Abstract: An aircraft wing including a wingbox with an upper cover, a lower cover, a forward spar and a rear spar. A leading edge of a trailing edge panel is attached to the wingbox. A support structure is attached to the wingbox. A kinked link includes a first arm, a second arm, and a corner where the first and second arms meet. The first arm of the kinked link is pivotally attached to the trailing edge panel at a first pivot joint, and the second arm of the kinked link is pivotally attached to the support structure at a second pivot joint.

Abstract: A wing assembly for an aircraft is disclosed having a wing and a wing tip device at the tip of the wing, wherein the wing tip device is moveable between a flight configuration and a ground configuration. The wing has a spar extension which extends spanwise away from a distal end of the wing, the spar extension having a first end portion fixed in the wing and a second end portion which, in the flight configuration, is disposed in the wing tip device such that, in the flight configuration, the spar extension transmits flight loads between the wing tip device and flight-load bearing structure in the wing. The wing assembly may have an actuation assembly to move the wing tip device.

Abstract: A fact checking system utilizes social networking information and analyzes and determines the factual accuracy of information and/or characterizes the information by comparing the information with source information. The social networking fact checking system automatically monitors information, processes the information, fact checks the information and/or provides a status of the information, including automatically modifying a web page to include the fact check results. The fact checking system is able to be implemented utilizing a drone device. The drone device is able to be implemented in conjunction with a security system.

Abstract: A tool positioning system of an unmanned aerial vehicle that is mountable relative to a power line to monitor a component of the line. The tool positioning system includes a displacement module having a first member mountable to one side of a body of the unmanned aerial vehicle, a second member movable vertically relative to the first member on the side of the body, and a tool holder pivotably coupled to the second member and couplable to a tool. The tool holder is movable relative to the body to mount the tool to or around the component.

Abstract: Described herein are systems and methods for structure scan using an unmanned aerial vehicle. For example, some methods include accessing a three-dimensional map of a structure; generating facets based on the three-dimensional map, wherein the facets are respectively a polygon on a plane in three-dimensional space that is fit to a subset of the points in the three-dimensional map; generating a scan plan based on the facets, wherein the scan plan includes a sequence of poses for an unmanned aerial vehicle to assume to enable capture, using image sensors of the unmanned aerial vehicle, of images of the structure; causing the unmanned aerial vehicle to fly to assume a pose corresponding to one of the sequence of poses of the scan plan; and capturing one or more images of the structure from the pose.

Abstract: An unmanned aerial vehicle according to the present invention may comprise: a rotor-blade for providing thrust according to generation of main stream; and a safety guard disposed to surround the rotor-blade. The safety guard may comprise: a guide member which is disposed coaxially with the rotor-blade while having a gap between the guard member and the end of the rotor-blade, so as to stabilize, when the rotor-blade rotates, a flow field suctioned by a negative pressure, and stably boost a discharge flow when the pressure is changed to a positive pressure; and a diffuser which is disposed coaxially with and radially spaced apart from the guide member, and generates a secondary flow toward the main stream to increase a flow rate.

Abstract: Underwing-mounted trailing edge flaps for wings of aircraft are disclosed. A flap pivotally coupled to the wing is movable between a stowed position located along a lower surface of the wing and a deployed position located rearward of a trailing edge of the wing. The flap includes a first edge, a second edge located opposite the first edge, a first surface extending between the first edge and the second edge, and a second surface located opposite the first surface and extending between the first edge and the second edge. The first edge is located rearward of the second edge when the flap is in the stowed position, and forward of the second edge when the flap is in the deployed position. A bullnose pivotally coupled to the flap at a location along the first edge pivots relative to the flap as the flap moves between the stowed and deployed positions.

Abstract: An unmanned aerial vehicle for application of an active ingredient to agricultural crops is configured to hold: a liquid comprising the active ingredient in at least one liquid reservoir housed within or attached to the unmanned aerial vehicle. At least one liquid application unit is housed within or attached to the unmanned aerial vehicle and in fluid communication with the at least one liquid reservoir. The housing of at least one sensor unit which is configured to determine sense information comprising sensing a functioning of one or more of: the at least one liquid reservoir, the at least one liquid application unit, the at least one operating unit. A processing unit determines an instruction to the unmanned aerial vehicle to dock with a base station and get a service from the base station. This determination step comprises utilization of sense information.

