Abstract: A braking system may include a controller, a first wheel and a second wheel. The first wheel may be laterally displaced from the second wheel by a first distance. A first wheel speed sensor may be coupled to the first wheel and a second wheel sensor may be coupled to the second wheel. The controller may be configured to determine at least one of a slip ratio, a coefficient of friction, or a braking pressure of the second wheel in response to failure of the first wheel speed sensor. The controller may be configured to calculate a consistency value of the at least one of the slip ratio, the coefficient of friction, or the braking pressure. The controller may be configured to adjust a braking pressure of the first wheel speed sensor based upon the consistency value and the first distance.

Abstract: The invention relates to a drive system for a vehicle, comprising at least one asymmetrical rotor (18), which has at least one rotor blade (20) extending radially from a rotor axle, and a counterweight (22) which is opposite the rotor axle, the system further comprising a control device for the electric motor (24), which connects the electric motor (24) to a battery for the power supply thereof, and is configured and designed, during a revolution cycle, which includes 1-3 revolutions of the rigid rotor blade (20), to bring about at least one acceleration phase, in which the electric motor (24) can be accelerated to accelerate the rotor (18), and at least one braking phase, in which the electric motor (24) can be braked, the control device being designed, during at least part of the braking phase, to connect the electric motor (24) to at least one battery element (28) in generator mode.

Abstract: The present invention provides a power assembly, including: a motor, a fixing base and a propeller. The fixing base is sleeved over a motor rotation shaft and is fastened to a base body of the motor, and the fixing base is provided with a first clamping portion. The propeller includes a base portion and a blade extending from the base portion, and the base portion is provided with a second clamping portion clamped to the first clamping portion. The propeller is detachably connected to the motor by engaging the first clamping portion with the second clamping portion, so that the propeller can be effectively prevented from loosening from the motor during the vibration or acceleration, and is easy to disassemble/assemble and carry.

Abstract: A rotary propulsion system for a tiltrotor aircraft operable to transition between rotary and non rotary flight modes. The rotary propulsion system includes an engine coupled to a freewheeling unit. A gear system positioned between the freewheeling unit and a proprotor assembly has a torque path coupling assembly disposed between an engine side gear assembly and a rotor side gear assembly. In a disengaged position, the torque path coupling assembly interrupts the torque path between the engine and the proprotor assembly. In an engaged position, the torque path coupling assembly completes the torque path between the engine and the proprotor assembly. A hybrid power unit is configured to accelerate the engine side gear assembly to match the output rotating speed to the input rotating speed enabling the torque path coupling assembly to shift from the disengaged position to the engaged position.

Abstract: A system and method for controlling a rotor of an aircraft is disclosed. A desired rotor speed for the rotor is received and a torque command that generates the received rotor speed is calculated. A fuel adjustment signal is calculated based on the torque command and a dynamic rotor measurement of the aircraft. The fuel adjustment signal is provided to the aircraft to track the rotor speed to the desired rotor speed.

Abstract: A rotor blade coupling device for coupling to a rotor mast having a rotor head centerpiece. The coupling device has at least three rotor blade mountings mounted on the rotor head centerpiece and accommodating at least three rotor blades lying in a rotor plane, and at least one connecting element between adjacent rotor blade mountings. The rotor blade mountings can carry out pivoting motions about a pivoting axis extending vertical to the rotor plane. The at least one connecting element is a damping device, and the rotor blade coupling device has a plate-shaped transfer element, which respectively crosses a rotor blade mounting and is coupled to at least one damping device. The rotor blade coupling device has a simplified design and ensures improved damping of lead-lag motions.

Abstract: A rotor system includes a hub assembly, a first, second, and third rotor blade rotatably attached to the hub assembly, a first, second, and third damper pivotally attached to the hub assembly and pivotally attached to the first, second, and third rotor blade, respectively, and a control system operably associated with the first, second, and third damper. A method to control vibratory forces exerted on the hub assembly via the first and second rotor blade includes separately controlling a dynamic spring rate of each of the first and second dampers with the control system.

Abstract: A flying machine includes: a flying machine body that includes a rotor blade; a protective member that forms a frame shape inside which the rotor blade is disposed, that is rotatably fixed to both end portions of the flying machine body, and that is pipe shaped; and a connecting wire that passes through an inner portion of the protective member to connect the flying machine body and an external device together.

