34th week of 2020 patent applcation highlights part 20 |
Patent application number | Title | Published |
20200262536 | BUOYANCY AERIAL VEHICLE - An aerial vehicle ( | 2020-08-20 |
20200262537 | HIGH ALTITUDE GRAVITY ENERGY STORAGE - The present invention is realized by apparatus and methods for harvesting, storing, and generating energy by permanently placing a large rigid buoyant platform high in the earth's atmosphere, above clouds, moisture, dust, and wind. Long, strong and light tethers can connect the buoyant structure to the ground which can hold it in position against wind forces. Weights suspended from the buoyant platform with cables are raised and lowered by electric winches to store and release gravitational potential energy. High voltage transmission lines electrically connect the platform to the earth's surface. Electrical energy from the high voltage transmission lines or from photovoltaic arrays on the platform can be stored as gravitational potential energy and subsequently released as electricity from generators driven from the stored gravitational potential energy and used on the platform or transmitted via the high voltage transmission lines. | 2020-08-20 |
20200262538 | Moisture Control Systems and Methods for Controlling Moisture in an Aircraft - A moisture control system includes an anode coupled to an insulation blanket that is positioned between an inner wall and an outer wall of an aircraft fuselage, a cathode coupled to an interior surface of the outer wall, and a power control unit coupled to the anode and the cathode to apply voltage across the anode and the cathode. When the voltage is applied across the anode and the cathode, moisture is drawn away from the anode and toward the cathode on the interior surface of the outer wall and guided along a drainage path provided via structural members disposed between the inner wall and the outer wall toward a drainage port. | 2020-08-20 |
20200262539 | PROPULSION UNIT FOR AIRCRAFT - In a propulsion unit for an aircraft, including a nacelle and a turbojet engine supported by a pylon, a nacelle includes an outer shroud, a fixed internal structure defining, with the outer shroud, an annular space in which a cold air stream can circulate, and a sealing ring positioned between the fixed internal structure and the pylon. The sealing ring is used to separate a cold pylon zone from a hot engine zone. The propulsion unit includes a ventilation device allowing a portion of cold air of the cold air stream to be deviated to the sealing ring in order to ventilate the sealing ring. | 2020-08-20 |
20200262540 | AERODYNAMIC BRAKE SYSTEM AND METHOD - An aerodynamic brake includes a rigid panel having a panel leading edge portion and a panel trailing edge portion. The panel trailing edge portion is pivotably coupled to a vehicle body. The aerodynamic brake also includes a flexible sheet having a sheet lower edge portion coupled to the vehicle body, and a sheet upper edge portion coupled to the panel leading edge portion. The aerodynamic brake further includes a panel actuator configured to pivot the rigid panel between a stowed position and a deployed position. In the stowed position, the rigid panel is located proximate the vehicle body and covers the flexible sheet in a folded state. In the deployed position, the panel leading edge portion is pivoted away from the vehicle body and the flexible sheet is in an open state exposable to an oncoming airflow for generating aerodynamic drag for slowing the vehicle. | 2020-08-20 |
20200262541 | SYSTEMS AND METHODS FOR DETECTING PROPELLERS - A propulsion assembly for an unmanned aerial vehicle (UAV) includes a motor configured to rotate in a first direction, a propeller seat configured to be driven by the motor to rotate in the first direction and to receive a propeller, and a sensor configured to collect sensing data useful for determining whether the propeller is locked to the propeller seat, without requiring operation of the motor. | 2020-08-20 |
20200262542 | SYSTEM AND METHOD FOR AIRCRAFT PROPELLER GOVERNING - Methods and systems for governing an aircraft propeller of an engine are described. The method comprises obtaining a fluid flow command for speed control of the propeller, determining pulse parameters of a pulse width modulated valve control signal for actuating a two-position solenoid valve in accordance with the fluid flow command based on an average fluid flow through the solenoid valve and an opening and closing time of the solenoid valve, generating the valve control signal with the pulse parameters as determined, and transmitting the valve control signal to the solenoid valve for actuating the solenoid valve, thereby controlling the speed of the propeller. | 2020-08-20 |
20200262543 | CONTROLLED FLIGHT OF A MULTICOPTER EXPERIENCING A FAILURE AFFECTING AN EFFECTOR - According to a first aspect of the invention, there is provided a method for operating a multicopter experiencing a failure during flight, the multicopter comprising a body, and at least four effectors attached to the body, each operable to produce both a torque and a thrust force which can cause the multicopter to fly when not experiencing said failure. The method may comprise the step of identifying a failure wherein the failure affects the torque and/or thrust force produced by an effector, and in response to identifying a failure carrying out the following steps, (1) computing an estimate of the orientation of a primary axis of said body with respect to a predefined reference frame, wherein said primary axis is an axis about which said multicopter rotates when flying, (2) computing an estimate of the angular velocity of said multicopter, (3) controlling one or more of said at least four effectors based on said estimate of the orientation of the primary axis of said body with respect to said predefined reference frame and said estimate of the angular velocity of the multicopter. The step of controlling one or more of said at least tour effectors may be performed such that (a) said one or more effectors collectively produce a torque along said primary axis and a torque perpendicular to said primary axis, wherein (i) the torque along said primary axis causes said multicopter to rotate about said primary axis, and (ii) the torque perpendicular to said primary axis causes said multicopter to move such that the orientation of said primary axis converges to a target orientation with respect to said predefined reference frame, and (b) such that said one or more effectors individually produce a thrust force along said primary axis. | 2020-08-20 |
20200262544 | FLY-BY-WIRE SYSTEMS AND RELATED OPERATING METHODS - Aircraft fly-by-wire systems and related vehicle electrical systems are provided. In one embodiment, an electrical system suitable for use with a control surface of a vehicle, such as an aircraft, is provided. The electrical system includes an asynchronous intermodule bus arrangement, a first vehicle control module, and a second vehicle control module. Each vehicle control module includes a respective interface arrangement to obtain and exchange data from different sensing arrangements with a first frequency, and a respective processing system to obtain the sensed data and determine actuator commands based on the sensed data with a lower frequency. | 2020-08-20 |
20200262545 | MICRO DETECTING DEVICE - A micro detecting device includes a flying main body, at least one fluid actuation system, an image capture system and a controller. The fluid actuation system is disposed within the flying main body and includes a driving module, a flow guiding channel, a convergence chamber, plural valves and a fluid discharging zone. The driving module is consisting of plural flow guiding units for transporting fluid. The flow guiding channel includes plural diverge channels which are in fluid communication with plural connection channels. The convergence chamber is in fluid communication between the corresponding diverge channels. The valves are respectively disposed in the corresponding connection channels and controlled in open/closed state for the corresponding connection channels. The fluid discharging zone is in communication with the connection channels. The image capture system is used to capture external image. The controller is connected to the valves to control the valves in the open/closed state. | 2020-08-20 |
