Abstract: In one possible embodiment, an amphibious unmanned aerial vehicle is provided, which includes a fuselage comprised of a buoyant material. Separators within the fuselage form separate compartments within the fuselage. Mounts associated with the compartments for securing waterproof aircraft components within the fuselage. The compartments each have drainage openings in the fuselage extending from the interior of the fuselage to the exterior of the fuselage.

Abstract: Hybrid unmanned vehicles are disclosed. An example vehicle includes a housing and a rollerball rotatably coupled to the housing and a propulsion system supported by the housing. The propulsion system is to generate lift to enable the vehicle to navigate in a first mode of operation. The vehicle includes a rollerball rotatably coupled to the housing. The rollerball to enable the housing to navigate in a second mode of operation different than the first mode of operation. The propulsion system is to generate a drive force to enable the vehicle to navigate in the second mode of operation via the rollerball.

Abstract: Embodiments relate to a client-facing application for interacting with a transport service that transports items via unmanned aerial vehicles (UAVs). An example graphic interface may allow a user to order items to specific delivery areas associated with their larger delivery location, and may dynamically provide status updates and other functionality during the process of fulfilling an aerial vehicle transport request.

Abstract: A high-flying solar unmanned aircraft system capable of extending endurance time is disclosed. The system includes a main aircraft, a separable auxiliary power source and a connection device. The main aircraft includes a first body, a second body, a first wing portion, a second wing portion, a third wing portion, a first propeller and a second propeller. The second wing portion locates between the first body and the second body, and the second wing portion connects the first body and the second body. The connection device connects the main aircraft and the auxiliary power source, and includes a separation device. When the system climbs, the separable auxiliary power source provides additional energy to assist the main aircraft to climb. When reaching a preset altitude, the separation device, by burning out a line of connection bent, is turned on such that the auxiliary power source is separated from the main aircraft.

Abstract: A tether compensated unmanned aerial vehicle (UAV) is described. In one embodiment, the UAV includes a winch with a tether to lower an item from the UAV for delivery, a tether compensation mechanism configured to contact the tether as it extends from the winch, and a flight controller to control a flight path of the UAV. The flight controller is also configured to direct the tether compensation mechanism to clamp the tether based on the flight path of the UAV. Further, based on movement identified in the tether using a sensor, a tether response controller can determine a complementary response and direct the tether compensation mechanism to brace the tether against the movement. Thus, the tether compensation mechanism can help stabilize sway or movement in the tether, which can help prevent the tether from undesirable swinging.

Abstract: A cargo unit for storage in a cargo hold of an aircraft including a housing and a storage rack arrangement, the housing enclosing the storage rack arrangement and including a transport opening. The cargo unit is connectable to a transport arrangement operable for removing objects from the storage rack arrangement and placing objects in the storage rack arrangement through the transport opening when the cargo unit is arranged in an operating position. The cargo unit includes a transport cover movable between a closed position where the transport cover closes the transport opening and an opened position where the transport opening is not covered by the transport cover. The transport cover is adapted to be only movable from its closed position to its opened position after engagement with a transport arrangement. A lower deck catering system including a cargo unit and a transport arrangement is described.

Abstract: A stowage bin assembly is within an interior cabin of a vehicle. The stowage bin assembly includes a weight sensor that is configured to detect the weight of the stowage bin assembly, and a stowage bin control unit in communication with the weight sensor. The stowage bin control unit is configured to automatically close the stowage bin assembly in response to a weight of the stowage bin assembly being within a predetermined range of a maximum weight threshold.

Abstract: A latch system that includes a paddle button assembly having a button that is movable between home and actuation positions, a latch assembly that includes a striker assembly with a striker and a hook assembly, and a cable that extends between the paddle button and latch assembly. The hook assembly includes a hook, a pivotal trigger arm, and a manual override switch that is movable between first and second positions when the trigger arm is moved from an engaged position to a disengaged position. Movement of the button from the home position to the actuation position pushes or pulls the cable, thereby pivoting the trigger arm from the engaged to the disengaged position and disengaging the hook from the striker. Pivotal movement of the trigger arm from the engaged to the disengaged position results in linear movement of the manual override switch from the first to the second position.

