40th week of 2021 patent applcation highlights part 22 |
Patent application number | Title | Published |
20210309335 | CONTROL DEVICE FOR BATTERY OF MARINE VESSEL, CONTROL METHOD THEREFOR, AND MARINE VESSEL - A control device for a battery of a marine vessel recovers a power storage amount of a chargeable lithium ion battery while protecting the same. When an acquired power storage amount of the lithium ion battery becomes equal to or less than a first predetermined power storage amount, a switch to connect the lithium ion battery and a line or a load is turned off. While the switch is off, as an electric power balance on the line, a power inflow amount, a first power outflow amount, and a second power outflow amount are acquired. Based on the electric power balance acquired while the switch is off, whether a chargeable condition in which the lithium ion battery is chargeable is satisfied is determined. When the chargeable condition is satisfied, the switch is turned on. | 2021-10-07 |
20210309336 | TRANSMISSION FOR HYBRID PROPULSION SYSTEM - A transmission system for a hybrid power plant, such as a hybrid propulsion system of a marine vessel, is described. The transmission is configured to selectively couple a primary mover and/or a secondary mover to an output of the transmission for providing a power output, and optionally selectively couple the primary mover to the secondary mover, decoupling the output, for electrical energy generation in a compact and light-weight design. | 2021-10-07 |
20210309337 | SYSTEM FOR THE STRUCTURE, CONTROL, AND ENERGY MANAGEMENT OF LOW-PRESSURE CELLS FOR AEROSTATIC LIFT - A structural system for lifting cells, constructed of modular, lightweight framing supporting thin, lightweight, single-ply or laminated, air-impermeable membranes, that maintain near constant-volume under low pressure for aerostatic lift in lighter-than-air aircraft; a system for controlling that aerostatic lift in a single or a plurality of such lifting cells, using electrically-powered vacuum pumps and valves; and a system for recovering electrical energy expended during ascent by using the inflow of air into the lifting cells during descent to generate electricity. | 2021-10-07 |
20210309338 | HIGH ALTITUDE BALLOON SYSTEMS AND METHODS - Described herein are features for a high altitude lighter-than-air (LTA) system and associated methods. A zero-pressure balloon (ZPB) is attached in tandem with one or more air super-pressure balloons (SPB). The ZPB provides lift for the system while the SPB may provide a variable amount of ballast air by pumping in or expelling out ambient air. Various advanced performance targets relating to ascent rate, descent rate, range and maximum altitude are achievable with various scaled versions of the basic design of the LTA system. Advanced navigation and control techniques, such as more efficient high altitude station-keeping approaches, made possible with the LTA system are also described. | 2021-10-07 |
20210309339 | HELICAL CABLE MANAGEMENT SYSTEM - Aspects of the technology relate to rotational electromechanical systems, in which data and or power are supplied to components while one part of the system is rotating relative to another part of the system. Repeated rotation may create strain on or otherwise cause the cables to intermittently or permanently fail. A helical cable management system is provided that enables full rotation to the extent permitted. One or more cables are wound in a helical shape around the axis of rotation, which distributes the deformation of the cable along the helical length. Rotation in one direction causes the helix diameter to increase, while rotation in the other direction causes the helix diameter to decrease. A structure is used to maintain the distance between helical turns, while permitting the increase and decrease of the helix diameter. This reduces the overall strain on the cables, which can significantly extend their useful lifetime. | 2021-10-07 |
20210309340 | AIRCRAFT PRESSURE DECK - Embodiments for aircraft pressure deck. One embodiment is a pressure deck of an aircraft. The pressure deck includes beams extending longitudinally along a fuselage of the aircraft, and a web attached to an underside of the beams, the web including arches between adjacent beams to allow the pressure deck to flex laterally. The pressure deck also includes a box structure between a middle pair of the beams and configured to transfer load forward to a rear spar of a wing of the aircraft and aft to an aft wheel well bulkhead of the aircraft. The pressure deck further includes a first intercostal outboard from the box structure and configured to stabilize a first outboard pair of the beams, and a second intercostal outboard from the first intercostal and coupled between a second outboard pair of the beams via a swing link to allow the second intercostal to flex laterally. | 2021-10-07 |
20210309341 | PRESSURIZED MONOCOQUE STRUCTURE WITH ABRUPT CHANGE IN SHAPE - A flexible strengthening joint for a pressurized vessel includes an outer skin having a localized abrupt change in shape. The outer skin includes a first skin section and a second skin section, the localized abrupt change in shape being located at a junction between the first skin section and the second skin section. A reinforcing bulkhead is located in the interior of the pressurized vessel. The reinforcing bulkhead includes a first bulkhead section that is directly attached to the first section of the outer skin and a second bulkhead section that unattached directly to the first section. A kick frame is located in the interior, the kick frame spanning at least the second bulkhead section. At least one intercostal is secured to the second bulkhead section. The at least one intercostal is also secured to the kick frame. | 2021-10-07 |
20210309342 | FRAME ASSEMBLY FOR UNMANNED AERIAL VEHICLE (UAV), AND UAV HAVING THE SAME - A frame assembly for an unmanned aerial vehicle includes an upper cover, a lower cover, a housing, and a circuit board. The housing includes electric chamber between the upper cover and the lower cover. The circuit board assembly is disposed in the electric chamber and includes a first circuit board arranged close to the upper cover and a second circuit board close to the lower cover. The first circuit board is spaced apart from the second circuit board. | 2021-10-07 |
20210309343 | FASTENING SYSTEM, MONUMENT AND METHOD FOR ATTACHING A FIXTURE TO A MONUMENT - A fastening system to attach a fixture to a monument installed in a passenger cabin including a wall portion of the monument having at least one first fastening element; and a frame having at least one second fastening element and which is configured to cover the fixture, at least in part, in a fastened state. The first and second fastening elements are configured to engage with one another and be movable relative to one another in a pre-assembled state, and to fix one another in the fastened state. The fastened state can be produced in that, in the pre-assembled state, the frame is moved relative to the wall portion in a fastening direction extending at least substantially parallel to a main extension plane of the wall portion. A method for attaching a fixture to a monument provided for installation in a passenger cabin via a fastening system is provided. | 2021-10-07 |
20210309344 | Composite Materials Having Reinforced Access Openings - Structurally reinforced composite components are disclosed having access openings reinforced to increase strain load and buckling load without adding weight to the composite components by inducing out-of-plane regions proximate to the access opening during composite prepreg laminate layup. | 2021-10-07 |
20210309345 | SYSTEM AND METHOD FOR JOINING STRUCTURES WITH LARGE THERMAL EXPANSION DIFFERENCES - A system and method are provided that enable joined materials to expand and contract at different rates while maintaining a structurally sound connection. A system for joining structures with differing coefficients of thermal expansion includes: a first structural element of a first material having a first coefficient of thermal expansion (CTE); a plurality of flexures each defining a first portion and a second portion and attached at the first portion to the first structural element; and a second structural element of a second material having a second CTE, where the second structural element is attached to the second portion of each of the plurality of flexures, where in response to relative movement between the first structural element and the second structural element, the plurality of flexures bend to accommodate the relative movement. | 2021-10-07 |
20210309346 | SELECTING PROPELLERS FOR PERFORMANCE AND NOISE SHAPING - Aerial vehicles may be operated with discrete sets of propellers, which may be selected for a specific purpose or on a specific basis. The discrete sets of propellers may be operated separately or in tandem with one another, and at varying power levels. For example, a set of propellers may be selected to optimize the thrust, lift, maneuverability or efficiency of an aerial vehicle based on a position or other operational characteristic of the aerial vehicle, or an environmental condition encountered by the aerial vehicle. At least one of the propellers may be statically or dynamically imbalanced, such that the propeller emits a predetermined sound during operation. A balanced propeller may be specifically modified to cause the aerial vehicle to emit the predetermined sound by changing one or more parameters of the balanced propeller and causing the balanced propeller to be statically or dynamically imbalanced. | 2021-10-07 |
