Abstract: A pitch trimmer assembly for an aircraft landing gear having a damping element arranged to be connected between a first and a second element of an aircraft landing gear and arranged to exert a first damping force when in a first state and a second damping force in a second state, the damping element being switchable between the first and second states in dependence on the relative positions of the first and second landing gear elements.

Abstract: Rotor assembly apparatus are disclosed. An example rotor assembly includes a twist actuator to drive a first rotation of a first shaft about a first axis, the twist actuator positioned at a center of rotation of the rotor assembly; and a first gear assembly to convert the first rotation into a plurality of second rotations of a plurality of second shafts, each of the second shafts to provide torque to a respective blade coupled to the rotor assembly.

Abstract: The present application provides a drive link for a constant-velocity joint of an aircraft rotor, the link connecting a drive hub attached to a driveshaft to a rotor yoke. The link comprises a leading bearing connected to the drive hub, a trailing bearing connected to the yoke, a central portion between the bearings, and a tension loop connecting the bearings. The tension loop is formed from a composite material and is formed as a continuous band. The tension loop transfers drive forces from the leading bearing to the trailing bearing for driving the yoke in rotation with the driveshaft.

Abstract: A vertical take-off and landing aircraft includes a propulsion mechanism that generates lift and thrust, a main frame that supports seating and a landing undercarriage, a sub-frame which supports the propulsion mechanism and is arranged so as to be swingable back and forth relative to the main frame, a motive power supply unit supported by the main frame and supplying motive power to the propulsion mechanism, a control stick connected to the sub-frame, and a main wing arranged on the propulsion mechanism, wherein the main wing is formed to be retracted to a position not interfering with an air flow of the propulsion mechanism in a normal time and to be movable to a position where lift is generated when thrust is lost. Gliding is made possible even if thrust is lost while increasing in size of a fuselage is avoided.

Abstract: This disclosure is generally directed to a High Speed vertical takeoff and landing (VTOL) aircraft that includes fixed wing flight capabilities. The High Speed VTOL aircraft may include at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a main wing, and at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a vertical wing. The rotors may be driven by electric motors. However, other power sources may be used such as combustion or hybrid engines. By adjusting the speed and/or the pitch of the rotors, the aircraft can transition from a vertical flight configuration to a horizontal flight configuration and back.

Abstract: A method includes operating an aerial vehicle in a hover-flight orientation. The aerial vehicle is connected to a tether that defines a tether sphere having a radius based on a length of the tether, and the tether is connected to a ground station. The method includes positioning the aerial vehicle at a first location that is substantially on the tether sphere. The method includes transitioning the aerial vehicle from the hover-flight orientation to a forward-flight orientation, such that the aerial vehicle moves from the tether sphere. And the method includes operating the aerial vehicle in the forward-flight orientation to ascend at an angle of ascent to a second location that is substantially on the tether sphere. The first and second locations are substantially downwind of the ground station.

Abstract: Systems and methods for the use of unmanned aerial vehicles (UAVs) in medical emergencies are disclosed herein. The systems and methods include receiving at a first UAV an indication of a medical emergency and coordinating with a second UAV based on the second UAV's capabilities. The first UAV determines if the capabilities of the second UAV complement the capabilities of the first UAV based on the indicated medical emergency. The disclosed systems and methods deploy both the first and second UAVs to the medical emergency if the capabilities of the second UAV complement those of the first UAV.

Abstract: Described are methods and apparatuses for synchronizing two or more sensors of an UAV. In the implementations described, a synchronization event is performed such that identifiable signals of the synchronization event can be collected by each sensor of the UAV. The synchronization event may be generated by a synchronization event component that generates multiple output signals (e.g., audio, visual, and physical) at approximately the same time so that different sensors can each collect and store at least one of the output signals. The collected signals are then compared and the sensors are adjusted to align the signals.

