Abstract: Chaser for cutting threads on a work piece, the chaser having thread cutting formations with crests and roots, one flank of each of said formations being relieved at a first angle from the region of the crest toward the root and being relieved at a greater angle in the region adjacent the root of the formation. The chasers may be provided in sets with odd numbered chasers being mirror images of the even numbered chasers.

Abstract: A turbocharger housing comprises a central housing portion having means for rotatably supporting the turbocharger shaft and a pair of end housing portions adapted to be bolted to the central housing portion at mating annular surfaces of each housing portion. In one advantageous form of the present invention, the end housing portions include a recessed wall for defining a flow passageway adjacent a radially expanded wall portion of the central housing, and a plurality of vanes are integrally formed on the end housing portion to extend outwardly from the recessed wall toward a mating annular surface on the central housing portion. One or more sets of radially spaced mating annular surfaces provides a secure engagement between the end housing portions and the central housing portion. Moreover, the end plates are removably secured to the central housing portion so that the turbocharger mechanism can be removed as a unit with the central housing portion.

Abstract: A thermocouple rake for measuring the temperature of heated fluids. The thermocouple rake is provided with a cooling chamber for circulating a coolant about individual thermocouple assemblies to cool the assemblies during use in the hot gas. A U-shaped channel is formed downstream in the flow of fluid to accept lead wires from the thermocouple assemblies to deflect the hot gas fluid from contacting the lead wires.

Abstract: A multiple wire joining device is disclosed which includes a generally tubular, deformable, electrically conductive housing having multiple apertures formed in the wall thereof. The apertures are axially spaced apart along the length of the housing and are each adapted to admit a wire therethrough so that it may entend axially along a length of the housing. The spacings between the apertures are sufficient to permit the admittance of a wire into the housing through each of the apertures a sufficient distance to enable the crimping of the housing adjacent each aperture to retain the respective wire therein.

Abstract: A turbocompound engine having a stratified charge or diesel cycle rotary internal combustion engine, with a first output shaft and a turbine engine with a second output shaft. The first and second output shafts are coupled together so that the shafts rotate in synchronism with each other and provide a rotary output from the turbocompound engine. A valve variably directs air inducted into the engine between the turbine engine and internal combustion engine in dependence upon engine operating conditions.

Abstract: A shipping container for transporting a variety of aircraft engines includes a base, a cover and a plurality of engine-engageable support portions carried on the base which are at least one of vertically, horizontally and angularly displaceable with respect to the base of the container. The cover is disposable over the base so as to contain the engine therebetween. The support portions are preferably formed on the surface of swing brackets pivotally mounted to vertically adjustable riser brakets, which are telescopically received in corresponding riser support brackets, which are in turn horizontally slidably affixed to base brackets on the container base. The cover and base are externally dimensioned so that one container can be stacked atop another container, or moved by a forklift, and so that individual bases are stackable as well.

Abstract: A system for training aircrews, particularly aircrews of relatively slow-moving aircraft such as helicopters in laser/electronic warfare countermeasure tactics and the use of laser/electronic warfare countermeasure equipment is provided. The system is operable with the aircraft's instruments to present the simulated threats whenever such threats are both with the line-of-sight of, and within the presentation range of the aircraft. Accordingly, such a system includes a plurality of independently operating threat-simulating transmitter units simulating both stationary and non-stationary threats by broadcasting omnidirectional radio frequency signals over a common carrier frequency. On-board equipment, carried on the aircraft determines whether the aircraft is both within the line-of-sight and within presentation range to the threat based upon receipt of the transmitter unit signals and the location of the threats relative to that of the aircraft.

Abstract: Apparatus for isolating a radar receiver from a radar transmitter in a continuous wave, single antenna radar system where a circulator connects transmitter, receiver, and antenna. The apparatus includes a reactive element which reflects back through the circulator a portion of a transmission signal provided from the transmitter through the circulator to the antenna. The reflected transmission signal portion is equal in magnitude and opposite in phase to a leakage portion of the transmission signal transmitted by the circulator from the transmitter to the receiver. The reflected and leakage signal portions cancel in the circulator to enhance the isolation of the receiver.

Abstract: A variable geometry device is provided for synchronous control of flow of fluid at the compressor inlet and outlet of a turbine engine. The turbine engine includes a support housing, a compressor contained within the support housing, a set of variable inlet guide vanes and a compressed air outlet in which a pair of spaced walls define an annular and radially extending diffuser passageway. The inner end of the diffuser passageway is open to the compressor outlet while the outer end of the diffuser passageway is open to the combustion chamber for the turbine engine. A plurality of circumferentially spaced diffuser vanes are mounted to one of the diffuser walls and protrude across the diffuser passageway. An annular recessed channel is formed around the opposite diffuser wall and an annular ring with a hollow cavity is mounted within the channel.

Abstract: A support spider for a surface heating element is formed from a single piece of sheet material by first cutting a blank defining three legs. Two of the legs extend oppositely along a common longitudinal extent, while the third leg extends parallel to one of the first and second legs and is connected thereto by a web of material forming an integral hinge. The third leg is first folded about the integral hinge so as to be substantially adjacent to, overlying, and coextensive with one of the first and second legs, and the two adjacent legs then spread apart so that a symmetrical three-leg spider is formed.