20200262546 | AERODYNAMIC ELEMENT PROVIDED WITH A CROSSFLOW CONTROL SYSTEM - The aerodynamic element includes an ionization system which ionizes flow of air flowing over the top face of the aerodynamic element and a control system which generates at least one electromagnetic force associated with an electrical current and a magnetic field, the at least one electromagnetic force being oriented in the direction opposite to that of the flow of the ionized air flow such that the electromagnetic force reduces the instabilities of the flow of the airflow. | 2020-08-20 |
20200262547 | NON-METALLIC ORIFICE PLATE - An orifice plate includes a wear-resistant inner diameter surface, an outer diameter surface, a first side surface extending between the wear-resistant inner diameter surface and the outer diameter surface, and a second side surface extending between the wear-resistant inner diameter surface and the outer diameter surface, the second side surface disposed opposite the orifice plate from the first side surface. The orifice plate may comprise a body portion comprising a first material. The wear-resistant inner diameter surface may comprise a second, wear-resistant material. | 2020-08-20 |
20200262548 | LOW-VIBRATION DRONE - A drone includes a fuselage and a plurality of housing structures for a plurality of engine units. The mechanical connection between each engine unit and each housing structure for the engine unit has: a ball joint arranged in the axis of rotation of the engine unit, opposite the rotor; and a flexible connecting member connecting the engine unit to the housing structure for the engine unit. | 2020-08-20 |
20200262549 | Vibration Isolation Systems for Advancing Blade Concept Rotorcraft - An advancing blade concept rotorcraft includes an airframe and a pylon assembly subject to vibration. The pylon assembly includes a dual rotor system having coaxially disposed top and bottom rotor assemblies that counter rotate relative to one another. The advancing blade concept rotorcraft includes a vibration isolation system including at least one pylon link coupled to the airframe and the pylon assembly. The pylon link includes a Liquid Inertia Vibration Eliminator unit operable to reduce transmission of the pylon assembly vibration to the airframe. The advancing blade concept rotorcraft includes active force generators adjacent to the pylon assembly. The active force generators include a first active force generator producing a force in a first direction and a second active force generator producing a force in a second direction to counteract multidirectional oscillations of the pylon assembly, thereby reducing vibration of the advancing blade concept rotorcraft. | 2020-08-20 |
20200262550 | Encapsulated Drone - Embodiments of the present invention enable a user of a drone to operate it more quietly. Embodiments of the present invention relate to such a system, apparatus, and a method of and for a drone that may be quiet, that can fly far while minimizing the need to recharge, that may have protective shells, that may employ operational redundancy, that may provide stealth capabilities due, for example, to the design of the shell, and that may allow a drone to stay in position at, for example, 329,999 feet for months. In one embodiment of the present invention, electro-magnetism is used to propel a drone while another embodiment uses an expandable outer shell. The embodiments, while also increasing a drone's range, provide enhanced maneuverability due to the unique shape and drive and steering systems of the drone. Embodiments may provide stealth and overall convenience, together potentially resulting in increased safety to creating a class of sub-space vehicles. | 2020-08-20 |
20200262551 | Bi-Planer Rotor Blade - A biplaner rotor blade has an upper airfoil section connected to a lower airfoil section such that the upper airfoil and lower airfoil are rotated in separate planes—an upper plane and a lower plane. The upper airfoil has a root end attached to a hub at an upper location of the hub and the lower airfoil has a root end attached to the hub at a lower location of the hub. The upper airfoil converges with the lower airfoil to form a blade tip end at the outermost portion of the blade, thus generating lift along two geometric planes. | 2020-08-20 |
20200262552 | TAIL ROTOR CYCLIC CONTROL FOR PITCH ATTITUDE ADJUSTMENT - A method of controlling a tail rotor system of a helicopter includes pivoting a swashplate of the tail rotor system about an axis passing through a diameter of the swashplate. Pivoting the swashplate causes a first linkage of a first pair of linkages coupled between the swashplate and a collective crosshead to move in a first direction and a second linkage of the first pair of linkages coupled between the swashplate and the collective crosshead to move in a second direction that is opposite the first direction. The movement of the first and second linkages causes a plane of rotation of a pair of rotors of the tail rotor system to cant relative to a centerline of a mast of the tail rotor system. | 2020-08-20 |
20200262553 | HYBRID ELECTRIC-JET POWERED - A hybrid electric jet powered aircraft including a fuselage member, a power unit, a set of wing members, and an emergency safety unit. The fuselage member includes a cabin having a plurality of enclosed seating elements for transporting a plurality of passengers and a cockpit having a plurality of seating elements for one or more operators of the aircraft. The power unit includes at least one electric powered motor and at least one jet fueled powered engine. The set of wing members for lifting the fuselage member. The set includes two pairs of wing members, wherein each pair of wing members is attached at its proximate end to the fuselage member on opposite sides of the fuselage member from one another. Each wing member has a tilting ducted fan attached to its distal end. Each ducted fan is tilted in a first position for horizontal forward flight and each ducted fan is tilted in a second position for vertical flight. The emergency safety unit for ejecting a parachute canopy when an emergency situation occurs in the aircraft. | 2020-08-20 |
20200262554 | METHODS AND SYSTEMS FOR WIRELESS POWER TRANSFER FOR ELECTRICALLY POWERED AERIAL VEHICLES - A method, system, and non-transitory computer-readable medium is provided for enabling a distributed power transfer network for an aerial vehicle, such as a drone. The distributed power transfer network may include wireless power transfer systems that may allow wireless charging and powering of devices within a distance of 10 meters. In some example embodiments, the distributed power transfer system may include at least one transmitter generating at least one transmission signal. The distributed power transfer system may further include a plurality of transducers each conducting a respective transmission signal of the at least one transmission signal, the plurality of transducers being positioned at respective different locations for producing from the respective transmission signals magnetic fields defining associated power transfer regions for transmitting wirelessly with the associated magnetic fields, power to aerial vehicles located in the power transfer regions. | 2020-08-20 |
20200262555 | METHOD FOR DETECTING MOUNTING ERROR OF ACCELEROMETER, DEVICE, AND UNMANNED AERIAL VEHICLE - A method for detecting a mounting error of an accelerometer includes acquiring actual output data of the accelerometer mounted to an unmanned aerial vehicle (“UAV”) while the UAV is in a hover state. The method also includes determining a mounting error angle of the accelerometer based on the actual output data. | 2020-08-20 |
20200262556 | METHOD AND APPARATUS FOR ECONOMICAL REFUELING OF DRONES - A drone control method is provided. The method may be responsive to drone recharge energy cost being greater than a predefined threshold and include commanding a processor of the drone to execute actions that preclude the drone from recharging. The method may also be responsive to drone charge level falling below a charge threshold selected only while the drone recharge energy cost exceeds the predefined threshold and include commanding the processor to execute actions to recharge the drone. | 2020-08-20 |
20200262557 | Tandem Wing Aircraft With Variable Lift And Enhanced Safety - A tandem wing aircraft having a fore wing, an aft wing, and a middle wing, attached relative to the aircraft and each other such that the middle wing provides a substantial portion of the total lift at landing speeds, and a minimal portion of the total lift at cruise speeds. At cruise speeds, induced drag is minimized, permitting higher speeds, greater fuel efficiency, and/or greater payload. Advantageously, the wing loading at cruise speeds is higher providing better passenger comfort while still providing controllability and safety at landing speeds. | 2020-08-20 |
