Abstract: An interior aircraft LED light unit includes at least one LED and a lens cover arranged over the at least one LED, the lens cover having a proximal side facing towards the at least one LED and a distal side forming an outside portion of the interior aircraft LED light unit, with the lens cover being made from a lens cover material exhibiting material-specific light transfer properties. The lens cover comprises a pattern of dots on the distal side, with each of the pattern of dots locally altering the material-specific light transfer properties of the lens cover.

Abstract: A mobile passenger entertainment and information system that includes a control device, a plurality of passenger devices, a satellite communication device, a set of managing software, a plurality of power connectors, and a plurality of theft prevention kits. The passenger device assigned to each passenger seat includes a display screen, data storage and wireless communication capabilities. The control device manages and maintains wireless communications, via various channels, for managing entertainment activities, updates, passenger data and vehicle data collection. The managing software running on the control device and the passenger devices automates system functions and manages user activities.

Abstract: Described herein are personal electronics device mounting assemblies including a passenger seat and a case assembly comprising a case configured to receive a personal electronic device and a male structure pivotally coupled to the case. The personal electronic device mounting assemblies may also include a mounting assembly comprising a female slot structure and a support bracket structure, the female slot structure may be configured to releasably receive the male structure and the support bracket structure may be configured to attach to the passenger seat. The mounting assembly may be configured to provide support to the case when the male structure is in an extended position and the female slot structure has received the male structure.

Abstract: A personal electronic device holder for a seat back that includes a support housing positioned on an upper shroud portion of the seat back and an upper support for supporting the top edge of the electronic device positioned in the support housing. The upper support is mounted for movement between a lowered, stowed position in the support housing and a raised, deployed position extending out of and above the support housing. A lower support is provided for supporting the bottom edge of the electronic device, and is positioned for movement between a stowed position covering the support housing and a deployed, lower position below the support housing. The upper support and lower support have respective engaging surfaces defining between them a user-selected space for engaging and holding the top edge and bottom edge of the electronic device in a use position.

Abstract: A stowable seat is provided. The stowable seat may comprise a housing, a back rest coupled to the housing at a top of the back rest, and a seat bottom coupled to a bottom of the back rest. A track may be coupled to a housing with the seat bottom configured to slide along the track. A linkage may be coupled between the housing and the track and configured to translate the track away from the housing.

Abstract: Described are seat units having a lower support structure with at least two leg supports, each leg support integrally formed into an arcuate shape, and an upper support structure having a seat pan and seat back integrally formed into a single component. Each leg support is coupled to at least two base frame tubes by insertion of each base frame tube through an aperture in each of the leg supports, wherein the aperture is shaped to prevent rotation of the leg support about a longitudinal axis of each of the at least two base frame tubes. Each seat support is coupled to the base frame tubes by insertion of each base frame tube through a slot in each of the upper support structure.

Abstract: Methods and systems are generally described that inhibit debris (such as ice) accretions and/or remove debris (such as ice) accretions from the exterior surface of an aircraft. In some embodiments, the invention is a system for an aircraft comprising: a component of the aircraft having a surface; a plurality of piezo-kinetic actuators each positioned proximate to a portion of the surface; and a control unit coupled to the plurality of actuators, the control unit configured to actuate one or more of the actuators at one or more frequencies; wherein the actuators are each configured to introduce a displacement of the surface in three dimensions to inhibit a formation of ice on at least the portion of the surface and to break up existing ice formations on at least the portion of the surface.

Abstract: A balloon system is provided including a balloon envelope, a payload secured to the balloon envelope, a first parachute positioned within a parachute container, the parachute container secured to the payload, a first bridle line having a first end secured to the balloon system and a second end secured to the parachute container, a controller positioned on the balloon system, wherein when the controller receives a signal to deploy the parachute container, the controller is operable to cause the parachute container to be released downwardly from the payload.

Abstract: An engine attachment system (EAS) includes a forward collar (202), an aft collar (204), at least one truss subassembly (216) disposed between the forward collar and the aft collar for supporting an engine, and at least one vibration isolator (206,208) integrated with each of the forward and aft collars for isolating engine vibration and reducing noise. A method of attaching a turboprop engine includes providing an EAS and hoisting a turboprop engine at least partially within the at least one truss subassembly (216).