Abstract: A galley cart system employs a housing with a door coupled to the housing, the door configured to be moved between a closed position and an open position. A vent plate in the housing communicates between a first compartment and a second compartment. A valve plate adjacent the vent plate is movable from a venting position when the door is in the closed position to a blocking position when the door is in the open position thereby preventing flow communication between the first and second compartment.

Abstract: An airplane seat device with at least one airplane seat is at least configured to be adjusted between a use position and a stowage position. In the stowage position, the airplane seat has a maximum height which is equal to or less than a maximum height in the use position.

Abstract: A pillow includes a support body. A shape-adapting frame is within the support body. The shape-adapting frame is configured to be moved into and maintained in a desired position. At least one sensor is configured to detect at least one condition. The sensor(s) may be in communication with a monitoring control unit of a monitoring system.

Abstract: Provided is a seat cushion for at least one vehicle seat, in particular an aircraft seat, including at least one bolster including at least one layer made of a plastic material. In the at least one plastic material layer at least one stabilizing means is embedded. The at least one stabilizing means has a bending stiffness which is higher with respect to the plastic material layer.

Abstract: An improved slider for use with a parachute, particularly a ram-air type parachute, is provided. The slider includes a generally rectangular piece of material having grommets in the corners through which the suspension lines of the parachute run. At least one retaining structure is attached to or made in the slider material for securing one or more stiffening elements. The stiffening elements are flexible enough to allow for the packing of the parachute, but stiff enough to keep the material of the slider spread open in the fore/aft direction across the short axis of the slider and thereby prevent the slider from folding and flapping once the canopy has opened.

Abstract: A restraint arrangement for an inflatable slide may comprise a releasable restraint and a yoke coupled to the releasable restraint. The yoke may comprise a first strap and a second strap. A first dampener may be coupled to the first strap. A second dampener may be coupled to the second strap. The first dampener and the second dampener may deform in response to a tensile load.

Abstract: A support arrangement for an inflatable evacuation system may comprise an inflatable member configured to be elongated and stiffened in a longitudinal direction in response to being in an inflated condition, a protrusion extending orthogonal to a surface of the inflatable member, a tensile member attached at least two locations to the inflatable member on opposing sides of the protrusion and being slidably engagable over the protrusion so as to maintain about equal tension in the tensile member on opposing sides of the protrusion, and a sleeve attached to the protrusion configured to maintain the tensile member laterally relative to the protrusion even as the tensile member is able to slide longitudinally.

Abstract: A system is described that includes a turbine engine including an engine fan including one or more variable-pitch blades driven by a shaft, which rotates at a rotational speed which depends on a pitch of the one or more variable-pitch blades of the engine fan. The system further includes a generator configured to produce alternating-current (AC) electricity at a particular frequency relative to the rotational speed of the shaft. The system also includes a propulsor, which includes a propulsor motor and a propulsor fan. The propulsor motor is configured to drive, based on the AC electricity produced by the generator, the propulsor fan. The system includes a controller configured to control the particular frequency of the AC electricity by at least controlling the pitch of the one or more variable-pitch blades of the engine fan and thereby the rotational speed of the generator.

Abstract: A hybrid propulsion system for an aircraft is provided that includes a turbine engine, a first electric machine assembly connected to the turbine engine, a second electric machine assembly driven by the first electric machine assembly, and multiple third electric machine assemblies driven by the first electric machine assembly, wherein the multiple third electric machines provide a thrust output to propel the aircraft.

Abstract: To allow the attachment of an engine of the “Open Rotor Puller” type to the rigid structure of an attachment pylon, an attachment structure comprises a first attachment structure shifted forwards with respect to the center of gravity of the engine and connected to the rigid structure through a pyramid, a second attachment structure laid out at the rear with respect to the first attachment structure and extending in a plane of a first stringer of the rigid structure, and a third attachment structure laid out at the rear with respect to the second attachment structure. The second attachment structure comprises two engine attachments for recovering the moment along the axis of the engine, laid out on either side of a horizontal symmetry plane of the engine.