20200262558 | DEVICE FOR SECURING AT LEAST ONE SLING FOR TRANSPORTING A LOAD - A device for securing at least one sling for transporting a load under a helicopter, the securing device comprising at least a first strap and at least a second strap, a connection mechanism configured, in the closed state, to connect the straps, to form a comprehensive security strap capable of supporting a sling and, in the open state, to release the straps for releasing the sling, and an actuator configured to open the connection mechanism following a mechanical effort being introduced, the connection mechanism comprising cascading reduction means configured to reduce the resistance force during the opening of the connection mechanism generated by the load connected to the sling. | 2020-08-20 |
20200262559 | SERVICE LIGHT INTEGRATED WITH READING LIGHT SWITCH - Embodiments are provided for a method and system for operating a service light integrated with a reading light. Some embodiments include providing a reading light and a service light, wherein the reading light and the service light are coupled to a switch, and receiving a first input to operate the reading light. Also, some embodiments include receiving a second input to operate the service light, wherein the first input and second input are received by the switch, and illuminating the reading light and the service light responsive to the first input and the second input, wherein the service light illuminates a switch cover operably coupled to the switch. | 2020-08-20 |
20200262560 | Bypass Flow Regulator - A bypass flow regulator for a vacuum waste system (VWS) is disclosed. The bypass flow regulator includes a valve assembly installable in an aircraft vent line leading outside the aircraft from an onboard VWS waste tank. The vent line directs an airstream pumped from the waste tank to an external outlet under suction (from which outlet the airstream is ejected from the aircraft). The valve assembly includes a group of valves (e.g., umbrella valves) set into the path of the airstream. The valves may collectively modulate the flow rate of the airstream by adjusting their effective flow area. | 2020-08-20 |
20200262561 | AIRCRAFT SEAT FOR CABIN CREW - A seat for cabin crew, intended to be installed in an aircraft, includes a seat structure intended to be fixed to a fixed portion of the aircraft, a seat slide provided with two arms positioned on either side of the seat portion, and a seat portion mounted slidably relative to the seat slide between a retracted position and an extended position. One of the elements among the seat portion and the seat slide includes rollers capable of sliding along corresponding rails provided in the other one of the elements among the seat portion and the seat slide. The rails have a curved shape so that the seat portion forms, in the extended position, an angle of more than 10 degrees, preferably of around 14 degrees, relative to a floor of the aircraft. | 2020-08-20 |
20200262562 | ARRANGEMENTS FOR AIRCRAFT PASSENGER CABINS WITH PRIVACY DIVIDER CONFIGURATIONS - Arrangements for an aircraft passenger cabin including a seating area containing first and second passenger seats, a monument disposed at one end of the seating area, and at least one privacy divider deployable in a longitudinal direction of the seating area to divide at least a portion of the seating area for privacy. In some embodiments, the at least one privacy divider includes a first privacy divider adapted to deploy to divide the seating area forward of the first and second passenger seats and a second privacy divider deployable to the seating area between the first and second passenger seats. | 2020-08-20 |
20200262563 | ENERGY ABSORBER FOR AIRCRAFT SEAT - The invention relates mainly to an energy absorber for an aircraft seat, notably for a helicopter seat, comprising at least one energy-absorption element having:
| 2020-08-20 |
20200262564 | ENERGY ATTENUATING MOUNTING FOOT FOR A CABIN ATTENDANT SEAT - In various embodiments, the present disclosure provides an energy attenuating mounting foot comprising a load beam having a longitudinal axis, a top surface, a bottom surface, an inner track interface lobe, and an outer track interface lobe, the inner track interface lobe and the outer track interface lobe extending laterally from the load beam, and a channel along the longitudinal axis having a depth extending from the load beam bottom surface toward the top surface. In various embodiments, the inner track interface lobe has a first length extending in a direction from the bottom surface towards the top surface and the outer track interface lobe has a second length extending in a direction from the bottom surface towards the top surface, the first length being less than the second length. | 2020-08-20 |
20200262565 | MULTI-POSITION ADJUSTABLE HEADREST ASSEMBLY - An adjustable headrest assembly attachable to a seat back and including a linear slide and rotating links that allow the headrest to translate forward, laterally and/or about axes parallel to the seat back to provide head support in various positions. The headrest may further include lateral parts independently adjustable in angle relative to a center part to provide enhanced lateral head support. The adjustable headrest assembly is attachable to a front side of a seat back or to other adjustment mechanisms such as a vertical adjustment mechanism for moving the headrest assembly up or down relative to a seat back. | 2020-08-20 |
20200262566 | EASY HOOK ARMREST ASSEMBLY FOR AIRCRAFT SEAT - An armrest for a seat may comprise paneling and an easy hook assembly. The easy hook assembly may include a flange and a keyhole protrusion. The flange and the keyhole protrusion may each extending beyond an exterior surface of the paneling. The flange and the keyhole protrusion may allow the armrest to be installed after the paneling is attached. | 2020-08-20 |
20200262567 | PASSENGER SERVICE UNIT WITH COVER - A passenger service unit assembly that includes a frame that defines at least an oxygen opening and a service opening, an oxygen mask housing positioned adjacent the oxygen opening, an oxygen mask housing cover positioned to cover the oxygen opening, and a service cover positioned to cover the service opening. An oxygen mask that is movable between a stowed position and a deployed position is positioned in the oxygen mask housing. The oxygen mask housing cover maintains the oxygen mask in the stowed position. The oxygen mask housing cover is movable between a closed position and an open position. When the oxygen mask housing cover is moved to the deployed position, the oxygen mask drops to the deployed position via gravity. The service cover is movable between a closed position and an open position and includes at least a first passenger service unit component associated therewith. | 2020-08-20 |
20200262568 | Passive Anti-frosting Surface Comprised of Microscopic Wettability Patterns Containing Sacrificial Ice - A method and device for reducing ice and frost on a surface comprising a wettable pattern on a surface. The pattern is wetted with water which is frozen into ice to create overlapping hygroscopic that cover the surface. | 2020-08-20 |
20200262569 | DAMPENING RISERS FOR PARACHUTES - A suspension line assembly for a parachute may comprise a plurality of suspension lines bound together at a confluence, and a dampening riser coupled to the confluence, wherein the dampening riser comprises a first length in the stowed position and the dampening riser is configured to extend to a second length in a deployed position in response to a tensile force applied to the dampening riser. | 2020-08-20 |
20200262570 | HIGH PRESSURE EVACUATION SLIDE WITH TRUSS-SHAPED SIDE RAILS - An evacuation slide may comprise a sliding surface extending from a head end of the evacuation slide to a toe end of the evacuation slide and a truss-shaped side rail located adjacent the sliding surface. An evacuation system may comprise the evacuation slide and a charge cylinder fluidly coupled to the truss-shaped side rail. | 2020-08-20 |
