Hughes Aircraft Company

Raytheon Company

Hughes Aircraft

Kenn S Bates

David B Chang

Brian M Pierce

Victor Vali

I-Fu Shih

Robert L Peirce

Slava A Pollack

Bradley R Risinger

Richard A James

Kenneth M Kunz

Barton H Rowlett

Gene Paul Cochran

An infrared camouflage textile, including an emissivity layer on one side of the textile and adapted to provide at least two different infrared emissivities in a pattern; a heating layer between the emissivity and insulating layers; and a power source to the heating layer. The emissivity layer may include a display module including pixel elements displaying the pattern, each pixel element including a display segment; a plurality of first charged pigments in the display segment each having a first charge; a plurality of second charged pigments in the display segment each having a charge opposite the first charge; an electrical contact coupled to the display segment to receive signals creating an electric field in the display segment; at least one computer-readable storage medium including code to transmit signals to the display module that create an electric field in a pixel element form the pattern in the emissivity layer.

Infrared camouflage textile

A method of testing a Laser Detection and Ranging (LADAR) or LIght Detection And Ranging (LiDAR) system includes receiving an input signal from the LADAR/LiDAR and triggering light/laser sources to output pulses. The method includes transmitting the light/laser pulses into a first end of two or more fiber optical delay lines. The method includes transmitting the pulses throughout a length of two or more fiber optical delay lines. The method includes after a delay time corresponding to the length of the fiber optical delay lines, transmitting the pulses out through a second end of the fiber optical delay lines arranged within a target plane. The pulses output yield a return signals transmission from the target plane to the LADAR/LiDAR. The return signal transmission is delayed by times for the light/laser pulses to traverse the length of the fiber optical delay lines.

Portable programmable ladar test target

According to one embodiment, a method includes receiving a first optical signal at a pulse detector. An electronic pulse of the first optical signal is received at an optical module. A second optical signal is generated at the optical module based on the electronic pulse. At least a portion of the first optical signal is received in a reverse direction at an optical isolator and the second optical signal is received in a forward direction at the optical isolator. The optical isolator substantially transmits the second optical signal to a target in the forward direction. The optical isolator substantially attenuates at least a portion of the first optical signal in the reverse direction.

System and method for using an optical isolator in laser testing

According to one embodiment, a target system includes a display module comprising a plurality of pixel elements operable to display target patterns. Each pixel element includes a display segment, a plurality of first charged pigments housed within the display segment each having a first charge, a plurality of second charged pigments housed within the display segment each having a second charge, wherein the first charge is opposite the second charge, and an electrical contact coupled to the display segment and operable to receive signals which cause an electric field to be present in the display segment. The system also includes at least one computer-readable tangible storage medium comprising executable code that, when executed by at least one processor, is operable to transmit signals to the display module that cause an electric field to be present in at least one pixel element of the plurality of pixel elements. In addition, the system includes a heating element coupled to the display module and operable to emit an infrared pattern that is modified by the plurality of pixel elements.

System and method to generate and display target patterns

An adiabatic liquid volume sensor system is described, which employs a main chamber in a back-to-back configuration with a reference chamber of known volume. The system measures liquid volume in the main chamber by making low frequency acoustic measurements of the acoustic pressure differences in the two closed chambers when driven with a sinusoidal frequency from the same speaker. Pressure transducers in each chamber measure acoustic adiabatic pressures in each chamber. The ratio of these pressures multiplied by the known volume of the reference chamber yields the volume of gas in the main chamber. The volume of liquid is equal to the known volume of the main chamber minus the calculated gas volume.

Acoustic adiabatic liquid quantity sensor

A measurement optical fiber is placed into contact with a geological structure, and a reference optical fiber of about the same length is not contacted to the geological structure. An input beam of light is transmitted down the lengths of the measurement and reference optical fibers, and the interference fringes formed between the reflected beams in the two optical fibers are counted to determine the geological displacement, and thence the geologic strain, experienced by the measurement optical fiber. Preferably, multiple pairs of the measurement and reference optical fibers are used, the optical fibers of the various pairs being of different lengths. The difference in displacement measured by any two pairs is a measure of the geological strain in the region between the ends of the two pairs. The multiple pairs are conveniently provided in two optical fiber cables, a measurement cable which contacts the geological structure and a reference cable which extends parallel and adjacent to the measurement cable.