Abstract: A nacelle may include fan cowl panels which may be opened to provide access to the fan case. A latching mechanism may latch a left fan cowl panel to a right fan cowl panel. As a handle is opened to unlatch the latching mechanism, the movement of the handle may cause a push pin to create a separation between the left fan cowl panel and the right fan cowl panel. The separation may create a visual indication that the fan cowl panels are not latched together, which may prevent an aircraft from inadvertently taking off with unlatched fan cowl panels. The push pin when extended may prevent closure of the fan cowl panels.

Abstract: A nacelle may include fan cowl panels which may be opened to provide access to the fan case. A latching mechanism may latch a left fan cowl panel to a right fan cowl panel. The latch may create a separation between the fan cowl panels when unlatched. A shoot pin latch may be aligned with a receiver cavity such that the shoot pin latch may be closed when the latching mechanism is closed. If the fan cowl panels are not fully closed, the shoot pin latch may be prevented from closing, and a high visibility handle may indicate that the fan cowl panels are not latched together.

Abstract: A latch handle is disclosed. The latch handle may comprise a first portion and a second portion. The first portion may comprise a high aspect ratio. The second portion may have a width greater than the second portion. A nacelle is disclosed. The nacelle may comprise a first panel and a latch assembly. The latch assembly may include a latch housing and a latch handle. The latch handle may include a first portion and a second portion. The first portion may comprise an aspect ratio greater than one. The second portion may have a width greater than the width of the first portion. A cut-out configured to accommodate the latch assembly may be disposed on the first panel. The first panel may be a fan cowl panel.

Abstract: A method to reduce aerodynamic drag of a engine exhaust/engine nozzle includes collecting data that is indicative of an instant flight condition, entering the data into a decision algorithm that, based on the data, outputs at least first and second drag control parameters corresponding, respectively, to an angle of one or more variable area turbines of a turbine engine and a position of a variable area exhaust nozzle of the turbine engine, and adjusting the angle of the one or more variable area turbines and the position of the variable area exhaust nozzle according to, respectively, the first and second drag control parameters to reduce aerodynamic drag of an engine exhaust/engine nozzle of the turbine engine.

Abstract: A flight controller system includes an electronic speed control throttle input from which an anticipated electrical power demand is determined. The flight controller system includes a controller that determines a throttle input for a generator in order to satisfy the anticipated electrical power demand. The flight controller system includes an electronic speed control throttle output providing a delayed electronic speed control throttle signal.

Abstract: An aircraft thermal management system includes a first fluid system containing a first fluid, a fluid loop containing a thermally neutral heat transfer fluid, a second fluid system containing a second fluid, a first heat exchanger configured to transfer heat from the first fluid to the thermally neutral heat transfer fluid, and a second heat exchanger configured to transfer heat from the thermally neutral heat transfer fluid to the second fluid. The fluid loop is configured to provide the thermally neutral heat transfer fluid to the first heat exchanger at a pressure that matches the pressure of the first fluid.

Abstract: In an intake structure of an aircraft that takes in air from a front side of an airframe, a bump is provided on a surface of the airframe of the aircraft at a portion immediately before an intake. The bump is formed so as to smoothly protrude from the front side of the airframe while having a width that is wider than a width of the intake.

Abstract: This aircraft heat exchanger includes a heat exchanger body, which includes: a temperature raising section configured at least to raise a temperature of the heat exchanger body locally; and a heat exchanging section configured to exchange heat between an aircraft fuel and oil. The temperature raising section has an inlet for the oil, and has its temperature raised by the oil that has entered the heat exchanger body through the inlet. The heat exchanging section has an outlet for the aircraft fuel. The oil that has passed through the temperature raising section is introduced into the heat exchanging section from around the outlet for the aircraft fuel. The heat exchanging section is configured to have counter flows.