20210309347 | PROPELLER STRUCTURE IN THE FORM OF TWIN MOBIUS BLADES FOR AIRCRAFT - A propeller structure in the form of twin Mobius blades for an aircraft is provided in which it is possible to easily control flight speed and posture by free movement and interlocking movement through supersymmetrical twisting, it is possible to selectively individually control the left and right propeller blades by rotating and operating the left and right propeller blades of an aircraft body in a spur gear scheme through one drive shaft connected by first to third motors and fourth to sixth motors, respectively, it is possible to enhance the propulsion and control each blade by forming a propeller with a structure a plurality of pairs of blades on both sides of the aircraft body, and it is easy to control the direction by rotating and operating the blades by a tilting scheme of a toothed gear through a drive shaft connected to a tail blade of the aircraft body by a seventh motor. | 2021-10-07 |
20210309348 | INERTERS WITH FRICTION DISK ASSEMBLIES, AND AIRCRAFT HYDRAULIC SYSTEMS AND AIRCRAFT INCLUDING THE SAME - Inerters with friction disk assemblies, and aircraft hydraulic systems and aircraft including the same. An inerter comprises an inerter housing containing an inerter fluid, a threaded shaft extending within the inerter housing and fixed relative to the first terminal, and an inerter rod extending at least partially within the inerter housing and fixed relative to the second terminal. The inerter further includes a friction disk assembly that, together with the inerter fluid, is configured to damp a motion of the second terminal relative to the first terminal. The friction disk assembly includes a fixed portion and a rotating portion, and is configured such that rotation of the rotating portion generates a frictional torque that opposes the rotation of the rotating portion. In some examples, the inerter is a component of a hydraulic actuator, an aircraft hydraulic system including the hydraulic actuator, and/or an aircraft including the aircraft hydraulic system. | 2021-10-07 |
20210309349 | SENSOR FOR MONITORING ROTORS - A sensor for monitoring rotors includes a rotating shaft coupled to a set of rotor blades and a non-rotating tube at least partially disposed within the rotating shaft and coupled to the rotating shaft. The non-rotating tube includes a first end and a second end, a sensor mount disposed within the non-rotating tube proximate to the second end of the non-rotating tube. One or more sensors are attached to the sensor mount. | 2021-10-07 |
20210309350 | Rotor Units Having Asymmetric Rotor Blades - An aerial vehicle is provided including rotor units connected to the aerial vehicle, and a control system configured to operate at least one of the rotor units. The rotor unit includes rotor blades, wherein each rotor blade includes a surface area, and wherein an asymmetric parameter is defined, at least in part, by the relationship between the surface areas of the rotor blades. The value of the asymmetric parameter is selected such that the operation of the rotor unit: (i) moves the rotor blades such that each rotor blade produces a respective vortex and (ii) the respective vortices cause the rotor unit to produce a sound output having an energy distribution defined, at least in part, by a set of frequencies, wherein the set of frequencies includes a fundamental frequency, one or more harmonic frequencies, and one or more non-harmonic frequencies having a respective strength greater than a threshold strength. | 2021-10-07 |
20210309351 | AIRCRAFT HAVING HYBRID PROPULSION - Aircraft having hybrid propulsion are disclosed. A disclosed example propulsion system for an aircraft. The propulsion system includes an engine, an electric motor, a first propeller mounted to an aerodynamic body of the aircraft, the first propeller driven by the engine, a second propeller mounted to the aerodynamic body and positioned outboard relative to the first propeller, the second propeller driven by the electric motor, and a selector to control whether the propulsion system is operated in a hybrid mode in which the first and second propellers are driven. | 2021-10-07 |
20210309352 | SYSTEMS AND METHODS FOR GENERATING EARTHMOVING PRESCRIPTIONS - A system for generating earthmoving prescriptions may include an unmanned aerial vehicle (UAV) to be flown across a worksite, at least one sensor supported on the UAV that generates data indicative of a surface profile of a surface of the worksite and data indicative of a plurality of soil layers below the surface of the worksite, and a computing system communicatively coupled to the at least one sensor. The computing system may receive the data indicative of the surface profile of the worksite and the data indicative of the plurality of soil layers of the worksite. The computing system may further receive an input associated with a target profile of the worksite. Additionally, the computing system may generate an earthmoving prescription map that maps the plurality of soil layers between the surface and target profiles of the worksite. | 2021-10-07 |
20210309353 | MODULAR UNMANNED AERIAL VEHICLE SYSETM FOR ADAPTABLE PARCEL DELIVERY - A modular unmanned aerial vehicle (UAV) system comprises a body module, a rotor module, and a wing module. The body module includes a flight controller and a power distribution device. The body module is releasably attachable to the rotor module or the wing module, and the body module is releasably attachable to the rotor module. The rotor module includes one or more motors and electronic speed controllers (ESCs), while the wing module includes a wing having a flap, elevator, aileron, or rudder. Various UAV configurations can be formed from the body module, the rotor module, and the wing module. Each configuration includes different advantages for flight time, distance, battery life, and payload capacity. A UAV can be configured to a particular configuration to optimize parcel delivery. | 2021-10-07 |
20210309354 | SYSTEM AND METHOD FOR PACKAGE TRANSPORTATION - The invention(s) include embodiments and applications of: a system for package handling, the system including: a flying vehicle comprising a nose portion; a storage region of the flying vehicle; a landing support subsystem coupled to the flying vehicle; one or more thrust generating devices coupled to the flying vehicle | 2021-10-07 |
20210309355 | QUICK DISASSEMBLING STRUCTURE AND UNMANNED AERIAL VEHICLE - A disassembling structure includes a first connecting piece, a second connecting piece and a guide and positioning piece; the guide and positioning piece is fixedly arranged on the first module; the second connecting piece is fixedly arranged on the second module; the second connecting piece and the guide and positioning piece are opposite to each other; the guide and positioning piece is attached to the outer side of the second connecting piece in a covering manner to guide and position the first module and the second module; the first connecting piece is detachably connected to the second connecting piece after passing through the guide and positioning piece. | 2021-10-07 |
20210309356 | ENERGY-LOAD ASSEMBLY AND UNMANNED AERIAL VEHICLE - An energy-load assembly includes an accommodating box, a power source, a load and an undercarriage. The accommodating box can be connected to a body of an unmanned aerial vehicle; the power source is arranged in the accommodating box, and can provide electric energy to the unmanned aerial vehicle; the load is arranged at the bottom of the accommodating box; and the undercarriage is connected to the accommodating box. The energy-load assembly provided integrates the power source, the load and the undercarriage. The corresponding power source and the load can be integrated according to different tasks performed. | 2021-10-07 |
20210309357 | FLYING VEHICLE SYSTEMS AND METHODS - An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a power supply mounted to the chassis, a control system operable to receive power from the power supply, at least one rotor operable to generate lift under control of the control system, and a winch mounted to the chassis. The winch includes a reel and a motor. The reel has a line wound thereon, the line having a free end. The reel includes a circumferential channel in which a wound portion of the line is wound onto the reel. The circumferential channel includes an inner portion, an outer portion, and a passage connecting the inner portion and the outer portion. The motor is operable to rotate the reel under control of the control system to thereby cause the line to wind onto and off of the reel, thereby causing the free end of the line to raise and lower. | 2021-10-07 |
20210309358 | FLYING VEHICLE SYSTEMS AND METHODS - An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a control system, and at least one rotor. The chassis includes a first battery compartment configured to receive sliding insertion of a first battery, and a second battery compartment configured to receive sliding insertion of a second battery. The control system is operable to receive power from the first battery and the second battery when the first battery is received in the first battery compartment and the second battery is received in the second battery compartment. The at least one rotor is operable to generate lift under control of the control system when both the first battery and the second battery are installed to the chassis. The control system is configured to remain at least partially active under power supplied by the first battery when the second battery is removed from the second battery compartment. | 2021-10-07 |
