Patents Assigned to Administration
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Patent number: 4790026Abstract: A pipelined image processor selectively interconnects modules in a column of a two-dimensional array to modules of the next column of the array of modules 1,1 through M,N, where M is the number of modules in one dimension and N is the number of modules in the other direction. Each module includes two input selectors (10,11) for A and B inputs, two convolvers (12,13), a binary function operator (15), a neighborhood comparison operator (14) which produces an A output and an output selector (16) which may select as a B output the output of any one of the components in the module, including the A output of the neighborhood comparison operator. Each module may be connected to as many as eight modules in the next column, preferably with the majority always in a different row that is up (or down) in the array for a generally spiral data path around the torus thus formed. The binary function operator (15) is implemented as a look-up table (20) addressed by the most significant 8 bits of each 12-bit argument.Type: GrantFiled: December 31, 1985Date of Patent: December 6, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Donald B. Gennery, Brian Wilcox
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Patent number: 4788271Abstract: New polyphenylquinoxalines have been prepared from the reaction of novel bis(.alpha.-diketones) with aromatic bis(o-diamines). These polyphenylquinoxalines have lower glass transition temperatures and melt viscosities and consequently better processability than known polyphenylquinoxalines. The properties of these new polyphenylquinoxalines (tensile strength, modulus, elongation, adhesive strength, fracture energy, and solvent resistance) are comparable with the properties of known polyphenylquinoxalines.Type: GrantFiled: March 23, 1987Date of Patent: November 29, 1988Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: Paul M. Hergenrother, Stephen J. Havens, Frank W. Harris
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Patent number: 4786168Abstract: A laser velocimeter signal processor for measuring the signal frequency within a signal burst. The input signal is converted to digital by an ADC 16 and then shifted into shift registers 30 and 31. An automatic gain circuit 15 controls the gain of the input signal. A signal integration circuit 32 determines when a signal burst has been captured by the shift registers and and then transfers the contents of the registers to data latches 33 and 34. The data in data latches 33 and 34 is processed by digital bandpass filters 57-63, square law detectors 64-70, burst counters 71-77 and signal processor 78 to determine the frequency of the signal within the captured signal burst.Type: GrantFiled: November 24, 1986Date of Patent: November 22, 1988Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: James F. Meyers, John W. Stoughton, James I. Clemmons, Jr., Sharad V. Kanetkar, Andreas E. Savakis
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Patent number: 4785608Abstract: An apparatus 10 for effecting sealing of a fused quartz ampoule 24 while maintaining a vacuum on the ampoule via system 12 is disclosed. A plug 28 of fused quartz is lowered into the vertically disposed ampoule 24 (while maintaining the vacuum thereon) and heat sealed therein to prevent any vapor escape from, or contamination of, the contained semiconductor growth charge 29 during subsequent semiconductor crystal growth processes. A rotary vacuum feed-through mechanism 16 selectively rotates axle 34 and spool 32 to unwind wire 30 for lowering of plug 28 into the reduced diameter portion 24b of ampoule 24. Ampoule 24 is hermatically connected to vacuum housing 18 by quick release flange 20 wherein O-ring 22 retains ampoule 24.Type: GrantFiled: June 30, 1982Date of Patent: November 22, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William J. Debnam, Jr., Ivan O. Clark
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Patent number: 4783994Abstract: The invention is a probe (10) for measuring changes in pressure in a high locity fluid streams over and adjacent the surface of an object. The probe (10) is formed of an exterior housing (11) having a closed pressure chamber (28) in which a piezo-electric pressure transducer (32) is mounted. An open connector tube (26) having a probe tip (29) passes a portion of said fluid stream into the closed pressure chamber (28), any change of pressure therein requiring a "settling-time" to appear in the closed pressure chamber (28) that is inversely proportional to the cross-sectional area of the connector tube (26). A cooling chamber (47) formed around the pressure chamber (28) is connected to a source of cooling fluid by means of inlet and outlet tubes (44) and (46), respectively.Type: GrantFiled: January 13, 1988Date of Patent: November 15, 1988Assignee: The Administrator of the National Aeronautics and Space AdministrationInventor: George C. Ashby, Jr.