Abstract: The present invention provides an arrangement for passing a line in a load-free manner through a pressure frame of a fuselage of an aircraft or spacecraft, including an opening penetrating the pressure frame, through which opening the line is passed, the line being mechanically decoupled from the pressure frame; and a flexible sealing device arranged outside the opening at least in portions, which sealing device is simultaneously operatively connected to the line and the pressure frame for the pressure-tight separation of a first side from a second side of the pressure frame. The present invention also provides a fuselage for an aircraft or spacecraft having an arrangement of this type and an aircraft or spacecraft having an arrangement of this type or having a fuselage of this type.

Abstract: An air data probe includes a probe head defining a longitudinal axis between a forward tip and aft base. The probe includes a thermocouple having a sense end in the forward tip to measure the temperature in the forward tip. The probe includes a port opening defined in a side of the probe head and opening at an angle with respect to the longitudinal axis. The probe includes a bulkhead within the probe head. The bulkhead has a chamber in fluid communication with the port opening. The chamber includes a single chamber inlet having an elongated cross-sectional shape. The single elongated chamber inlet is in fluid communication with two downstream pressure conduits to provide redundancy in case one of the two pressure conduits is blocked.

Abstract: A method and apparatus for a wingtip control system. The wingtip control system comprises a switch system for a flight deck of an aircraft and a controller. The switch system is configured to be placed into an armed state and generate an armed signal. The controller is in communication with the switch system. The controller is configured to receive the armed signal from the switch system, visually indicate a desired position for a wingtip of the aircraft in the switch system in response to an event occurring during operation of the aircraft, and generate a movement command to move the wingtip.

Abstract: A method of marking a landing zone on ground for an aircraft in flight. The aircraft projects on the ground a light shape referred to as a “projected light shape” comprising at least one line of light defining a geometrical surface, the aircraft tending to place at least a portion of landing gear of the aircraft on the geometrical surface, the projected light shape being identical regardless of the position of the projector in air space.

Abstract: An aircraft power distribution system (22) includes at least one DC power source, a first DC power distribution bus and a second DC power distribution bus (36), a tie bus (33) coupling the at least one DC power source, first DC power distribution bus, and second DC distribution bus, wherein the first or second DC power distribution buses are selectively coupled and decoupled to the tie bus by means of a solid-state poer controller (SSPC) (46, 48, 62, 64, 66).

Abstract: An at least partially transparent exterior aircraft light cover includes at least one protrusion provided at a lateral end of the exterior aircraft light cover, wherein the at least one protrusion is configured to be introduced into a corresponding reception provided at an exterior aircraft light casing and wherein the protrusion is formed for allowing the cover to pivot, with the protrusion providing a fulcrum, when the protrusion is introduced into the reception.

Abstract: An exterior aircraft navigation light for an aircraft having a nominal forward flight direction and being able to fly into the nominal forward flight direction as well as into a plurality of further flight directions, such as sideways or backwards, has at least one light emission unit and control circuitry coupled to the at least one light emission unit, wherein the exterior aircraft navigation light is configured such that each of the at least one light emission unit has a unit-specific light emission direction that has a pre-defined horizontal angle with respect to the nominal forward flight direction, and wherein each of the at least one light emission unit includes a multi-color light source configured to emit red light, white light and green light, and an optical system for conditioning the red light, the white light and the green light emitted by the multi-color light source.

Abstract: A method, a computer program product, and a system is disclosed of obtaining aerial images from an aerial vehicle to avoid shadows produced by the sun, the method comprising: providing the aerial vehicle with one or more cameras configured to capture images of a landscape; and arranging the one or more cameras to capture the images from an angle which is opposite in direction of the sun.

Abstract: In one embodiment, a device includes a spine, a first support coupled to a first end of the spine, a second support coupled to a second end of the spine, and a plurality of fixtures coupled to the spine. The plurality of fixtures are configured to couple an aircraft flight control apparatus to the spine.

