Abstract: This invention provides a roller screw drive mechanism (60) driven by an electric torque motor (50) through a gear drive (58,58',58") associated with either the screw (64,94) or nut (62,92) member of the roller screw drive mechanism. Rotation of the gear drive (58, 58', 58") by the torque motor (50) effectively moves the other member of the roller screw drive mechanism into axial engagement with the brake pressure plate (32) for braking action in response to an electrical control signal fed to the torque motor. A plurality of torque motor driven roller screw drive mechanisms are mounted in a balanced arrangement about the axis of the wheel and brake assembly to effectively apply and release a brake pressure force on the brake pressure plate in response to an electrical control signal to the torque motors.

Abstract: An assembly comprises drive key wearplates mounted in pairs to longitudinal side surfaces of each of a plurality of wheel key bosses and retaining members are fastened transversely across the top of a boss to engage both wearplates of the pair. A heatshield is positioned within the wheel bore between adjacent wheel key bosses and its opposite lateral edges engage respective wearplates in a manner such that it may not move either axially or radially within the bore.

Abstract: A transparent polyurethane has exceptionally high heat distortion temperatures, that is at least 280.degree. F. at 264 psi, as well as good light transmission, ultraviolet light resistance, abrasion resistance, and the like. The urethane intermediate is one or more very low equivalent weight, multifunctional hydroxy containing compounds so that when reacted with a polyisocyanate and cured with a low equivalent weight, multifunctional polyol, a highly crosslinked polyurethane is produced.

Abstract: A nosepiece for the forward end of a missile that is launched into the atmosphere for a ballistic trajectory and a water entry impact comprises a frangible base and a separable nosecap, the base having multiple segments of rigid foam defining an axial bore into the base and a volume of soft cellular foam within the bore to protect the forward end of the missile. The nosecap is in seated relationship within the bore opening on the tip end of the base during airborne flight and separates therefrom to expose the axial bore opening prior to water entry impact such that upon impact the base is fractured by the force of water entering the exposed bore and thus separated from the missile.

Abstract: A method of fabricating a multilayer circuit board assembly capable of operating at microwave frequencies. Specifically, multilayer circuits such as complex beam forming networks and antennas having internal via holes may be fabricated in a single bonding cycle. This is accomplished by first preparing individual circuit boards (10) by pre-forming holes (18) through circuitry (14,16) etched on opposite sides of a substrate (12). The holes (18) are next selectively plated with a conductive layer (20) and then with a material (24) capable of forming a melted fusion bond and/or a solid-state fusion bond. Bonding film (56) is placed between each board-to-board interface of a multi-board assembly and the assembly of boards is subjected to a bonding cycle of heat and pressure wherein an integral unit is effected.

Abstract: A digital antiskid system for utilization with the braking system of an aircraft. Analog wheel speed signals are digitized and manipulated by a digital processor, under program control, to generate a control signal as a function of the deceleration activity of the wheels. The digital control signal is converted to an analog signal for application to a brake valve to effect application or release of brake pressure.

Abstract: Fail-safe brake valve driver (10) is provided for controlling a dual coil (A,B) brake valve. A pair of identical circuits (12, 14) are each uniquely associated with one of the brake valve coils. By means of control of an operational amplifier (16) and dual-stage current driver (18), the circuits (12, 14) each provide one-half of the current necessary for achieving brake valve control under normal operations. In the event that one of the coils (A, B) or circuits (12,14) fails, relays (56, 156) are provided for removing the failed circuit or coil from operation and allowing the remaining coil and circuit to carry the full operational load.

Abstract: An airborne system (10) and method of dispensing a plurality of sub-units (22) such that the ground plane impact pattern of the plurality of sub-units (22) substantially corresponds to a particular geometric target area. An onboard control module (150) including a microprocessor (130) which receives flight data (138) and a selected target data (140) also has a program store of sub-unit ejection sequences (132) and a logic selection of sub-unit ejection velocities (134). The microprocessor (130) selects an appropriate sub-unit ejection sequence and individual sub-unit ejection velocity in accordance with the flight and selected target data and effects a release of the plurality of sub-units in a manner such that they disperse and impact in the pattern of the selected target.

Abstract: An airborne spin dispensing apparatus (100,101) and method of dispensing a plurality of sub-units (60) such that the ground plane impact pattern of the plurality of sub-units substantially corresponds to a particular geometric ground target. An onboard microprocessor (24) which receives flight data (26) and a selected target data (28) also has a program store of sub-unit ejection sequences each of which corresponds to a particular target impact geometry. The microprocessor (24) selects an appropriate sub-unit ejection sequence in accordance with the flight and selected target data and effects a release of the sub-units (60) from the spinning apparatus such that their ground impact pattern substantially matches the geometry of the ground target.

Abstract: An apparatus (32) and technique for compensating for motion in an electro-optical camera system. An image system is maintained on an aircraft for generating an image of terrain while the aircraft is in flight. A high resolution linear array (24) generates an image from a field of view (30), while a rectangular array (26) generates a corresponding image on a periodic basis. The rectangular image serves as a reference for the pixels of the linear array for determining if features in the linear array have shifted or distorted. An error is generated corresponding to the differences between the linear array and the rectangular array, the linear array being corrected as a function of the error.