Abstract: A drone capture aerial vehicle includes a fuselage and a drone capture device. The drone capture device includes a middle post and a plurality of foldable frame arms; the middle post includes a first end and a second end; and each foldable frame arm includes a plurality of ribs and a plurality of links. A method of capturing a drone includes providing a drone capture aerial vehicle, the drone capture aerial vehicle having a drone capture device and the drone capture device having a foldable capture net; flying the drone capture aerial vehicle toward the drone; activating the drone capture device to deploy the foldable capture net; and capturing the drone with the capture net.

Abstract: Components of a device may transmit signals between one another using piezo electric transducers (PETs). In a basic system, a first PET may be coupled to and/or in contact with a first location on a member. A second PET may be coupled to and/or in contact with a second location on the member and separated from the first PET by a distance. The first PET may receive a signal (e.g., an electrical voltage) and convert the signal to a mechanical force/stress causing vibration of the member. The vibration may propagate through the member to other locations about the member. The second PET receive the vibration and may convert the vibration back to the signal, such as by converting mechanical force/stress to the electrical voltage (i.e., the signal). A similar process may be performed in reverse to enable the first and second PET to provide two-way communication.

Abstract: A method is provided. An unmanned aerial vehicle (UAV) can be operated in an autonomous mode, performing course corrections from sensor data using an object detection processor and a decision processor. The UAV can then enter a hover mode if an override condition is present and enter a remote-control mode once the UAV is in the hover mode. In the remote-control mode, flight control commands can be received via the cellular module so as to position the UAV in response to the flight control command.

Abstract: Aspects described herein relate to an apparatus, system, and method for the airborne launch of inflatable, lighter-than-air devices from aircraft. In some instances, a container comprising a drag parachute and a main parachute assembly may be deployed from an aircraft. Drag forces on the container may cause the drag parachute to be expelled from the container. Drag forces on the drag parachute may cause the main parachute assembly to be expelled from the container. The main parachute assembly may include a canopy with an opening and a release channel connecting the opening with the container. The container may further include a balloon inflation mechanism, which may be used to inflate one or more balloon envelopes. The one or more balloon envelopes, after being inflated, may be configured to be released from the container, traverse the release channel, and exit the main parachute assembly through the opening.

Abstract: A power control arrangement for an aircraft galley including a power control unit and an interface unit. A power input of the power control unit includes a main switch and connects to a power feed. Each of a power outlets of the power control unit includes an outlet switch and connects to a galley insert. A main switch interface on the interface unit is provided for switching of the main switch. Each outlet switch interface of the interface unit is associated with one of the outlet switches for switching the outlet switch. The interface unit is arranged remote from the power control unit and the switch interfaces are connected to the corresponding switch via an electrical, radio or optical connection for controlling switching of the switches. Further, an aircraft galley and an aircraft are disclosed.

Abstract: Vertical take-off and landing (VTOL) aircraft can provide opportunities to incorporate aerial transportation into transportation networks for cities and metropolitan areas. However, VTOL aircraft can be sensitive to uneven weight distributions, e.g., the payload of an aircraft is primarily loaded in the front, back, left, or right. When the aircraft is loaded unevenly, the center of mass of the aircraft may shift substantially enough to negatively impact performance of the aircraft. Thus, in turn, there is an opportunity that the VTOL may be loaded unevenly if seating and/or luggage placement is not coordinated. Among other advantages, dynamically assigning the VTOL aircraft payloads can increase VTOL safety by ensuring the VTOL aircraft is loaded evenly and meets all weight requirements; can increase transportation efficiency by increasing rider throughput; and can increase the availability of the VTOL services to all potential riders.

Abstract: A system including a base provided with the means in the form of clamping and locking jaws for clamping and locking of the system into position in the rail, the means in the form of clamping jaws being movable between a first position and a second position by making use of maneuvering means that are operable by an operator between an unlocking position and a locking position, wherein the maneuvering means includes a clamping screw engaged in a hole and adapted so as to cooperate with a threaded hole and in that it has a smooth section in order to allow the screwing thereof into the threaded hole only when the base and the means in the form of clamping jaws are in the correct position of fastening in the rail.

