein the output orifice is at a second position on the channel different from the first position. In another embodiment, the gear shrouding further includes a second output orifice at a third position on the channel different from the first and second positions. | 2022-04-28 |
20220127013 | SECURE AVIONCS WIRELESS ACCESS POINT DEVICE WITH HEAT SINK ENCLOSURE - The present application provides a thermal design of device enclosures for aviation cyber security hardware products. A secure avionics wireless access point device with heat sink enclosure is provided that provides security processing and interconnectivity while being small in size, not requiring supplemental cooling and may operate outside of the aviation pressure cabin. The device may be installed in-line with networking devices and avionics to monitor and protect an aircraft's onboard network. | 2022-04-28 |
20220127014 | DRONE DOCKING STATION AND DOCKING MODULE - A mechanically secure docking platform for unmanned VTOL aircraft (“drone”) or other automated vehicle, acting as an automated battery recharging system for drones or a battery quick change system for drones. The system also is capable of enabling an automated data logistics system for drones, an autonomous guidance system for landing and docking for drones, and/or an autonomous guidance system for undocking and takeoff for drones. | 2022-04-28 |
20220127015 | CONVEYING SYSTEM HAVING VERTICALLY TRAVELING DRIVERLESS TRANSPORT VEHICLES - A driverless transport vehicle, a conveying system, and a method for transporting piece goods. The driverless transport vehicle overcomes a climbing section equipped with a primary side of an energy transmission device. The driverless transport vehicle, which can be moved individually and autonomously on a conveying plane, has a secondary side for energy pick-up in order, assisted by the energy pick-up, to overcome a height difference of the climbing section and/or a transition between the conveying plane and the climbing section. The formation of a connection between the primary side and the secondary side and the overcoming of the climbing section and of the transition between the conveying plane and the climbing section take place at a throughput speed without a slowing-down. | 2022-04-28 |
20220127016 | GAS DISSOLUTION PREDICTION SYSTEM AND METHOD FOR AN AIRCRAFT SHOCK STRUT - Techniques and methodologies for servicing a shock strut are provided that account for the variability in gas solubility of the shock strut while in-service. These examples incorporates knowledge of the shock strut's stoke history in order to estimate/predict the amount of gas in solution, its percentage saturation, etc. This may permit a more refined knowledge of the true servicing state of the shock strut. | 2022-04-28 |
20220127017 | A FLOATING PLATFORM FOR LAUNCHING A SPACE ROCKET FROM A HEIGHT AND METHOD FOR LAUNCHING A RIGID -WALLED BALLOON INTO THE SPACE - The subject of the present invention relates to a floating platform ( | 2022-04-28 |
20220127018 | SPACECRAFT AND CONTROL SYSTEM - A spacecraft for changing an orbit or an attitude of a target in outer space by irradiating the target with a laser, the spacecraft includes: a laser apparatus configured to generate the laser; a focusing unit configured to converge the laser; a detecting unit configured to acquire detection information including a distance between the spacecraft and the target; and an irradiation control unit configured to control the focusing unit on the basis of the distance so that the laser converges on the target. | 2022-04-28 |
20220127019 | ROCKET PROPULSION SYSTEM, METHOD, AND SPACECRAFT - A rocket propulsion system comprising a first cryogenic tank and a second cryogenic tank, wherein the first cryogenic tank is filled with a first propellant, and the second cryogenic tank is filled with a second propellant, for purposes of feeding at least one repeatedly ignitable main propulsion unit in a propulsion phase of the rocket propulsion system. For purposes of tank pressurization via at least a low level of acceleration in a ballistic phase, a first auxiliary propulsion unit can be operated by means of a first gas pressure accumulator, and at least one further auxiliary propulsion unit can be operated by means of a further gas pressure accumulator, and the rocket propulsion system is assigned an energy conversion unit, which is designed at least to charge the first and the second gas pressure accumulator, preferably in the ballistic phase. | 2022-04-28 |
20220127020 | SPACE DEBRIS ENGAGEMENT AND DEORBIT SYSTEM - Exemplary embodiments described herein include innovative engagement devices. Exemplary engagement devices may include on or more tape spring systems. The tape spring system may include a continuous or segmented bi-stable tape spring. The tape spring can be stowed in a rolled up configuration, extended to a deployed configuration, and then triggered to return to a retracted configuration. | 2022-04-28 |