Abstract: An aircraft air conditioning device provided in an aircraft includes: a plurality of base units each of which is provided with two electric compressors connected in series to an air flow path; a temperature controller which is configured to adjust a temperature of air discharged from a compressor of the two electric compressors; and a control device which is configured to control the plurality of base units and the temperature controller and each of the plurality of base units is configured to supply compressed air discharged from the temperature controller to an air-conditioned space as conditioned air.

Abstract: An environmental control system of an aircraft including a plurality of inlets for receiving a plurality of mediums including a first medium, a second medium, and a third medium and an outlet for delivering a conditioned flow of the second medium to one or more loads of the aircraft. The environmental control system additionally includes a first compressing device and a second compressing device. The second compressing device is arranged in fluid communication with the first compressing device and the outlet. An inlet of the second compressing device is directly connected to an outlet of the first compressing device, and the first compressing device is driven by energy extracted from the first medium. The first medium is a flow of bleed air.

Abstract: Examples described herein provide a computer-implemented method that includes receiving static data about an aircraft. The method further includes receiving dynamic data about flight conditions for a flight of the aircraft. The method further includes determining, based on the static data and the dynamic data, an amount of air pressure and a volumetric air flow to apply from an electric pump to a deicing device. The method further includes controlling the electric pump to cause the electric pump to apply the amount of air pressure and the volumetric air flow to the deicing device.

Abstract: An emergency vision system includes a housing; an inflatable main enclosure having an inflated state and a deflated state, the main enclosure in the deflated state is disposed in the housing, the main enclosure in the inflated state is configured to be stationarily disposed between a user and a source of information required to be seen by the user during a smoke emergency; and a movable hand-held enclosure having an inflated state and a deflated state, the hand-held enclosure in the deflated state is disposed in the housing, the hand-held enclosure in the inflated state is configured to be used by the user to view a second source of information not visible through the main inflatable enclosure.

Abstract: An electric architecture for a twin-engined, hybrid thermal/electric propulsion aircraft and, for each turboshaft which includes a high-voltage DC propulsive electric distribution network, a non-propulsive electric distribution network which is connected to loads of the aircraft, and an electric distribution network which is connected to loads of an electrified control system of the turboshaft engine, and wherein power supply sources are shared for these different networks.

Abstract: A fuel pipe assembly is disclosed including a connector having a socket and a lug arrangement extending from the socket, a pipe having a first end portion adapted to fit within the socket, and a retainer having first and second parts which together form a collar configured to retain a pipe. The retainer has an open condition in which a pipe is insertable, and a closed condition. The retainer also has a channel arranged, in the closed condition, to capture the lug arrangement.

Abstract: A fastening system for an aircraft configured to fasten at least one tank intended to contain liquid hydrogen includes a longitudinal box, an upper structure fastened to an upper side of the longitudinal box, a lower structure fastened to a lower side of the longitudinal box and at least two fastening frames including, on either side of the vertical plane of symmetry (P1), a fastening device for connecting a tank to the upper structure. The fastening system further includes at least two fastening devices for connecting a fastening point of the tank to the longitudinal box and at least two fastening devices for connecting a fastening point of the tank to the lower structure. The fastening system makes it possible to securely fasten at least one hydrogen tank on board an aircraft (AC).

Abstract: A method for air separation module management includes determining an amount of nitrogen-enriched-air to be supplied to each fuel tank of a plurality of fuel tanks of an aircraft. The method also includes evaluating a status and usage of each air separation module of a plurality of air separation modules onboard the aircraft. The method additionally includes determining an optimal distribution of workload among the plurality of air separation modules based on the amount of the nitrogen-enriched-air to be supplied to each fuel tank and the status and usage of each air separation module. The method further includes regulating a valve associated with each air separation module or a group of air separation modules based on the optimal distribution of workload to each air separation module.

Abstract: A fuel tank protection system having an outer wall for a fuel tank, an inner wall for the fuel tank, a gap between the inner wall and outer wall, and an intumescent material located within the gap between the inner wall and the outer wall.