Abstract: A rear engine attachment for an engine of an aircraft which comprises a pylon having a bottom face, the rear engine attachment comprising a first fitting configured to be fixed against the bottom face and having a wall, a second fitting configured to be secured to a structural casing of the engine, two front links and two rear links, which are fixed by one and the same main link point to the wall and by two link points on either side of the second fitting. Such a motorization assembly allows for a reduction of the bulk, in particular at the rear engine attachment, which helps in improving the overall performance of the motorization assembly.

Abstract: A vertical take-off and landing (VTOL) aircraft is provided and includes wings, first and second nacelles supported on each of the wings, each of the first and second nacelles including a propeller drivable to generate aircraft thrust, and an asymmetrical power generation unit. The asymmetrical power generation unit includes a single engine unit disposed in only one of the first and second nacelles to generate power to drive the propellers of both the first and second nacelles.

Abstract: Methods, systems, and apparatus, including computer programs encoded on a computer storage medium, for receiving data related to a first flight risk factor and a second flight risk factor where the first and second risk factors include one of: a proficiency risk factor, an equipment risk factor, an environmental risk factor, or a performance risk factor. Applying a first weighting to the first flight risk factor to generate a first weighted flight risk factor, and applying a second weighting to the second flight risk factor to generate a second weighted flight risk factor. Assessing a flight risk level for a flight based on the first weighted flight risk factor and the second weighted flight risk factor, Providing data indicating the assessed flight risk level for the flight for display to a user.

Abstract: An actuator failure or disconnection detection device for an aircraft leading edge slat comprises a base and a biasing assembly mounted to the base and movable relative thereto. The base and biasing assembly are removably mountable between a fixed structure in the aircraft wing and the slat at an actuator location. The device further comprises an indicator for indicating the amount of movement of the biasing assembly in a direction towards the base when the slat is retracted towards the wing leading edge. The indicator may be a collar slidably mounted on the device.

Abstract: A remote optical control surface indication system comprising mechanisms configured to engage heads of respective fasteners that attach an alignment indexing plate to a vehicular structure having a control surface coupled thereto. The system further comprises: a camera having a field of view that encompasses a portion of an end face of the control surface when the mechanisms are engaged with the fasteners and when the control surface is in a neutral position; a source of light that is activatable to project light that illuminates the end face of the control surface; a display screen comprising an array of pixels; and a computing system configured to process image data captured by the camera to determine a current position of a centerline of the end face of the control surface relative to a baseline position and control the display screen to display symbology indicating the current position relative to the baseline position.

Abstract: An aircraft having a warning device for generating a whistling sound has a fuselage and a warning device. The warning device has a sound-generating element which is designed to generate a whistling sound if the aircraft is in an uncontrolled dive in the direction of the surface of the earth and there is a flow of fluid against the sound-generating element. The warning device is at least partially arranged on the fuselage of the aircraft.

Abstract: A method of slowing an aircraft overrunning a runway, including paving an area immediately beyond the end of a runway with foamed glass bodies to define a bed, covering the bed with a layer of cementitious material to define a composite bed, and crushing at least a portion of the composite bed with an oncoming aircraft, wherein crushing the at least a portion of the composite bed removes kinetic energy from the oncoming aircraft to slow the oncoming aircraft. The composite bed is generally resistant to fire.

Abstract: Airfield lights, components thereof, and associated methods. An airfield light can include one or more heat sink modules secured to a heat sink base to form a heat sink module on which light sources are mountable. A method includes assembling a heat sink and mounting light sources thereon. A platform of an airfield light permits mounting of a light assembly in a selected orientation on the platform.

Abstract: According to an embodiment, a system includes a controller configured to determine a set of background light intensities associated with a satellite, where each background light intensity corresponds to at least one of an orientation and a position of a light source relative to the satellite, to determine a set of relative orientations of the light source corresponding to the set of background light intensities, and to generate an image of the satellite based, at least in part, on the determined set of background light intensities and the determined set of relative orientations of the light source.