Abstract: An aviation mask is disclosed which includes a first set of sensors that monitors cockpit ambient air and health of an aircraft crew member for detecting parameters that cause respiratory disorder to the aircraft crew member an oxygen regulator that switches between a dilution mode, an emergency mode, and a recirculation mode to supply respiratory gas to the aircraft crew member, an augmented reality visor, a second set of sensors that detects a portion of a cockpit area that is viewed by the aircraft crew member, and a display computational unit that projects a prestored image associated with the portion onto the augmented reality visor which is superimposed over the portion of the cockpit area. The first set of sensors also monitors aircraft cockpit area for detecting vision obscured emergencies. The superimposed prestored image is used to identify objects in the portion during the vision obscured emergency.

Abstract: A sleeping box for installation in an aircraft comprises a casing which is suitable for accommodating a person located in a reclining position parallel to a longitudinal axis of the casing and which has an access aperture in the area of a front side which extends perpendicularly to the longitudinal axis of the casing. The sleeping box also comprises a fastening apparatus which is configured to fasten the sleeping box within a passenger cabin of the aircraft in such a way that the longitudinal axis of the casing extends perpendicularly to a longitudinal axis of the passenger cabin and the access aperture of the casing borders on an aisle which is present within the passenger cabin.

Abstract: An aircraft galley power and control system is disclosed having a plurality of electrical appliances within a monument, the galley control system including a control panel removed from the electrical appliances that include controls for operating each of the electrical appliances, The galley also includes a galley controller interface for receiving commands from a display screen on the control panel and communicating the commands to the electrical appliances.

Abstract: A door module for a vehicle lavatory that includes a bi-fold door having a first panel and a second panel each having an inner surface and an outer surface. The first and second panels are pivotably connected together by a living hinge. The living hinge includes a hinge member that extends between first and second securing members, wherein the first securing member extends along and is attached to an inner edge of the first panel and the second securing member extends along and is attached to an inner edge of the second panel.

Abstract: Described is a passenger seat that includes a seat back with a lower portion disposed adjacent to the seat bottom, and recline mechanism configured to move the passenger seat between an upright position and a reclined position. The recline mechanism may move the passenger seat in two directions. The recline mechanism may include a plurality of corresponding members configured to interface with a plurality of elongate motion members.

Abstract: A system, which includes a plurality of heat exchangers and a compressing device, is configured to prepare in parallel a medium bled from a low-pressure location of an engine and flowing through a plurality of heat exchangers into a chamber. The compressing device is in communication with the plurality of heat exchangers and regulates a pressure of the medium flowing through the plurality of heat exchangers.

Abstract: A replacement system, which includes a plurality of heat exchangers and a compressing device, is configured to prepare in parallel a medium bled from a low-pressure location of an engine and flowing through a plurality of heat exchangers into a chamber. The compressing device is in communication with the plurality of heat exchangers and regulates a pressure of the medium flowing through the plurality of heat exchangers. The replacement system employs a subsystem to treat the medium from the low-pressure location of the engine before it is received by the inerting system.

Abstract: A deicer boot includes a plurality of first elastomer fibers and a first carbon allotrope material selected from the group consisting of carbon nanotubes, graphene, graphite and carbon black. The first carbon allotrope material is aligned with one of the first elastomer fibers. The deicer boot also includes a plurality of second elastomer fibers and a second carbon allotrope material selected from the group consisting of carbon nanotubes, graphene, graphite and carbon black. The second carbon allotrope material is aligned with one of the second elastomer fibers. The second elastomer fibers are different from the first elastomer fibers.

Abstract: A deicer includes an aircraft structure and an outer layer with a sheet having a brittle point lower than ?40° C. (?40° F.). The sheet includes a polyether urethane elastomer. A deicer includes an aircraft structure and an outer elastomer layer. The outer elastomer layer includes a non-woven fabric having polyether urethane fibers and one of (1) a carbon allotrope material aligned with at least one of the polyether urethane fibers and (2) a polyester urethane composition located on a portion of the non-woven fabric. A method of forming a layer of a deicer boot includes forming a polyether urethane elastomer sheet having a brittle point lower than ?40° C. (?40° F.) and incorporating the polyether urethane elastomer sheet onto an aircraft structure.