20210309359 | FLYING VEHICLE SYSTEMS AND METHODS - A method according to certain embodiments generally involves operating a system including an unmanned aerial vehicle (UAV) and a base station. The base station includes a nest including an upper opening having an upper opening diameter and a lower opening having a lower opening diameter less than the upper opening diameter. The lower opening is accessible from within the base station. The method generally includes landing the UAV within the nest such that a portion of the UAV is accessible via the lower opening, releasably attaching a load to the UAV, and operating the UAV to deliver the load to a destination. | 2021-10-07 |
20210309360 | APPARATUS FOR AERIAL TRANSPORTATION OF PAYLOAD - Disclosed is an apparatus ( | 2021-10-07 |
20210309361 | Apparatus, Systems and Methodologies Configured to Enable Electrical Output Management of Solar Energy Infrastructure, Including Management via Remotely Operated Coating Application System and/or Wireless Monitoring Systems - Apparatus, systems and methods for dispensing a coating material onto a solar power infrastructure unit ( | 2021-10-07 |
20210309362 | REDUCTION OF THE VISUAL & AUDIBLE SIGNATURES OF THE UAV TO MINIMISE DETECTION DURING LONG DURATION SURVEILLANCE OPERATIONS - The invention comprises of a UAV designed to limit visually contrast and audibility in flight for covert surveillance operations, a method of configuring the UAVs structure to further reduce its visual signature to take account for the atmospheric and terrestrial environment it will operate in and a method of conducting a covert surveillance operation to actively minimise the UAVs visual & auditory signature from the viewpoint of an individual under surveillance. Both passive and active illumination are used to reduce the visual signature of the UAV. The UAV is actively camouflaged using lighting techniques that utilises the limitations of the human visual system and the optical effects of light interacting with the terrain, atmosphere and aircraft. The visual camouflage is directional. The audible signature of the UAV is reduced through the design of the propulsion system and the mode in which the UAV is operated. | 2021-10-07 |
20210309363 | PARCEL TRANSPORT SYSTEM AND INSTALLING METHOD THEREOF - A parcel transport system is provided, which comprises an interface assembly, a storage assembly and a transport assembly. A storage box of the storage assembly is provided with a first access opening and a second access opening, the storage box is movable to enable the first access opening to be exposed and to be blocked; the interface assembly is used for a parcel transfer to or from an external equipment; and wherein the transport assembly is capable of reaching into the storage box via the second access opening, and carrying out the parcel transfer to/from the external equipment or the interface assembly at the interface assembly, enabling the transport assembly to deliver the parcel between the interface assembly and the storage box. | 2021-10-07 |
20210309364 | AUTOMATIC RETURN METHOD, APPRATUS AND UNMANNED AERIAL VEHICLE - Embodiments of the present invention relate to the technical field of unmanned aerial vehicles (UAV), and specifically discloses an automatic return method, device and UAV. By means of the foregoing technical solutions, the embodiments of the present invention can estimate a minimum power consumption required for the UAV to return from the current position to the return point in a more accurate way, so as to avoid forced landing of the UAV due to an excessively low battery level during a flight or a return. | 2021-10-07 |
20210309365 | SYSTEM FOR INTERNAL PAYLOAD EXTENSION AND RETRACTION WITH LOCKING MECHANISM - A system is described and includes at least one track attached to an upper interior surface of a payload bay and extending along a bottom surface of a vehicle structure external to the payload bay, wherein the track comprises a horizontal flange; a rack moveably connected to the at least one track via at least one carrier assembly; and a payload actuator system for selectively extending the rack from the payload bay along the at least one track to a position from which payload carried by the rack may be safely deployed and retracting the rack into the payload bay along the at least one track. | 2021-10-07 |
20210309366 | FLYING VEHICLE SYSTEMS AND METHODS - An example carriage is configured for mounting to an unmanned aerial vehicle. The carriage generally includes a housing assembly configured for mounting to the unmanned aerial vehicle, a movable grip mounted to the housing assembly for movement between a capturing position and a releasing position, a latch device, and a driver. The latch device has a latching state and an unlatching state, is configured to retain the movable grip in the capturing position when the latch device is in the latching state, and is configured to permit movement of the movable grip from the capturing position to the releasing position when in the unlatching state. The driver is operable to transition the latch device from the latching state to the unlatching state. | 2021-10-07 |
20210309367 | MECHANICAL PACKAGE RELEASE SYSTEM - A package release system for delivering packages using radio controlled or autonomous vehicle like a drone. The package is carried at a first angle then released when the package changes angles such as when set on the ground. | 2021-10-07 |
20210309368 | HIGH-ALTITUDE JETTISONING AIMING METHOD AND SYSTEM APPLIED TO UNMANNED AERIAL VEHICLE AND STORAGE MEDIUM - A high-altitude jettisoning aiming method and system applied to an unmanned aerial vehicle and a storage medium, the method includes collecting a current inclination angle and height information of the unmanned aerial vehicle when the unmanned aerial vehicle is hovering at a fixed point over a target position; calculating a current wind speed and wind direction according to the inclination angle; estimating an offset between an actual jettisoning position of a jettisoned object and the target position according to the wind speed, the wind direction and the height, the offset including an offset orientation and an offset distance; and controlling, according to the offset, the unmanned aerial vehicle to adjust the hovering position such that the actual jettisoning position of the carried object overlaps the target position after the adjustment. | 2021-10-07 |
20210309369 | Method and Apparatus Used for Biological Control of Agricultural Pests - An apparatus for biological control of agricultural pests and for reducing damage to crops. The apparatus includes a container for holding biological organisms or material. The container also includes first and second ends and an opening formed at the first end for receiving the biological organisms. The apparatus has a dispensing port disposed at the second end for dispensing the biological organisms over a target location. The apparatus further includes an auger, driven by a motor and having a plurality of spiral like wire brushes, said auger mounted to and driven by a first motor; a spreader motor mount having a motor mount holding area for holding a second motor, the spreader motor mount having a motor mount connection area for connecting to the second end; and a spreader agitating device used for spreading the biological organisms or material over the target location. | 2021-10-07 |
20210309370 | CARGO DOORS FOR PAYLOAD BAY HAVING INTERNAL PAYLOAD EXTENSION AND RETRACTION MECHANISM - A system is described and includes a rack for carrying payload disposed in payload bay; a rack extension assembly for affecting linear displacement of the rack between a first position in which the rack is stowed within the payload bay and a second position in which the rack is supported outside the payload bay; a payload actuator system for selectively causing the rack extension assembly to move the rack between the first and second positions; a payload bay door; and a door actuator system for selectively opening and closing the payload bay door. | 2021-10-07 |
20210309371 | SYSTEM FOR INTERNAL PAYLOAD EXTENSION AND RETRACTION USING TELESCOPING MECHANISM - A system is described and includes a rack for carrying payload disposed in a payload bay; and a payload extension assembly for affecting linear translation of the rack between a first position in which the rack is fully retracted within the payload bay and a second position in which the payload extension assembly is fully extended and the rack is supported outside the payload bay. The payload extension assembly comprises forward and aft tracks respectively attached to forward and aft walls of the payload bay; a first stage for providing linear translation of the rack relative to the forward and aft tracks; and a second stage for providing linear translation of the rack relative to the first stage. The system further comprises a payload actuator system for selectively causing the rack extension assembly to move the rack between the first and second positions. | 2021-10-07 |