Abstract: A method and apparatus for the control of the attitude of earth orbiting satellites and the orbit and attitude control of a novel gravitational wave detection satellite configuration located near the sun-earth Lagrangian points L3, L4 and L5, utilizing the control of solar radiation pressure by the use of electrically controllable variable reflection glass panels to provide the torques and forces needed.

Abstract: A system, method, and apparatus for a vented launch vehicle adaptor (LVA) for a manned spacecraft with a “pusher” launch abort system are disclosed. The disclosed LVA provides a structural interface between a commercial crew vehicle (CCV) crew module/service module (CM/SM) spacecraft and an expendable launch vehicle. The LVA provides structural attachment of the module to the launch vehicle. It also provides a means to control the exhaust plume from a pusher-type launch abort system that is integrated into the module. In case of an on-pad or ascent abort, which requires the module to jettison away from the launch vehicle, the launch abort system exhaust plume must be safely directed away from critical and dangerous portions of the launch vehicle in order to achieve a safe and successful jettison.

Abstract: An ablator is provided to improve a fuselage protection performance while having flexibility. The ablator includes a base material formed from fiber, granular resin, and binder resin impregnated in the fiber to couple the granular resin and the base material.

Abstract: A display system can be configured to receive image data derived from the plurality of photographs and to derive a plurality of sets of identifiers such that each of the sets is associated with a photograph. Each set of identifiers can correspond to a space object and can include a name identifier, a time identifier, a latitude identifier, a longitude identifier, and/or a scalar identifier. The system may automatically identify a first orbital object in at least one of the plurality of photographs and/or receive a user selection of a second orbital object in the at least one of the plurality of photographs. In response to the user selection of the second orbital object in the at least one of the plurality of photographs, the system may derive a second set of identifiers corresponding to the second orbital object.

Abstract: A packaging system for high flexibility and speed box-last packaging comprises one or more dimensional scanning sensors that are configured to scan a group of one or more target products that are to be boxed and gather dimension information describing physical dimensions of the group of one or more target products. The system also comprises one or more packaging-production machines that are configured to generate custom-made packaging templates that conform to a pre-determined set of packaging template types. Additionally, the system comprises a packaging template buffer that comprises physically divided sections that contain multiple packaging templates selected from the pre-determined set of packaging template types that are generated by the one or more packaging-production machines. Each of the packaging templates are organized within the physically divided section based upon packaging template type.

Abstract: A packaging section of a tablet packaging device includes: a placement base of a tray; a drawer storing the placement bas; a carrier provided with compartments corresponding to the storage concave portions of the tray; a drive device of the carrier; a shutter opening/closing; a bottom of the carrier; and an opening/closing device of the shutter. The drive device performs a step of defining a tablet discharge position on the tray as an original position and returning to the original position through a tablet reception start position and a tablet reception end position which are set below a discharge opening. A step of sequentially moving each compartment of the carrier below the discharge opening from the tablet reception start position to the tablet reception end position during the step to receive one tray of tablets is performed. When the carrier returns to the discharge position, the shutter is opened.

Abstract: A method of packaging a product within a bag includes the step of providing for at least one product security element to be present on or within the bag, in a region of where the bag will be sealed. The method also includes the steps of filling the bag with the product, and subsequently sealing the bag, using heat sealing apparatus, whereby the seal thus formed passes through at least a portion of the at least one product security element, thereby permanently heat sealing the product security element to the bag.

Abstract: The invention relates to a folding device (10) for transporting an outer cardboard package (20) having folding lines and for folding at least one side flap (21) of the outer cardboard package (20). The folding device (10) comprises at least one conveyor system with a guiding unit (11) and with at least two transporting and folding shuttles (30) disposed on the guiding unit (11) for the transport of the outer cardboard packages (20) in a transport direction (TR). The at least two shuttles (30) are disposed in a row at the conveyor system and are transported in a transport direction (TR) through and/or by the conveyor system. Each shuttle (30) comprises its own, individually controllable drive (32) and further at least one folding unit (35) for folding over at least one side flap (21) of an outer cardboard package (20).