20220127021 | SOLAR SAIL FOR ORBITAL MANEUVERS - A solar sail includes a bus and a plurality of separate movable vanes coupled to the bus. Each movable vane includes a reflective surface for generating solar radiation pressure and propel the solar sail in space. Each vane may be movable relative to the bus in a fully deployed configuration such that an amount of thrust generated by solar radiation pressure on each vane is controllable. | 2022-04-28 |
20220127022 | MULTIPLE SPACE VEHICLE LAUNCH SYSTEM - A space vehicle system, a method of manufacturing a multiple space vehicle system, and a method of disposing space vehicles into Earth orbit are disclosed. The space vehicle system may include a first space vehicle including a first core structure with a first wall thickness. The space vehicle system may include a second space vehicle including a second core structure with a second wall thickness, the second wall thickness different from the first wall thickness, and the second core structure releasably attached to the first space vehicle in a stacked configuration. | 2022-04-28 |
20220127023 | SPACECRAFT WITH UNIVERSAL TEST PORT - A universal test port is connected to the different functional sub-systems of a spacecraft, allowing the sub-systems to be tested from a single location of an assembled spacecraft. The universal test port is mounted on an external surface of the spacecraft and configured to connect to the different functional sub-systems (such as power, propulsion, and command and data handling, for example) of the assembled spacecraft, allowing for the streamlining of testing operations by electrical ground system equipment during assembly, integration, and test (AIT) operations and reducing the risk of collateral damage to spacecraft hardware during testing in AIT. | 2022-04-28 |
20220127024 | PHARMACY PACKAGING SYSTEM - A packaging unit for packaging pharmaceuticals into a pouch includes packaging equipment operable to form the pouch, a track configured to direct the pharmaceuticals toward the packaging equipment, and a receptacle coupled to the track upstream of the packaging equipment to receive the pharmaceuticals from the track. The receptacle includes a plunger. The pouch is formed around the plunger. | 2022-04-28 |
20220127025 | FLOW REGULATION SYSTEM FOR THE FILLING OF A SACK WITH A GRANULAR PRODUCT, AND CORRESPONDING MACHINE AND METHOD - A flow control system ( | 2022-04-28 |
20220127026 | FOOD PRODUCT AMENDMENT APPARATUS AND METHOD OF USE THEREOF - The invention comprises an apparatus and a method for amending an incomplete product and/or a product to form an amended product, such as by receiving the original product in a first pressurized container, breaking a pressure seal of the first pressurized container, adding tetrahydrocannabinol (THC) to the first pressurized container, and resealing the first pressurized container, such as where optionally a portion of the amendment process is at a second physical location separated from a first location by a state line and/or a legislative boundary. | 2022-04-28 |
20220127027 | FRONT FLAP LIFTING MECHANISM - A lifting apparatus for a case on a conveyor system. A chain vertically hangs over a conveyor belt. A hook is positioned on an end of the chain. A piston retracts and releases the chain. The hook interacts with and moves front flaps on cases traveling on the conveyor system. | 2022-04-28 |
20220127028 | COMPONENT MOUNTING SYSTEM AND TAPE SCRAPS COLLECTING DEVICE - A component mounting system including: a component mounting device group in which a plurality of component mounting devices that mount components supplied to a board transported in from an upstream side by a tape feeder and transport out the board to a downstream side, and cut a carrier tape after supplying the components by a cutter device and discharge scraps of carrier tape, are installed on a floor surface while being arranged in a direction of conveying the board; a main conveyor that is installed along an arrangement direction of the plurality of component mounting devices in a region on the floor surface under the component mounting device group, and transports the scraps of carrier tape discharged from each of the plurality of component mounting devices; and a scraps storage that is installed outside the region and stores the scraps of carrier tape transported by the main conveyor. | 2022-04-28 |
20220127029 | METHOD FOR PACKAGING ARTICLES AND PACKAGING SYSTEM FOR ARTICLES SUCH AS BEVERAGE CONTAINERS OR THE LIKE - Disclosed is a method for packaging articles ( | 2022-04-28 |