Abstract: This recovery system is used mainly for the recovery of liquid propellant rocket engines, so that they can be reused once or more times, in first stages (one-and-a-half) boosters. The technological goal of this invention is improved reliability of recovery systems. This goal is achieved by the rocket engine recovery system representing of a capsule comprised of a protective bottom and a lateral cover; the capsule includes a parachute bay and a landing gear bay; the capsule is attached to the engine thrust frame; at least one stabilizing parachute; at least one main parachute; at least one landing set of landing gear; the bay with the landing gear is located in the protective bottom of the capsule; the parachute release, the landing gear inflation, and the soft landing engines ignition are initiated, using simplest automatic devices.

Abstract: A landing inflation system may include a compressed gas source, an airbag assembly fluidly coupled to the compressed gas source and configured to receive compressed gas, and a command processor configured to: (1) generate an inflation initiation command signal in response to an initiation signal, (2) generate an inflation cessation command signal in response to a nominal fill pressure signal, and (3) generate a vent command signal in response to an impact pressure signal.

Abstract: A three-dimensional map of an environment with buildings is used to computationally predict locations and times of global navigation satellite system (GNSS) blockages. For example, in urban environments some of the GNSS satellites are occluded by buildings. These blockages can be modeled. A computing system can make a map showing which satellites are or are not visible as a function both of location and time. The map can be used by a mobile GNSS receiver to determine which satellites to use or whether to use a backup system for navigation. The system can determine when a given satellite will enter or leave a GNSS receiver view during a route. The map can be stored in the GNSS receiver (or a host of the GNSS) or can be stored by a network service. This mapping can be used to predict multi-path effects of a satellite transmission at a location.

Abstract: Apparatus useful for feeding a particulate starter material comprising nutrient and bacteria to a mixing tank, for solubilizing the starter material inside the mixing tank, for promoting growth of the bacteria and for discharging an aqueous slurry comprising the bacteria from the mixing tank. The apparatus preferably has a gravity-flow feeder and discharge port, does not require a pump, and comprises disposable parts.

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: Improved object wrapping materials exhibiting a number of beneficial properties to overcome prior deficiencies are provided. Such properties include the inclusion of a separation interface overlay that allows for greater rigidity at the leading and trailing edges of such wraps. Also, the inclusion of shear-reducing wrap material portions is described, as well as recoil reduction structures within the leading edge regions. Furthermore, core adhesive additions allow for greater resiliency to the base wrap material as it unwinds therefrom, reducing potential waste wrap products by permitting greater amounts of wrap materials in use. Other considerations include the ability, through proper configuration designs, to position a wrap separation indicator within a certain range of distances from the trailing edge, thereby providing greater reliability of wrap application device disengagement during wrap application.

Abstract: A portable tool for tying an object, in particular a cable harness, using a strip, comprising a tool element with a cycle controller arranged in the tool element, a clamping device, and a drive for the clamping device. The drive is designed as a dual drive such that the cycle controller and the clamping device each have a dedicated drive, said drives being actuated independently by a controller. By providing a dedicated drive for the clamping device in this manner, interfering influences from the cycle controller are eliminated. Thus, a more precise clamping process can be carried out with high reproducibility, thereby improving the quality of the tying process.

Abstract: The present application in particular is related to a vacuum packaging arrangement. The vacuum packaging arrangement (2) comprises a drawer (4) configured to cooperate with a kitchen cabinet (3), and a vacuum packaging device (5). The vacuum packaging device (5) is functionally integrated in a ready-to-operate configuration within the drawer (4) and provides, within the drawer, an operational interface to receive a minor first section (27) of a vacuum bag (17), and to vacuum the vacuum bag upon activation of the vacuum packaging device (5). The vacuum packaging device (5) is implemented such that a major second section of the vacuum bag (17) comprising a closed end of the vacuum bag (17) is arranged outside of the vacuum packaging device (5).

Abstract: The invention relates to a method for producing a packaging and a system for such. The method includes the following steps: providing a precut blank (1) consisting of a foldable material having a bottom (3) and hinged to it, lateral panels (4), a rear panel (6) and a front panel (5), fastening of an unstressed elastic element (15) to the front panel (5) or to connecting flaps (7) that are hinged to the front panel (5), erecting the lateral panels (4), the rear panel (6) and the front panel (5) out of a flat transport condition into an unfolded usable condition and connecting the lateral walls (4) with the rear panel (6) and the front panel (5) and tensioning the elastic element (15).