Abstract: A device (10) for optically controlling a face (13) of a blank (12) has a vacuum conveyor (20) capable of transporting the blank (12) along a path of travel (15) and which includes a conveyor belt (22) having an apertured structure of which the conveying path follows the path of travel (15) of the blank (12). A suction device (40) is suitable for pressing the blank (12) against the conveyor belt (14). An inspection device (30) inspects the face (13) of the blank (12) during its conveyance by the vacuum conveyor (20). The inspection device is located on the side opposite the vacuum conveyor (20). The suction device (40) delimits three separate successive suction sections (41, 42, 43) along the path of travel (15), including a central suction section (42) that extends opposite the inspection device (30), an upstream suction section (41) and a downstream suction section (43).

Abstract: The present disclosure relates to a method for producing an oral pouched snuff product comprising a filling material (29, 10) and a saliva-permeable pouch (43) enclosing the filling material (29, 10), the product (29, 10) having a moisture content of at most 20% by weight, in particular at most 10% by weight, based on total weight of the product (29, 10), the saliva-permeable pouch (43) having one or more seals (45, 46), and said filling material (29, 10) comprising at least 20% by weight, based on dry weight of the filling material (29, 10), of at least one ingredient having a melting temperature below 180° C., the method comprising ultrasonically welding and cutting an advancing web (32) of packaging material (7) to which the filling material (29, 10) has been supplied. The present disclosure also provides an oral pouched snuff product which is obtainable by this method.

Abstract: A method for converting a web of preformed pouches to on-demand inflatable packaging. The method may include moving the web along a path of travel, attaching an outer skin to the outside of the web, and packaging the web into a non-inflated and stored configuration. The method may also include moving the web along a path of travel, depositing at least one product into each of a plurality of the preformed pouches, and inflating each of the preformed pouches to form a cushioning material.

Abstract: A cleansing and packaging system for pipeline preparation of specialty medical instruments and method for cleansing and packaging instruments are provided herein. The cleansing and packaging system includes a first sealable cleansing compartment and a second sealable packaging compartment. A conveyor device transports medical instruments to be cleansed through a sealing entry door to the cleansing compartment, then to the packaging compartment through a sealing joining door, and then out of the packaging compartment through a sealing exit door. The cleansing compartment includes a sanitation system and a sterilization system, each which includes its own inspection devices that operate continuously to confirm the success of sanitation and sterilization operations. The packaging compartment includes a packaging system, which may include its own inspection devices that operate continuously to confirm the quality of the packaging of medical instruments.

Abstract: A method for dividing a blister strip having a plurality of blister-packaged drugs apportioned into separate sections of the blister strip is provided. A blister strip with a substrate having a plurality of depressions for drug portions is provided and an image of the substrate is generated by a 3D-sensor device. A control device evaluates the image with image analysis. Based on the analysis results, an arrangement of the depressions is determined and control signals for a separating device are generated. The blister strip is then divided into a plurality of blister strip parts based on the control signals. A blister strip dividing device is also provided.

Abstract: A bale processing machine that removes a binding from a bale allows for rapid bale processing. A method for removing the binding from the bale includes supporting the bale with a bale support at an elevated positon and securing the binding to a binding engagement device. The method also includes cutting the binding and removing the bale support from beneath the bale, such that at least a portion of the bale falls by gravity away from the binding secured to the binding engagement device.

Abstract: An innovative neck (301) configuration is suggested in order to reduce the weight of a large container for beverage dispenser. The neck (301) comprises a neck finish (303) which extends in length (Ltot) starting from the wide mouth (302) of the container to an annular support ring (305) and a smooth surface cylindrical portion (306) which joins the annular support ring (305) to the body (309) of the container. For functional reasons, the total length (Ltot) of the innovative neck (301) remains the same as the usual traditional necks for this type of container, but due to the short length (Ltot) of the neck finish (303) and said cylindrical portion (306), the weight is reduced.