Abstract: A system comprises a heat source. The system also comprises a bladder comprising opposing thin-walled sheets and a fluid flow conduit defined between the opposing thin-walled sheets. The fluid flow conduit comprises an inlet and an outlet. The system further comprises a first fluid line coupled to the heat source and the inlet of the bladder. The system additionally comprises a second fluid line coupled to the heat source and the outlet of the bladder. The system also comprises fluid flowable through the first fluid line from the heat source to the inlet, from the inlet through the fluid flow conduit to the outlet, and through the second fluid line from the outlet to the heat source.

Abstract: An example hybrid aircraft propulsion system includes a plurality of power units configured to output electrical energy onto one or more electrical busses; one or more propulsors; and one or more electrical machines, each respective electrical machine configured to drive a respective propulsor of the one or more propulsors using electrical energy received from at least one of the one or more electrical busses.

Abstract: An assembly is provided for an aircraft propulsion system. The assembly includes a tubular inner housing, a tubular outer housing and a bifurcation. The bifurcation includes a leading edge structure structurally connected to the inner housing and the outer housing.

Abstract: A rear engine attachment includes a beam attached to the reactor strut, a rudder mounted by a pivot connection on the beam about a main rotational axis, and two thrust rods each exhibiting a first end attached to the rudder and a second end attached to a front section of an engine, the two thrust rods and the rudder attached to the beam together defining a primary thrust path between the engine and the reactor strut to bear the engine thrust. For each thrust rod, the rear engine attachment exhibits a waiting fail-safe system activated in the event of a failure of the primary thrust path. The rear engine attachment includes, for each thrust rod, a break detector integral with the rudder which is provided to come into contact with the beam in the event of a failure of the primary thrust path. The attachment allows a quick inspection to be made to determine whether there has been a failure of the primary thrust path.

Abstract: An optical foreign object detection (FOD) system for a gas turbine engine includes a multiple of emitters arranged about an inner periphery of a fan cowl, a multiple or receivers arranged about the inner periphery of the fan cowl, each of the multiple of receivers receiving a beam from one of the multiple of emitters to form a beam matrix; and a control system in communication with the multiple of emitters and the multiple of receivers, the control system operable to detect a minimum sized object in response to breaking at least one beam of the beam matrix.

Abstract: In an example, method of controlling thrust produced by a plurality of engines on an aircraft for assisting with nose-down recovery of the aircraft is described. The method includes selecting a maximum value of an aircraft parameter, measuring a value of the aircraft parameter while the aircraft is in flight, based on a comparison of the maximum value and the measured value determining that the measured value exceeds the maximum value, and reducing a thrust produced by each of the engines of the plurality of engines to bring the measured value of the aircraft parameter below the maximum value of the aircraft parameter.

Abstract: A propulsion system for an aircraft includes at least one gas turbine engine, an electric auxiliary fan driving motor configured to selectively receive electric power input from one or more electric power sources, and at least one auxiliary propulsion fan configured to selectively receive a motive force from either or both of the at least one gas turbine engine and the electric auxiliary fan driving motor. The propulsion system also includes a controller configured to establish a plurality of takeoff thrust settings of the at least one gas turbine engine and the electric auxiliary fan driving motor such that a minimum total aircraft thrust required for takeoff of the aircraft is produced.

Abstract: An aircraft electrical system includes a controller system having a self-testing system configured to test an operability of a transient voltage suppression device. A single line communication bus is connected to a communications output of the controller. A first lightning protection device including the transient voltage suppression device is configured to protect the controller from transient voltages. An enable/disable circuit comprising a normally closed switch connects a low side of the lightning protection device to a neutral.

Abstract: A method and apparatus for strong bonded wide joints for cryogenic applications. In one advantageous embodiment, an apparatus may comprise a three-dimensional preform and a plastic matrix. The plastic matrix may be impregnated in the three-dimensional preform to form a softening strip that may be capable of remaining flexible at a temperature at which a gas may have a liquid form.

Abstract: A controller arrangement includes a controller, an actuator, and a measuring element. The measuring element captures a control variable with a predetermined sampling rate in consecutive sampling cycles and transmits it to the controller. The controller compares the control variable with a predetermined reference variable and determines how the control variable differs from the reference variable. The controller, in a first cycle, starts with a predetermined regulating variable and outputs it to the actuator, and subsequently determines how the control variable differs from the reference variable; in a second cycle, the controller varies the regulating variable based on the difference of the control variable from the reference variable in the first cycle, and outputs it to the actuator, and subsequently determines how the control variable differs from the reference variable; in a third cycle, the controller varies the regulating variable and outputs it to the actuator.