20220127030 | SYSTEM FOR FORMING AN ARTICLE ARRAY IN A CONTAINER - A head for use in forming an article array in a container cavity (“cavity”) by sequential placement of adjacent article rows in the cavity, including a gripper having a frame having a longitudinal axis, the gripper adapted to selectively engage and disengage an article row for permitting placement thereof; and a flexible layer connected to the frame and extending parallel to the longitudinal axis and positioned to one side of the gripper. During formation of the article array in the cavity, the flexible layer preventing contact between a most recently positioned article row in the cavity and a corresponding article row being positioned in the cavity, including filling a remaining unfilled portion of the cavity between a penultimate article row and the container for receiving the final article row having a width approximately equal to or less than a width of the final article row. | 2022-04-28 |
20220127031 | AN INDUCTION HEAT SEALING DEVICE AND A METHOD FOR TRANSVERSALLY SEAL A TUBE OF PACKAGING MATERIAL - An induction heat sealing device ( | 2022-04-28 |
20220127032 | PACKAGING APPARATUS WITH PACKAGE DIVIDING SEAL MECHANISM - Packaging apparatuses for loading and sealing products into a web of interconnected bags, and methods of using them, are provided. In one aspect, the packaging apparatus includes an intermittently advancing web conveyor that also indexes vertically to facilitate stacked loading of products into the bags. In another aspect, the packaging apparatus includes a dividing seal station that applies a center seal dividing the bag into separate sealed subcompartments, some of the bag contents being distributed to each compartment, such as one of two trays to each subcompartment. To facilitate distribution of contents and even sealing, the dividing seal station may include a dividing sealer lower support that oscillates vertically to promote settling of contents and gases in the bag before applying a dividing seal. | 2022-04-28 |
20220127033 | APPARATUS FOR SEPARATING A RIGID BODY FROM ITS CONTENTS - A high-speed automated separation apparatus includes a pair of flexible discs, a driver to rotate the flexible discs, a feeder to position a rigid body at a first location between the flexible discs, a spreader and a converger operable upon the flexible discs such that opposing portions of the flexible disc converge upon the positioned rigid body. The rotating flexible discs rotate the rigid body beyond the first location, and content from the rigid body is expelled. The rigid body and the expelled content are then available for reuse. | 2022-04-28 |
20220127034 | Mechanism for Label Size Selection - A mechanism used to select a label size to be applied to a cable in a label applicator. The mechanism includes an index plate, an index arm, and a wedge carrier. The index arm is pivotably mounted to the index plate and the wedge carrier is mounted to the index plate. The wedge carrier has guide rollers that dictate a label path. The index arm moves the index plate which linearly moves the wedge carrier thereby adjusting the label path in the label applicator. | 2022-04-28 |
20220127035 | System and Method for Printing Labels and Applying a Printed Overlaminated Label Set on an Object - The present invention relates to a method for printing labels and applying a laminated printed label on to an object | 2022-04-28 |
20220127036 | METHOD OF MAKING ARTICLE WITH VISUAL EFFECT - Method of making a blow molded article from a preform including: a) providing a preform of a thermoplastic material having a plurality of effect structures each having an effect surface having a normal with an orientation, the preform having a body with one or more walls and an opening, wherein at least a portion of the one or more walls of the preform has a three-dimensional pattern of cavities and/or protrusions thereon; and b) blow molding the preform to form a blow molded article, wherein the step of blow molding the preform changes the orientation of the normal of at least some of the effect surfaces of the effect structures to create a visual effect in at least one wall of the blow molded article. | 2022-04-28 |
20220127037 | LIQUID CONTAINER MADE ENTIRELY FROM NATURAL PLANT MATERIALS - A liquid container made entirely from natural plant materials is revealed. The liquid container includes a cap and an upper portion made from plant fiber by mold injection, a body made of a spiral paper tube having at least two-layer structure, and a base produced by molding of composite paper. The body and the base are connected by adhesives. A fastening member is disposed on an area where the upper portion and the body are connected for improving reliability and structural strength of the area while a mounting groove formed by rolling is arranged at an area where a bottom end of the body and the base are connected by adhesives. The fastening member and the mounting groove improve connection reliability and structure strength. The liquid container with excellent structural strength is more resistant to pressure in radial and longitudinal directions and used to fill pressurized beverages or liquid such as carbonated drinks. | 2022-04-28 |
