Abstract: Carbon/carbon materials are joined together by the placement of a brazing alloy between the materials to be joined applying a clamping pressure and passing an electric current through the parts and brazing alloy until the brazing.multidot.k15H alloy melts and when allowed to solidify forms a unitary structure from the parts.

Abstract: This invention includes an apparatus and method for molding and curing a curable composite patch used for repairing damaged contoured surface structures. The molding apparatus has a fluid impermeable outer container having a flexible outer wall. A flexible, fluid impermeable inner container containing a moldable granular material is positioned within the outer container and has a flexible molding wall on which the composite patch can be placed. Inner and outer ports are located on the inner and outer containers for evacuating the inner and outer containers. A model of an undamaged surface is formed by positioning the molding wall of the inner container against an unaffected surface and evacuating the inner container so that the granular material is rigidly held in a molded form. The patch is placed on the molding wall and the outer container is sealed with the outer wall positioned over the patch and molding of the inner container.

Abstract: Disclosed are formulations for producing chemical solvent admixtures that can be employed to clean a surface for further work; and that can be applied to cloths for the cleaning operation yet alleviate problems with solvent evaporation into the atmosphere to cause many legal and environmental problems, and a method of storing and disposing of cloths soaked with the formulation that alleviates current problems.

Abstract: The invention is a propulsion system for a lighter-than-air vehicle. In detail the propulsion system includes a pylon having a longitudinal axis and first and second ends, the first end of the pylon rotatably mounted to the vehicle and the second end extending outward from the vehicle. The pylon is rotatable about the first end in a plane perpendicular to the longitudinal axis of the vehicle. A thrust producing assembly is mounted on the second end of the pylon and is rotatable about an axis of rotation in a plane perpendicular to the longitudinal axis of the pylon. A powerplant assembly is coupled to the thrust producing assemblies to provide power thereto. An actuation system is provided for rotating the assembly about the axis of rotation. A second actuation system is provided for rotating the pylon about the first end.

Abstract: The invention is a hollow tubular member with an integral attachment end fitting.

Abstract: The invention is a cargo compartment for a lighter-than-air vehicle, the vehicle having a longitudinal, vertical and lateral axis. In detail, the cargo compartment includes a cargo carrying structure mounted to the bottom of the vehicle, the structure extending along at least a portion of the longitudinal axis of the vehicle and having a plurality of passageways extending along the longitudinal axis of the vehicle. Each of the passageways is aligned with the lateral axis of the vehicle and extend completely through the structure, and is adapted to simultaneously unload cargo from one end and load cargo from the opposite end. A cargo moving system is mounted in the floor of each passageway for moving the cargo in one end and out the opposite end of the passageway and intermediate positions therebetween. A cargo securing system is mounted on the floor of the passageway for releasable securing the cargo within the passageway at the intermediate positions.

Abstract: A device will detect man-made objects by using a polarizer mounted to a video camera. The polarizer rotates about an axis in front of a lens array of the video camera. The rotation of the polarizer alternately polarizes light received in proportion to the speed of rotation. This produces flashing in intensity for detecting the object as well as background rejection due to its lack of polarization. A man-made object having both horizontal and vertical surfaces of a type that will reflect light that can be polarized will provide flashing through the lens array as the polarizer passes through horizontal and vertical position. On the other hand, backgrounds don't have polarized components and won't flash. Attention is drawn to the man-made target. A high pass filter between the video signal processor and the monitor reduces background from the observed scene, permitting precise lock-on to the target.

Abstract: A frequency hopping spread spectrum receiver that does not require an independent synchronization source to receive and track a frequency hopping transmitter signal. In a search mode, the receiver of this invention hops in a reverse direction and at a faster rate than the transmitter hopping pattern. This results in faster signal acquisition time. The receiver uses the audio data tones of the transmit signal to detect and synchronize to the transmitter signal. Once in track mode of operation, a frequency hopping hysteresis ensures against erroneous detection of signal loss by tracking the transmitter hopping pattern for several consecutive hops before switching back to search mode.

Abstract: The invention is a ballonet system for a lighter-than-air-vehicle, the vehicle having a lift producing gasbag and a longitudinal, vertical and lateral axis. In detail, the ballonet system includes a plurality of ballonets located within the gasbag positioned along the longitudinal axis and on each side of the vertical axis of the vehicle. Each of the ballonets include a flexible sheet joined at its periphery thereof to a portion of the wall of the gasbag. A ballonet pressurization system is coupled to each ballonet for pressurizing them with air that includes the portion of the wall of the gasbag forming the ballonet having a plurality of holes therethrough. A manifold having an inlet port is joined to the wall covering the holes therein and is adapted to diffuse the pressurized air entering therein. Also included is at least one fan having an inlet port coupled to ambient atmosphere and an outlet port coupled to the inlet port of the manifold for providing pressurized air to the interior thereof.

Abstract: A protective coating process is described for simultaneously sealing and priming the anodic coating applied to a metal compound without the need for elevated temperatures during a subsequent curing step. The process comprises the steps of anodizing the component to be coated, applying the coating composition at an elevated temperature of about 150 degrees F. to thereby simultaneously seal and prime the component and curing the sealed and primed component at ambient temperatures. If cross-linking agents are employed then elevated cure temperatures are utilized.