Abstract: A packaging system (20) for forming and filling a transportable container (22) of plurality of bulk goods includes a frame (26) having a bottom support (48) and an upper support (32). An upper turntable (34) is rotatably supported within the upper support (32) and a lower turntable (50) is rotatably supported on the bottom support (48). A drive system (58) includes at least one pulley system (62, 64, 66) interconnected to the upper and lower turntables (34, 50) for simultaneously driving and synchronizing rotation of the upper and lower turntables (34, 50) with the at least one pulley system (62, 64, 66). A slip frame former (42) extends downwardly from the upper turntable (34) and a roll of stretch wrap (92) is disposed in overlapping relationship with the slip frame former (42) and the bottom support (48) during simultaneous and synchronized rotation of the turntables (34, 50) with the at least one pulley system (62, 64, 66).

Abstract: A fitment mounting apparatus for mounting a hold open fitment to flexible packaging, wherein the hold open fitment has a flexible configuration variable between a first un-distended shape and a second stably distended shape, including a frame forming a holder configured for holding more than one of the hold open fitments within the holder, a flexible packaging positioning system arranged for positioning flexible packaging for mounting the hold open fitment to the flexible packaging, and an applicator coupled to the frame configured to engage at least one edge of the hold open fitment in the holder and bias the at least one edge so that the hold open fitment is singulated, from others of the more than one hold open fitments in the holder, and issued from the holder into the flexible packaging on the flexible packaging positioning system substantially simultaneous with singulation

Abstract: A product packaging system comprises a plurality of product sources (2, 4, 6) delivering product to a final collating and packaging line (10). The output from each machine is delivered by separate conveying means (8) delivering the products directly into a collating conveyor (20) which in turn delivers the collated products to a packaging line. The collating conveyor comprising an endless conveyor carrying a plurality of compartments, each compartment receiving from said conveying means products to be packaged. The compartments are configured to enable their sizes to be changed, and the endless conveyor comprises a track arranged in a vertical loop and a plurality of product supporting members mounted for movement along the track, each supporting member being driven along the track and controllable independently of the other supporting members.

Abstract: A label application apparatus comprising: an input station, at which a succession of separate labels is formed; an application station, at which each of the labels is applied on a respective article advancing along an article path; a transfer drum configured to retain each label on an outer lateral surface of the transfer drum by suction and to rotate about an axis to transfer each of the labels from the input station to the application station along a label path; a glue applicator arranged peripherally with respect to the transfer drum between the input and application stations with reference to the label path; and a laser emitter arranged peripherally with respect to the transfer drum and configured to generate a laser beam towards the transfer drum to remove at least one of dirt or glue residues from the outer lateral surface of the transfer drum.

Abstract: The present invention provides a container cup having a substantially frustoconical shape and comprising a side wall and a bottom wall, the container cup is characterized in that said side wall has an annular region which comprises at least one or more stiffening grooves, and an outer annular member arranged externally onto said cup wall and at said at least one or more grooves.

Abstract: A container with at least two compartments, at least one connecting section connecting two adjacent ones of the at least two compartments and extending along a connecting section axis and at least one strengthening structure in each one of the at least one connection section and extending between the at least two adjacent compartments. Each one of the at least one connecting section comprises a separation strip extending along the connecting section axis and defining a weakened section thereof along which the at least two adjacent compartments can be separated from one another. The at least one strengthening structure extends substantially perpendicular to the connecting section axis of the corresponding connecting section.

Abstract: A blank of foldable sheet material is provided. The blank includes a bottom panel, a first bottom side panel and a second opposing bottom side panel extending from opposing side edges of the bottom panel, and a front panel extending from a front edge of the bottom panel. The front panel includes opposing side edges. The blank also includes a first and a second diagonal panel extending from a front edge of the first and second bottom side panels, respectively, and a third and a fourth diagonal panel extending from each side edge of the front panel. The third and fourth diagonal panels have a length greater than a length of the first and second diagonal panels. The blank includes a first and a second corner panel, wherein the first corner panel is hingedly connected to the first and third diagonal panels and the second corner panel is hingedly connected to the second and fourth diagonal panels.