20220127038 | MODULAR PACKAGING SYSTEM - A packaging system includes a container with a bottom wall, a first end wall connecting to the bottom wall, a second end wall opposed to the first end wall and connecting to the bottom wall, at least a portion of a first side wall connecting between the first and second end walls, at least a portion of a second side wall opposed to the first side wall and connecting between the first and second end walls, and a plurality of corner walls. At least one corner wall connects the first end wall to the portion of a first side wall. | 2022-04-28 |
20220127039 | BOX DIVIDER SYSTEM - The present disclosure relates to compartment system for storing and organizing various items and objects. The compartment system includes an exemplary divider which fits within pre-existing boxes and separates the same into various storage compartments. The divider is generally made of one or more sidewalls, one or more transverse divider walls, and optionally one or more axial divider walls. Methods of forming the exemplary dividers are also disclosed. | 2022-04-28 |
20220127040 | RESEALABLE EASY OPEN LID - A resealable easy open lid that is composed of a lid and a pull ring riveted on the lid; the rear end of the pull ring is composed of an outer ring body and an inner tongue of the pull ring; the tongue is provided with an arched deformation area along the edge; the arched deformation area is an edge inclined to the inner side of the lid which is formed by die stamping on the tongue of the pull ring; the tongue is provided with a part arching to the outside of the lid; after the pull ring is rotated around the riveting point, the tongue of the pull ring covers the opening zone, and when the middle part of the tongue is pressed, the arched deformation area can be overturned and deformed to make it contact with the edge of the opening area to seal the area. | 2022-04-28 |
20220127041 | THC BEVERAGE CONTAINER APPARATUS AND METHOD OF USE THEREOF - The invention comprises a method and apparatus for holding a | 2022-04-28 |
20220127042 | Means to hold together multiple containers and securely fasten interchangeable decorative coverings - In its preferred embodiment, my invention presents a product and method whereby a series of containers can be held together along a longitudinal axis, a decorative covering can be held securely to a container, and an individual can easily and quickly change the appearance of the container by removing the attached covering and securely attaching another without need of an additional securing means included in either of the coverings. Changing the covering can be for reasons such as matching the look to a specific color scheme or to the surroundings it is in, to coordinate colors/theme of a specific holiday, or to align with a child's interests, such as a favorite sport they are involved in or a field of interest they follow. | 2022-04-28 |
20220127043 | REINFORCING MEMBER AND STORAGE BOX HAVING THE SAME - This patent provides a reinforcing member which is applied to a storage box. The reinforcing member is roughly in a shape of a frame, comprising a first annular structure, a second annular structure, and a positioning portion. The thickness of the second annular structure is not greater than the thickness of the first annular structure, and the second annular structure is surrounded by the first annular structure. There is a gap between the first annular structure and the second annular structure wherein the gap length of the gap is not shorter than 0.5 cm. The positioning portion is disposed in the gap. Wherein the storage box includes a box body, a bottom surface of the box body includes a positioning structure, and the positioning portion of the reinforcing member may be connected to the positioning structure. | 2022-04-28 |
20220127044 | SUPPORT FOR A WORK OF ART - The invention is directed to a support for a work of art comprising a base element for fixing the support to an interior wall of a shipping container and a clamping element for clamping the work of art and wherein the base element and the clamping element are fixed to each other by wire rope isolators. | 2022-04-28 |
20220127045 | CAN SAFE - A sanitary cover/adhesive seal placed onto a drinking can for users to simply peel off of the can before consuming the beverage. The sanitary cover/adhesive seal's primary purpose is to protect consumers from consuming any bacteria, dirt, residue, virus (Covid-19) enzymes that could make them sick. The sanitary cover/adhesive seal would cover part of or the entire top of the can and surround parts of the wall of the can as well. | 2022-04-28 |
20220127046 | BAG WITH TEXT DISPLAY - The invention provides such a bag that a person can easily recognize the message text displayed thereon. A plastic bag ( | 2022-04-28 |
20220127047 | CLOSURE SYSTEM FOR CONTAINER - A closure system for a container having a body is provided. The body includes a top edge and defines an internal volume extending from the top edge. The closure system includes a drawstring configured to close the top edge. The closure system also includes an internal flap spaced apart from the top edge. The internal flap includes a first side and a second side. The first side is attached to an inner surface of the body. The second side is detachably connected to the inner surface of the body. The internal flap is configured to cover the internal volume upon connection of the second side to the inner surface of the body. | 2022-04-28 |