Abstract: Shown and described is a device for the drying of packaging, in particular composite packaging for foodstuffs, including: a conveyor belt with cells for receiving the packaging, and at least one drying facility for drying the packaging. In order to achieve particularly efficient drying of the packaging, it is envisaged that the drying facility has at least one contact element with at least one contact surface. Also shown and described are the use of such a device for the drying of packaging filled with foodstuffs, method for drying packaging, and a packaging for foodstuffs.

Abstract: A system for loading an accumulated article group into a case is provided. The system includes an article accumulation station, a grouped article loading station, and a pusher assembly. The accumulation station includes an article receiver assembly in furtherance of delimiting an accumulated article group, and a grouped article guide structure within which the accumulated article group is positionable by operation of the article receiver assembly. The grouped article loading station includes a gate assembly, having first and second operable configurations, and an actuatable gate through which the accumulated article group passes during loading of the group into a case presented for receipt of same.

Abstract: An ejection head for an ejection device of a sealing machine for sealing a container includes a supporting element with a supporting axis and a sliding end, and a sliding element for sliding the supporting element along a sliding profile of the sealing machine. The sliding element is arranged at the sliding end and a force acting essentially in the direction of the supporting axis is capable of being transmitted via the sliding element to the supporting element. So that the sliding element and the sliding profile are subject to reduced wear, the sliding element is a rotatable rolling element, so that in the operating state the supporting element is capable of being unrolled over the rotatable rolling element along the sliding profile.

Abstract: A machine and a method for forming a two-compartment pouch having a lower compartment and an upper compartment The method includes the steps of drawing a film over a pair of fill tubes; sealing side edges of the film to form a sleeve; forming a bottom seal on the sleeve; pulling the sleeve downwardly; filling a bottom portion of the pouch using one of the fill tubes; forming a second seal over the filled bottom portion; filling an upper portion of the pouch using the other fill tube; and sealing the upper portion.

Abstract: The present invention relates to a device and a method for decanting a beverage initially contained in one or more closed bottles into smaller containers. The device comprises an enclosure under an inert atmosphere, provided with an inlet port comprising receiving means, into which inlet port the neck of the bottles is fitted, and an outlet port through which the hermetically sealed containers are evacuated. The device contains an opening station for opening the bottles fitted into the receiving means, a collection vessel that collects the liquid flowing out of the bottles, a filling station for filling the containers from the collection vessel, and a sealing station for hermetically sealing the containers. In the method, the steps of opening and emptying the bottles, and of filling and hermetically sealing the containers, are all carried out under an inert atmosphere.

Abstract: A unit for mixing and dispensing an aerosol precursor composition, and containers to be dispensed therefrom. The unit includes a plurality of bulk material filling stations, the plurality of bulk material filling stations have at least one first filling station with aerosol former and at least one second filling station with a flavor material for creating the aerosol precursor. The unit also includes a bulk consumable pack staging a plurality of containers configured to receive the aerosol precursor, and a robot configured to retrieve a container from the bulk consumable pack and move the container through at least two dimensions to stop at least two of the plurality of bulk material filling stations.

Abstract: A convertible shipping container for goods includes a tray portion that includes a first wall. The first wall is configured to be oriented as a front wall of the convertible shipping container in a first display configuration and as a bottom wall of the convertible shipping container in a second display configuration. The convertible shipping container also includes a cover portion removably coupled to the tray portion such that the cover portion is coupled to the tray portion in the first display configuration and is detachable from the tray portion to form the second display configuration.

Abstract: A vertical form fill and seal apparatus, for packaging particulates, includes a package sealing assembly that has opposed sealing jaws operatively coupled to each other by mechanical connection at a common pivot point. A first jaw actuator is mechanically coupled to the opposed sealing jaws to pivot the jaws in a controlled manner about the common pivot point. A second actuator is mechanically coupled to the package sealing assembly and is configured to impart controlled reciprocating motion to the package sealing assembly. A controller is configured to control the first actuator and to control the second actuator thereby causing the jaws to describe a preset locus of travel, allowing flexibility of type of bag being made without change-out of jaws. The packaging film may move continuously, or may optionally be controlled to move intermittently through the VFFS.