Abstract: The invention relates to a precut blank (1) consisting of a foldable material such as corrugated cardboard, paperboard or carton for producing automatically erectable packaging, in particular, a tray. The precut blank has a bottom (3) and hinged to it, two lateral panels (4), a rear panel (6) and a front panel (5), as well as two connecting flaps (7, 8) hinged to the front panel (5) and two hinged to the rear panel (6). According to the invention, an unstressed elastic element (15) is fastened at the connecting flaps (7) that are hinged to the front panel. Further, the invention relates to packaging erected from the precut blank (1).

Abstract: A one-piece shipping and display container is formed from a single unitary blank of corrugated paperboard. The one-piece shipping and display container includes opposed parallel side walls, opposed parallel end walls, bottom flaps, and top flaps all of which are foldably joined to one another for closing bottom and top portions of the one-piece shipping and display container. The one-piece shipping and display container includes a supporting insert panel that is removed from the container when the container is in a knock-down position. The supporting insert panel is inserted back into the container before or after the container is filled with products to provide protection for the products and further enhances the strength of the container during shipping and transportation.

Abstract: A chafer wire stand has an upper rim of a closed rectangle and a lower rim of wire metal of similar, but smaller shape. The chafer stand is nestable such that straight wire section extending between the upper and lower rim touch each other when nested and the upper rims of the nested stands are held close to each other. The upper and lower rims are connected by at least two wires substantially identically shaped and bent with each wire being unitary and having a segment thereof attached to the upper rim and extending outwardly therefrom to form a handle element for the chafer wire stand. Each wire is attached to the lower rim and extends therefrom to form two supporting legs for the chafer wire stand.

Abstract: Disclosed is a packaging device for a liquid crystal panel, including a first main body having a bottom and a plurality of sidewalls connected to sides of bottom. The sidewalls define at least one opening. At least one second main body has a bottom and sidewalls connected to the bottom and define an opening that is movably received in the at least one opening of the first main body such that the packaging device is expandable by moving the second main body in a direction away from the first main body.

Abstract: Disclosed is a packaging device for a liquid crystal panel, including a first main body having a bottom and a plurality of sidewalls connected to sides of bottom. The sidewalls define at least one opening. At least one second main body has a bottom and sidewalls connected to the bottom and define an opening that is movably received in the at least one opening of the first main body such that the packaging device is expandable by moving the second main body in a direction away from the first main body.

Abstract: The present invention describes a container for drinking liquids, equipped with electronic elements, which enable it to monitor the physical and chemical characteristics of the liquid to be drunk, the movement of the container that holds said liquid, and also transmits the information related to the use of said container. Further advantages of the invention are described in the summary of the invention. Regarding the field of the invention, the present invention is generally related to containers for drinking liquids, and is specifically related to containers for drinking liquids equipped with electronic elements, which enable it to monitor the physical and chemical characteristics of the liquid to be drunk, the movement of the container that holds said liquid, and also transmits the information related to the use of said container.

Abstract: A compartmentalization assembly is provided. The compartmentalization assembly includes a base having a surface with shaft seats and at least one separator including a panel and one or more shafts, each of the shafts can each be fittingly received into one of the shaft seats.

Abstract: A bathroom tissue spray caddy that hangs or otherwise affixes to a bathroom tissue dispenser. The caddy provides easy access to a bottle dispensing a cleansing fluid to bathroom tissue, for enhanced cleanliness and comfort. The caddy includes a retaining receptacle with an open top and closed bottom to hold a bottle. The receptacle contains an inner dimension suitable for accepting and retaining a bottle therein without the bottle falling out yet with sufficient space to permit ease of tilting and lifting the bottle out of the receptacle by the user. The receptacle is provided with a releaseable hanging or fastening element or elements such as a hook to enable the retaining receptacle to be affixed to a fixed position element of a bathroom tissue dispenser, such as a side bar, in such as way that the bathroom tissue spray bottle contained in the receptacle is in an upright position.