20210309372 | TURBINE HOUSING FOR A TWO WHEEL AIR CYCLE MACHINE - A turbine housing for a two-wheel air cycle machine includes a first side of the turbine housing, a second side of the turbine housing, a central axis, an outer housing portion, an inner housing portion, a plurality of struts between the inner housing portion and the outer housing portion and a plurality of cooling slots between the plurality of supports. The outer housing portion includes an inner surface, an outer surface, a cooling inlet extending from the outer surface of the outer housing portion and a cooling outlet opposite the cooling inlet and extending from the outer surface of the outer housing portion. The inner housing portion includes a thrust bearing support surface substantially parallel to the second side of the turbine housing and a journal bearing bore extending between the first side of the turbine housing and the thrust bearing support surface. | 2021-10-07 |
20210309373 | PERSONAL HEATING VENTILATION AND AIR CONDITIONING SYSTEM IN AIRCRAFT SEAT - A personal heating ventilation and air conditioning system (HVAC) for an aircraft seat includes at least one aircraft seat, a heating/cooling device disposed on the at least one aircraft seat and at least one branch configured to provide at least one flow path from the heating/cooling device. The system also includes at least one sub-branch provided within the at least one aircraft seat. The at least one sub-branch is configured to provide flow from the at least one branch through the at least one aircraft seat. The system also includes means for expelling air from the at least one sub-branch to an interior surface of the at least one aircraft seat. | 2021-10-07 |
20210309374 | AIRCRAFT ANTI-ICING SYSTEM - An aircraft anti-icing system is disclosed. A tube having a plurality of outlet ports is disposed within an interior of an outer housing in spaced relation to a closed end of this outer housing. The exterior of the outer housing includes a leading edge at its closed end. The tube is anchored relative to the outer housing by one or more brackets that extend from the tube to the outer housing. An open end of the outer housing may be closed by an aft wall that encloses the tube within an interior compartment of the outer housing. | 2021-10-07 |
20210309375 | CONTINUOUS STACKED DUAL WRAP TUBE END CLOSURE FOR ANTI-ICING SYSTEMS - An anti-icing system may comprise a deicing boot of an elastomeric material comprising a plurality of tubes, wherein the deicing boot comprises a first set of tubes and a second set of tubes, wherein each of the first set of tubes and the second set of tubes have a corresponding end, and wherein the corresponding end is coupled to a continuous dual wrap end closure. | 2021-10-07 |
20210309376 | INTEGRATED BUSBAR HEATER FOR ICE PROTECTION SYSTEMS - An ice protection system may comprise an electrical heating mat of an electrically resistive material, wherein the electrically resistive material defines at a first spanwise zone and a first chordwise zone, wherein at least one of the first spanwise zone or the first chordwise zone include a first busbar portion contiguous with the electrically resistive material. | 2021-10-07 |
20210309377 | ENERGY ABSORBING DEVICE ADAPTED FOR A MILD IMPACT OF AN AIRCRAFT, UAV, EQUIPPED WITH A PARACHUTE - An energy absorbing device provided at the parachute riser strap of an aircraft, UAV, etc., adapted to reduce the otherwise high forces resulting from the weight of the aircraft, the speed of descent and, ultimately, the speed of impact, activated by the pilot or by means of the photoelectric cell attached underneath the aircraft measuring the distance from the ground. | 2021-10-07 |
20210309378 | LUMBAR SUPPORT SYSTEMS FOR EJECTION SEAT - A lumbar support system for use in an ejection seat of an aircraft, comprising may comprise a pump; a plurality of bladders fluidly coupled to the pump; and a controller electrically coupled to the pump, the controller operable to: select a bladder in the plurality of bladders to fluidly isolate the bladder from a remainder of bladders in the plurality of bladders; and command the pump to inflate the bladder. | 2021-10-07 |
20210309379 | SEAT CUSHION LENGTH ADJUSTER FOR EJECTION SEAT - A cushion length adjusting system for use in an ejection seat of an aircraft may comprise a seat pan and first cushion length adjuster coupled to the seat pan. The cushion length adjuster may be hingedly or slidingly coupled to the seat pan. The cushion length adjuster may be configured to adjust a leg support length for greater ergonomics for a pilot of an aircraft. | 2021-10-07 |
20210309380 | LATERAL SUPPORT SYSTEM FOR EJECTION SEAT - A lateral support system for use in an ejection seat of an aircraft may comprise a pump; a first side bladder fluidly coupled to the pump; a second side bladder fluidly coupled to the pump, the second side bladder configured to be disposed opposite the first side bladder. The first side bladder and the second side bladder may be coupled to a seat pan pad or a seat back pad. The lateral support system may further include a third side bladder and a fourth side bladder coupled to a seat pan pad, and the first side bladder and the second side bladder may be coupled to a seat back pad. | 2021-10-07 |
20210309381 | HYBRID TILTROTOR DRIVE SYSTEM - An exemplary tiltrotor aircraft with a hybrid drive system includes a first propulsion system having a first engine and a first supplemental driver operably coupled to a first proprotor that is operable between a helicopter mode and an airplane mode and a second propulsion system having a second engine and a second supplemental driver operably coupled to a second proprotor that is operable between a helicopter mode and an airplane mode. | 2021-10-07 |
20210309382 | SMART COMBUSTION ENGINE - Systems, devices, and methods are provided for a power delivery and drive system. A power delivery system can include an engine governing unit configured to deliver electrical power to a first electrical component. The power delivery system can include a smart engine electrically connected to the engine governing unit, the smart engine configured to deliver electrical power to the engine governing unit. The system can include a smart fuel tank operably connected to the smart engine and engine governing unit. And the system can include a battery operably connected to the engine governing unit, the smart battery configured to deliver electrical power to the engine governing unit. | 2021-10-07 |
20210309383 | SYSTEMS AND METHODS FOR MAINTAINING ATTITUDE CONTROL UNDER DEGRADED ENERGY SOURCE CONDITIONS USING MULTIPLE PROPULSORS - A system for maintaining attitude control under degraded or depleted energy source conditions using multiple electric propulsors includes a plurality of propulsors, at least an energy source providing electric power to the plurality of propulsors and a vehicle controller communicatively coupled to each propulsor and configured to calculate initial power levels for the plurality of propulsors, the initial power levels including an initial power level for each propulsor, determine an energy output capacity of the least an energy source under load, calculate, by the vehicle controller, an aggregate potential demand of the plurality of propulsors as a function of the initial power levels, determine that electric potential is insufficient to match the aggregate potential demand, and for each initial power level generate a reduced power level, the reduced power level less than the initial power level and direct a corresponding propulsor to consume electrical power at the reduced power level. | 2021-10-07 |
20210309384 | USAGE BASED PROPELLER LIFE MONITORING - A system for monitoring propeller health includes a processing unit having a processor which is programmed to apply a plurality of algorithms to inputted aircraft parameter data. The system also includes a plurality of data inputs for inputting aircraft parameter data into the algorithms, wherein the processor is configured to apply the physics based algorithms to the aircraft parameter data to determine at least the fatigue life consumption of one or more critical components of a propeller. In addition, the system includes an output device which is able to output an indication of the determined fatigue life consumption to an observer. | 2021-10-07 |
20210309385 | METHOD AND A DEVICE FOR MANAGING RISKS AND ALERTS - A method of managing risks and alerts for a system. The system includes source modules and auxiliary modules for identifying actual or potential risks of failures or of malfunctions of the system. A central module of the system serves to determine actual or potential risks of failures or of malfunctions of the system and actual or potential risks associated with parameters external to the system and that might have impacts on operation of the system. Then, an overall risk level is determined by combining the various actual or potential risks and their effects on the system, and then an action and information interface may be controlled as a function of the overall risk level, e.g. for modifying a display of information relating to the system and/or to its environment, or indeed for automatically performing an action on the system. | 2021-10-07 |
20210309386 | SPECTRA FILL - A system for providing full spectrum light in an enclosed space. The system includes a first light source based on a red-green-blue (RGB) model, located in the enclosed space, and configured to generate a first light. The system further includes a second light source separate from the first light source, based on an alternative to the RGB model, located in the enclosed space, and configured to generate a second light such that a combination of the first light and the second light has a greater color rendering index (CRI) than the first light alone. | 2021-10-07 |
