Abstract: A heat absorbing coating having a plurality of micro-capsules each being an encapsulant shell and a heat absorbing material within the shell, and a carrier adherable to a substrate and throughout which the micro-capsules are dispersed. The heat absorbing material is preferably a phase change material and can be non-limitedly chosen from the group consisting of polyethylene, polypropylene, polywax, and combinations thereof. Shell material can be a metal such as copper, for example, or a polymer. The carrier can be a sprayable polymer mix which provides significant efficacy in uniform application to a substrate. An inventive substrate structure, such as an aircraft structure for example, has thereon the above-defined coating in an amount sufficient to absorb a sufficient amount of heat from the substrate to substantially inhibit thermal erosion in normal operating environments.

Abstract: An on-site environment monitoring system including at least one on-site environment condition sensor, an on-site alarm signal, and an on-site alert system. The monitoring system includes an on-site alert system having an on-site programmable microprocessor for activating the on-site alarm signal and in communication with the at least one environment condition sensor. The microprocessor is programmable to thereby provide pre-set respective ranges of environment condition values such that activation of the on-site alarm signal occurs when at least one on-site sensed environment condition value is below or above the programmed pre-set range of values. The present system achieves local control of environmental factors by providing on-site monitoring coupled with on-site alerting to thereby facilitate correction of unwanted ambient conditions by on-site personnel without requiring network-monitoring interaction and consequent time consumption.

Abstract: A compact universal apparatus which is mountable within an optimally sized weapons bay of a conventional fighter aircraft, which includes an automatic scissors or trapeze type lowering linkage mechanism for a conventional or inventory bomb ejector rack unit (BRU) having automatic latching, release and forced ejection mechanisms for conventional inventory weapons, characterized by an adaptor designed for the fixed attachment of the bomb ejector rack unit to the linkage of the lowering mechanism of the apparatus. The ejector rack unit is one adapted to the forced ejection of large bombs, attached or latched directly thereto, and to the rail launching of missiles having launching rails attached or latched directly to the ejector rack unit, with conventional automatic latch up of the bail lugs of the bombs to the launch rack lugs of the ejector rack unit, for forced ejection of the bombs, and with conventional automatic latch up of launch rails of conventional missiles for rail launching of the missiles.

Abstract: A non-chrome process for the pretreatment of substrate surfaces to simultaneously clean them and improve their bonding strength for organic coatings such as adhesives, protective primers, sealants, paints, composites and similar materials conventionally bonded to such substrates, including non-chromated or chromated curable organic resin protective coatings applied directly to bare aluminum substrates. The invention involves the use of novel wipe solvent compositions containing a major volume of an environmentally-safe volatile organic solvent which has a low composite vapor pressure or is otherwise exempt from federal, state or local regulations, and a minor volume of a polyfunctional coupling agent, preferably of the silane type.

Abstract: In accordance with the present invention, there is provided an aerodynamic control device for use with an aerodynamic lifting member. The lifting member is defined by a horizontal reference plane disposed therethrough. The control device is provided with at least one support rotor extending from the lifting member. The support rotor is sized and configured to rotate about a rotor axis of rotation which is disposed generally parallel to the horizontal reference plane. The support rotor has an inboard segment which is disposed along the rotor axis of rotation and in rotational communication with the lifting member. The support rotor has an outboard segment disposed off-set from the rotor axis of rotation. The control device is further provided with a control device body which is engaged with the outboard segment of the support rotor. The control device body is sized and configured to translate generally orthogonal to the horizontal reference plane in response to rotation of the support rotor.

Abstract: A method and apparatus for decoding a phase encoded data signal utilizes windowed data which is transformed into real and imaginary frequency components thereof. The real and imaginary frequency components are converted into phase and magnitude information. The magnitude information is used to calculate a threshold based upon a signal-to-noise ratio, and the phase of the data signal is corrected by identifying and sorting magnitude peaks. The data signal is differentially demodulated and the demodulated data is then multiplied by a correlation sequence so as to facilitate its being converted into a binary number.

Abstract: A personal communications system has a plurality of personal communications units defining a network. The personal communications units are configured to send and receive digital communications among one another via the network. A wireless interface adaptor further defines the network and is configured to function as a repeater. The personal communications units are configured to cooperate with the wireless interface adaptor when the wireless interface adaptor is available. The wireless interface adaptor coordinates access of each personal communications unit to at least one other personal communications unit. The personal communications units are further configured to cooperate with one another to effect communications therebetween when no wireless interface adaptor is available.

Abstract: A tail fin assembly for a munition having a housing configured for attachment to the munition, at least one flight control surface, an actuator for effecting movement of the flight control surface(s), so as to facilitate guiding of the munition, and a guidance system for controlling the actuator mechanism. The guidance system has a global positioning system (GPS) receiver for effecting control of the actuator mechanism.

Abstract: A heat-resistant, thermally insulative, ductile turbocharger housing 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 form and fibers. The material, being for the most part ceramic, provides the heat-resistance and thermal insulating capabilities of the FRCMC material, while the fibers produce a desired degree of ductility in the FRCMC material.

Abstract: Presented in this invention is a technique for producing a null in the frequency spectrum of an FM signal pulse, the null matching an interference that has been superposed on the signal pulse. By matching the null to the interference, the energy in the frequency spectrum is shifted in such a way that when the interference is rejected by a band elimination filter, none of the useful energy would be discarded along with the rejected interference. Consequently, a signal resulting from the technique has a much higher amplitude than previously filtered signals. This leads to the signal being more readily recognized by detection systems, such as a radar detector.