20200262571 | AIRCRAFT ASSEMBLY COMPRISING A MOUNTING PYLON, A WING AND TWO FIXING SYSTEMS FIXING THE MOUNTING PYLON TO THE WING - An assembly comprising a wing with lower spars, a mounting pylon having an upper spar and two lateral panels, a front fixing system and a rear fixing system, each comprising a beam pierced with a principal bore and, for each beam, an upper bore traversing the upper spar and a shear pin positioned in the upper bore and in the principal bore. The assembly also comprises, for each fixing system, bolts, the nut of which is accommodated in a secondary hole of the beam and the screw of which traverses the upper spar and the beam in order to be screwed into the nut. | 2020-08-20 |
20200262572 | SYSTEM COMPRISING AN AIR INTAKE OF AN AIRCRAFT ENGINE AND AN INFLATABLE PROTECTION ITEM FOR SAID AIR INTAKE - A system comprising a trolley which comprises a platform and wheels attached beneath the platform, an air intake of an aircraft engine, where the air intake rests on the platform so as to have its narrowest part at the top and its widest part at the bottom, and an inflatable protection item in the form of a closed envelope which is placed around the widest part of the air intake. A system of this kind makes it possible to protect the air intake from collisions that it might experience during movement of the trolley, and to increase safety by avoiding collisions between operators and the air intake. | 2020-08-20 |
20200262573 | METHOD FOR PROPELLING AN AIRCRAFT, PROPULSION SYSTEM, AND AIRCRAFT - In the method for propelling an aircraft, to obtain electric energy, a fuel is combusted, and an electric machine is used, wherein the fuel is used to cool at least one part of the electric machine and contains natural gas. The propulsion system is configured to propel an aircraft, in particular according to the above-mentioned method. The propulsion system has an electric machine configured to obtain electric energy by combusting a fuel. The propulsion system further includes a natural gas tank configured to supply the fuel formed with natural gas, and a cooling device configured to cool at least one part of the electric machine. The aircraft has such a propulsion system. | 2020-08-20 |
20200262574 | VERTICAL TAKE-OFF AND LANDING AIRCRAFT AND TRANSFORMATION GEAR SETS FOR SAME - A vertical take-off and landing aerial vehicle (VTOL) includes a plurality of rotors for producing lift. For each respective rotor the VTOL has an auxiliary power source (APS) and a transformation gear set (TGS) both being associated with the respective rotor, and the VTOL further includes at least one main power source (MPS). Each TGS is configured to form an outgoing power towards its respective rotor from input powers received into the TGS from the MPS and from the APS associated with the respective rotor. | 2020-08-20 |
20200262575 | METHOD AND ELECTRONIC DEVICE FOR DETERMINING AT LEAST ONE FUEL CONSUMPTION DOMAIN FOR AN AIRCRAFT, RELATED COMPUTER PROGRAM AND ELECTRONIC DISPLAY SYSTEM - This method for determining at least one fuel cosumption domain for an aircraft is implemented by an electronic device. It comprises acquiring a flight envelope as a function of the altitude and a propulsion variable. | 2020-08-20 |
20200262576 | FUEL PUMP MANAGEMENT SYSTEM AND METHOD OF OPERATING A FUEL PUMP MANAGEMENT SYSTEM - A method of and a system for operating a fuel pump management system of an aircraft. The method comprises receiving, from a fuel gauge, an electronic reading of a level of fuel fluid contained in a fuel tank; and analysing the electronic reading of the level of the fuel fluid, the analysing comprising upon determining that the level of fuel fluid is equal or below a predetermined fuel level threshold, causing a fuel pump in communication with the fuel tank to be shut down. | 2020-08-20 |
20200262577 | Crash Force Attenuating Fuel System - A fuel system for a rotorcraft is provided. The fuel system comprises a housing, a fuel bladder located within the housing, a first fuel reservoir, and a number of pressure relief valves. The first fuel reservoir is in fluid communication with the fuel bladder and stowed within the housing. The number of pressure relief valves are configured to divert fuel from the fuel bladder into the first fuel reservoir at a predetermined pressure such that the first fuel reservoir expands to reduce forces on the housing during a crash event. | 2020-08-20 |
20200262578 | SYSTEM AND METHOD FOR DETECTING A FUEL LEAK IN AN AIRCRAFT - A method of and a system for detecting a fuel leak in an aircraft, the aircraft comprising a first engine and a second engine. The method comprises upon determining that the aircraft has reached a first mode of operation: acquiring a first baseline fuel flow of the first engine; acquiring a second baseline fuel flow of the second engine. The method further comprises monitoring a first current fuel flow measured at the first engine and a second current fuel flow measured at the second engine; and triggering a fuel leak detection based on an analysis of the first baseline fuel flow, the first current fuel flow, the second baseline fuel flow and the second current fuel flow. | 2020-08-20 |
20200262579 | MODULAR POWER UNITS FOR AIRCRAFT - Systems and methods are disclosed for providing flexible, scalable, and controllable electrical power to an aircraft. In some embodiments, a modular power unit comprises a container containing a power generation unit, a control system, a conditioning system, and an environmental control system. The power generation unit produces a generated power. The control system provides control signals to the power generation unit and controls at least one parameter of the generated power. The conditioning system receives and conditions the generated power and provides an output power to the power bus of the aircraft. The environmental control system provides a temperature regulating fluid to the power generation unit. | 2020-08-20 |
20200262580 | WIRELESS LIGHTING SYSTEM FOR AIRCRAFT EVACUATION SYSTEMS - A wireless lighting system for an aircraft evacuation system. The wireless lighting system includes a wireless controller disposed in the aircraft having at least a transmitter configured to communicate an activation under an aircraft evacuation event when the aircraft evacuation system is deployed, and a first light source disposed on the aircraft evacuation system, the first light source configured to provide illumination to the aircraft evacuation system. The wireless lighting system also includes a first energy storage device disposed on the aircraft evacuation system and a first wireless receiver disposed on the aircraft evacuation system and configured to receive the activation signal from the wireless controller. The first wireless receiver is operably connected to the first energy storage device and the first light source and configured to activate the first light source based on the activation signal. | 2020-08-20 |
20200262581 | PAYLOAD MOUNTING PLATFORM - An apparatus for supporting a payload includes a payload mount configured to be coupled to the payload to secure the payload, a first support member coupled to one side of the payload mount in a single arm configuration and including a first actuation unit configured to rotate the payload mount around a first rotational axis relative to the first support member, and a single flexible member including a branched configuration. The branched configuration includes at least a first end that is electrically coupled to the payload mount and a second end that is electrically coupled to the first actuation unit. | 2020-08-20 |
20200262582 | DUST-PROOFING STRUCTURE, BINOCULAR SENSOR AND UNMANNED AERIAL VEHICLE - A sensor includes a camera and a dustproof structure. The dustproof structure includes a case accommodating the camera. The case includes a lens hole at a position corresponding to the camera. The dustproof structure further includes an airflow generating device configured to blow airflow to form an airflow barrier between the camera and the lens hole. | 2020-08-20 |
20200262583 | LANDING STRUCTURE FOR AN UNMANNED AERIAL VEHICLE - A system for landing an unmanned aerial vehicle has an unmanned aerial vehicle and a ground-based platform. A guide structure for receiving the unmanned aerial vehicle is mounted on the ground base platform. The guide structure has an inner diameter greater than a smallest outer diameter of the unmanned aerial vehicle landing gear and less than the largest outer diameter of the unmanned aerial vehicle landing gear. | 2020-08-20 |