Abstract: The invention herein relates to a computer organization capable of rapidly processing extremely large volumes of data. A staging memory is provided having a main stager portion consisting of a large number of memory banks which are accessed in parallel to receive, store, and transfer data words simultaneous with each other. Substager portions interconnect with the main stager portion to match input and output data formats with the data format of the main stager portion. An address generator is coded for accessing the data banks for receiving or transferring the appropriate words. Input and output permutation networks arrange the lineal order of data into and out of the memory banks.

Abstract: This radar system makes it possible to collect complete stereo data in a single pass by utilizing an orbiting, side looking, bi-static, synthetic aperture radar. This system utilizes at least two orbiting spacecraft in synchronous parallel orbits with each other and separated by a tether. A transmitter transmits radar signals to a planet's surface which are reflected back and received by two receivers, one carried by each spacecraft. When the signals are combined, the layover produces a three dimensional picture in which vertical height information may be determined.

Abstract: An aircraft-launched, ram-air inflatable, passive radar decoy (10) has a substantially cylindrically shaped body (12) having an open forward end (14) and a closed porous rearward end (16), the body comprised of a fabric reinforced composite having a high radar reflectivity coating on at least it interior surfaces (12i, 16i). A rod-shaped weight (22) is attached at the forward end (14) by way of shroud lines (20), the weight (22) providing the highest weight-to-drag-area ratio for the particular size body. The decoy (10) provides a high radar cross section and broad angle coverage to ground-based source of radar when it is ram-air inflated upon ejection by the aircraft into its adjacent windstream.

Abstract: An efficiency monitor circuit for an antiskid system is provided. The efficiency of the antiskid system is determined by monitoring the antiskid signal as to peak positive and peak negative moves thereof. The difference in these two signals corresponds to the efficiency of the antiskid system. This difference signal is compared to a threshold signal for comparison of the efficiency to a signal corresponding to an acceptable minimum value. Should the efficiency of the antiskid system fail to meet the minimum value, an alarm is activated.

Abstract: A torque tube (50) having a cylindrical body (50a) is characterized by a plurality of key surfaces (50k) which extend radially from the surface (50s) and extend longitudinally from an inboard end (50i) to terminate at an outboard end (50o) in a radius (R3) which defines a transition (50t) into a radially extending rib (50r). The cylindrical body portion between adjacent keys (50k) also extends at the outboard end (50o) into a flange (50f) which is continuous about the outboard end of the tube. The combination of radially extending ribs (50r) and flange (50f) define T-sections at the outboard end (50o) which provide the strength requirements of the torque tube in its intended service application.

Abstract: A split retaining ring for locking a separable tire bead flange on a wheel rim has inboard and outboard facing portions and two circumferentially aligned terminal ends, each terminal end characterized by an outboard facing tab having a drilled-through bore. A buckle member having a pair of apertures is mounted on the retaining ring such that each tab passes through a respective aperture and the buckle functions to maintain the terminal ends of the retaining ring in a specific orientation when it is mounted on a wheel rim. A wire fastener is positioned through each drilled bore in a tab to retain the buckle member on the split retaining ring.

Abstract: An airborne spin dispensing apparatus (100,101) and method of dispensing a plurality of sub-units (60) such that the ground plane impact pattern of the plurality of sub-units substantially corresponds to a particular geometric ground target. An onboard microprocessor (24) which receives flight data (26) and a selected target data (28) also has a program store of sub-unit ejection sequences each of which corresponds to a particular target impact geometry. The microprocessor (24) selects an appropriate sub-unit ejection sequence in accordance with the flight and selected target data and effects a release of the sub-units (60) from the spinning apparatus such that their ground impact pattern substantially matches the geometry of the ground target.

Abstract: This invention provides for heating a brake assembly electrically to prevent it from freezing. More specifically this invention provides for heating electrically an aircraft multi-disk brake assembly.An electric resistance heating element 12 is adapted to form a heater 10 to provide heating to a brake stack 44. Heat may be transferred either directly to the brake stack 44 or indirectly by first heating a member of the brake assembly 36. This member in turn transfers heat to the brake stack.The heater 10 may be formed to fit within the cavity formed by a torque tube 26 wherein the heater abuts a substantial portion of the torque tube 26.Signals from a thermocouple may be used for activation and deactivation of the heater 10.

Abstract: A plurality of polyurethane layers, some of which have a contrasting color with respect to an adjacent layer is formed into a laminate. During preparation, each layer is separately formed, as by spraying, and the contrasting color ensures that the preceding layer can be fully covered. The laminate can be utilized to cover areas or objects which are otherwise difficult to ensure that it has a continuous or complete coating. The invention is suitable for use as a coating and for the preparation of various in situ articles or enclosures, for example a fuel tank, such as commercial and military aircraft.

Abstract: A spray nozzle extension is affixed to the output of a conventional spray gun apparatus to allow an operator to spray a polymeric elastomer into enclosed spaces of an integral fuel tank cavity such as to form an in situ tank within the cavity. The nozzle tip is extended from the spray gun by a flexible hose and the complete unit includes variously arranged in-line filter and swivel connectors to achieve dispersion of lumps in the spray material and axial, yaw, and pitch rotation of the nozzle tip respectively.