20210309387 | ELECTRONIC SYSTEM FOR CONTROLLING THE DOCKING OF A VEHICLE WITH A DOCKING AREA, AND CORRESPONDING METHOD - An electronic system and method controls automatic or semi-automatic docking of a vehicle with a given docking area, applicable, in particular, to the docking of an airport vehicle, such as a baggage belt loader, a catering vehicle, etc., to the fuselage of an aircraft, for example to the door of such an aircraft. The given docking area comprises at least one target. The system includes first determination device configured to determine the position of the docking area by determining the type of target from a set of given types and its position, second determination device configured to determine a guide path for guiding the vehicle towards the given docking area depending on the position of the docking area, and third determination device configured to determine the type of docking destination, the second determination device being capable of determining one or more exclusion areas depending on the type of docking destination, by comparing the type of docking destination with types of docking destination, stored in a database in association with exclusion areas, such that the guide path for guiding the vehicle towards the given docking area does not pass into any of the exclusion areas. | 2021-10-07 |
20210309388 | FLYING VEHICLE SYSTEMS AND METHODS - An example charging station for an unmanned aerial vehicle (UAV), the charging station generally including a nest and a charging device. The nest includes an upper portion and a lower portion. The upper portion defines an upper opening sized and shaped to receive a landing apparatus of the UAV, and a diameter of the nest reduces from a first diameter at the upper opening to a second diameter at the lower portion. The charging device is mounted in the nest, and includes a first contact pad and a second contact pad. The charging device is configured to apply a voltage differential across the first contact pad and the second contact pad such that the charging station is operable to charge a power supply of the UAV via the landing apparatus. | 2021-10-07 |
20210309389 | SYSTEMS AND METHOD FOR AUTOMATED SERVICING OF SHOCK STRUTS - A system for servicing a shock strut may comprise a system controller and a tangible, non-transitory memory configured to communicate with the system controller. The tangible, non-transitory memory may have instructions stored thereon that, in response to execution by the system controller, cause the system controller to perform operations, which may comprise: receiving, by the system controller, a hydraulic fluid volume difference or a pressurized gas volume difference from a ground support controller; determining, by the system controller, a desired fluid flow rate based on the hydraulic fluid volume difference or the pressurized gas volume difference; and outputting, by the system controller, a desired fluid flow rate signal corresponding to the desired fluid flow rate to at least one of a hydraulic fluid flow controller or a pressurized gas flow controller. | 2021-10-07 |
20210309390 | METHOD AND APPARATUS FOR LOCATING AND FORMING FASTENER HOLES IN A REPLACEMENT TIP SECTION OF A ROTOR BLADE - A system for regenerating fastener holes in a replacement tip section of a rotor blade includes a first fixture, a second fixture, and a third fixture positionable adjacent a tip section of the rotor blade. The first fixture is used to verify a position of an opening formed in the spar. The second fixture includes a removable bushing having a drillable opening. The drillable opening is aligned with the at least one opening formed in the spar and defines at least one hole to be formed in the replacement tip section. The third fixture includes a countersink opening. The countersink opening is aligned with the at least one hole to be formed in the replacement tip section and the at least one opening formed in the spar to define a countersink feature to be formed in the at least one hole. | 2021-10-07 |
20210309391 | Arm Removal System - An arm removal system for removing an arm. The system includes an anvil, and a removal assembly with at least two jackscrews. The arm has an extension radially extending from the arm and an arm outer surface. The arm is disposed within a wedge shaped collet that is disposed within a socket in an aircraft with an aircraft outer surface. The removal assembly includes an extension engaging surface and threaded jackscrew holes for accepting the jackscrews, such that when the jackscrews are tightened within the jackscrew holes, the jackscrews apply force on the anvil and the aircraft outer surface in the direction away from the removal assembly such that the arm is eventually removed entirely from the aircraft. | 2021-10-07 |
20210309392 | SYSTEMS AND METHODS FOR IN-FLIGHT OPERATIONAL ASSESSMENT - A method of in-flight operational assessment for an electric aircraft comprising detecting by a sensor an electrical parameter of an energy source. The method further includes receiving by a controller the electrical parameter from the sensor and determining a power-production capability of the energy source, using the electrical parameter. The method further includes calculating, by the controller, a projected power-consumption need of the electric aircraft and comparing the determined power-production capability of the energy source to the projected power-consumption need. The method includes generating a power production command datum as a function of the comparison of the power-production capability and the projected power-consumption need. | 2021-10-07 |
20210309393 | SATELLITE DEPLOYER DOOR WITH CLUTCH BEARING - A satellite dispenser door assembly is disclosed. In various embodiments, a satellite dispenser door assembly as disclosed herein includes a dispenser door having a hinge pin; and a one way clutch bearing within which the hinge pin is free to rotate in a first rotational direction associated with a transition from a closed position of the dispenser door to an open position of the dispenser door. | 2021-10-07 |
20210309394 | ANTI-GRAVITY DRIVE - An apparatus comprised of positionally directable masses attached to a binding component that includes a coupling device for payload to reduce gravitational deviation of the apparatus' trajectory by alternatingly accelerating and retracting physically bound component masses in equal and opposite directions to the extents of their bindings, initially and optimally perpendicular to the gravitational field and perpendicular to the apparatus trajectory by using in built transduction componentry located within the masses or the binding componentry or both that utilises electromagnetic forces, forces generated by chemical reactions, or other applied or responsive motive force to positionally direct the bound directable masses. | 2021-10-07 |
20210309395 | A PROPULSION SYSTEM - A propulsion system for a spacecraft includes at least one chemical propulsion engine, at least one electrical propulsion engine, and a propellant feed system that includes a propellant supply system including at least one tank to store a common propellant. The propellant supply system is configured to deliver a controlled flow of the common propellant to both the chemical propulsion engine and the electrical propulsion engine. Also disclosed is the use of a common propellant in a spacecraft and a method of providing a common propellant to an electrical and a chemical propulsion engine. | 2021-10-07 |
20210309396 | A PROPULSION SYSTEM - A propulsion system for a spacecraft includes at least one electrical propulsion engine comprising at least one neutraliser; and a pressurant gas system comprising a pressurant gas which is fed directly into the at least one neutraliser. | 2021-10-07 |
20210309397 | SYSTEM FOR SATELLITE DOCKING FOR EXTENSION OF ITS USEFUL LIFE, OR FOR ORBIT MODIFICATION, INDLUCING SATELLITE DE-ORBITING AND ASSOCIATED CONTROL METHOD FOR SATELLITE DOCKING - A service satellite having a body, a controller and a docking unit including a telescopic arm, mounted on a 6-DOF parallel manipulator, and two additional gripping arms. The telescopic arm, deployed from the 6-DOF manipulator, is equipped with a pair of rapid closure digits. The telescopic arm facilitates capturing the launch adaptor ring of a client spacecraft, even during tumbling. The 6-DOF parallel manipulator has force sensors and can accommodate post capturing relative motion through active compliance control and controlled de-tumbling, for avoiding generation of high forces in the telescopic arm. After relative rate annihilation, the telescopic arm retracts and the client ring is secured to the 6-DOF manipulator with the help of a pair of clamps. After the ring is secured, two additional gripping arms secure a rigid connection with the launcher ring so that the docking connection comprises three equally spaced connections. | 2021-10-07 |
20210309398 | Method And System For Producing Sterile Solution Product Bags - A method for producing sterile solution product bags includes positioning a manifold assembly onto a filling machine. The manifold assembly includes a plurality of bags, a first filter, and a connection line in fluid communication with the first filter. Each of the plurality of bags includes a bladder and a stem in fluid communication with the bladder and with the connection line. The method includes activating a pump and at least partially filling one or more of the bladders by pumping fluid through the feed line, the first filter, and the connection line. The method includes sealing the stem of each of the filled product bags at a location between the connection line and the bladder, thereby creating one or more at least partially filled and sealed product bags. The method includes separating each of the at least partially filled and sealed product bags from the connection line. | 2021-10-07 |