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Patent number: 4783822Abstract: A headband for a headset has separate coarse and fine adjustment features. The adjustments may be to the axial distance between at least one earpiece element and a side support. Such adjustment to the axial distance varies the pressure exerted on the head of the user. The present fine adjustment feature may be used while the headset is being worn, thereby permitting a user to optimize the amount of pressure between the contending criteria of comfort and keeping the headset in place on the user's head.Type: GrantFiled: August 8, 1986Date of Patent: November 8, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Pierce C. Toole, Howard E. Chalson, Walter S. Bussey
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Patent number: 4781326Abstract: To accomplish the removal of warm fog about an area such as an airport runway (11) shown in FIG. 1, a plurality of nozzles (17) along a line (15) adjacent the area propelled water jets (19) through the fog to heights of approximately twenty-five meters. Each water jet (19) breaks up forming a water drop size distribution that falls through the fog overtaking, colliding, and coalescing with individual fog droplets and thereby removes the fog. A water retrieval system (15) is used to collect the water and return it to reservoirs (21) for pumping it to the nozzles (17) once again.Type: GrantFiled: July 23, 1984Date of Patent: November 1, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Vernon W. Keller
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Patent number: 4781993Abstract: A strong and tough SiC/RBSN composite material comprises silicon fibers and a reaction bonded silicon nitride matrix. This composite material may be used at elevated temperatures up to at least 1400.degree. C.Type: GrantFiled: April 15, 1987Date of Patent: November 1, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Ramakrishna T. Bhatt
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Patent number: 4780276Abstract: About ten weight percent nickel is added to a Fe-base alloy which has a ferrite microstructure to improve the high temperature castability and crack resistance while about 0.2 weight percent zirconium is added for improved high temperature cyclic oxidation and corrosion resistance. The basic material is a high temperature FeCrAl heater alloy, and the addition provides a material suitable for burner rig nozzles.Type: GrantFiled: October 14, 1987Date of Patent: October 25, 1988Assignee: The Unites States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Charles A. Barrett, William H. Holt
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Patent number: 4779428Abstract: A bi-directional Joule Thomson refrigerator is described, which is of simple construction at the cold end of the refrigerator. Compressed gas flowing in either direction through the Joule Thomson expander valve and becoming liquid, is captured in a container in direct continuous contact with the heat load. The Joule Thomson valve is responsive to the temperature of the working fluid near the valve, to vary the flow resistance through the valve so as to maintain a generally constant mass flow between the time that the refrigerator is first turned on and the fluid is warm, and the time when the refrigerator is near its coldest temperature and the fluid is cold. The valve is operated by differences in thermal coefficients of expansion of materials to squeeze and release a small tube which acts as the expander valve.Type: GrantFiled: October 8, 1987Date of Patent: October 25, 1988Assignee: United States of America as represented by the Administrator, National Aeronautics and Space AdministrationInventors: Chung K. Chan, John R. Gatewood
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Patent number: 4778268Abstract: The invention is an apparatus for training of the human visual accommodation system. Specifically, the apparatus is useful for training a person to volitionally control his focus to his far point (normally infinity) from a position of myopia due to functional causes. The functional causes could be due, for example, to a behavioral accommodative spasm or the effects of an empty field. The device may also be used to measure accommodation, the accommodation resting position and the near and far points of vision. The device comprises a number of optical elements arranged on a single optical axis (74). Several of the elements are arranged in order on a movable stage (20) in fixed relationship to each other: a light source (30), a lens (32), a target (36), an aperture (42), (48) or (52) and second lens (58). On base (18) and in fixed relationship to each other are eyepiece (70) and third lens (64).Type: GrantFiled: February 6, 1986Date of Patent: October 18, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Robert J. Randle
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Patent number: 4777823Abstract: A system is described for use with acoustic levitators, which can prevent rotation of a levitated object or control its orientation and/or rotation. The acoustic field is made nonsymmetrical about the axis of the levitator, to produce an orienting torque that resists sample rotation. In one system, a perturbating reflector is located on one side of the axis of the levitator, at a location near the levitated object. In another system, the main reflector surface towards which incoming acoustic waves are directed is nonsymmetrically curved about the axis of the levitator. The levitated object can be reoriented or rotated in a controlled manner by repositioning the reflector producing the nonsymmetry.Type: GrantFiled: August 20, 1987Date of Patent: October 18, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Martin B. Barmatz, Mark S. Gaspar, Eugene H. Trinh
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Patent number: 4779222Abstract: An Laser Doppler Velocimeter multiplexer interface (20) includes an event pulse synchronizer (162), which synchronizes data pulses from events A, B and C. Clock control (164) is connected to receive timing information on the data pulses from the synchronizer (162). Displays (24, 26, 28) are connected to receive clock signals from the clock control (164) for indicating a data rate for each of the measured events A, B and C. Display (30) is connected to receive clock signals from the clock control (164) to indicate a coincidence rate between data pulses for any selected combination of the measured events A, B and C. A multiplexer (156) receives the data pulses from the events A, B and C and rate data from the clock control (164). Multiplexer (156) has output (180) for supplying the data pulses and rate data to a single input of a data processing system.Type: GrantFiled: April 22, 1985Date of Patent: October 18, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Dean R. Harrison, James L. Brown
