Abstract: A multi-channel receiver which exploites the parallel processing advantages of an optical signal processor is used to facilitate 100 percent intercept of an incomming RF signal in a dense RF environment. The receiver performs real time parallel signal processing to effectively capture a given signal of interest. The receiver modulates a laser beam with incoming RF signals. The modulated laser beam is then Fourier transformed, channelized into an array of signals of varying frequencies, optically filtered and then down converted into their original radio frequencies with only the pass characteristics altered so that the captured signal can be readily identified. An electronic controller is used to control the pass structure of the optical filter which can be reconfigured in real time to selectively pass signals having the desired characteristics.

Abstract: Tooling apparatus comprises opposing first and second dies adapted to receive a three-dimensional honeycomb core article therebetween and including opposedly aligned arrays of elongated mutually parallel translating pins, each terminating at a tip end and arranged in a matrix for longitudinal movement between a retracted position and an extended position engageable with the article. A controller individually moves each of the translating pins in a coordinated manner between the retracted and extended positions and into engagement with the article to form it to a predetermined contour.

Abstract: In accordance with the present invention, there is provided an aerodynamic control system which is attachable to an aircraft body and is operable between enhanced control and radar evasive modes. The aerodynamic control system is provided with an aerodynamic support structure which extends from the aircraft body. The support structure is rotatably attached to the aircraft body about a support structure rotational axis. The support structure has an outboard support and an inboard support which is disposed adjacent the aircraft body. The aerodynamic control system is further provided with an elongate torque member which extends from the aircraft body. The torque member has a torque rotational axis which is co-linear with the support structure rotational axis. The torque member further has an outboard end which is fixedly attached to the outboard support of the support structure. In the normal fight mode the inboard and outboard supports cooperatively rotate in response to rotation of the torque member.

Abstract: A riveting mechanism (10) is disclosed which includes a riveter (26) having a lower upset post (32) with a vertical member (48) mounting a cylinder (50) having a piston (52). At the end of the piston (52) is a roller (54). The cylinder can be actuated to move the piston and roller so that the roller contacts the outer side (66) of a intermediate arm (64) to move a stringer (14) against the lower upset post (32) to precisely locate the stringer relative the skin and lower upset post for riveting.

Abstract: A radar transponder and transponder system is provided for providing transponder communications signals embedded within radar interrogation and reply signals. The radar interrogation signals include transponder interrogation signals embedded within the bandwidth thereof. The transponders include a receiver for extracting the transponder interrogation signal and an offset frequency generator for up-converting or down-converting the transponder interrogation signal while remaining within the bandwidth of the radar signal. The transponders may be selectively enabled in response to interrogation signals having particular frequencies and/or in accordance with preset date or time schedules. The transponder outputs may be phase coherent with the interrogation signals and generated less than 10 nsec after receipt of the transponder interrogation signal. As such, the transponder reply signals are difficult to distinguish from the radar interrogation/reply signals.

Abstract: A pollutant-reducing catalytic converter for an internal combustion engine. The catalytic converter is of ceramic and operates at higher temperatures for increased efficiency. A ceramic foam is used as the substrate for the catalyst. The foam is an open-celled foam and the substrate is deposited on the walls of the cells. Thus, there is a maximum area of catalyst with a minimum amount of catalyst required. The catalytic converter can be placed in the engine compartment adjacent the engine for maximum efficiency without causing temperature problems within the engine compartment.

Abstract: A fuel containment area, and method of forming the same are disclosed herein. A fuel containment area is defined in part by a vehicle interior structure, such as an aircraft wing. Portions of the fuel containment area are provided with elastomeric partial bladders or appliques to bridge sections of the vehicle interior structure, to provide additional container integrity, and/or to segregate fuel from certain areas of the vehicle interior, e.g., about electrical components, mechanical leakages, or high temperature areas. The appliques are sealed to the vehicle interior by flexible transition joints to define a continuous, hybrid fuel container.

Abstract: A computer controlled optical system for angular alignment of structures which uses an optical imaging system input to a computer to synthesize regularly spaced reference and test line patterns replicated from binarized edges taken from the optical images of structures to be aligned. The two patterns are then combined resulting in an interference pattern in which the spacing of moire fringes indicates the amount of movement of the structures required to bring them to a predetermined alignment. All of the procedures are observable on the interference display. These moire fringe pattern are a quantitative measure of angular alignment between the reference and test images and of the edges from the structures from which they were taken. An operator programmed and controlled template automatically processes moire edge alignment measurements. An automatic template processor generates a test sequence template from the chosen areas for measurement by the operator.

Abstract: A system that partitions or divides the functions of a radio into channels and divides the functions of each channel into two major functions: 1) antenna interface and power amplification; and 2) hardwired mixing, modulation/demodulation and signal processing and further partitions the mixing through signal processing functions into the functions of a) programmable analog mixing and b) programmable digital modulation/demodulation and signal processing. Control and user interface functions, if needed for a particular application can also be functionally partitioned.

Abstract: In accordance with the present invention, there is provided an aerodynamic control device for integrated use with an aircraft having an inboard lifting member. The inboard lifting member having a leading edge, a pair of opposing distal edges and a trailing edge. The control device is provided with a movable outboard member which extends substantially about the leading, distal and trailing edges of the inboard lifting member and is spaced apart therefrom. The outboard member is provided with a leading edge portion, a pair of opposing distal edge portions, and a trailing edge portion which are collectively movable in unison in relation to the inboard lifting member to form an uninterrupted airfoil surface extending about the inboard lifting member and the outboard member for achieving desired aerodynamic control of the aircraft.