20200262584 | BOARDING BRIDGE HAVING TRANSPARENT DISPLAY, AND METHOD OF CONTROLLING SAME - Disclosed is a boarding bridge having a transparent display. The boarding bridge includes a first tunnel connected to a terminal gate, a second tunnel connected to be capable of overlapping with the first tunnel, and a control unit. The first tunnel and the second tunnel each have a plurality of transparent displays, and include at least one overlap detecting sensor unit. Through the overlap detecting sensor unit which detects whether a transparent display of the first tunnel and a transparent display of the second tunnel overlap, the controller can selectively control the playback of images on the transparent displays of the first and second tunnels. | 2020-08-20 |
20200262585 | BATTERY DRIVEN GROUND POWER UNIT WITH IMPROVED CONSTRUCTION, OPERABILITY, DURABILITY AND MAINTENANCE - An airport ground power unit for supplying electric current to a parked aircraft and a related system and method. The ground power unit includes a first electric battery, an inverter for transforming an output current of the battery to an alternating output current to be supplied to the aircraft, and one or more first electronic switches for connecting and disconnecting the first battery to and from the inverter. The first switches are connected in serial to the first battery, and together connected to the inverter. A first controller unit controls at least one of the one or more first switches. The ground power unit further includes a second electric battery and second electronic switches for connecting and disconnecting the second battery. The second switches are connected in serial to the second battery and are together connected to the inverter such that they are in parallel to the serially connected first battery and the first switches. At least one of the second switches is controlled by the first or a second digital controller unit. | 2020-08-20 |
20200262586 | METHOD FOR ASSEMBLING TWO COMPONENTS AND METHOD FOR ASSEMBLING TWO PORTIONS OF AN AIRCRAFT - A method for assembling two components and method for assembling two portions of an aircraft. A method for assembling first and second components includes, prior to the setting in place of temporary linking elements in the first and second starter holes, producing the first starter holes in the first component, depositing a sealing mastic on at least one of the first and second contact faces of the first and second components, placing the first and second components against one another, and producing second starter holes in the second component using a drilling tool connected to a suction system and equipped with a drill bush including a first part that has an outside diameter less than or equal to that of the first starter holes and a first end bearing against the second contact face of the second component upon production of the second starter holes. | 2020-08-20 |
20200262587 | ASSEMBLY METHOD FOR AN AIR INTAKE OF A JET ENGINE OF AN AIRCRAFT - An assembly method for an air intake of a jet engine of an aircraft, comprising providing an acoustic panel, an outside panel, flanges and a collar, arranging a rear edge of the acoustic panel on an assembly chassis. The flanges and the collar are attached at the rear edge of the acoustic panel. A rear edge of the outside panel is attached to the attached collar. A first set of geometric data of a front edge of the acoustic panel is measured and a second set of geometric data of a front edge of the outside panel is measured. A U-shaped lip as a single element is produced based on the two sets of geometric data. An inside leg of the lip is attached to the front edge of the acoustic panel and an outside leg of the lip is attached to the front edge of the outside panel. | 2020-08-20 |
20200262588 | AIRCRAFT LANDING GEAR MONITORING SYSTEMS AND METHODS - Landing gear monitoring systems and methods for an aircraft include a landing gear timing analysis control unit that is configured to analyze one or both of landing gear motion of one or more landing gears of the aircraft or door motion of one or more doors proximate to the landing gear(s) to determine an operational status of one or both of the landing gear(s) or the door(s). | 2020-08-20 |
20200262589 | ATTITUDE RATE MITIGATION OF SPACECRAFT IN CLOSE PROXIMITY - Technique for altering a client spacecraft's rotational rate including the precise positioning of a servicing spacecraft in close proximity of a client spacecraft, alignment of a fluid release output device on the servicing spacecraft that imparts a force on the client spacecraft by means of fluid release, and subsequent use of the fluid release output device to mitigate tumbling of the client spacecraft. This allows the servicing spacecraft to slow the rotation of a tumbling client spacecraft in order to perform additional servicing operations. | 2020-08-20 |
20200262590 | ATMOSPHERIC THRUST STAGES, MULTI-STAGE LAUNCH SYSTEMS INCLUDING THE SAME, AND RELATED METHODS - Atmospheric thrust stages, multi-stage launch systems including the same, and related methods. A multi-stage launch system includes a launch vehicle configured to transport a payload to a payload destination. The launch vehicle includes an atmospheric thrust stage (ATS) with a plurality of airbreathing engines configured to provide thrust to the launch vehicle for a vertical launch of the launch vehicle The ATS is configured to be retrieved and reused subsequent to returning to Earth. A method of transporting a payload to a payload destination includes powering a launch vehicle that includes an ATS and a second stage by providing thrust with a plurality of airbreathing engines of the ATS to propel the launch vehicle, decoupling the second stage from the ATS, powering the second stage to transport the payload to the payload destination, and returning the ATS to Earth. | 2020-08-20 |
20200262591 | HAND HELD STRAPPING TOOL - A strapping device includes a handle, a body, and an actuator. The handle includes an input device and a switch, the input device spaced from the switch by a biasing element that applies a bias force to the input device. The input device moves from a first state spaced from the switch to a second state contacting the switch responsive to receiving a force greater than the bias force. A circuit of the switch is closed responsive to the input device moving from the first state to the second state. The switch outputs an actuation signal responsive to the circuit being closed. The body includes a tensioner and a base including a strap receiver opposite the tensioner. The actuator moves the tensioner from a first tensioner position to a second tensioner position further from the strap receiver based on a movement force greater than the bias force. | 2020-08-20 |
20200262592 | STRAPPING DEVICE - A strapping device includes a body, a tensioner, and a handle. The body can have a first body end, a second body end, and a base extending between the first body end and the second body end. The tensioner can be coupled with the body and adjacent to the base, the body defining a strap axis between tensioner and the base, the tensioner applies a force to a strap received by the body along the strap axis. The handle can extend between a first handle end coupled with the first body end and a second handle end coupled with the second body end. The handle can be oriented at an angle relative to a plane parallel to the strap axis, the angle greater than or equal to 15 degrees and less than or equal to 45 degrees. | 2020-08-20 |
20200262593 | STRAPPING TOOL - A strapping tool has a tensioner for tightening a strap, a sealer for fixing together ends of the strap, a base, and a drive mounted on the base for operating the tensioner and sealer. The sealer or tensioner is a module removably attached to the base. A transponder is provided on the module and a reader on the base for wirelessly communicating with the transponder. A controller is connected to the reader for operating the tool. | 2020-08-20 |
20200262594 | BAG PRODUCTION DEVICE AND METHOD - Apparatus and method of manufacturing open-mouth bags ( | 2020-08-20 |
20200262595 | APPARATUS FOR PACKAGING SHEET MATERIAL - An apparatus is arranged for packaging sheet material, in particular banknotes, vouchers, checks, separation cards, etc., with a packaging device, packaging material dispensed from a roll for packaging the sheet material, and a control device controlling the apparatus. A monitoring device is provided for the packaging material, and the control device evaluates a signal of the monitoring device during the packaging of sheet material, in order to derive therefrom whether packaging material is present on the roll. | 2020-08-20 |