20210309399 | PROCESS AND APPARATUS FOR LINE PRODUCTION OF PLANT GROWTH MEDIUM POTS OR BAGS - A process for line production of plant growth medium pots or bags with a closed bottom end includes the steps of: i) continuously folding the free end of a continuous length of water and air permeable sheet material into a sheet material tube around and beyond a free end of a growth medium feeding tube; ii) forming a first sealing in the sheet material tube; iii) filling the sheet material tube with a measured amount of growth medium; iv) forming a second sealing in the sheet material tube; v) separating the part of the sheet material tube positioned downstream from the second sealing to form a first plant growth medium pot or bag with a closed end, repeating as needed to form a plurality of plant growth medium pots or bags. | 2021-10-07 |
20210309400 | PACKING TOOL CAPABLE OF DISPLAYING TENSION - A packing tool capable of displaying tension includes a body and a control device. The body includes a strap winding device. A handle and a ratchet gear are fitted on the strap winding device. The ratchet gear abuts against a first abutting member. The control device is connected to the handle and includes a processing unit. The processing unit is electrically connected to a detection unit and a display unit. The detection unit is used to detect the amount of deformation of the first abutting member and then calculate and output a tension value to the display unit, so that the user can pay attention to the tension value applied to a packing strap by the packing tool at any time, so as to achieve the purpose of fast packing. | 2021-10-07 |
20210309401 | FILM DISPENSER FOR A WRAPPING APPARATUS AND RELATED METHODS - There is provided a film dispenser including a pre-stretch assembly, a dancer bar and a dancer bar control assembly. In response to a variation of a film feed requirement, the dancer bar is movable over a displacement range between a first position and at least one second position. The dancer bar is in the first position when a tension in the material web is below a threshold and in the at least one second position when the tension in the material web is equal to or above the threshold. The dancer bar control assembly is connected to the pre-stretch assembly and the dancer bar and is configured to bias the dancer bar with a constant force over the displacement range, monitor a displacement of the dancer bar and generate a speed command based thereon, and send the speed command to a motor to adjust the film delivery speed. | 2021-10-07 |
20210309402 | SIZE REDUCTION OF MAILERS - A system includes a forming funnel, a cutting element, and a fusing device. The forming funnel has divergent surfaces arranged to receive a mailer in an insertion direction between the divergent surfaces. The forming funnel includes a slot that constrains the mailer after the mailer is inserted between the divergent surfaces. The cutting element cuts off a portion of the mailer and to forms a cut end of the mailer as the mailer is moved through the slot in a sliding direction. The fusing device applies pressure to an exterior of the cut end of the mailer and applies heat to the cut end of the mailer as the mailer is moved through the slot. The pressure and the heat applied by the fusing device cause portions of the cut end to fuse together to close the mailer. | 2021-10-07 |
20210309403 | Method of Performing a Task in Registration With a Seal In Materials and Flexible Containers Made By Method - A method for performing a task in registration with a discrete seal in at least one material is described herein. The method involves simultaneously forming a discrete seal and a fiducial/eye mark in the at least one material. The method includes providing a detection device; providing a unit operation mechanism; and performing an operation on the material(s) in registration with the discrete seal. The task performed in registration with the discrete seal is based upon the location of the eye mark that was simultaneously formed with the discrete seal. A method of making flexible containers using cutting to form the outer periphery of the packages is described herein. Also described herein are flexible containers and container blanks made by such a method. | 2021-10-07 |
20210309404 | BAG EMPTIER DEVICE - The invention relates to a device for processing dust- and substantially air-tight sacks ( | 2021-10-07 |
20210309405 | SAFETY LIFTING DEVICE - A safety lifting device for positioning a labelling unit in a vertical direction (Z) in relation to a flow of objects where the labelling unit is arranged for printing labels and/or applying labels to the objects. The lifting device includes a linear actuator, a balancing unit, a drive unit connected to the linear actuator, and a movable section. The labelling unit is connected to the movable section. The linear actuator is connected to the movable section and arranged to control the position of the labelling unit. The balancing unit is arranged to counterbalance the gravitational force exerted on the linear actuator. The movable section of the lifting device includes an upper stand unit, and the lifting device further includes a lower stand unit. The upper stand unit is movably arranged in relation to the lower stand unit in the vertical direction. | 2021-10-07 |
20210309406 | Label Wrapper With Soft-Touch Jaws - Systems and methods include a label wrapper assembly that can retain elongate objects while adhering a label thereto. The assembly can include a wrapping subassembly with a wrapping subassembly axis that can be configured to apply a label to an elongate object by rotating around the elongate object about the wrapping subassembly axis. A set of clamp assemblies can be axially spaced apart along the wrapping subassembly axis on both sides of the wrapping subassembly. Each of the clamp assemblies can have a set of clamp members slidably movable relative to each other between an open position and a clamping position, and the clamp members can provide a clamping force in the clamping position. Each of the clamp members can have a retention element to retain the elongate object therebetween when in the clamping position, and the retention elements can be elastomeric. | 2021-10-07 |
20210309407 | Systems and Methods for a Label Wrapper - Systems and methods include an assembly for a label wrapper to adhere a label to an elongated object, such as a wire. The assembly can include a roller having a roller axis and a compliant block with a notch. The notch can be parallel with the roller axis. The compliant block and the roller can be biased toward each other, and when the elongate object is received between the roller and the compliant block, a pressure can be applied to the elongate object whereby the compliant block at least in part conforms to the elongate object. | 2021-10-07 |
20210309408 | CONTAINER FOR LIQUIDS - A container for liquids that allows the contents to be emptied out quickly without spattering or gurgling. A sealed closure within the neck of the container can be opened by pulling a ring on the bottom of the container to open both an air inlet in the bottom of the container and the closure in the neck of the container. A connecting rod within the container opens the closure in the neck of the container in response to opening of the air inlet closure at the bottom of the container, to allow the contents of the container to flow out through the neck, while air enters into the container through the opening at the bottom of the container. | 2021-10-07 |
20210309409 | Foldable box connection structure, foldable box and method of using the same - The invention provides a foldable box connection structure, a foldable box and a method of using the same. The foldable box connection structure comprises a first side plate, a second side plate, a first hinge, a first top plate, a seam cover plate and a positioning plate. The first hinge is used to connect the first top plate and the second side plate. The seam cover plate can be folded to cover the first hinge, and the seam cover plate and the positioning plate are configured to secure the first hinge. The foldable box includes the above-mentioned connection structure. In the present invention, the first top plate is hooked by the first hinge and the seam cover plate, and a second top plate is hooked by a third hinge, so that the foldable box has a fixed structure. That is, in an expanded configuration, the first top plate and the second top plate are tightly attached to a top of the second side plate to prevent forming gaps between the first top plate and the second side plate, and between the second top plate and the second side plate, which greatly increases the compactness of the box and makes the box have simple and beautiful contour. | 2021-10-07 |
