Abstract: A flush-mounted articulated window assembly for use in a vehicle, the window assembly adapted to be mounted in a window opening such that, when closed, it is generally flush with the exterior surface of the vehicle. The window assembly includes a transparent sheet with at least one window-mounting member bonded by two separate adhesives to an inner surface of the sheet. The mounting member includes projections which space the mounting member from the inner sheet surface, and/or perforations which allow air and moisture to reach the space provided between the mounting member and the inner sheet surface. A first adhesive temporarily fixtures the mounting member to the sheet. A second adhesive permanently bonds the mounting member to the inner sheet surface. The bond created is sufficiently strong such that application of a load sufficient to cause a failure results in a failure other than in the adhesion of the adhesive to the mounting member and the panel.

Abstract: A window assembly for use in a vehicle comprises a glass panel having inner and outer sides. A latch element having a latch attachment portion and at least one hinge element having a hinge attachment portion are joined via a substantially cured adhesive at the inner side of said glass panel such that there is no exposure of the latch element and the hinge element on the outer side of the glass panel. The substantially cured adhesive is selected from the group consisting of a moisture-activated adhesive, a thermally-activated adhesive, a chemically-activated adhesive, an aerobically-cured adhesive, an anaerobically-cured adhesive, and a radiation-cured adhesive. The window assembly is adapted for mounting on the vehicle such that when fitted within a generally vertical window opening of the vehicle, the glass panel will be generally vertically mounted, and the window assembly preferably comprises one of a side window, rear window, and lift gate window of the vehicle.

Abstract: A system and method for electromagnetically arresting an aircraft landing on an undersized runway, as on an aircraft carrier. The system preferably comprises a cross-deck pendant cable coupled to two purchase cables that are wound around low inertia purchase cable spools on opposite ends. The shafts of the purchase cable spools are mechanically coupled to one or more low inertia induction machines used to arrest the landing aircraft. As the aircraft contacts the cross-deck pendant cable and extends the purchase cables down the runway, power electronics in the system apply a torque based on closed-loop feedback to the induction machine acting as a generator, and the mechanical energy of the aircraft is converted to electrical energy at the generator and is dissipated as heat in an attached resistor. The one or more induction machines are preferably cup-type generators, and the generators may be briefly run as motors to initially reduce the tension on the purchase cables.

Abstract: A superconducting coil conductor composed of a plurality of strands (10) twisted together to form a cylindrical structure, each strand (10) being composed of a core (2) composed of a plurality of parallel filaments of a superconducting material, enclosed by a metal sheath (4) forming a matrix in which at least some of the filaments are embedded, and a tubular member (6) enclosing the sheath (4) so as to be in intimate electrical contact with the sheath (4) and support the core (2).The conductor is held in support plates (16) each presenting a U-shaped conductor support channel (20) spaced inwardly from an exterior surface of the support plate (16) which is in contact with the cryogen, and a conductor compression wedge (18) inserted in the channel (20) for holding the conductor in place.The solenoid coil further includes insulating members (38) interposed between the support plates (16) and projecting radially beyond the conductor support system.

Abstract: A submersible electric propulsion motor includes a sealed cylindrical stator housing defining a central flow passage and a cylindrical rotor core disposed within the stator housing passage such that the stator housing encompasses the rotor core. The rotor core defines a center flow opening which communicates with inlet and outlet ends of the stator housing passage. The motor also includes a propulsion propeller having a plurality of radial blades and a central cylindrical hub. The propeller is disposed within and across the rotor core opening with its periphery being rigidly connected to the rotor core. A support structure has end portions disposed at and rigidly attached to the stator housing inlet and outlet ends, and an axial portion which extends axially through the stator housing passage and rotor core opening and is rigidly attached to the radial portions.

Abstract: A vehicle seat belt system operational as a passive two-point or as a part passive and part active three-point seat occupant restraint. A continuous belt 15 coupled at one end to a retractor mechanism 16 mounted within a vehicle door passes through a guide ring 19 on the door frame and extends diagonally downwardly across the seat 13 to a second guide ring 23 anchored to the floor. The terminal end of the belt projects through the guide ring 23 and carries a buckle engaging element 27 that engages the guide ring 23 to prevent retraction of the belt 15, whereby the latter automatically operates as a two-point restraint system.The seat occupant has the option of extending the belt 15 as a lap belt to a buckle device 32 on the outboard side of the seat. This changes the belt system to a partially passive and partially active three-point restraint system.