Abstract: An internal combustion rotary engine has a housing which has a plurality of outer rotors and stators and bearings, the outer rotors having a plurality of curved channels on inner surfaces thereof and one of the stators having intake ports and a port for a spark plug; a shaft which is rotatably supported by the bearings and has a plurality of holes communicating with a center passage formed therein for flowing of a coolant; a central rotor being formed as a frustum and fixedly supported by the shaft and having a plurality of curved channels overlapping with the channels on the rotors at ends thereof, but in a reversed direction, and on a first conical surface at a middle portion thereof and a second conical surface with a larger slope than the first conical surface at a front portion thereof to define a combustion chamber.

Abstract: A diverter valve arrangement for a fluid flow duct having selectively alternative outlets. In order to avoid an over-area condition during transition an additional valve is provided to delay the effect of operating the main changeover valve. The diverter valve comprises a sleeve valve which covers/uncovers side outlet ports in the duct wall and a blocker valve made up of a plurality of segments pivoted to the inside of the sleeve valve. As the sleeve translates to uncover the side ports the blocker valve leaves deploy to obstruct axial flow. The additional sleeve valve acts as a shuttle and temporarily follows the main sleeve to delay uncovering the side ports.

Abstract: Juxtaposed recirculation zones for the pilot in the burner of an augmentor for a gas turbine engine is created by fabricating the engine's tail cone in two components and including an annular gap defined between the juncture of both components that injects a stream of cooling air radially into the augmentor's gas path for eliminating or minimizing screeching in the augmentor.

Abstract: A circumferential element discourages the flow of hot gases exiting from a labyrinth or other type of seal in a gas turbine engine. This seal exit flow discourager may be integrally incorporated in the honeycombed seal surface of a labyrinth seal or in the ring supporting the honeycombed seal surface. The seal exit flow discourager has a generally radial surface upon which impinges the jet of hot gases exiting from the labyrinth seal. This surface prevents the exiting hot gases from impinging directly on the low-pressure turbine shaft. At the same time low-temperature air from the compressor is flowing through an annular passageway located between the labyrinth seal and the low-pressure turbine shaft. The seal exit flow discourager diverts the hot gases exiting from the labyrinth seal into the stream of cooling air, thereby causing turbulent mixing of the hot gases and cool air.

Abstract: A modular reusable rocket motor combined with reusable, disposable, and expendable assemblies to provide customized operational characteristics for a rocket launched therewith.

Abstract: The valve assembly for a rotary compressor includes an elongated valve member which rests on pads on each side of the valve seat and includes an intermediate sealing section normally sealing against the valve seat. An elongated valve spring biases the sealing section toward engagement with the valve seat. An elongated spring backer sits on one end of the valve spring and the other end of the valve member. One end of each of the valve member, valve spring and spring backer are bolted to the compressor end plate. The other end of the spring backer permits the corresponding end of the valve member to slide along the end plate as the valve member moves between its open and closed positions, while restraining the end of the valve member from moving away from the end plate. A backer support, positioned between the spring backer and the head of the bolt, spreads the clamping force and defines a line about which the valve member and valve spring flex.

Abstract: A vane pump includes a pump housing formed with a cylindrical inner space, intake ports and exhaust ports, a rotating shaft rotatably supported by the pump housing, a rotor received in the cylindrical inner space to be rotated by the rotating shaft, a cam ring disposed in the cylindrical inner space, a plurality of vanes held by the rotor to define plural pump chambers between the rotor and cam ring. Fluid sucked from the intake ports is pressurized and discharged to the exhaust ports. The vane pump is further provided with first and second pressure chambers and a throttle passage connecting the first and second pressure chambers. Pressurized fluid discharged from one of the exhaust ports is led to one of the two pressure chambers and pressurized fluid discharged form the other of the exhaust ports is led to the other of the pressure chambers while pressurized fluid is taken out from the second pressure chamber to be supplied to a fluid device.