Abstract: A deicer boot includes an aircraft structure and an outer layer. The outer layer includes a plurality of elastomer fibers and a carbon allotrope material. The carbon allotrope material is aligned with at least one elastomer fiber belonging to the plurality of elastomer fibers. A method of forming a layer of a deicer boot includes aligning a carbon allotrope material with a first elastomer fiber, joining the first elastomer fiber with a plurality of additional elastomer fibers to form a non-woven fiber fabric, and incorporating the non-woven fiber fabric into a sheet.

Abstract: A method for anti-ice performance analysis may comprise cycling a flow of heating air through an aircraft structure, measuring a temperature of the aircraft structure to generating an oscillatory signal, measuring a minimum temperature value of the oscillatory signal, and calculating anti-ice conditions of the aircraft structure based on the minimum temperature value.

Abstract: A tool to aid with pulling a closing loop cord through grommets in closing flaps on a parachute container. The cord is looped in a “U” shaped arrangement with two pulling “legs” of equal length being wrapped around a handle to provide a better grip. Only one leg of the cord can be permanently attached to the handle as the other leg must be removable for fishing through the grommets. The handle must have a diameter to permit passage through the eye of the grommet with the two legs of the cord trailing behind. With existing handles, the removable end of the cord slides off the end of the handle when passing through the grommet. An “O” ring placed on one or both ends of a radial groove in the handle holds the cord captive when passing the handle through the grommets to prevent the cord from sliding off.

Abstract: A method and an apparatus for controlling an aircraft are disclosed. The method includes: determining a horizontal velocity Vh and a vertical velocity Vv of the aircraft; acquiring, along a moving direction of the aircraft, an object having a distance that is no greater than a preset distance L away from the aircraft; predicting, according to the horizontal velocity Vh, the vertical velocity Vv, and the preset distance L, a position relationship between the aircraft and the object after the aircraft flies the preset distance L; and controlling the aircraft, by using a preset control measure, if the position relationship meets a preset relationship.

Abstract: An aircraft comprises at least first and second gas turbine engines arranged in a line extending generally normally to an aircraft longitudinal axis (A), each engine comprising at least one compressor or turbine rotor disc defining a respective rotational plane (D32-D42). The rotational plane (D32-D42) of at least one of the rotors of at least one of the engines is angled relative to the aircraft longitudinal line (A) such that a burst disc plane of the respective engine is nonintersecting with another engine.

Abstract: A method is provided of inerting one or more fuel tanks of an aircraft. The method comprises: providing a temperature value indicative of a temperature at the aircraft's destination; comparing said temperature value with a predetermined value; and on the basis of said comparison, controlling the provision of inerting gas to the one or more aircraft fuel tanks. An aircraft fuel tank inerting arrangement, a software product and an aircraft are also provided.

Abstract: An engine assembly for use as an aircraft auxiliary power unit, having internal combustion engine(s) in driving engagement with an engine shaft, a generator having a generator shaft directly engaged to the engine shaft such as to be rotatable at a same speed, a compressor having an outlet in communication with the internal combustion engine inlet, and a turbine having an inlet in communication with the internal combustion engine outlet. The turbine may be a first stage turbine, and the assembly may include a second stage turbine having an inlet in communication with the first stage turbine outlet. A method of providing electrical power to an aircraft is also discussed.

Abstract: A rotorcraft winch lighting device, which is attachable to a rotorcraft winch, mounted to a rotorcraft such as a helicopter, the rotorcraft winch including a stationary portion and a mobile portion which is movable with respect to the stationary portion, includes: a stationary unit including a stationary coil and a mobile unit. The mobile unit is movable with respect to the stationary unit and includes at least one light source, at least one electrical storage device, and at least one mobile coil, which is electrically connected to the electrical storage device and/or the at least one light source. The stationary coil and the mobile coil are configured for transferring electrical energy from the stationary unit to the mobile unit when the at least one mobile coil is positioned in an energy transfer position in the vicinity of the at least one stationary coil.