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Patent number: 4777656Abstract: An emergency locating transmitting (ELT) system comprising a legislated ELT modified with an interface unit and connected by a multiwire cable to a remote control monitor (RCM), typically located at the pilot position. The RCM can remotely (1) test the ELT by disabling the legislated swept tone and allowing transmission of a single tone, (2) turn the ELT "on" for legislated ELT transmission, and (3) reset the ELT to an "armed" condition. The RCM also provides visual and audio indications of transmitter operating condition as well as ELT battery condition. Removing the RCM or shorting or opening the interface input connections will not affect traditional ELT operation.Type: GrantFiled: September 28, 1984Date of Patent: October 11, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: William R. Wade
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Patent number: 4776531Abstract: This invention relates to airfoils which have particular application to rotors of helicopters and rotorcraft and to aircraft propellers. Two airfoil profiles, the RC(4)XX and RC(5)XX are shaped to permit (1) the development of high air loads without causing an extensive separation of the boundary layer air, (2) a distribution of airloads which results in a near zero pitching moment coefficient about the quarter chord for a range of lift coefficients from -0.2 to 1.0 for Mach numbers up to 0.63, and (3) the development of a local supersonic flow field which is so shaped that the wave losses are minimal until higher free stream Mach numbers over a range of lift coefficients from 0.0 to 0.30. Thus, both airfoils have high maximum lift coefficients, low pitching moment coefficients, and high drag divergence Mach numbers to result in improved rotor or propeller performance. The two invention airfoils are related in shape and purpose.Type: GrantFiled: September 5, 1986Date of Patent: October 11, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Kevin W. Noonan
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Patent number: 4776541Abstract: Large angular control moments and torques are developed by controllably circulating a relatively small mass of liquid (22) through small diameter pipes (20) describing a large diameter loop (15f,a,b). The loop (15), by thus generating and storing angular momentum, can thereby provide efficient cancellation of periodic, non-accumulating, externally induced rotational disturbances. The loop (15) is preferably located on or near the periphery of a structure (10) which is to be thus stabilized.Type: GrantFiled: February 27, 1987Date of Patent: October 11, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Ronald S. Maynard
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Patent number: 4777658Abstract: A receiver and transmitter are provided for a distress incident locating telecommunications system. The receiver is a superheterodyne AM receiver which applies the received distress transmissions to a normally unlocked phaselock loop which locks onto the unmodulated carrier signal portion of the distress transmission. The duration of the phaselock loop being locked, and unlocked immediately after being locked, are measured and compared to predetermined values to find a match. Each of the predetermined values corresponds to an item of information, and if a match is found, the receiver indicates it. The receiver is also capable of extracting audio information present in the distress transmission. The transmitter generates three signals which can be applied to a transmitting antenna. These signals are a radio frequency carrier signal, and a carrier signal modulated by a distress waveform or by an audio signal.Type: GrantFiled: October 21, 1986Date of Patent: October 11, 1988Assignee: The United States of America as represented by the United States National Aeronautics & Space AdministrationInventor: Paul E. Wren
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Patent number: 4775740Abstract: The subject invention pertains to a novel class of fire- and heat-resistant bisimide resins prepared by thermal polymerization of maleimido or citraconimido substituded 1-[(dialkoxyphosphonyl)-methyl]-2-4 and -2,6-diaminobenzenes. Typical polymer presursors have the chemical structure: ##STR1## wherein R is alkyl, substituted alkyl or aryl, and R.sup.1 is hydrogen or lower alkyl.The polymer precursors are prepared by reacting 1-[(diorganooxyphosphonyl)methyl]-2-4 and -2,6-diaminobenzenes with maleic anhydride or citraconic anhydride in a mole ratio 1:2. Chains extension of the monomers is achieved by reacting the mono-N-maleimido derivatives of 1-[(diorganooxyphosphonyl)methyl]-2,4 and -2,6-diaminobenzenes with aryl tetracarboxylic dianhydrides, such as benzophenone tetracarboxylic diandydride, or aryl diisocyanates, such as methylenebis(4-phenylisocyanate), in a mole ratio 2:1.Type: GrantFiled: April 10, 1986Date of Patent: October 4, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: James M. Beggs, John A. Mikroyannidis, Demetrius A. Kourtides
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Patent number: 4774835Abstract: Disclosed is a method of visualizing laminar to turbulent boundary layer transition, shock location, and laminar separation bubbles around a test surface. A liquid crystal coating is formulated using an unencapsulated liquid crystal operable in a temperature bandwidth compatible with the temperature environment around the test surface. The liquid crystal coating is applied to the test surface, which is preferably pre-treated by painting with a flat black paint to achieve a deep matte coating, after which the surface is subjected to a liquid or gas flow. Color change in the liquid crystal coating is produced in response to differences in relative shear stress within the boundary layer around the test surface.Type: GrantFiled: November 13, 1986Date of Patent: October 4, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Bruce J. Holmes, Peter D. Gall
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Patent number: 4773620Abstract: A device which actuates aircraft control surfaces is disclosed. The actuator 19 is disposed entirely within the control surface structure 15. Because the actuator 19 is disposed entirely within the control surface 15, the gap 14 between the wing structural box 13 and control surface 15 may be reduced. Reducing the size of the gap 14 is especially desirable for wings with high aspect ratio, wherein the volume of structural box 13 is at a premium.Type: GrantFiled: March 23, 1987Date of Patent: September 27, 1988Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Gerhard E. Seidel