20200262596 | SYSTEM, METHOD AND APPARATUS FOR PROCESSING CARTRIDGES EN MASSE - A cartridge processing system can have a base to support cartridges on an underlying support surface. The base can include a rack with support holes to support respective ones of the cartridges. In addition, a tray having a tray bottom can be removably placed on tops of the cartridges. A platform with platform holes can be substantially coaxially aligned with respective ones of the support holes. The tray can have a funnel extending from the platform. The funnel can form a perimeter around the platform holes, such that the platform holes can be conduits for product to be placed in the cartridges. | 2020-08-20 |
20200262597 | SYSTEM, METHOD AND APPARATUS FOR PROCESSING CARTRIDGES EN MASSE - A cartridge processing system can have a base to support cartridges on an underlying support surface. The base can include a rack with support holes to support respective ones of the cartridges. In addition, a tray having a tray bottom can be removably placed on tops of the cartridges. A platform with platform holes can be substantially coaxially aligned with respective ones of the support holes. The tray can have a funnel extending from the platform. The funnel can form a perimeter around the platform holes, such that the platform holes can be conduits for product to be placed in the cartridges. | 2020-08-20 |
20200262598 | HIGH SPEED DUAL LABEL APPLICATOR - A labeling system includes a frame component pivotal between a label load position, a first label apply position and a second label apply position. A vacuum applicator is carried on the frame component for movement with the frame component. A first actuator is configured for pivoting the frame component between the label load position and the first label apply position. A second actuator is configured for pivoting the frame component from the label load position to the second label apply position. The second label apply position is located between the label load position and the first label apply position. The labeling system can be used to apply one label to the leading side of an item moving along a conveyance path, and to apply another label to the lateral side of the same item. | 2020-08-20 |
20200262599 | A METHOD FOR PRODUCING A CONTAINER FROM A CONTAINER BLANK, IN PARTICULAR WITH A REDUCTION IN THE HEIGHT OF THE CONTAINER BLANK - The invention relates to a method comprising, as method steps,
| 2020-08-20 |
20200262600 | PLASTIC PREFORM AND CONTAINER - A container assembly suitable for holding pressurized content includes a plastic container and a base cup. The plastic container may include a including a rounded base portion, and the base cup may be connected to the container and configured to support the plastic container. In embodiments the plastic container and the base cup are comprised of plastic, and may be comprised of substantially the same recyclable plastic material. In embodiments, the base cup may be thermoformed, and/or the container assembly may be comprised of 80% or more, by weight, of PET. | 2020-08-20 |
20200262601 | Container - A container for storing a liquid or a solid may include a container body having a container side wall and a container bottom and a container lid having a pop top arm to pivot and cooperate with a weakened area to provide access to the interior of the container body. The container body may be formed from plastic and the container lid is formed from metal, and the container body may include a vertical neck. The container body may include a lip, and the bottom wall may include a center protrusion. The bottom wall may include a depression, and the bottom wall may include a radial extending depression. | 2020-08-20 |
20200262602 | PACKAGING - Packaging includes a sleeve and a re-configurable container. The re-configurable container comprises a box and a front flap which are hinged together and are pivotable between a folded-together configuration in which the front flap rests against a front panel of the box and the container is insertable into and removable from the sleeve and an unfolded configuration in which an aperture in the front panel of the box is accessible to give access to a first compartment of the box. A printed document is removably secured to a front face of the front flap and the arrangement is such that, when the container is inserted in the sleeve, the sleeve covers the printed document and, when the container is removed from the sleeve, the printed document is accessible and is removable from the front flap. | 2020-08-20 |
20200262603 | HONEYCOMB STRUCTURE - A honeycomb structure is disclosed. The honeycomb structure includes a plurality of first partitions and a plurality of second partitions. The plurality of first partitions has a plurality of first honeycomb partitions. The plurality of second partitions has a plurality of second honeycomb partitions, and the plurality of first honeycomb partitions and the plurality of second honeycomb partitions are fitted to each other such that the plurality of second partitions and the plurality of first partitions are interdigitated to form at least one receiving portion, wherein the plurality of Its first honeycomb partitions have at least one die line. One part of at least one first honeycomb partition is bendable at least one die line to change the size of an opening size of the receiving portion corresponding to the at least one first honeycomb partition which is bended. | 2020-08-20 |
20200262604 | PACKAGING BOX - Disclosed is a packaging box which includes a box body. The packaging box includes a cavity defined in the box body and a side wall surrounding the cavity, a support frame that disposed on an inner side of the side wall, and a bottom plate that is disposed in the cavity and at an end of the support frame. The support frame is integrated with the box body, an opening is provided in the box body, and the support frame is formed by bending the side wall located at the opening toward the cavity. | 2020-08-20 |
20200262605 | TAMPERPROOF FOOD BOX - A re-closable tamperproof food box, including first and second main panels connected with a rear panel, the first main panel forming the bottom and the second main panel forming the top. The first main panel has two side panels and a front panel attached. The second main panel has two side panels and a front panel attached. The second main panel is connected along fourth edge to the rear panel connected along a fourth edge of the first main panel. At least one strip of adhesive is disposed on one of the two opposing side panels and the front panel of the first main panel A perforation is disposed along the second main panel, forming a tear strip. A continuous length of material on an interior surface of the second main panel, to tear through the tear strip. | 2020-08-20 |
20200262606 | PACKAGING - A display carton includes a base tray having upstanding front, side and rear walls and a cover which is detachably connected to the base tray along lines of weakness. The cover includes an inner front wall positioned above the front wall of the base tray and an outer front wall which is provided by a distal end of a forwardly extending lid of the cover. The inner front wall comprises left and right portions which are connected together by a line of weakness. A bottom end of the outer front wall is tucked into a slot formed between a bottom edge of the inner front wall and a top edge of the front wall of the base tray. | 2020-08-20 |
20200262607 | MULTI-CARTON CONTAINER - A multi-carton container can be separated into a first carton and a second carton. The top wall of each of the first carton and the second carton can be at least partially connected to each other along a line of weakness. Side walls of each of the first carton and the second carton can also be at least partially connected to each other along lines of weakness. | 2020-08-20 |
20200262608 | CONTAINER WITH HIGH MOISTURE BARRIER PROPERTIES AND A RECLOSEABLE POUR SPOUT - A paperboard substrate that can be used to provide a food packaging particle is provided having a water vapor barrier layer comprising HDPE in combination with a nucleating agent which is extruded on to a paperboard substrate. The resulting substrate has sufficiently good water vapor barrier when properties that dry foods such as cereals do not require a bag or inner liner as a separate moisture barrier. | 2020-08-20 |