Abstract: An aircraft locating device for locating an aircraft that has crashed into a body of water. The aircraft locating device includes a housing having a base, one or more sidewalls, an upper wall, defining an interior volume, wherein at least one wall can be secured to an aircraft. The housing includes one or more openings removably covered by one or more gates that open when the housing is submerged in liquid. A plurality of buoyant objects are disposed in the interior volume of the housing, wherein the buoyant objects can be released therefrom when the gates are open, thereby leaving a visual trail in a body of water in order to allow emergency responders to identify where an aircraft may be located.

Abstract: The disclosure provides a rapid UAV launcher comprising an upper shuttle assembly and typically a plurality of rail systems. Each rail system comprises a lower shuttle assembly extending into a rail channel and translating over a rail surface. The rail channels of each rail system e generally parallel. The lower shuttle assembly of each rail system is coupled to a winch strap at a first end and an intermediary rope toward the intended direction of launch. The intermediary rope extends through the rail channel, through a brake disposed in the rail channel, around a pulley, and couples to a forward bungee connector coupled to an elastic unit. During a launch sequence, a rear mounted winch reels the winch strap to pull the lower shuttle assembly toward the winch, elongating the elastic unit, and providing individual tension forces to the lower shuttle assembly of each rail system.

Abstract: Embodiments of the present invention include systems for launching primary or secondary payloads or actuating other launch vehicle or payload or instrumentation devices. The system includes an adapter assembly and at least one sequencer mounted to the adapter assembly. The sequencer includes: controller boards, each of the controller boards having a controller for controlling deployment of the payloads and data files; output ports coupled to the controller boards and configured to transmit signals from the controller boards to dispensers therethrough, deployment mechanisms containing the payloads, the adapter assembly having channels for accommodating the dispensers; and a detector coupled to the controller boards and adapted to detect an external signal and, in response to the external signal, to send an initiation signal to the controller boards. The system also includes at least one power supply coupled to the sequencer and adapted to provide an electrical power to the sequencer.

Abstract: An inertial actuation magnetohydrodynamic wheel (2) comprising a torus-shaped fluid ring (3) filled with a conductive liquid, at least one effective area (24, 26, 28) for setting the liquid into motion, and at least one magnetohydrodynamic pump (4, 6, 8). The ratio of the set back distance of any magnetic conduction element (24, 26, 28) of the air gap of any electromagnetic pump (4, 6, 8) over the internal size of the fluid ring (3) is greater than or equal to 0.5 and the fluid ring (3) comprises at least two distinct effective areas (24, 26), for setting the conductive liquid into motion, angularly spaced apart by at least 120°.

Abstract: A habitation module with a gravity chamber that provides an artificial gravity environment. In one embodiment, the gravity chamber is annular and includes an outer cylindrical wall, an inner cylindrical structure, and opposing side walls that connect the outer cylindrical wall and the inner cylindrical structure. The gravity chamber attaches to an outer surface of a hull of the habitation module with support bearings. The support bearing includes an inner race attached to the outer surface of the hull, and an outer race attached to the gravity chamber. A drive mechanism drives the outer race of the support bearing to rotate the gravity chamber about an axis to simulate a gravitational force within the gravity chamber.

Abstract: Items may be packaged for shipping or storage using additive manufacturing techniques, also known as three dimensional (3-D) printing. Packages made by such processes may be referred to as 3-D printed packages. A packaging system may include a 3-D printer and a computing device communicatively coupled to the 3-D printer. The computing device may obtain a packaging model describing a package for one or more items. A print module of the computing device may include instructions to print the package at least partially about the item(s) according to the packaging model. The configuration of a 3-D printed package may be based at least in part on one or more other packages. A 3-D printed package may include multiple separable compartments. A unit of 3-D printed packages may include multiple separable packages.

Abstract: The present application provides an automated beverage dispenser for dispensing a beverage and ice into a cup. The automated beverage dispenser may include an ice dispensing station with an ice auger and a weight sensor, a beverage dispensing station, and a control device. The control device instructs the ice auger to fill the cup with a predetermined amount of ice and instructs the beverage dispensing station to fill the cup with a predetermined amount of the beverage in response to a weight of the cup as determined by the weight sensor.