Abstract: Refueling devices for use in in-flight refueling operation are provided, including a body configured for being towed by a tanker aircraft and having a boom member that has a fuel delivery nozzle, a spatial control system and a longitudinal control system. The longitudinal displacement control system includes at least one panel element defining a front panel projected area orthogonal to a body longitudinal axis, each panel element being controllably and reversibly deployable incrementally to each one of a plurality of successive deployed positions between a fully retracted position and a fully deployed position, to provide a respective reversible incrementally increasing aft force to the refueling device at least during the in-flight refueling operation.

Abstract: A satellite refueling system has a refueling satellite carrying fuel, a fuel hose connected to the fuel carried by the refueling satellite, with a maneuverable end effector at a deployed end of the fuel hose, the end effector comprising a fuel supply nozzle connected to the fuel hose, a plurality of thrusters on the end effector providing thrust in a plurality of directions, an imaging device on the end effector capturing images in an immediate environment of the end effector, and computerized circuitry operating individual ones of the plurality of thrusters in response to the images captured by the imaging device. The refueling satellite deploys the fuel hose, and the computerized circuitry operates the thrusters to maneuver the end effector, bringing the fuel supply nozzle to a location to deliver fuel.

Abstract: An engine inlet cover and a method for covering an engine inlet are provided. A method for covering an engine inlet includes providing a collapsible cover comprising a connection pin defining an axis; a frame including interconnected arms; and a web. Further, the method includes storing the collapsible cover in a stowed configuration in which the arms are aligned. Also, the method includes rotating the arms from the stowed configuration to an operating configuration in which the arms are radially spaced about the axis, enclosing the frame in the operating configuration with the web to define an interior volume, and placing the cover over the engine inlet.

Abstract: Wing panels having composite wing skins and stringers are produced on a moving production line. The wing panels are formed on mandrels that move through workstations along the production line where laminators layup the wing skins and pick-and-place machines place stringers on the wing skins that are supplied by stringer feeder lines.

Abstract: A method is specified for producing a structural component, in particular for an aircraft, ground vehicle, or watercraft, or for a rotor blade of a wind turbine, in which method an arrangement of fibers and plastic material is laid in a mold and subjected to an increased pressure and an increased temperature, wherein a mold is used which comprises at least one recess in which a reinforcing element is arranged. The object is to be able to cost-effectively produce a structural component of this type. For this purpose, it is provided that the reinforcing element is laid in the recess together with a core, wherein a differential volume between the recess and core, at least in a predetermined region, is chosen such that it is smaller than a segment of the reinforcing element arranged in said region by a predetermined amount.

Abstract: A tail boom support stand assembly for a tail boom of a helicopter includes a forward structure including a forward telescopic support assembly; a webbing arrangement mounted between a first and second boom support of the forward telescopic support assembly to provide a non-rigid cradle for the tail boom; an aft structure comprising an aft telescopic support assembly; a boom support channel of the aft telescopic support assembly to provide a rigid cradle for the tail boom; and a frame structure that interconnects the forward structure and the aft structure.

Abstract: A representative system includes an alignment tool for aligning attachment interfaces of horizontally-oriented launch vehicle portions. The tool can include a receiver assembly for connecting to a first launch vehicle portion and an actuation assembly for connecting to a second launch vehicle portion. When a first connecting element of the receiver assembly is engaged with a second connecting element of the actuation assembly, the second connecting element can apply force to the receiver assembly, and the actuator assembly applies an opposite force to the second launch vehicle portion, to align fastening features in the launch vehicle portions and/or to reshape the launch vehicle portions. A representative method includes connecting the alignment tool to the launch vehicle portions and operating the tool to apply oppositely-directed forces to align the launch vehicle portions for installing fasteners to connect the launch vehicle portions. One or more bracing beams can connect two tools together.

Abstract: A system monitors the health of a helicopter, and includes a device for determining a change of state of the engine and is configured to collect data measured by engine and external conditions sensors during a stable flight phase and to process the measured data.

Abstract: A service satellite having a body, a controller and a docking unit including a telescopic arm, mounted on a 6-DOF parallel manipulator, and two additional gripping arms. The telescopic arm, deployed from the 6-DOF manipulator, is equipped with a pair of rapid closure digits. The telescopic arm facilitates capturing the launch adaptor ring of a client spacecraft, even during tumbling. The 6-DOF parallel manipulator has force sensors and can accommodate post capturing relative motion through active compliance control and controlled de-tumbling, for avoiding generation of high forces in the telescopic arm. After relative rate annihilation, the telescopic arm retracts and the client ring is secured to the 6-DOF manipulator with the help of a pair of clamps. After the ring is secured, two additional gripping arms secure a rigid connection with the launcher ring so that the docking connection comprises three equally spaced connections.