20200262609 | PRE-STERILIZABLE CARRIER SYSTEM - A method for filling dual-chamber systems in pre-sterilizable carrier systems includes providing at least one washed, siliconized and sterilized dual-chamber system in a magazine. The dual-chamber system includes respective separating elements separating the two chambers from each other. The magazine accommodates at least one dual-chamber system and is arranged in a container that is sealed with a closing element. The method additionally includes introducing the container into a clean room; opening the container and filling a first chamber of the at least one dual-chamber system; and closing the first chamber. The method further includes filling a second chamber of the at least one dual-chamber system; closing the second chamber; and removing the system from the clean room. | 2020-08-20 |
20200262610 | STORAGE SYSTEM HAVING STACKABLE AND ENGAGEABLE VESSELS - A storage system includes a plurality of vessels each shaped to engage with an adjoining vessel in a top-to-bottom orientation. The volume of the vessels may vary. The lip of each vessel includes a plurality of radially positioned flanges, and the bottom of each vessel includes a plurality of radially positioned locking lugs that correspond and engage with the flanges upon rotation of one vessel relative to the other. | 2020-08-20 |
20200262611 | MODULAR CONTAINER SYSTEM HAVING AN INTERIOR DIVIDABLE INTO COMPARTMENTS OF VARIABLE SIZE - A modular container system has an interior dividable into compartments of variable size and includes a base having a bottom and sidewalls extending from the bottom to define an interior volume. At least one opposing pair of the sidewalls have regions arranged opposite each other, each of the regions including protrusions to form pairs of opposing protrusions, each of the regions further including indents positioned in correspondence with the protrusions. At least one barrier extends between the opposing protrusions to divide the interior volume of the base into a plurality of compartments. The barrier has an elongate body and a tab portion extending from each end of the body. Each tab portion is bendable to orient an underside of each tab portion to face a respective protrusion, a longitudinal end of each said tab portion engaging with a corresponding indent, to form a press-fit coupling. | 2020-08-20 |
20200262612 | CONTAINER FOR STORING PERSONAL CARE ITEM - A container for storing at least one personal care item includes a base plate and well. The base plate defines an aperture and has top and bottom surfaces. The well passes through the aperture and has: an open top portion and a closed bottom portion collectively defining a chamber accessible through the top portion, a seat abutting the bottom surface, and a flange overlying a portion of the base plate. A cap is removably secured atop the chamber and abuts the flange such that the flange seals between the cap and the base plate when the cap is secured atop the chamber. The well has an uppermost point and a lowermost point and a height defined therebetween, and the lowermost point is collapsible toward the uppermost point to a maximum distance of: at least forty percent of the height and no more than sixty percent of the height. | 2020-08-20 |
20200262613 | BULK BAG HAVING A MULTI-SIDED SHAPED BOTTOM - A fabric bulk bag and a method for constructing the same, the bag including a continuous sidewall, a top portion, and a bottom, all defining a bulk storage space therein; the bottom further comprising eight sides which define an octagonal shape having an enlarged footprint so that the bag wall is sewn to the bottom in less time than a round shaped bag, yet when filled stands more upright with less tendency to lean than the current square shaped bags thereby providing a safer more dependable stacking bulk bag. In the method of producing the fabric bulk bag, the bag is constructed in less time than the prior art round bottom bags, uses less wall fabric than prior art square bottomed bags and when constructed and filled, supports itself more stable on a floor or pallet because it provides substantially more base for the product to rest on. In other embodiments, the bag would be multi-sided with greater than four sides. | 2020-08-20 |
20200262614 | Fluorescent Bulb Bag - A florescent bulb bag having a body with first and second elongated panels extending along a first axis and composed of material having top, bottom and side edges that are connected to one another along their bottom and side edges in overlying relation to one another and defining a cavity therebetween that is accessible via through the top edges; and a plurality of elongated sleeves formed in the cavity each of which extends along respective, parallel axes and all of which are parallel to the first axis, wherein each sleeve is sized and shaped to comfortably receive one fluorescent bulb therein. | 2020-08-20 |
20200262615 | SQUEEZE TUBE AND METHOD OF MAKING A SQUEEZE TUBE - A squeeze tube includes a fluid-discharge container and a fluid-discharge closure mated to the fluid-storage container. The fluid-discharge closure is coupled to one end of the fluid-storage container and configured to discharge selectively fluid stored in a product-storage region formed in the fluid-storage container. | 2020-08-20 |
20200262616 | CLOSURE - A canister includes a closure configured to mount on a container to close an open mouth into a product storage region formed in the container. The closure includes a lid and a lid retainer coupled to the lid. The lid retainer is configured to mate with an external thread on the container to retain the closure in a mounted position on the container. | 2020-08-20 |
20200262617 | PVC-FREE CLOSURES - The present invention relates to compositions (compounds) which can be used as seal material in vessel caps, even under pasteurization conditions and possibly sterilization conditions. More specifically, the invention relates to such compositions that are suitable for vessel caps that can be unscrewed, such as lug screw caps and in particular Press-on/Twist-off® caps, and that result in a reduced migration of undesirable substances. | 2020-08-20 |
20200262618 | Double Button Safety Match Box - This disclosure relates generally to a safety match box and comprises a cover member of a generally box-like configuration which has a slidable tray having a pack of matches fastened thereto which fits within the cover member. The general object of this invention is the provision of a very simple device which is adapted to hold a box of matches, a shelf, and lock the box thereto permitting the box to be opened and the matches removed whenever desired. This invention is to provide a child-proof safety match box wherein the tray cannot be completely withdrawn from the cover and particular manipulative steps must be taken in order to open the container. | 2020-08-20 |
20200262619 | GLASSWARE LID AND GLASSWARE WITH SAME - The present invention relates to and provides a glassware lid and a glassware with same. After food is heated, the lid is covered; a first end of the air hole sliding lid is turned so that the air hole is communicated with outside atmosphere to avoid forming a vacuum state inside; when the lid needs to be taken out, the first sliding parts and the second sliding parts continue to slide to separate the hoop from the glassware body, which is convenient to operate. The structure is compact and the arrangement is reasonable. | 2020-08-20 |
20200262620 | CONTAINER SYSTEM WITH BASE AND FOLDABLE LID - A container system, including a base with a rim having a pair of protrusions on opposite sides of the base extending into the base; and a lid having a peripheral outer rim. The lid includes a pair of partial peripheral troughs positioned radially inward of the outer rim, ends of the partial peripheral troughs being spaced apart to form a pair of peripheral gaps on opposite sides of the lid to receive the pair of protrusions of the base to attach the lid to the base. The lid has a hinge about which the lid folds as a first part of the lid is lifted to provide access to the interior volume of the base while a second part of the lid on an opposite side of the hinge remains attached to the base. | 2020-08-20 |
20200262621 | Beverage Can Cap - A beverage can cap is outfitted upon an upper portion of a beverage can for enabling a user to selectively cover the upper portion. The upper can portion has an upper can rim and a can capping plate. The beverage can cap essentially includes an upper cap rim, a cap plate centrally located relative to the cap rim, and a cap opening. | 2020-08-20 |