20210309410 | CONTAINERS FOR TRANSPORTING ITEMS AND METHODS OF ARRANGING SUCH CONTAINERS - Containers for storing and transporting items such as but not limited to traditional disposable aluminum pans, and methods of arranging such containers. A first container includes a base panel, four side panels coupled to the base panel, two cover panels pivotally coupled to two of the side panels, and two top panels pivotally coupled to the other two side panels. A second container includes a base panel, four side panels coupled to the base panel, two cover panels pivotally coupled to two of the side panels, a top panel pivotally coupled to another of the side panels, a front panel pivotally coupled to the top panel, and a separation panel pivotally coupled to the last of the side panels. The containers are configured to be arranged in assembled configurations that define enclosed compartments suitable for storing items. | 2021-10-07 |
20210309411 | Shippers with a Constant Depth - A container includes a blank having a plurality of panels foldably connected to one another and erected about an interior space, and a plurality of top flaps foldably connected to the plurality of panels to enclose a top end of the interior space, and a plurality of bottom flaps wherein each of the bottom flaps is foldably connected to a corresponding panel of plurality of panels to enclose a bottom end of the interior space. The blank includes a line of weakness pattern configured to allow a user to break the top flaps from a closed configuration enclosing the interior space to an open configuration allowing access to the interior space. | 2021-10-07 |
20210309412 | SHELF-READY PACKAGING AND METHODS FOR TRANSPORTING AND DISPLAYING FOOD PRODUCTS - A shelf-ready packaging (SRP) and method for transporting and displaying food products are provided, the SRP configured to be efficient in transporting a high number of the food products while also still being able to fit on a retail store shelf. To this end, the SRP includes a cover element and a base tray including first and second tray portions connected along a single tear line. To convert the SRP from a first transport configuration to a second display configuration, the cover element is lifted off the base tray and the first and second tray portions are separated along the tear line, which thereby changes the overall length of the SRP such that it can fit on the standard retail store shelf. The SRP provides a clean, uniform appearance when in the second display configuration while providing maximum visibility and access to the food products stored therein. | 2021-10-07 |
20210309413 | FOLDABLE CONTAINER - This application discloses a foldable container. The foldable container has a base and two pairs of opposite side plates. The side plates are hinged to the base. Adjacent side plates are capable of being engaged with each other through engaging structures and being locked with each other through locking mechanisms to form a container body. At least one of the side plates is arranged such that when being unlocked from an adjacent side plate, it can be rotated towards the inner side of the container body and can be also rotated towards the outer side of the container body relative to the base. At least one side plate of the foldable container in this application can be rotated towards the inner side of the container body and can be rotated towards the outer side of the container body, and can be removed after being rotated, thereby greatly facilitate accessing goods, especially bulky and heavy goods. | 2021-10-07 |
20210309414 | ENCLOSURE FOR SPACEFLIGHT HARDWARE - An enclosure is disclosed for transporting articles upon a satellite. The enclosure is composed of a plurality of interconnected walls coupled via elongated edge connecting members to define an internal space shaped and dimensioned for receiving an article to be transported upon a satellite. The walls are honeycombed aluminum sheets or solid aluminum panels and the edge connecting members are lightweight high strength members shaped and dimensioned for secure attachment to the walls without the use of mechanical coupling members. | 2021-10-07 |
20210309415 | Subterranean Storage Container - A Subterranean Storage Container used to store retrievable items beneath the surface of ground, sand, terrain, material, or collection of snow, by means of a helical screw blade around the outside of container. The Subterranean Storage Container is used to store retrievable items. This Subterranean Storage Container encloses with accompanying lid, and may be designed with locking system to provide added security. The Subterranean Storage Container may be used with or without an originally designed towel or fabric, which may attach to Subterranean Storage Container, which is used to cloak and conceal the location of the Subterranean Storage Container from view. The originally designed towel or fabric may be used to store accessories, as drying towel, as wearable towel, as beach towel, or in any creative way the original design may permit. | 2021-10-07 |
20210309416 | Universal Handle Attachment Tool for Manipulating Different Containers - A universal handle attachment tool comprises a body having a plurality of tool sides each having a container interface surface operable to engage a face of a particular container, and having a container handle interface slot operable to receive a handle of the container. The slot can comprise a keyed profile operable to interface and lock the handle attachment tool to the container. The container interface surface extends in opposing directions beyond the slot to facilitate distribution of one or more loads acting between the face of the container and the handle attachment tool to facilitate manipulation of the container. A container for storage of at least one object comprises a container body defined by a plurality of sidewalls, and a recessed portion formed a sidewall defining a recessed cavity. The container has a handle spanning the recessed cavity, whereby the recessed cavity facilitates clearance of at least one finger of a user upon grasping the handle. | 2021-10-07 |
20210309417 | Universal Handle Attachment Tool for Manipulating Different Containers - A universal handle attachment tool comprises a body having a plurality of tool sides each having a container interface surface operable to engage a face of a particular container, and having a container handle interface slot operable to receive a handle of the container. The slot can comprise a keyed profile operable to interface and lock the handle attachment tool to the container. The container interface surface extends in opposing directions beyond the slot to facilitate distribution of one or more loads acting between the face of the container and the handle attachment tool to facilitate manipulation of the container. A container for storage of at least one object comprises a container body defined by a plurality of sidewalls, and a recessed portion formed a sidewall defining a recessed cavity. The container has a handle spanning the recessed cavity, whereby the recessed cavity facilitates clearance of at least one finger of a user upon grasping the handle. | 2021-10-07 |
20210309418 | BAG SUPPORT STRUCTURE - A bag support has an inner surface and outer surface. The bag support includes a first generally planar side opposite a second generally planar side; a first foldable side opposite a second foldable side. The bag support is movable between an operation state and a storage state, the first and second foldable sides unfold to define the operation state and fold to define the storage state, and in the operation state, the inner surface, when bounded by a flat bottom and a flat top of which there is none, defines a volume within which a bag may be placed to receive objects, wherein the bag extends from the volume to engage the outer surface. | 2021-10-07 |
20210309419 | TRANSPORT POUCH - A transport pouch includes a flap portion and a body portion separated from each other by a folding portion. The transport pouch also includes a front panel and a rear panel, an adhesive closure, at least one removable cover, and a form closure. When the flap portion of the transport pouch is folded onto the body portion of the transport pouch, the flap area of the adhesive closure is adhered to the body area of the adhesive closure, and the form closure is closed, the folding portion of the transport pouch acts as a barrier that prevents billowing of the body portion of the transport pouch, caused by a relative pressure increase in the transport space due to a pressure drop in the surroundings of the transport pouch, from tearing open the form closure and thus from tearing open the adhesive closure. | 2021-10-07 |
20210309420 | FLUID CONTAINER CLOSURE SYSTEM - A fluid container closure system includes a fluid outlet, a neck finish adjacent to the fluid outlet, wherein the neck finish includes a retaining rim, protruding in a radial outward direction and encircling the neck finish. A screw cap includes a base with a top deck and a skirt and a tamper evident band with a base having a lateral inner surface. The screw cap includes a predetermined breaking structure along which the skirt and the tamper evident band are interconnected. The tamper evident band includes a lip extending along the inner lateral surface of the tamper evident band base and inwardly therefrom, wherein the lip includes a hinge section and a retaining surface configured so when the screw cap is initially applied to the fluid container, the lip is folded upward about the hinge section such that the retaining surface in an applied position of the screw cap is positioned underneath the retaining rim. | 2021-10-07 |