Abstract: An automated sandwich wrapping system is disclosed herein. In some embodiments, an automated sandwich wrapping system includes a folding subassembly having a plurality of folding plates to inwardly fold side portions of sandwich wrapping paper extending past ends of a sandwich, a roller subassembly having at least one roller to rotate the sandwich to wrap the sandwich, and a controller preprogrammed to control and coordinate operation of the folding subassembly and the roller subassembly. The folding plates move between an idle position and an active position.

Abstract: An apparatus for attaching a label to a moving cable, the apparatus comprising: a roller for pressing a label against the moving cable, wherein the label has a first attaching edge and a second attaching edge and wherein the roller comprises: a first roller for pressing the label against the moving cable, wherein the label is pressed against the moving cable with the first attaching edge and the second attaching edge of the label on opposites sides of the moving cable; a first roll down roller for folding the second edge of the label against the moving cable; and a second roll down roller for folding the first edge of the label against the moving cable.

Abstract: A plastic container includes a neck portion, a sidewall portion, and a base portion. The neck portion includes a plurality of threads, which may be configured to retain and/or secure a cap or lid. In embodiments, the threads may be blown and/or the neck portion may include a neck rib provided vertically above the threads.

Abstract: The embodiments disclose a tray method and devices including a method including creating a half-cylindrical tray with anti-slide features on an interior surface and a flexible pull tab at one end of the half-cylindrical tray, forming a child proof bottle with child proof bottle security tabs wherein the tray can be inserted, forming a child proof cap with child proof cap security tabs corresponding to the child proof bottle security tabs for securing the child proof cap to the child proof bottle, and wherein storing gelatin edible wafers in the tray includes gelatin edible candies and gelatin wafer products with infused medicinal ingredients.

Abstract: A twin-sheet, thermoformed pallet is configured with a bottom-opening recess shaped to receive and hold in place a signal transmitting device. The recess has undercuts that allow the device to be snapped in and held against the floor of the recess and well above the bottom surface of the pallet body. The recess is provided with access for a tool to pry the device out for replacement or servicing.

Abstract: A storage device includes a base, and a number of side panels selectively coupled to the base. Each of the side panels include a protrusion. The base includes a number of voids defined therein. The protrusions, once inserted into the voids, restrict movement of the side panels relative to the base in at least two coordinate directions.

Abstract: A nestable crate includes a base, a pair of opposed side walls extending upward from the base, and a pair of opposed end walls extending upward from the base. The side walls and end walls include an upper band portion and a lower portion connecting the base to the upper band portion. A center structure extends from one of the end walls to the other of the end walls. The center structure includes a plurality of center column portions extending down to the base. The center structure further includes an upper handle portion partially defining a handle opening therebelow. The upper handle portion includes spaced-apart handle side walls defining openings upward of the crate.

Abstract: A display container (200) includes one or more sidewalls (102,103,107) defining a receiving recess (207). A dispenser (201) can define a front side of the display container. Where this is the case the dispenser has a height (208) less than the one or more sidewalls. The dispenser includes an aperture (324). A plurality of sample product, such as disposable gloves (210) can be placed within the dispenser. One or more packages (203,204,205,206) of product corresponding to the sample product can be situated within the receiving recess.

Abstract: A beverage container including a main body, a cover and a sucking unit is provided. The main body includes an interior space for containing a beverage and a top wall having an inner rim which defines an opening communicated with the interior space. The cover removably seals the opening. The sucking unit is mounted within the main body adjacent to the opening and includes a partition wall extending into the interior space to define a channel which fluidly communicates the opening with the interior space. The sucking unit is configured to enable a person to suck up the beverage contained in the interior space through the channel and the opening after removal of the cover.

Abstract: A modular interchangeable vessel system is disclosed, which comprises a flexible and flat-foldable waterproof vessel having a sealed end and an unsealed end disposed distal from the sealed end, the unsealed end having a kayak shaped endpiece sealingly coupled thereto.