Optical fiber apparatus and method for measuring geological strains

An electro-optical target comprising an emissivity target and a controlled background source that has a temperature greater than, less than or equal to the temperature of the emissivity target. Appropriate adjustment of the temperatures of the emissivity target and heated controlled background source causes the 'apparent' temperature of the emissivity target to be less than the specular ambient or background temperature, effectively emitting a negative temperature (delta T) relative to the background temperature produced by the controlled background source. It is useful to have an electro-optical target that emits a negative temperature (delta T) for minimum resolvable temperature testing of FLIR systems, for example, without cooling any of the components of the electro-optical target.

Emissivity target that provides positive and negative differential

An apparatus for measuring the conductivity of a fluid is disclosed. The invention 10 provides both a contact and non-contact monitoring of fluid conductivity by measuring the A.C. dielectric properties of the fluid. The invention 10 transmits an electromagnetic wave into the fluid 22 and analyzes the transmitted and reflected waves providing an indication of the conductivity of the fluid 22. The invention 10 is versatile in that it allows for the fluid to be in the form of a spray. In a specific illustrative implementation, a novel nozzle is provided to monitor the conductivity of paint spray 22 as it passes therethrough.

Apparatus for measuring the conductivity of a fluid

An acoustic fuel (or other liquid, powder or solid) sensor is disclosed. The sensor measures the volume of fuel in a container of known size. The air within the container is excited by an acoustic transducer. The transducer is driven by a frequency scanning source, and the frequency response of the air cavity within the container is monitored. This frequency response is then processed to determine the volume of air in the container, and the fuel volume is determined to be the total container volume less the air volume. In one embodiment, a tube connects the transducer through an orifice to the air volume, and the frequency response is observed to determine the resonant frequency of the air cavity within the container. The volume of the air cavity is then determined from the resonant frequency. The volume of the fuel is then determined from the tank volume minus the volume of the air cavity.

Low frequency acoustic fuel sensor

A sensor for detecting the presence of a particular chemical by determining the absolute frequency shift in the oscillating frequency of an antibody-coated oscillator. Specific antibodies deposited on a high Q crystal oscillator detect the change in frequency as chemical particulates become trapped by the antibodies and change the effective mass of the crystal. In one embodiment, two oscillating crystals are used, one that has been coated with the antibodies, and one that is uncoated. This permits detection of frequency differences between the oscillating frequencies of the two crystals, thus eliminating pressure, temperature, and humidity corrections that conventionally must be made. The sensor maintains a high specificity by using antibodies that are specifically related to the chemical to be detected, while achieving relatively good sensitivity by using high Q oscillators, such as quartz or sapphire, and eliminating drift problems due to temperature, pressure, and humidity. In a second embodiment, a single crystal is used having antibodies coated at specific nodal locations associated with harmonics of the fundamental frequency of oscillation of the crystal. Harmonic amplitudes are measured to determine the presence of the chemical of interest.

Antibody coated crystal chemical sensor

An apparatus and method for measuring the conductivity of a fluid. The apparatus 10 provides both a contact and non-contact monitoring of fluid conductivity by measuring the A.C. dielectric properties of the fluid. The apparatus 10 transmits an electromagnetic wave into the fluid 22 and analyzes the transmitted and reflected waves providing an indication of the conductivity of the fluid 22. The apparatus 10 is versatile in that it allows for the fluid to be in the form of a spray. In a specific illustrative implementation, a novel nozzle is provided to monitor the conductivity of paint spray 22 as it passes therethrough.

Apparatus for measuring the conductivity of paint spray using an

A miniature infrared test target that comprises a heated four-bar test target operated at a high temperature and a physically separated ambient field operated at ambient temperature. A beamsplitter is disposed relative to the test target and the field in a position to combine and transmit images thereof along a common axis. A lens is disposed along the common axis and forms a combined image of the test target and the field at its image plane. Separation of the test and field targets permits miniaturization of the test target while maintaining a temperature difference between the field and the bars that is proportional to the true temperature difference. The target overcomes the difficulty of maintaining an extremely high temperature gradient in the target. It provides a greater contrast range than that provided by conventional miniature targets. The miniature infrared test target is made with surfaces approximating a blackbody, thereby providing immunity from the Narcissus problem and the effects of complicated environmental changes.

Growing community of inventors

Long Beach, CA, United States of America

Kenn S Bates