Abstract: The invention is a propulsion system for powering an aircraft in both vertical and horizontal flight modes. In detail, the invention includes a pair of ducted lift fans mounted in the aircraft for providing thrust in the vertical flight mode. A pair of ducted cruise fans are mounted in the aircraft for providing thrust in the horizontal flight mode. Two sets of turboshaft engines are mounted in the aircraft with each of the sets comprising a plurality of the turboshaft engines, each turboshaft engine including an output shaft and having an optimal power output sufficient for powering one of the pair of ducted cruise fans in the horizontal flight mode. Each of the sets includes a sufficient number of the turboshaft engines to provide an optimal power output for powering one of the pair of ducted lift fans and one of the pairs of ducted cruise fans the vertical flight mode. A shafting system is mounted in the aircraft for coupling all of the turboshaft engines to the pairs of ducted fans.

Abstract: The invention is a propulsion system for powering an aircraft in both vertical and horizontal flight modes. In detail, the invention includes first and second gas-driven ducted lift fans mounted in the aircraft for providing thrust in the vertical flight mode. First and second shaft-driven ducted cruise fans that have inlet ducts and bypass air ducts that are mounted in the aircraft for providing thrust in the horizontal flight mode and supercharged air for the engines in all flight modes. First and second gas transfer ducts couple the bypass air ducts of the first and second ducted cruise fans to the first and second turbo compressors, respectively. First and second shaft-driven turbo compressors are mounted in the first and second gas transfer ducts, respectively. First and second high-pressure feed ducts couple the first and second shaft-driven turbo compressors to the first and second ducted lift fans, respectively.

Abstract: A dual mode semi-passive nosetip cooling system for a hypersonic weapon. A cone shaped capsule or pressure vessel is positioned within the nosetip and it is filled with a sublimating material in solid state. The capsule has a nozzle formed adjacent its forward end that directs a steady impingement stream of sublimation material to the back side of the nosetip shell in its stagnation region when the sublimating material is being heated by the surface heat on the nosetip itself. The concept is based on utilizing the advantages of both a subliminating and impingement cooling system designs.

Abstract: The invention is a propulsion system for powering an aircraft in both vertical and horizontal flight modes. In detail, the invention comprises a gas-driven ducted lift fan mounted in the aircraft for providing thrust in the vertical flight mode. A turbofan engine is mounted in the aircraft that comprises a fan section for providing thrust in the horizontal flight mode and a turboshaft engine having an output drive shaft coupled to the fan section for driving same. A gas transfer duct is mounted in the aircraft having a first end adapted to receive exhaust air from the fan section and a second end coupled to the lift fan. A turbocompressor is mounted in the transfer duct and a combustor is mounted in the transfer duct between the turbocompressor and the lift fan, the combustor for receiving and burning fuel and providing combustion gases for driving the ducted left fan. A shafting system couples the turbocompressor to the output shaft of the turboshaft engine.

Abstract: A method for reducing the length of the forebody strakes along a fighter airplane involves modifying the outer contours of intermediate frame members. The original skin panels are removed. A strake contour portion on each intermediate frame member is then cut away. A replacement outer support will be secured to each intermediate frame member to fill the gap left by the cutting away of the strake contour portion. The replacement outer edge support is secured by fasteners and new skin panels then secured in place.

Abstract: A method and system for controlling the transmission of radio frequency energy through an imperforate multi-layer fiber and resin composite structure. Multiple segments of conductive mesh are embedded between layers of fiber and resin in at least partially overlapping positions. Apertures within the conductive mesh are limited to diameters substantially smaller than the wavelengths of the radio frequency energy utilized; however, the apertures are large enough to permit resin to flow into those apertures during the cure process, thereby limiting the possibility of delamination during loading of the resultant composite structure. By utilizing nonconductive materials, such as glass fibers and a resin material having an appropriate dielectric constant, it is possible to create a radio frequency energy guide or capacitive structure which permits the controlled transmission of radio frequency energy through an imperforate composite structure.

Abstract: A device will detect man-made objects by using a polarizer. The polarizer rotates about an axis in front of a lens array. The rotation of the polarizer alternately polarizes light received in proportion to the speed of rotation. This produces flashing in intensity for detecting the object as well as background rejection due to its lack of polarization. A man-made object having both horizontal and vertical surfaces of a type that will reflect light that can be polarized will provide flashing through the lens array as the polarizer passes through horizontal and vertical position. On the other hand, backgrounds don't have polarized components and won't flash. Attention is drawn to the man-made target. The background can also be electronically eliminated from the observed scene, permitting precise lock-on to the target.

Abstract: A supplemental cooling system is provided for selectively boosting the cooling capacity of a primary cooling system having a cooling duct for feeding cooling air to an electrical device to be cooled. The supplemental cooling system includes a source of cryogenic coolant and a control valve for controlling the amount of cryogenic coolant fed to the cooling duct of the primary cooling system. Also provided is an injection nozzle for injecting the cryogenic coolant into the cooling air duct and a mixer for mixing the cryogenic coolant with the cooling air of the cooling duct so that, as the cryogenic coolant evaporates, the cooling capacity of the primary cooling system is boosted. A controller controls the operation the control valve to regulate the amount of cryogenic coolant released into the cooling duct and thereby set the amount of increased cooling provided.

Abstract: A variable load cell arrangement operative for precisely measuring loads over a range beyond the range of a single conventional single low range load cell. The arrangement includes a low range measuring element positioned in a case and having one end adapted to be connected through the case to a load and the opposing end coupled to a fixed reference. A variable pressure means, such as a controllable bellows, is interposed in the case between the load element and an end of the case whereby a predetermined force may be selectively applied to the load measuring element in a direction opposing the load to relieve the strain on the element and permit it to continue to function in an extended range. Electrical circuits, including Wheatstone bridges, are coupled to the load measuring element and provide an electrical output indicative of the applied load and an electrical output that is used to control the variable pressure means.