Abstract: A transition section forms a continuous contour across a gap between a pair of structures. The transition section comprises at least one rib mounted within the gap and being pivotable relative to the structures. A tip may be mounted to an aft end of the rib and may be rotatable about a tip axis. A skin panel may extend between the structures and may at least partially cover the tip. The skin panel may be deformable during pivoting of the rib such that the tip may rotate into substantial alignment with the skin panel.

Abstract: A method of alerting an occupant of a seat assembly of the occurrence of a triggering event comprising the steps of monitoring for the occurrence of the triggering event, vibrating the seat assembly and/or probing the seat assembly.

Abstract: An attachment system for mounting a tile of a thermal protection system to a substructure comprises a post assembly configured to interconnect the tile to the substructure. The post assembly is configured to allow relative sliding movement between the tile and the substructure along a plane which is generally parallel to the tile. The attachment system facilitates installation and removal of the tile from the substructure for inspection, maintenance and repair of the tile and/or the substructure.

Abstract: An attachment assembly may be adapted for securing a panel member such as a class divider or a secondary door to a mating structure. The attachment assembly comprises at least one structural pin configured to be extendable from a retracted position to a deployed position. The attachment assembly may include a base support configured to be placed in overlapping contact with the panel member. The attachment assembly may include a primary support configured to be mountable such as in overlapping contact to the base support and having at least one sleeve sized and configured to receive the structural pin which is telescopically movable. A locking mechanism such as a quick release pin may be inserted through bores formed in the sleeve and in the structural pin to prevent axial movement of the structural pin relative to the sleeve.

Abstract: A propulsion system may be operated by determining pressure in a cryogenic liquid tank storing a fluid and cooling the cryogenic liquid tank in response to determining that the pressure is greater than a predetermined value. The cryogenic liquid tank may be pressurized by admitting a gaseous form of the fluid into the cryogenic liquid tank in response to determining that the pressure in the cryogenic liquid tank is less than a predetermined value.

Abstract: A pull tool for handling an elongate article comprises a panel having opposing panel sides and opposing panel ends and a fastening mechanism extending along at least a portion of the panel sides. The fastening mechanism is configured to join the panel sides to form the panel in a sleeve configuration for encasing the elongate article therewithin. The panel of the pull tool has inner and outer surfaces with the outer surface having a substantially low coefficient of friction.

Abstract: A crawler assembly includes an attachment mechanism that is removably attachable to a stringer. The stringer has a vertical web and a longitudinal axis. The crawler assembly includes a longitudinal slider that is engageable to the attachment mechanism and having a normalizing mechanism disposable in bearing contact against the vertical web for maintaining an orientation of the longitudinal slider relative to the stringer. The longitudinal slider is movable along a direction parallel to the longitudinal axis. The crawler assembly includes a lateral slider that is mountable to the longitudinal slider and is movable along a direction perpendicular to the longitudinal axis. The lateral slider includes a drill bushing. The longitudinal and lateral sliders cooperate to move the drill bushing to at least one predetermined hole location.

Abstract: A system for forming a composite structure comprises an electromagnetic press including an upper die, a lower die and an electromagnet. The lower die may be mounted in spaced relation to the upper die for receiving a composite layup therebetween. The electromagnet is energizable such that the upper and lower dies apply a compressive force to the composite layup.

Abstract: A variable porosity system for an aircraft includes a first layer, a second layer and an actuator mechanism. Each of the first and second layers has at least one pore and are slidable relative to one another. The actuator mechanism is operative to move the first and second layers relative to one another such that the pores are movable into and out of at least partial alignment with one another to allow for fluid communication therebetween. At least one of the first and second layers is substantially continuous with an outer mold line surface of an aerodynamic member such as an aircraft wing. The actuator mechanism is configured to modulate the frequency of the opening and closing of the pores with respect to flight conditions of an aircraft.

Abstract: A wrench for engaging a workpiece comprises a pair of fixed jaws and a pair of movable jaws being movable relative to the pair of fixed jaws. The workpiece includes a plurality of flats which may be adjoined at a plurality of corners. The pairs of fixed and movable jaws may be configured to engage the workpiece in at least one of a flat engaging position and a corner engaging position. The flat engaging position comprises the pairs of fixed and movable jaws being engaged to one of the flats on each one of the opposing sides of the workpiece. The corner engaging position comprises the pairs of fixed and movable jaws being engaged to an adjacent pair of the flats on each one of the opposing sides of the workpiece.

Abstract: A door assembly has a first door integrated with a second door. The first door has a first door cowl. The second door is pivotably mounted to the first door and has a second door cowl forming at least a portion of the first door cowl. The door assembly includes at least one actuator coupled to the first and second doors. Each one of the first and second doors is pivotable between open and closed positions and defines an opening when moved to the open position. The openings of the first and second doors face in opposite directions. The actuator is operative to pivotably move at least one of the first and second doors between the open and closed positions.