Abstract: Various embodiments of the present disclosure are directed to a mobile strapping device for wrapping material to be packed with a strap, the device comprising: a tensioning unit for applying a strap tension to a loop of a strap, a welding unit for producing a welded connection on two superimposed regions of the strap loop, a housing with a front housing region formed as a cover for the tensioning unit and a rear housing region for receiving a rechargeable energy store, and a handle arranged between the front and the rear housing regions for holding the strapping device. The device also includes a display device arranged on the rear housing region and configured to display operating information of the strapping device.

Abstract: The invention provides a vacuum packaging method and a vacuum packaging apparatus that can sufficiently degasify the inside of a packaging bag without any trouble and in which bubbles are less likely to remain inside the packaging bag after vacuum packaging, even if a liquid is included in a packaged object.

Abstract: A flexible structure inflation device, comprising an inflation assembly configured for insertion between first and second overlapping film layers of a web of material, the inflation assembly having a fluid conduit configured directing a fluid in between the layers to inflate the web; and a cutting member held magnetically in an operative position adjacent the inflation assembly to cut the film passing over the inflation assembly.

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: The present invention discloses a biomimetic bag opening device for an automatic filling line, comprising brackets left and right symmetrically arranged on the filling line for filling bags, the symmetrically arranged brackets moving in a horizontal relative motion respectively driven by a pull rod, a push bag plate facing the filling bag provided at a front end of the bracket, a row of gripper holes provided on the push bag plate in the upper and lower of the horizontal level respectively, two rows of grippers provided on the brackets behind the push bag plate and corresponding to the two rows of gripper holes, a gripper drive device driving two rows of grippers open or closed, and grasping fingertips of the grippers projecting or retracting from two rows of the upper and lower of the gripper holes.

Abstract: A packaging method includes the steps of (a) detecting whether a height (104) of contents (105) in a container (106) exceeds a predetermined height (112), and (b) indicating how much dunnage to dispense based on predetermined criteria, including whether a detected height exceeds a predetermined height that is less than a height of the container. The indicating step includes indicating a quantity of dunnage to dispense selected from a plurality of predetermined quantities of dunnage. If no detected height is greater than the predetermined height, the indicating step includes indicating that a regular amount of dunnage should be dispensed. And if a detected height is greater than the predetermined height, the indicating step includes indicating that either zero or less than the regular amount of dunnage should be dispensed. The detecting step also can include detecting whether any contents in the container have a height above the height of the container.

Abstract: A system for individually packaging medicine is provided with a medicine inspection device that is capable of performing inspection of medicine that is individually packaged using a device for individually packaging medicine or the like. The control device of the medicine inspection device is provided with an inspection database in which images of medicine are stored as master images and is capable of carrying out an inspection task using image matching processing that involves an image acquired by imaging. The control is also capable of performing similarity determination for determining whether a medicine that is similar to a medicine that is packaged in an individual wrapper is present in the inspection database in a state in which the reference scope of the inspection database is restricted.

Abstract: An end plug to be inserted axially into the centre of an end of a roll of paper, includes a holding element adapted to hold and/or guide the end of the roll of paper in correct position in a dispenser. The end plug includes an outer sleeve having an outer end and an inner end and the holding element is connected to the sleeve by elements allowing the holding element to be axially moved from a first position to a second position, in which the holding element protrude outwardly from the outer end of the sleeve, the holding element being releasably held in the first position when moved thereto. A roll of tissue paper including such an end plug and a dispenser provided with such a roll are also disclosed.

Abstract: Label constructions and labeled containers are described which exhibit reduced label defects. The label constructions can be applied relatively soon after manufacture of the container and thereby avoid a requirement of storing containers for pre-designated dwell times. Also described are related methods of eliminating or at least reducing the occurrence of label defects by use of the label constructions and techniques of selecting the label constructions.

Abstract: A finish portion for a plastic container includes a threaded portion having at least one helical thread and a substantially flat thread positioned beneath the helical thread. The helical thread is merged into the flat thread. A transfer bead is positioned beneath the threaded portion and a gripping indentation is defined between the threaded portion and the transfer bead for facilitating automated conveyance. The gripping indentation may be shaped so that no separate ledge is defined between the threaded portion and the transfer bead. The gripping indentation may have a height that is at least about 0.085 inch. The finish portion has a maximum thread diameter and a maximum height, and a ratio of the maximum thread diameter to the maximum height may be at least about 2.3.