Abstract: A method for producing a self decontaminating surface to decontaminate chemical and biological contaminants that are deposited on the surface and decontaminatable through reaction with free hydroxyl radicals. The method first includes determination of a surface to be treated and which is exposable to ultraviolet light. Second, a coating of nanoparticles of a transition metal oxide, non-limitedly exemplified by anatase titanium dioxide, is applied to the chosen surface. Application of the coating is accomplished by spraying heated nanoparticles or clusters thereof from a feed stock onto the surface to form a nanoparticle coating, with the nanoparticles being at a temperature of at least about 750° C. upon exit from a spray apparatus and of a size between about 5 nm and 100 nm.

Abstract: A method for rapidly manufacturing “green-state” ceramic matrix composite components, components made from this method, and a resin/catalyst precursor mixture used in the method. The method includes manufacturing a component by preparing the precursor mixture by mixing a requisite quantity of a polymer-derived ceramic precursor resin, a catalyst, a discontinuous reinforcing fiber and filler material, and then loading this precursor mixture in a preheated mold. The precursor mixture then is cured in the mold to form the component which is porous. Thereafter, the component is reinfilitrated with a resin to at least partially fill the pores of the component. This method yields a ceramic matrix composite component that is cured in approximately one minute as well as a resin/catalyst precursor mixture that can be stored in excess of four weeks.

Abstract: A vibration-absorbing end effector of an automated drill and countersink machine having a shock to mitigate communications of vibrations to the drill tool, while simultaneously dampening the vibrations at their source, in order to increase control of a drill tool during drilling and countersinking operations. The end effector comprises a measurement scale to ensure that the depths of holes to be drilled and countersunk can be checked and corrected in accordance with corresponding ideal depths stored in a memory of the computer already interfaced to the end effector. Furthermore, the pressure foot of the end effector is upwardly rotatable to access the drill tool to the chuck.

Abstract: A personal communication system provides full duplex digital communications between multiple users for both audio and data. A universal adaptor interface receives a plurality of wireless communications. The wireless adaptor interface multiplexes the plurality of wireless communications into a composite signal. The universal adapter interface transmits the composite signal wirelessly. At least one personal communications unit receives the composite signal. Multiplexing the plurality of wireless communications facilitates simultaneous reception thereof by the personal communications units.

Abstract: The present invention is embodied in an automated system for the positioning and support of a machine tool within a workpiece supporting assembly, comprising a pair of generally parallel, planar longitudinal translation modules affixed to the assembly and having longitudinal sliding pads and a longitudinal movement device, a transverse translation module affixed to the longitudinal sliding pads in a generally perpendicular orientation to the longitudinal modules and having transverse sliding pads and a transverse movement device.

Abstract: Aerodynamic control apparatus which deflects a control-surface-member into the airstream for creating drag on an aircraft. This drag flap mechanism includes a strut and hinge plate which together constrain the control-surface-member to move in a coupled manner about mutually perpendicular axes. There is an actuator from the controls of the pilot which moves the hinge plate which in turn moves the control-surface-member in that coupled manner. It moves between a fully feathered position presenting minimal resistance to the airstream and a fully operative position presenting maximum resistance to the airstream. The preferred embodiment of the drag flap mechanism is as a continuation of the wing tips where two control-surface-members are hinged about a common axis on the hinge plate so they can open like a split flap. The motion of these two control-surface-members are constrained to allow the force of the air opening the two surfaces to assist in pushing the two surfaces more into the airstream.

Abstract: A strain gage assembly 10 includes a mounting substrate 12 having an adhesive surface 14 and a gage surface 16. The adhesive surface 14 of the mounting substrate 12 includes an adhesive layer 18 disposed thereon operable to affix the mounting substrate 12 to a component. The adhesive layer 18 is further operable to allow ready detachment of the mounting substrate 12 from the component. The gage surface 16 of the mounting substrate 12 includes a strain gage 20 disposed thereon. The mounting substrate 12 may be formed from a material operable to reduce a strain level received by the strain gage 20.

Abstract: A Yagi antenna array is specifically designed for insertion in a thin wing leading edge radome. Tubular elements for driver, director components are inserted within the structural web of the radome and critical dimensions of antenna components, relative to wavelength, help achieve superior performance in the compact package.

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. The leading, distal, and trailing edge portions are movable in relation to the inboard lifting member to form an airfoil surface extending about the inboard lifting member and the outboard member for achieving aerodynamic control of the aircraft.

Abstract: A target base (10) for attaching an apparatus (13) to an object (11) has a substantially rigid body (12) with a mount surface (14) adapted to couple the apparatus (13) to the body (12), and a base surface. A suction cup (46) affixed to the base surface (18) of the target base (10) has a suction cavity (62) defined by a deformable sealing lip (64) at the perimeter of the suction cup (46). The sealing lip (64) and suction cavity (62) form with the object (11) a vacuum chamber (66). A vacuum system (44) includes vacuum passages (50, 52) for communicating a vacuum pressure to the vacuum chamber (66). One or more contact members (60) are affixed to the body and have contact surfaces which engage the object (11) to provide consistent off-set positioning of the target base (10) with respect to the object (11).