Abstract: Satellite systems and methods to perform rendezvous and docking between a servicer satellite and an on-orbit satellite, and specifically to satellite systems and methods to perform rendezvous and docking between a servicer satellite and an on-orbit client satellite using electric propulsion thrusters. In one aspect, a servicer satellite with a set of thruster arms each attached to an electric propulsion thruster performs acceleration, deceleration, and steering maneuvers through six degree of freedom positioning of the thrusters, the same set of thruster arms and thrusters performing station keeping of the docked servicer-client satellite system.

Abstract: An engine device for an unmanned flying apparatus that provides good weight balance for the flying apparatus; cancels the gyroscopic effect; and has auto rotating propellers. The engine device includes a first cylinder and a second cylinder arranged horizontally and opposed to each other, and pistons within the cylinders advance and retract in opposite directions to each other; a first crankshaft and a second crankshaft arranged in the vertical direction, driven by the first cylinder and the second cylinder, respectively, and rotate in opposite directions; a first centrifugal clutch and a second centrifugal clutch rotate in opposite directions to each other; a final drive shaft transmitting rotational force to a gear mechanism comprising orthogonal transform gears, to rotate a propeller shaft; a one-way clutch arranged between the first crankshaft, the second crankshaft and the final drive shaft, and driven by both the first crankshaft and the second crankshaft.

Abstract: A flying object 20 is provided with a rotor blade 200 that generates lift and thrust by rotating and a rotating electrical machine unit that rotates the rotor blade 200. The rotor blade 200 receive wind power and rotate when not flying. The rotating electrical machine unit generates electric power based on a power that rotates the rotor blades 200 when not flying. In addition, the flying object 20 may be provided with a power storage device 230 that stores electric power generated by the rotating electrical machine unit. In addition, the flying object 20 may be provided with a detachably connected cartridge 260 that has a desired function.

Abstract: The present disclosure relates to a landing device capable of allowing an unmanned aerial vehicle to be accommodated in a compact manner. A landing device includes a first leg portion that is swingable with a first end portion on a main body side of an unmanned aerial vehicle as an axis; and a second leg portion that is detachably attached to a second end portion of the first leg portion such that the second leg portion extends in an axial direction of the first leg portion. The present disclosure can be applied to, for example, a drone including a camera at a bottom of a main body.

Abstract: An unwinding apparatus associable with a wrapping machine for delivering films comprises a supporting frame to rotatably support a first reel of a first film; adjustment elements to rotatably support a second reel of a second film and to arrange it in one of a plurality of operative positions, in which the second reel is staggered with respect to the first reel; guiding rollers to guide and partially overlap the first film and the second film at a longitudinal partial overlapping band; joining assembly for joining the first film and the second film along a longitudinal joining band made inside a width of the longitudinal partial overlapping band so as to obtain a single-body composite film; the joining assembly comprises a welding device or a gluing device.

Abstract: A needle has a hollow shaft, a tip formed at one end of the shaft, one or more ports in fluid communication with the interior of the hollow shaft, and a closure. The closure and/or the shaft is movable between (i) a first position wherein the closure closes the port(s), and (ii) a second position opening the port(s).

Abstract: An orientation module including a base configured to support at least one container, a camera positioned to scan the at least one container, a processor operatively connected to the camera configured to analyze an initial orientation of the container and determine a secondary orientation of the container, and a turning member positioned above the base configured to turn the corresponding container according to a command from the processor to rotate the container to the secondary orientation.

Abstract: A multifunctional vacuum sealing machine which includes a shell, and a vacuumizing device and a sealing device which are arranged in the shell, wherein the sealing device includes a hot welding device; cross sealing can be performed at a connector position twice, thus forming a completely-closed sealing line; and during vacuumizing, while a bag to be vacuumized is clamped and sealed by an upper cavity and a lower cavity, the bag is punched by a cutter head in the upper cavity, the bag is vacuumized, a punching position is in a closed area surrounded by one sealing line with the adjacent first heating wires and the second heating wire or in a closed area surrounded by the first heating wires and the second heating wires, and after vacuumizing, an opening is sealed at an original position, so that it is guaranteed that air cannot enter the vacuumized bag during sealing.