Abstract: Disclosed are preforms which incorporate improvements in the region of the neck and upper segment of the body to allow the production of lightweight containers, such as bottles suitable for containing water or other beverages. In accordance with certain embodiments, the improvements include a thinner neck finish area than conventional bottles, where the thinner area is extended into the upper segment of the body portion below the support ring. Reducing the thickness in these areas of the bottle allows for less resin to be used in forming the preform and bottle.

Abstract: The invention relates to a method for providing a packaging for modified atmosphere packaging, which method comprises the steps of: providing an unfolded sheet for folding a box; folding the unfolded sheet to a box having at least an access opening and flange parts bordering the access opening, which flange parts compose an endless circumferential flange; providing a plastic foil; heating the plastic foil; pressing the heated plastic foil against the inner wall of the box and covering the circumferential flange, such that the plastic foil is laminated to box. The invention further relates to a packaging.

Abstract: A paperboard servingware container is provided. This paperboard servingware container may include a bottom panel; a curved transition portion located at the periphery of the bottom of panel. An upwardly extending wall extends from the curved transition portion opposite the bottom panel. An angled peripheral transition located adjacent the upward extending wall opposite the curved transition portion. A ledge portion that extends from the angled peripheral transition opposite the upward extending wall and away from the upward extending wall. A folded over flange portion that is bent downwardly with respect to the ledge portion.

Abstract: A corrugated box container with a main component including a base section and first and second side sections. The box container additionally includes first and second side support components associated with the first and second side sections for reinforcing the first and second side support sections. The box container further includes a cover component that is capable of engagement with the main component or the first and second side support components, such that the main component and the cover component present a fully enclosed space within the box container. The box container is erected from a knockdown configuration by folding the first and second side sections until the side sections are generally perpendicular with the base section; connecting the first and second side support components with the first and second side sections respectively; and connecting the cover component with the main component or the first and second side support components.

Abstract: A container system comprising a hollow body defined by a continuous outer peripheral wall having a first cavity and a second cavity opposing the first cavity and separated by a dividing wall, a neck opening into the first cavity and a wider open mouth at the end opposing the neck for receiving a base container therein having a lid that engages the inner surface of the outer peripheral wall to secure the base container in the mouth and substantially seal the second cavity.

Abstract: A modular pallet formed from a plurality of frame members and a plurality of deck members. The deck members extend between the frame members to define an upper deck surface and optionally a lower deck surface of the pallet. A plurality of spaced-apart channels are formed in at least an upper surface of the frame members to receive the deck members. In some embodiments the pallet may be configured as a stringer pallet and in other embodiments the pallet may be configured as a block pallet. In some embodiments the frame members are unitary stringers. In other embodiments the frame members are modular structures each comprising a block pallet subassembly and a deck support panel. The number, size, orientation and spacing of the channels formed in the frame members and the corresponding arrangement of the deck members may vary in different embodiments of the pallet. Once assembled, the frame members and deck members may be integrally connected, such as by heat welding.

Abstract: A container having a center portion and two side portions each situated at an angle to the center portion and extending in opposite directions such that the a left half of the container is substantially identical to a right half of the container. The container includes recesses and protrusions which enable the container to stack in two orientations generally perpendicular to each other.

Abstract: A stackable container, including a body and a cap threadingly engageable with a neck portion of the body and having a top portion formed with a depression for selectively oriented snap-registered engagement with a base portion of a counterpart of the body, the cap further including handle projections and a skirt. Opposite stop structures prevent rotation of the cap relative to the body beyond predetermined threaded engagement; a detent releasably captures the body in the predetermined threaded engagement. A base portion of the body having inclined side walls facilitates rotation of the body with respect to the cap. The skirt extends downwardly more than an axial length of the neck portion for guiding the body into alignment with the cap. A consumable product such as a cosmetic can extend into the cap from the body.