Abstract: A blow-molded container including a finish and a base portion. The finish defines an opening at a first end of the container that provides access to an internal volume defined by the container. The base portion is at a second end of the container opposite to the first end. The base portion includes a fold proximate to a sidewall of the container.

Abstract: A blank of sheet material for forming a container is provided. The blank includes a series of four generally rectangular panels connected along a plurality of substantially parallel fold lines. The panels include a first spaced-apart pair of panels and a second spaced-apart pair of panels. Each of the second spaced-apart pair of panels is connected to at least one panel of the first spaced-apart pair of panels. The blank also includes a corner panel extending from each side edge of each panel of the first pair of panels, and a lateral flap extending from each side edge of each panel of the second pair of panels, wherein each lateral flap has free side edges.

Abstract: A package includes an outer sleeve (60) and a lockable receptacle (50). The package has a two-part locking mechanism for locking the lockable receptacle within the outer sleeve. The package also has a release mechanism including a moveable tab (76) that may be depressed to cause the two-part locking mechanism to be unlocked as well as to case the lockable receptacle to be at least partially withdrawn from the outer sleeve. The moveable tab is oriented at a non-normal angle relative to a lateral axis (x) of the outer sleeve. The non-normal angle is defined as a first angle (?) between the lateral axis and a notional axis (C) which runs centrally of the moveable tab through the anchored portion and to a medial point (M) of the front edge.

Abstract: A multicompartment ventilated box is shaped by folding and attaching one or more blanks of a material. One or more attachment portions enable forming at least one compartment. The box may comprise an upper and a lower compartment and perforations that permit air flow between the compartments and to the exterior of the box. The compartments may be separated by a tray portion which transitions between an elevated and a collapsed position.

Abstract: A packing box has a bottom panel, end panels raised from first edges of the bottom panel, side panels arranged adjacently to the end panels, edge panels connected to side edges of the end panels via outer panel fold lines, fold-back panels arranged on inner side surfaces of the edge panels, inner panels arranged on inner side surfaces of the end panels, and reinforcing panels continuously formed with the fold-back panels via first fold lines and the inner panels via second fold lines. The reinforcing panel 16 is formed in an inwardly projecting manner between the fold-back panel and the inner panel. Any of the first and second fold lines positioned on a side closer to the outer panel fold line than a projecting top portion is arranged away from the outer panel fold line by a distance.

Abstract: A blank of sheet material is provided for forming a container convertible from a shipping configuration to a display configuration. The blank includes a glue panel, a front panel, a top panel, a rear panel, and a bottom panel coupled together in series by a plurality of generally parallel fold lines. The glue panel includes an opening mechanism and is configured to couple in face-to-face relationship to the bottom panel when the container is formed. The blank also includes a pair of top side panels extending from opposing side edges of the top panel, and a pair of bottom side panels extending from opposing side edges of the bottom panel. An edge perforation line extends along an edge between the top panel and the rear panel, and a face of each of the top panel, the bottom panel, and the pairs of side panels is devoid of perforation lines extending therethrough.

Abstract: A pull-tab sealing member for a container containing an upper laminate forming a pull-tab bonded to a lower laminate capable of being heat sealed to a container's mouth or opening. The upper laminate defines the pull tab wholly within a perimeter or circumference of the seal. The sealing member further includes a sub tab layer or member under the gripping tab for structural support.

Abstract: A corrugated pallet produced from two flat blanks is provided. The pallet may include a pallet top, a pallet bottom, and a plurality of corner straps locking the pallet top to the pallet bottom. Each of the pallet top and the pallet bottom may include folded portions, the folded portions of the pallet top interlocking with the folded portions of the pallet bottom when the pallet top and the pallet bottom are assembled to each other in nested relation. The pallet top may define a top surface of the pallet. The pallet bottom may define a bottom surface of the pallet. The corner straps may lock into one or both of the pallet top and the pallet bottom from the top or bottom surfaces of the pallet.