Abstract: A filling machine configured to form, fill, and seal individual packages is provided. The filling machine comprises a sterilization station configured to provide a flow of gaseous sterilizing agent towards open ends of ready-to-fill packaging containers passing through said sterilization station. The filling machine comprises at least one clean air supply and at least one baffle plate arranged above the at least one clean air supply, wherein the air supply is configured to direct a stream of clean air towards the ready-to-fill packaging containers. The clean air supply in turn comprises at least one distribution pipe and wherein the distribution pipe extends in a horizontal direction, the horizontal direction being in the direction of the flow of packages through the filling machine.

Abstract: A method, apparatus and program product may evaluate a packaging material to determine various metrics associated with the packaging material. A test apparatus may be used to evaluate packaging material using a take up drum capable of sensing containment force imparted upon the drum by packaging material applied thereto, and in some instances, simulated flaws may be formed in a web of packaging material to evaluate a packaging materials response to such flaws when under tension.

Abstract: A system includes a film processing module, a processor, and memory. The processor and memory are in communication with the film processing module. The processor is configured to dynamically coordinate movement of the film processing module relative to a moving web of film and to perform a function on the web of film with the film processing module.

Abstract: Described herein is a package (10) for a foodstuff product, in particular a confectionery product, comprising a wrapping sheet (2) wrapped around said product (P) so as to enclose it within a cavity (C) delimited by said sheet and so as to remain adherent to the outer surface of said product (P). The package is characterized in that it envisages a sealing portion (4), which is folded adherent to the portion of the sheet that defines the inner cavity (C) and which is provided with a point (6) of facilitated opening.

Abstract: A bottle can made of aluminum alloy has a base portion; a cylindrical body portion connected to an upper end of the base portion; a reduced diameter portion where a diameter reduces from an upper end of the cylindrical body portion to an upper side; a neck portion provided at an upper side of the reduced diameter portion; and a mouth portion having a male thread portion and a bulge portion provided at an upper side of the neck portion. The reduced diameter portion has: a convex curved portion continuing to the upper end of the cylindrical body portion; a concave curved portion continuing to an upper end of the convex curved portion; a lower convex portion continuing to an upper end of the concave curved portion; and an upper concave portion continuing an upper end of the lower convex portion and a lower end of the neck portion.

Abstract: A container for food liquids, in particular for the storage and/or fermentation of alcoholic beverages, has a body in which a substantial portion of the walls of the container is made of a ceramic material with controlled porosity. The body of the container is shaped as a truncated pyramid, in which each of the faces of the side wall includes a slab of ceramic material with controlled porosity, and in which a support structure made of cementitious material is formed along the external corners of the side wall and in correspondence with the bases of the truncated pyramid. Axial openings are defined in the bases of the container and are adapted to cooperate with suitable closing members.

Abstract: A high-strength foam bearing pallet is disclosed. The foam bearing pallet comprises a foam bearing plate and supporting legs configured on the lower end of the foam bearing plate. The foam bearing plate comprises a foam core and a PET reinforcing film covering the outer surface of the foam core to increase its strength. The PET reinforcing film is made of a PET sheet heated and fixed to the outer surface of the foam core through vacuum forming. The PET reinforcing film limits and tightens the foam core to prevent the foam core from deformation or fracture. As the outer surface of the foam core is wholly covered by the reinforcing film, and the reinforcing film limits and tightens the foam core, the foam bearing pallet will have higher strength.

Abstract: A dunnage support assembly for a transportation or storage container may include pair of panels each defining a channel at a top end thereof, the panels being configured to be received within a transportation or storage container with a top edge of one side wall thereof received within the channel of one panel such that the panel is supported on and by the one side wall, and with a top edge of another side wall thereof received within the channel of the other panel such that the other panel is supported on and by that side wall. One or more elongated support rails are secured to the each panel and oriented to be substantially parallel with the channels, and the support rails are configured to support a plurality of dunnage pouches therebetween and slidable relative thereto.