Abstract: A turbocharger having a main housing with a throughbore in which a tubular bearing carrier is mounted. A main shaft having a turbine at one end and a compressor at its other end extends through the bearing carrier and is rotatably mounted to the housing by two spaced bearing assemblies. A lubrication system supplies lubricant to a squeeze film damper for hydrostatically damping the shaft vibrations and the discharge of the lubricant from the squeeze film damper is employed to lubricate the bearing assemblies.

Abstract: An ultraviolet radiation dosimeter is to be employed by a person the skin of whom has been protected by a substance tending to inhibit the transmission of the radiation therethrough and which substance has a predetermined value of inhibition. Disposed to the radiation is a sensor that develops a signal in correspondence to the level of the radiation. Responding to that signal is a processor which accumulates a representation of the magnitude of the signal as effectively integrated with an elapsed time of exposure of the sensor to the radiation. An indication of the degree of the accumulation is yielded in response to the representation of the magnitude. The value of inhibition is used in order selectively to adjust in correspondence thereto the determination of the degree at which the indication is yielded. Both analog and digital circuitry are presented, along with variations and additions such as also adjusting response in accordance with the skin type of the user.

Abstract: The present invention provides a two stage fuel pump which is particularly suited for piston aircraft engines. The fuel pump includes a housing having a fuel inlet and a fuel outlet where the fuel inlet is open to a cylindrical swirl chamber formed in the housing. The first pump stage has its inlet open to the inlet chamber and its outlet open to an intermediate chamber formed in the housing. The second pump stage has its inlet open to the intermediate chamber while its outlet is fluidly connected through a fuel control valve to the fuel outlet. A pressure responsive valve is fluidly connected between the intermediate chamber and inlet chamber and recirculates fuel from the intermediate chamber and to the inlet chamber whenever the pressure in the intermediate chamber exceeds a predetermined pressure.

Abstract: A low cost, integrated, aircraft fuel management system. A system control unit receives engine variable signals and provides a signal to a motor control unit which thereby controls a variable speed motor. The motor drives a positive displacement pump which delivers and meters fuel to a slinger type turbine engine capable of handling slurry fuels. In a preferred embodiment, compressor discharge pressure (CDP) is supplied to the airframe fuel reservoir thereby pressurizing the fuel supply and minimizing the power requirements of the motor driving the fuel pump.

Abstract: A novel turbine inlet nozzle assembly is provided for use with a gas turbine engine and includes unique nozzle cooling means. The turbine inlet nozzle of the present invention comprises an inner annular shroud, an outer annular shroud coaxial with and spaced radially outwardly from the inner shroud and a plurality of circumferentially spaced vanes extending between the shrouds. The shrouds and the vanes, moreover, are of integral construction with each other and, preferably, each vane has a hollow interior. An annular impingement plate is fixedly secured about each axial end to the outer periphery of the outer shroud while, similarly, a second impingement plate is secured at each axial end to the inner periphery of the inner shroud. Moreover, the impingement plates include a plurality of holes formed therethrough and through which a portion of the turbine compressor output is bled to cool the inner and outer shrouds.

Abstract: A self-lubricating die cylinder assembly is provided containing a cylinder, piston, expansion reservoir and working chamber. A lubricating oil recirculation means is provided to transport oil between the working chamber and the expansion reservoir during each of the piston strokes. A flow restrictor is provided to create a pressure differential between the two chambers during movement of the piston thus creating a jet mixture of compressible working fluid and lubricating oil spraying onto the walls of the cylinder.

Abstract: A torque meter is provided for use in conjunction with a layshaft having a forward and rear end and which is rotatably mounted in a housing. The layshaft is axially movable with respect to the housing between a forward and a retracted position while a gearing arrangement in mesh with the layshaft urges the layshaft towards its forward position with a force proportional to the shaft torque. The torque meter comprises a body secured to the housing adjacent the front end of the layshaft which forms a chamber open to the front end of the layshaft while a piston is axially slidably mounted within the chamber. The chamber is pressurized with a fluid, such as oil, which urges the piston against the front end of the layshaft with a force proportional to the pressure so that the piston balances the layshaft against the axial force imposed by the engine. A fluid pressure gauge determines the pressure within the chamber which varies proportionately with the layshaft torque.

Abstract: A press cushion assembly includes a variable volume chamber which is expanded during operation of the press to an open condition and is contracted during operation of the press to a closed condition. During expansion of the variable volume chamber, a flow of lubricating liquid is conducted to the variable volume chamber from a reservoir. At the same time, a flow of gas is also conducted from the reservoir to the variable volume chamber. Upon closing of the press and contraction of the variable volume chamber, a flow of lubricating fluid and gas is conducted from the variable volume chamber back to the reservoir. The cushion assembly may include a manifold plate in which a plurality of piston and cylinder assemblies are mounted. A reservoir disposed in the manifold plate is connected in fluid communication with the piston and cylinder assemblies by a plurality of passages. Check valves may be provided in the passages so that the lubricating fluid can flow in only one direction.