20220127048 | CONTAINER CLOSURE OF SYNTHETIC RESIN - A container closure of synthetic resin is used for a container having a mouth-and-neck portion formed with an external thread on its outer periphery and an engaging jaw portion positioned below the external thread. The closure including a body and a tamper evident skirt portion is not entirely separated from the mouth-and-neck portion of the container even after unsealing the container at the mouth-and-neck portion. The container closure is improved such that the body is held sufficiently reliably at a required opening position when the body detached from the mouth-and-neck portion is pivoted to the opening position even if the container closure has a relatively short axial length. Furthermore, when the body is pivoted again to the opening position, a sound recognizable for a consumer is generated with sufficient certainty. At least in an angle region in which a protruding piece formed on the skirt wall of the body is present, an extending portion is formed at an engaging piece formed on the tamper evident skirt portion. In a state where the container closure of synthetic resin is mounted on the mouth-and-neck portion, the extending portion is positioned between the engaging jaw portion of the mouth-and-neck portion and the tamper evident skirt portion. | 2022-04-28 |
20220127049 | LID ASSEMBLY FOR A CONTAINER - This disclosure relates to a lid assembly that has a lid assembly for a container, such as a drinking container, that includes a lid member, and a pouring member, wherein the lid member and pouring member are releasably connected to the container. The lid member may include a body member, a handle portion connected to the body member, an internal threaded portion, an internal receiving portion, and a lid gasket member arranged in the internal receiving portion. The pouring member may include a spout collar, a spout, and a spout opening extending through the spout, wherein the spout extends from the spout collar and includes an upper end above an upper surface of the spout collar. The lid assembly has a closed orientation that prevents liquid from flowing through the opening of the pouring member and an open orientation that allows liquid to flow through the opening of the pouring member. When the lid assembly is in the closed orientation, the lid gasket member contacts both the upper end of the spout and the upper surface of the spout collar. | 2022-04-28 |
20220127050 | One-button-opened cup cap and cup - The present invention discloses a one-button-opened cup cap and cup. The cup comprises a cup body and a cup cap partially inserted into the cup body. The cup cap comprises a pressing assembly, a water shutoff assembly and an exhaust assembly. The water shutoff assembly comprises a main cap, a sealing cap and a linkage component. The pressing assembly is connected with the main cap. The linkage component is provided with an air outlet hole plugged by the exhaust assembly. The pressing assembly is longitudinally pressed under the action of external force to act on the exhaust assembly and unblock the air outlet hole. The main cap restricts the pressing assembly from positioned at two longitudinal positions different in height. The present invention has the advantages of need of only pressing the pressing component when disconnecting the cup cap from the cup body, and simple and quick disconnection operation. | 2022-04-28 |
20220127051 | CHOICE CAN - A can-top reservoir attached to a lid of a beverage container is provided. The pull tab is used for opening a beverage container and dispensing edible material into the beverage container. The pull tab comprises a reservoir for storing an edible material, different than the beverage container. The reservoir is provided with a sealing element which when manipulated to selectively dispense the edible material from the reservoir to the mouth of the beverage container via an egress of the reservoir. | 2022-04-28 |
20220127052 | CONTAINER CARRIER - A container carrier for unitizing a plurality of containers. The carrier includes a planar sheet of a material and a plurality of container receiving apertures within the planar sheet and arranged in longitudinal rows and transverse ranks. Each of the plurality of container receiving apertures includes a central opening shape and a plurality of clefts radially extending in the planar sheet outward from the central shape to form a plurality of container friction flaps each adapted to extend along a side wall of a corresponding container of the plurality of containers. | 2022-04-28 |