Abstract: A metamaterial has a magnetic permeability response at frequencies sufficient to generate a repulsive force between a fluid and a surface to which the metamaterial may be applied. The metamaterial may be nanofabricated such that an absolute value of the magnetic permeability of the metamaterial is substantially greater than an absolute value of an electric permittivity of the metamaterial. The metamaterial may generate a repulsive force between the surface and the fluid moving relative to the surface and thereby reduce viscous drag of the fluid on the surface. A method of reducing the viscous drag of the fluid moving past the surface includes producing relative motion between the surface and the fluid and generating the repulsive force between the surface and the fluid.

Abstract: A cutting tool includes a tool body having proximal and distal ends and defining a central axis. The tool body includes a shank portion and a fluted portion. The shank portion may be configured to be rotatably engageable to a milling machine. The fluted portion may include a plurality of teeth disposed about a circumference thereof and being formed at a radius relative to the central axis. In one embodiment, the teeth may be divided into first and second tooth sections with the teeth in the second tooth section being formed at a reduced radius relative to the teeth in the first tooth section.

Abstract: A blade actuation system comprises at least one motor coupled to a rotor blade for changing the pitch angle of the rotor blade. The motor is configured to wirelessly communicate with at least one flight control computer to modulate the pitch angle. At least one generator may be mounted on a rotor shaft to generate power during rotation of the rotor shaft. The generator may provide power to the motor. The flight control computer is operative to provide control signals to at least one of the generators and motors for regulation thereof. The flight control computer, motor and generator may be configured to wirelessly communicate with one another.

Abstract: A calibration tool for an air data sensor of a vehicle comprises a target surface which is disposable on the vehicle. The calibration tool may further comprise a light pointer which is mountable on the air data sensor and which is operative to project a beam of light toward the target surface. The air data sensor may be configured as a flow direction sensor which may include at least one of an alpha vane for measuring angle of attack or a beta vane for measuring sideslip. The flow direction sensor may be mountable in spaced relation to the vehicle via a standoff. The flow direction sensor may include a hollow pivot arm having a laser pointer mounted therewithin for projecting a beam of laser light onto the target surface.

Abstract: A system for swappable battery pack for electric vehicle is disclosed. Each battery pack units is comprising a battery compartment housing, a battery carrier rack which is slidable within the battery compartment housing via at least one linear actuator. The battery carrier rack also contains a plurality of modulated battery packs nested into its docking enclosures. In order to transfer or swap the modulated battery packs, the slidable battery carrier rack must projects out from its compartment in predetermined direction and distance and then the nested modulated battery packs can easily be detached from its docking enclosures.

Abstract: A painting apparatus for applying a coating material to a member surface of a member comprises a housing, at least one slide rail, a rack assembly, a cross beam and a spraying device. The slide rail may be mountable within the housing and may have a plurality of rack positions. The rack assembly is mountable within the housing at one of the rack positions. The rack assembly is configured to support the member such that the member surface is exposed. The cross beam may be coupled to the slide rail. The cross beam is movable along the slide rail and is positionable at the rack positions. The spraying device is mountable on the cross beam and is configured to move along the cross beam while spraying the coating material onto the member surface.

Abstract: A purging system for a laminar flow control system comprises an air scoop and a diffuser fluidly connected thereto. The air scoop is disposable into an external flow of an external atmosphere. The diffuser is configured to fluidly connect the air scoop to a suction cavity of the laminar flow control system wherein the suction cavity may be disposed adjacent a porous skin of an airfoil such as adjacent a leading edge of the airfoil. The laminar flow control system may be configured to suction boundary layer flow passing over the porous skin by drawing a portion of the boundary layer flow through a plurality of pores formed in the porous skin. The diffuser ducts high pressure flow captured by the air scoop to the suction cavity for discharge through the pores to reduce the potential of blockage thereof.

Abstract: A self-contained crawler assembly is engageable to a stringer and is adapted to position a drill bushing along the stringer for performing machining operations. The crawler assembly includes a longitudinal slider, a lateral slider and a controller for regulating operation of the longitudinal and lateral sliders for positioning the drill bushing at a hole location. In a further embodiment, the crawler assembly may include a longitudinal friction drive which is directly engageable to the stringer and which is operative to move in a direction parallel to the stringer.

Abstract: A calibration system for an infrared imaging system includes an infrared sensor having a sensor model for imaging a target having a target spectral signature. The infrared imaging system includes an atmospheric model having atmospheric spectral values. The calibration system comprises a blackbody calibration source having a calibration source spectral signature and a computer for receiving the sensor model, the target spectral signature, the calibration source spectral signature and the atmospheric spectral values. The computer predicts a target spectral signature propagation at the infrared sensor and matches the target spectral signature propagation with the calibration source spectral signature propagation to determine a blackbody calibration source temperature for radiometric calibration of the infrared sensor.