20210309421 | CONTAINER, CLOSURE, AND METHODS FOR MANUFACTURE - In some embodiments, apparatuses and methods provided herein are useful for dispensing a fluid, such as a thixotropic fluid. In some embodiments, a bottle having a closure cap includes a flip top, a base, and a disk, where the base and disk define a mixing chamber configured to facilitate mixing of any serum or liquid separated from the fluid back therein. In some configurations, the base has a central opening through which the fluid exits and an internal shaft with a non-planar end surface opposite the central opening. In some configurations, the non-planar end surface and the disk define channels between the mixing chamber and the internal shaft. In some embodiments, the disk includes a central opening, a plurality of partial annular openings through a planar surface of the disk, and projections extending into the mixing chamber. | 2021-10-07 |
20210309422 | CONTAINER, CLOSURE, AND METHODS FOR MANUFACTURE - In some embodiments, apparatuses and methods provided herein are useful for dispensing a fluid, such as a thixotropic fluid. In some embodiments, a bottle having a closure cap includes a flip top, a base, and a disk, where the base and disk define a mixing chamber configured to facilitate mixing of any serum or liquid separated from the fluid back therein. In some configurations, the base has a central opening through which the fluid exits and an internal shaft with a non-planar end surface opposite the central opening. In some configurations, the non-planar end surface and the disk define channels between the mixing chamber and the internal shaft. In some embodiments, the disk includes a central opening, a plurality of partial annular openings through a planar surface of the disk, and projections extending into the mixing chamber. | 2021-10-07 |
20210309423 | CONTAINER, CLOSURE, AND METHODS FOR MANUFACTURE - In some embodiments, apparatuses and methods provided herein are useful for dispensing a fluid, such as a thixotropic fluid. In some embodiments, a bottle having a closure cap includes a flip top, a base, and a disk, where the base and disk define a mixing chamber configured to facilitate mixing of any serum or liquid separated from the fluid back therein. In some configurations, the base has a central opening through which the fluid exits and an internal shaft with a non-planar end surface opposite the central opening. In some configurations, the non-planar end surface and the disk define channels between the mixing chamber and the internal shaft. In some embodiments, the disk includes a central opening, a plurality of partial annular openings through a planar surface of the disk, and projections extending into the mixing chamber. | 2021-10-07 |
20210309424 | VENTED SPOUT FOR A LIQUID STORAGE CONTAINER - The vented pouring spout includes a main body and a valve system movable between a normally closed position and a fully opened position. The main body includes a first member and a second member. The valve system includes a valve member and two spaced-apart and parallel stems projecting from an inner side of the valve member into the first member. A push button is mounted within a housing and is in an axial force-transmitting engagement with the stems. The spout, among other things, can include a child-resistant closure (CRC) device that can be operated using a single finger, for instance the thumb or any other finger, and while holding a small container. | 2021-10-07 |
20210309425 | CONTAINER, CLOSURE, AND METHODS FOR MANUFACTURE - In some embodiments, apparatuses and methods provided herein are useful for dispensing a fluid, such as a thixotropic fluid. In some embodiments, a bottle having a closure cap includes a flip top, a base, and a disk, where the base and disk define a mixing chamber configured to facilitate mixing of any serum or liquid separated from the fluid back therein. In some configurations, the base has a central opening through which the fluid exits and an internal shaft with a non-planar end surface opposite the central opening. In some configurations, the non-planar end surface and the disk define channels between the mixing chamber and the internal shaft. In some embodiments, the disk includes a central opening, a plurality of partial annular openings through a planar surface of the disk, and projections extending into the mixing chamber. | 2021-10-07 |
20210309426 | EXPANDED SLIT SHEET CUSHIONING PRODUCTS WITH NOVEL REDUCED DIMENSION SLIT PATTERNS - In the preferred embodiments, the present invention provides substantially improved slit sheet cushioning products by advantageously combining novel paper properties with novel slit patterns for improved features and characteristics. In some illustrative and non-limiting example embodiments, cushioning products of the present invention can include, e.g., a novel slit sheet material in combination with extensible paper employed as, e.g., a cushioning pad or as cushioning within an envelope product, wherein the cushioning product can be substantially more resilient, but, yet, e.g., thinner for better utilization of space. | 2021-10-07 |
20210309427 | ANTI-MICROBIAL PACKAGING ASSEMBLY - An anti-microbial packaging includes an innermost decontamination layer defining an inside and exposed surface of the packaging against which items in the packaging would contact. A fiber substrate layer is fixed to the innermost decontamination layer which itself is a metal or a metallic-alloy layer. | 2021-10-07 |
20210309428 | LIQUID REPELLENT LAYER-FORMING RESIN COMPOSITION, AND LIQUID REPELLENT FILM, LIQUID REPELLENT LAMINATE, PACKAGING MATERIAL, AND CONTAINER USING SAME - A liquid-repellent layer forming resin composition comprises a polypropylene resin (A) and a silylated polyolefin (B), wherein the polypropylene resin (A) comprises a random polypropylene resin (Al) and a block polypropylene resin (A2) with a mass ratio (Mass of random polypropylene resin (A1)/Mass of block polypropylene resin (A2)) in the range of 20/80 to 80/20. | 2021-10-07 |
20210309429 | CONTAINER BAG MADE OF SHEET MATERIAL - To provide a container bag | 2021-10-07 |
20210309430 | FILM AND POUCH - An object of the present invention is to provide a film and a pouch having basic characteristics such as a strength and barrier properties and achieving good openability. A film ( | 2021-10-07 |
20210309431 | Break-Open Single-Dose Packages - A break-open single-dose package includes a panel defining one or more frangible regions, one or more sheets coupled to the panel and defining one or more pockets therebetween for storing one or more spreadable consumables, and an applicator. The frangible region(s) are adapted to form one or more openings through which the spreadable consumable(s) can exit in response to folding of the panel. The applicator may include one or more optional features such as a chamber, a backing, a tab, a blade, a grip, etc. to permit a user to spread on a surface any spreadable consumable(s) that exit the pocket(s) using the applicator without requiring the user's hand(s) to contact the spreadable consumable(s). | 2021-10-07 |
20210309432 | ONE OR MORE BLISTER PACKAGES CONTAINING ACTIVE MATERIAL AND METHODS OF MAKING AND USING SAME - A blister pack having a backing having a first side and an opposing second side. Each of the first and second side is flat or planar. The blister pack can also include a cover having a first side and an opposing second side. At least a portion of the second side of the cover is adhered to the first side of the backing to form a sealed package for containing product. The cover can include at least one blister. The blister pack can also include an active member positioned within each blister. Each active member can be in the form of a ring with an opening extending therethrough or a depression formed therein. | 2021-10-07 |
20210309433 | FITMENT FOR DISPENSING FLUIDS FROM A FLEXIBLE CONTAINER AND RELATED APPLICATIONS - A fitment assembly for use with a spout of a fluid container. The assembly includes a fitment and a poppet seal with a flexible element. The fitment includes a top portion and a bottom portion. The poppet seal extends from the bottom portion into the top portion. An attachment portion secures the flexible element within the bottom portion of the fitment. The flexible element provides a closing force to move the poppet seal from a closed to an open position. The poppet seal has a closed position, an open position, and a transport position. The poppet seal has a central support member that extends from the sealing surface of the poppet seal into the top portion of the fitment in the closed and transport condition. | 2021-10-07 |
20210309434 | PACKAGE CAPABLE OF RELEASING PRESSURE - The present invention relates to a package capable of releasing pressure formed therein. Said packaging comprises a container portion which is formed for accommodating product, and a flexible film part comprising at least one pressure-releasing design on an external surface of said part, characterized in that said pressure-releasing design comprises a score of at least two identical or different patterns combined together such that no less than three intersections of the patterns are formed and at least one said pattern is a closed-shape pattern. Moreover, the present invention relates to the pressure-releasing design for a flexible film, characterized in that said pressure-releasing design comprises a mark of at least two identical or different patterns combined together such that no less than three intersections of the patterns are formed and at least one said pattern is a closed-shape pattern. | 2021-10-07 |