20220127053 | SEALED PACKAGING FOR ELECTRONIC ACCESSORIES FOR MEASURING FIT OF ELECTRONIC DEVICES - The present invention provides a novel sealed retail package for selling a retail electronic mobile accessory, e.g., cell phone/tablet case or a cell phone/tablet screen protector. The novel structure of the sealed retail package permits a retail customer to compare the size of the retail electronic mobile accessory to the customer's electronic mobile device, e.g., a cell phone/tablet. Preferably, the sealed retail package is a retail package containing at least one electronic mobile accessory having a particular preset size. The retail package has a planar front surface and a planar back surface with a shaped recessed indentation on the planar back surface of the retail package. The shaped recess indentation has a configuration for receiving the customer's electronic mobile device within the recessed indentation, for determining if the customer's electronic mobile device fits the electronic mobile accessory being offered for sale. In alternate embodiments, the application includes various other types of sealed packages with shaped recesses. | 2022-04-28 |
20220127054 | Child-Resistant Packaging - Child-resistant packaging ( | 2022-04-28 |
20220127055 | PACKAGE STRUCTURE FOR CURTAIN - This application provides a package structure for a curtain, which relates to a technical field of a package. The package structure for the curtain includes a package body used for placing the curtain; the package body is provided with more than one first area through which the curtain inside the package body can be viewed; the package body is further provided with more than one second area on which information is printed; and the first area is adjacent to the second area. This application has the following beneficial effect: the appearance of the curtain when the curtain is hung is viewed even if the curtain is inside the package structure. | 2022-04-28 |
20220127056 | VEHICLE FUEL TANK FOR IMPROVED CRASHWORTHINESS - A compartment for storing fuel in a vehicle having a protective outer structure and an inner structure. The protective outer structure is maintained in position relative to the vehicle during normal operation of the vehicle. The inner structure, which holds fuel, is positioned in the outer structure. The inner structure is maintained in position relative to the outer structure and relative to the vehicle during normal operation of the vehicle. During an impact to the vehicle, the inner structure is configured to move independent of the outer structure. | 2022-04-28 |
20220127057 | MULTI-USE BOTTLE SHIPPING ASSEMBLY WITH RESILIENT ELEMENTS - A packing tray ( | 2022-04-28 |
20220127058 | FOOD / BEVERAGE NOOTROPIC AMENDMENT APPARATUS AND METHOD OF USE THEREOF - The invention comprises a method and apparatus for amending a food product, comprising the steps of: (1) forming a nootropic emulsion comprising a nootropic, an emulsifier, and water, the nootropic including at least one of: | 2022-04-28 |
20220127059 | Composite Liquid Agent Package and Method for Manufacturing Same, and Kit for Preparing Multicomponent Liquid Composition Using the Composite Liquid Agent Package and Method for Manufacturing Same - A composite liquid agent package containing a first pouch filled with a first liquid and a second pouch filled with a second liquid; and a kit for preparing a multicomponent composition, the kit including an outer bag housing the composite liquid agent package. With an opposite end section of the first pouch and an opposite end section of the second pouch being superposed, the superposed parts are heated and pressurized to exclude sealants, which are present within the opposite end sections, outwardly of the extremities of the outer layers of the opposite end sections, while heat-fusing the two extruded sealants together to join the two pouches. | 2022-04-28 |
20220127060 | VENTED SEALABLE BAG - A vented sealable bag comprises a container, a two-part seal and a vent. The container has opposing sidewalls and a bottom defining a cavity. The sidewalls form a neck defining an opening opposite the bottom, The sidewalls have an inner surface facing the cavity and an outer surface external to the container and the sidewalls have a thickness. A two-part seal is formed on the inner surface of the sidewalls adjacent the neck. The two-part seal has a hook formed on one sidewall and a clasp formed on an opposite sidewall. The hook and clasp are arranged on the inner surface of the sidewalls to form an airtight seal isolating the cavity from an external environment when the hook is embedded in the clasp but otherwise maintain the opening in the container. A vent is integrally formed in one of the sidewalls. The vent is further comprised of a dimple having a thickness that is thinner than the thickness of the sidewalls. The dimple is concave when viewed from the cavity and has a slit formed at an apex that is closed except when the container is sealed and an internal pressure is created that is higher than an external pressure on the outer surface of the sidewalls. | 2022-04-28 |