Abstract: A customizable storage system includes at least one removable storage container and a container caddy. The at least one removeable storage container includes a container shell and a tilt bin located in the container shell and configured to tilt relative to the container shell. The container caddy includes a container support frame having first and second container docks that each define first and second container-receiving spaces the receive the at least one storage container and a carrying handle coupled to and extending away from the container support frame.

Abstract: A container has a base material and a coating layer which is disposed on at least a portion of the base material, contains a composition containing at least one kind of metal component selected from the group consisting of Ti, Al, Mg, Zr, Hf, Fe, Ni, Sn, Zn, Cr, and Mo, and has a thickness equal to or greater than 50 ?m. In a case where the composition contains one kind of metal component, a ratio RCAs calculated by CA1s/CA2s is less than 1.0. Alternatively, in a case where the composition contains two or more kinds of metal components, in at least a portion of the coating layer, an average of RCAs determined for each of two or more kinds of the metal components is less than 1.0.

Abstract: Provided is a container including a container body, and an image on the container body. The image includes a plurality of dented portions and non-dented portions. Each of the dented portions is formed of a plurality of processed portions. The plurality of processed portions are disposed linearly, contacting or overlapping each other along a first scanning direction. A width of each of the dented portions in a second scanning direction orthogonal to the first scanning direction changes cyclically along the first scanning direction. Each of the dented portions has bossed portions along the first scanning direction between adjoining ones of the processed portions.

Abstract: A closure for a container is provided. The closure comprises a cap and a retaining ring arranged under the cap for retaining the closure on the container in use. The cap and ring are joined by a pair of connecting arms. A first arm is non-frangibly connected to the cap at a cap tether end and circumferentially anticlockwise therefrom is non-frangibly connected to the ring at a ring root end. A second arm is non-frangibly connected to the cap at a cap tether end and circumferentially clockwise therefrom is non-frangibly connected to the ring at a ring root end. The cap can be tilted away from the ring with the arms providing a hinge-like function, and each of the arms twists between its cap tether end and its ring root end, whereby tension is generated in the arms.

Abstract: A container system including a lid and a container is provided. A locking structure on the skirt of the lid is situated on a tear off portion and comprises a plurality of flexible tabs positionable in an upwardly biased locked position each independently engaging the container within an annular cut away on the container wall below a locking rib. If the lid is removed with tear off strip still engaged, the flexible tabs are biased downwardly and may break off, exposing tampering.

Abstract: A collapsible box includes a plurality of side panels including a first side panel and a second side panel, each of the plurality of side panels defining a side panel top edge; a box bottom; and a box top comprising a plurality of top panels including a first top panel extending from the side panel top edge of the first side panel and a second top panel extending from the side panel top edge of the second side panel, the second top panel comprising an overlapping portion; wherein, in a folded-down configuration of the collapsible box: the first side panel confronts the second side panel; and the overlapping portion of the second top panel is folded over a top panel top edge of the first top panel.

Abstract: Examples provide a configurable divider bridge system. A divider bridge includes a tab at opposite ends of the divider bridge. The tabs insert into receiving slots inside a container, such as a display case or packing container. The receiving slots guide the tabs downward between the interior sides of the container and items placed inside the container. As the tabs slide down into the receiving slots, the side panels of the divider bridge are guided into an unfolded configuration. The slots permit installation of the divider bridge into the container which already contains soft product easily while preventing damage to the divider or the soft product. The divider bridge can be placed inside the container in a variety of configurations and/or orientations to accommodate a variety of sizes and shapes of containers and types of items being stored, transported, or displayed within the containers.

Abstract: A multi compartment package with slide openings for storing and dispensing two different types or flavors of solid pourable product such as candies or mints is made from a single blank having a number of panels extending lengthwise and all foldably connected. From the blank the exterior of the package is formed having a front panel and a rear panel, and the interior having two compartments. The front panel has cut outs for dispensing the pourable product, and the rear panel connects to package enclosure tabs. Each compartment has a detachably connected slide, and the slides are glued to the package enclosure tabs to seal the package. To open the package, the slides are detached and moved to expose the cut outs through which the pourable product is dispensed. Conveniently, if all the product is not immediately consumed, the slides may be closed to retain freshness.