20200262622 | PROTECTIVE CAP FOR A DISPENSER AND DISPENSER FOR DISCHARGING PHARMACEUTICAL AND/OR COSMETIC LIQUIDS - A protective cap for a dispenser for discharging pharmaceutical and/or cosmetic liquids. The dispenser has a liquid reservoir and a discharge opening through which the liquid can be dispensed into a surrounding atmosphere. The protective cap has at least one ventilation opening for establishing communication between an interior and an outer surrounding area, and a sterile filter which covers the at least one ventilation opening is arranged on the protective cap in order to reduce or prevent an introduction of microbes into the interior of the protective cap via the at least one ventilation opening. | 2020-08-20 |
20200262623 | SEAL BOTTLE ASSEMBLY - A seal bottle assembly includes a bottle and a cap is removably mounted to the top opening of the bottle to seal the first room. The cap includes a radial hole defined radially therethrough. A switch unit includes a seal part located in the cap, and a control part located outside of the cap. When the control part is pushed toward the seal part, the pressure in the cap and the bottle is the same as that of outside of the bottle assembly so that the cap is removable relative to the bottle. When the control part is pulled away from the seal part and the seal part is moved to seal a communication between the first and second rooms. The pressure in the cap and the bottle is different from that of outside of the bottle assembly so that the cap is not removable relative to the bottle. | 2020-08-20 |
20200262624 | HANDLING SYSTEMS, CONTAINERS FOR FOOD AND BEVERAGE, AND CARRIERS - A handling system suitable for interaction with both a plurality of containers suitable for carrying hot and cold beverages and a plurality of carriers suitable for carrying a plurality of containers; said plurality of containers comprising a base; a walled portion upwardly extending from said base; and a lid for attachment to said walled portion; said plurality of carriers comprising at least one compartment for receiving lids and at least a second compartment for receiving containers; wherein both said carriers and said containers comprise a remotely interrogatable tag for respectively identifying said carrier and said container; wherein said system further comprises a remote processing module; and a plurality of points of interaction with said remotely interrogatable tags which provide one or more of the following factors: a date and time stamp of an interaction, an identification of the point, an identification of an individual interacting with the system and an identification of the container or carrier which interacts with said system; and a communication link for dispatching signals representative of said factors to said remote processing module. | 2020-08-20 |
20200262625 | CONTAINER WITH MULTI DEPRESSIBLE CAP PRESS TOP - A substance container has a cap that defines a cap space for an additive. The cap has a cap space opening closed by a seal which may or may not be pre-weakened, and a flexible press top having a pushing mechanism that reaches through the cap space attached on one end to the flexible top, while another end of the pushing mechanism is directed to the opening. The flexible press top has an upper side and an opposite lower side arranged such that upon depression the pushing mechanisms means hold fixed radial positions during translation to the opening, contact with the seal and push through the seal. | 2020-08-20 |
20200262626 | TAMPER-EVIDENT DEVICE - A device adapted to provide evidence of tampering. The device comprises a sleeve and an insert that is positioned within the sleeve. The insert comprises a flap that is movable between a closed position and an open position. In particular, the flap is adapted to move from a closed position to an open position when the position of the sleeve relative to the insert is changed a predetermined amount to try to open the container. As a result, an open position of the flap would readily indicate tampering to a user. A system comprising a tray adapted to receive at least one said device is also provided. | 2020-08-20 |
20200262627 | PLASTIC BOTTLE EQUIPPED WITH A TAMPERPROOF DEVICE AFTER ITS OPENING - A plastic bottle equipped with a tamperproof device after its opening comprises a neck ( | 2020-08-20 |
20200262628 | LAMINATE, PACKAGE, AND PACKAGED ARTICLE - Provided is a laminate including a base material layer, an adhesive layer having a thickness in a range of 0.1 μm to 1.0 μm, and a non-oriented sealant layer having a thickness in a range of 10 μm to 40 μm and made of a cyclic polyolefin resin, wherein one main surface of the sealant layer constitutes an outermost surface of the laminate, the other main surface of the sealant layer is bonded to the base material layer via the adhesive layer, and an adhesion strength between the base material layer and the sealant layer is 0.8 N/15 mm or more. | 2020-08-20 |
20200262629 | PACKAGING FOR POWDERED EXPLOSIVE-DETECTION TRAINING AIDS AND USES THEREOF - The present application is directed to a packaging for a powdered explosive-detection training aid which may include first and second opposing flexible sheets heat sealed together along less than a periphery thereof and defining a storage compartment therebetween, wherein an unsealed portion of the periphery defines an opening to the storage compartment, wherein at least a portion of the first opposing flexible sheet is a semipermeable material permeable to a vapor emitted from the powdered explosive-detection training aid, with the second opposing flexible sheet being impermeable to the powdered explosive-detection training aid vapor; and a sealing member, wherein the sealing member is secured to the first opposing flexible sheet and, in a closing position, covers the semipermeable portion of the first opposing flexible sheet. | 2020-08-20 |
20200262630 | SEALED PACKAGE CONTAINING A SQUEEZABLE PRODUCT - There is provided a pack ( | 2020-08-20 |
20200262631 | Package With Unique Opening Device and Method of Producing Packages - A package and a method for producing the packages are provided. The packages may comprise an enclosure configured to receive at least one product, the enclosure being sealed from the surrounding environment by two tab areas, one tab area formed at one side of the enclosure and the other tab area formed at the opposite side of the enclosure. The two tab areas are formed by selectively sealing two opposing films, each of the two tab areas comprising at least one breachable bubble configured to be breached upon application of pressure by a user, separating a sealed portion of the two films that form the surrounding tab area, allowing access to the enclosure from either or both sides of the enclosure. | 2020-08-20 |
20200262632 | POUCH WITH INTEGRATED SPOUT AND RECLOSABLE FEATURE FOR DISPENSING AND ASSOCIATED METHODS - A package and method of creating a package for dispensing a product are disclosed. The package comprises a flexible pouch comprising an elongated spout and a flowable product disposed within the pouch. A spout retainer is disposed on an exterior surface of the pouch adjacent to the spout, with opposite ends of the spout retainer attached to the exterior surface of the pouch to form two bridges, each of the bridges having a bridge width that is wider than a spout width to allow the spout to pass underneath each of the two bridges. The package may be manufactured on a vertical form-fill-seal machine where the pouch and spout retainer are formed from different supplies of film material. | 2020-08-20 |
20200262633 | Spout-Connector Assembly For Fluid Dispensing From Flexible Bags - The present invention relates to a universal fitment, method of assembling the universal fitment, and method of dispensing liquids using such universal fitment. The universal fitment of the present invention has features to engage a quick-connect-disconnect dispensing connector or a screw-on connector dispensing connector for the dispensing of liquids and semi-liquids from a collapsible bag. | 2020-08-20 |
20200262634 | Dish Dilly - Certain exemplary embodiments can provide a device that comprises a plastic bag. The plastic bag comprises a slider seal closure. The plastic bag comprises air pillows. The air pillows cushion items placed in the plastic bag from impacts. The plastic bag can comprise polyethylene. The plastic bag can be substantially optically transparent. | 2020-08-20 |
20200262635 | TOY CAP - A toy cap for a pouch is provided which comprises a closing body and a rotation structure projecting axially and terminating with a support to stand the toy cap up and impart manually to the toy cap a rotation around the main axis, so as to use the toy cap for a spinning top. | 2020-08-20 |