Abstract: Disclosed is a flexible packaging container, in particular a plastic film pouch or bag for bulk goods, comprising a front wall (2) and a rear wall (3) as well as a holding space (15) between said walls (2, 3) for goods to be stored; the walls (2, 3) are made at least in part of a film material; the flexible packaging container further comprising an intermediate space (14) which is formed by an inner ply (4) and is separated from the holding space (15) by said inner ply (4); the holding space (15) can be evacuated into the intermediate space (14) via at least one holding space evacuation hole (7) in the inner ply (4), and the intermediate space (14) can be evacuated out of the packaging container (1) via at least one additional evacuation hole (11) that interrupts a transverse seam; the front wall (2) does not comprise any of the longitudinal seam (12) that seals the packaging container (1) in the peripheral direction; the inner ply (4) is formed by a strip (4) which is located on a side of the front wall (2)

Abstract: Flexible packaging (1) of the bag type for loosely packaged perishable food products, comprising: a front wall (2) and a rear wall (3) situated opposite each other, defining on the upper part a closing fin (4) and laterally connected together by two gusset walls (5); and a reclosing device comprising a first planar portion (12) and a second planar portion (13) fixed to the front wall (2) and to the rear wall (3) respectively and equipped with means (7; 8) for mutual connection in an overlapped configuration; wherein, in a shelf configuration, said package (1) has the closing fin (4) folded over on top of said rear wall (3), the first planar portion (12) and the second planar portion (13) of the reclosing device being arranged side-by-side and integrated in a planar insert (10) which can be broken along a separation line (1) between said first portion (12) and said second portion (13).

Abstract: A reclosable plastic zipper assembly, method of mounting and method of manufacturing of such, wherein the assembly has a ribbon with a first zipper strip profile and a second zipper strip profile, the first zipper strip profile includes at least one rib, and where the second zipper strip profile includes at least one recess, with the at least one rib and the at least one recess having complementary mating shapes for mating along the length of the plastic zipper assembly, the reclosable plastic zipper assembly also having a bead and a pair of perforations and the zipper strip profiles being capable of mating by folding the ribbon along the length of the plastic zipper assembly around the bead, and having a first perforation on the ribbon between the bead and the first zipper profile and a second perforation on the ribbon between the bead and second zipper profile.

Abstract: The present invention relates to a tank cap including a lever member that is constrained from moving to the standing position contrary to the intention of the operator. The tank cap comprises a slide member disposed in the cap body so as to be adjacent to the lever member, and provided with a cam contact portion that is to come into contact with a cam portion of the lever member, and a coil spring disposed between the slide member and the bottom of the cap body. The resilience of the coil spring causes the cam contact portion to press the cam portion and retains the retracted position.

Abstract: A tamper evident food container is provided. The container comprises a base hingedly connected to a lid. The lid includes an outer raised portion having an integrally connected inner recessed portion formed therein, wherein the inner recessed portion includes a peelable flap portion partially detachable from the inner recessed portion for lifting the peelable flap upwardly from the inner recessed portion; an upper flange extending perpendicularly outward from a perimeter of the lid and having a connecting member located between extending latching portions extending outwardly from the upper flange and adapted for being received in the two latch receiving openings; and a tab connected to the peelable flap portion on a first end and detachably connected to the connecting member on a second end, where the tab is configured for pushing inward to detach the second end from the connecting member allowing the peelable flap portion to be lifted upwardly.

Abstract: A pourer includes a pour spout, wherein the pour spout is configured to serve as a spout for a content liquid stored in a container main body, and is configured to be attached to a mouth part of the container main body, wherein the pour spout includes a surplus resin part provided on a part of a top surface of the pour spout through which the content liquid passes, and wherein the surplus resin part protrudes outwardly in the radial direction from an outer peripheral edge of the top surface of the pour spout.

Abstract: A cap for a variable pour flow device is configured to close an opening of a container holding a liquid when assembled with the container. The cap includes a spout in communication with an interior of the container when the cap is assembled with the container. The cap is further configured to provide a first fluid flow in which fluid flows through a first passage and the spout when the container with the cap assembled thereto is tilted from an upright position toward the spout to an intermediate degree. The cap is also configured to provide a second, greater fluid flow in which fluid flows through the first passage, a larger second passage, which is spaced from the first passage, and the spout when the container with the cap assembled thereto is tilted further toward the spout from the intermediate degree.