Abstract: A moving target simulator for testing a radar system has a radio frequency receiver, a digital radio frequency memory in electrical communication with the radio frequency receiver for storing a signal received thereby, a digital delay circuit in electrical communication with the digital radio frequency memory for providing a time delay between reception and transmission of the radio frequency signal, an amplitude modulation circuit in electrical communication with the digital radio frequency memory for modulating an amplitude of the radio frequency signal, a Doppler modulation circuit in electrical communication with the digital radio frequency memory for providing a Doppler-modulated signal, and a radio frequency transmitter for transmitting the radio frequency signal after it has been delayed, amplitude-modulated, and/or Doppler-modulated.

Abstract: A heat-resistant, thermally stable, ductile piston ring for an internal combustion engine having a structure comprised at least partially of fiber reinforced ceramic matrix composite (FRCMC) material. The FRCMC material includes a polymer-derived ceramic resin in its ceramic state and fibers. The ceramic portion of the material for the most part provides the heat-resistance of the FRCMC material, while the fibers produce a desired degree of ductility in the FRCMC material. Filler materials may incorporated into the piston ring to produce the desired degree of hardness and/or coefficient of friction.

Abstract: An integrated brake pad and back plate having a brake pad section formed from a first fiber reinforced ceramic matrix composite (FRCMC) material and a back plate section formed from a second FRCMC material. The brake pad and back plate are integrated because the sections are molded together to form an integral, unitary structure. The first FRCMC material used in the brake pad section includes a pre-ceramic resin in its ceramic state, fibers and possibly a filler material. The types and amount of these constituents are generally chosen so as to impart characteristics desirable in brake pads, such as high temperature and erosion resistance, and a high coefficient of friction. The second FRCMC material used in the back plate section includes a pre-ceramic resin in its ceramic state and fibers.

Abstract: A square wave power inverter includes a transformer having a primary winding and a secondary winding, first and second input voltage sources, and a pair of power switching transistors connected series between the first and second voltage sources for selectively connecting the first and second input voltage sources to the primary winding of the transformer. A pair of output terminals is connected to the secondary winding of the transformer for receiving a load. An inverter control is connected to the gates of the switching transistors for generating a gate drive signal. The inverter control generates a low impedance, substantially square wave, gate drive signal, producing a substantially square wave inverter output when a substantial load is connected to the output terminals, and a high impedance gate drive signal, producing a trapezoidal inverter output when a light load is connected to the output terminals.

Abstract: An improved shimming process and release composition for filling the gap between a releasable composite skin and a supporting body with a liquid shim material, using a novel viscous liquid release composition free of volatile vehicle. The liquid release composition is viscous and easy to apply by brushing or wiping, and enables complete and clean release of the composite skin without delamination. The release composition is easy to clean from the parted surfaces of the cured shim material on the composite skin and the supporting body.

Abstract: A deformable aircraft door which is movable between open and closed positions and is adapted to substantially maintain contact with the door frame for reducing a perimeter gap between the door and the door frame. The aircraft door comprises an edge portion which is formed to engage the door frame, and an elastic portion which is attached to the edge portion. The elastic portion is selectively expandable and contractible for permitting movement of the edge portion relative to the door frame when the aircraft door is in the closed position so as to substantially maintain contact between the edge portion and the door frame despite changes in the geometry of the door frame.

Abstract: Aqueous ceramic slurry compositions comprising a critical mixture of lithium silicate, sodium silicate, zirconia powder, glass frit and a magnetic filler, within predetermined amounts, and process of coating substrates therewith by spray or brush methods, and rapidly curing at low temperatures, up to about 500.degree. F. and as low as below about 375.degree. F. This provides a solid, protective, electromagnetic ceramic layer which is resistant to high humidity degradation or blistering after exposure to temperatures of about 1000.degree. F., such as 0.4 mach hot gas.

Abstract: In accordance with the present invention, a store covering for reducing the radar observability of an externally mounted store is provided with a non-rigid body covering. The body covering is provided with a radar reflective material. The body covering is formed to fit around a portion of the externally mounted store. The body covering is in slidable engagement and disengagement about at least a portion of the externally mounted store to allow repeated installation and removal.

Abstract: A method and a stable local oscillator system for providing a signal centered at a frequency of interest to a radio frequency (RF) converter. The method includes the following steps: (a) generating an output signal which comprises a fundamental signal centered at a fundamental frequency and a harmonic signal centered at the frequency of interest which is equal to an integral multiple of the fundamental frequency; (b) amplifying the output signal such that the harmonic signal is amplified more than the fundamental signal; and (c) bandpass filtering the amplified output signal such that the amplified fundamental signal is substantially suppressed and the amplified harmonic signal is used as a local oscillator in the RF converter. An example is given for the case where the fundamental frequency is 1.67 gigahertz (GHz), and the frequency of interest is 3.34 GHz which is the second harmonic.

Abstract: A supersonic ground vehicle having a housing configured from a pair of back-to-back symmetric housing components, and a shock-reflecting surface which extends in the direction of travel of the housing and which aerodynamically interacts with the housing to form a supersonic biplane, thereby substantially reducing aerodynamic pressure drag.