Patents Represented by Attorney, Agent or Law Firm Kenneth L. Warsh
  • Patent number: 5649064
    Abstract: The method and apparatus includes a neural network for generating a model of an object in a wind tunnel from performance data on the object. The network is trained from test input signals (e.g., leading edge flap position, trailing edge flap position, angle of attack, and other geometric configurations, and power settings) and test output signals (e.g., lift, drag, pitching moment, or other performance features). In one embodiment, the neural network training method employs a modified Levenberg-Marquardt optimization technique. The model can be generated "real time" as wind tunnel testing proceeds. Once trained, the model is used to estimate performance features associated with the aircraft given geometric configuration and/or power setting input. The invention can also be applied in other similar static flow modeling applications in aerodynamics, hydrodynamics, fluid dynamics, and other such disciplines.
    Type: Grant
    Filed: May 19, 1995
    Date of Patent: July 15, 1997
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Charles Jorgensen, James Ross
  • Patent number: 5633975
    Abstract: An optically responsive electronic lock is disclosed comprising an optical fiber serving as a key and having Bragg gratings placed therein. Further, an identification system is disclosed which has the optical fiber serving as means for tagging and identifying an object. The key or tagged object is inserted into a respective receptacle and the Bragg gratings cause the optical fiber to reflect a predetermined frequency spectra pattern of incident light which is detected by a decoder and compared against a predetermined spectrum to determine if an electrical signal is generated to either operate the lock or light a display of an authentification panel.
    Type: Grant
    Filed: November 14, 1995
    Date of Patent: May 27, 1997
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Charles K. Gary, Meric Ozcan
  • Patent number: 5629780
    Abstract: A method for performing color or grayscale image compression that eliminates redundant and invisible image components. The image compression uses a Discrete Cosine Transform (DCT) and each DCT coefficient yielded by the transform is quantized by an entry in a quantization matrix which determines the perceived image quality and the bit rate of the image being compressed. The present invention adapts or customizes the quantization matrix to the image being compressed. The quantization matrix comprises visual masking by luminance and contrast techniques and by an error pooling technique all resulting in a minimum perceptual error for any given bit rate, or minimum bit rate for a given perceptual error.
    Type: Grant
    Filed: December 19, 1994
    Date of Patent: May 13, 1997
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Andrew B. Watson
  • Patent number: 5618766
    Abstract: Lightweight, monolithic ceramics resistant to oxidation in air at high temperatures are made by impregnating a porous carbon preform with a sol which contains a mixture of tetraethoxysilane, dimethyldiethoxysilane and trimethyl borate. The sol is gelled and dried on the carbon preform to form a ceramic precursor. The precursor is pyrolyzed in an inert atmosphere to form the ceramic which is made of carbon, silicon, oxygen and boron. The carbon of the preform reacts with the dried gel during the pyrolysis to form a component of the resulting ceramic. The ceramic is of the same size, shape and form as the carbon precursor. Thus, using a porous, fibrous carbon precursor, such as a carbon felt, results in a porous, fibrous ceramic. Ceramics of the invention are useful as lightweight tiles for a reentry spacecraft.
    Type: Grant
    Filed: July 22, 1996
    Date of Patent: April 8, 1997
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Daniel B. Leiser, Ming-Ta Hsu, Timothy S. Chen
  • Patent number: 5616104
    Abstract: A human powered centrifuge has independently established turntable angular velocity and human power input. A control system allows excess input power to be stored as electric energy in a battery or dissipated as heat through a resistor. In a mechanical embodiment, the excess power is dissipated in a friction brake.
    Type: Grant
    Filed: August 10, 1995
    Date of Patent: April 1, 1997
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Gerald M. Mulenburg, Joan Vernikos
  • Patent number: 5545273
    Abstract: A method is provided for closing out the edges of a flexible ceramic insulation member including inner and outer mold line covering layers. A rigid, segmented, ceramic frame is placed around the edges of the insulation member and exposed edges of the inner and outer mold line covering layers are affixed to the ceramic frame. In one embodiment wherein the covering layers comprise fabrics, the outer fabric is bonded to the top surface and to a grooved portion of the side surface of the frame. In another embodiment wherein the outer cover layer comprises a metallic foil, clips on the edges of the frame are used to engage foil extensions. The ceramic frame is coated with a high emittance densifier coating.
    Type: Grant
    Filed: August 18, 1995
    Date of Patent: August 13, 1996
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Daniel J. Rasky, Demetrius A. Kourtides
  • Patent number: 5543961
    Abstract: A diffuse reflector is provided which isotropically reflects the infrared and far-infrared regions of the spectrum. The reflector includes a metal plate having one surface that is roughened by an electric discharge machine so as to have an r.m.s. roughness large enough to diffusely reflect far-infrared radiation. The roughening process creates facets having cavities which trap and diffusely reflect normally incident far-infrared radiation. An example of a reflector so produced has an isotropic bidirectional reflectance distribution function approximately equal to 1/.pi. sr.sup.-1 between the wavelengths of 5 .mu.m and 100 .mu.m.
    Type: Grant
    Filed: June 10, 1993
    Date of Patent: August 6, 1996
    Assignee: The United States of America as represented by the Administator of the National Aeronautics and Space Administration
    Inventor: Sheldon M. Smith
  • Patent number: 5536562
    Abstract: A low-density resin impregnated ceramic article advantageously employed as a structural ceramic ablator comprising a fired preform of ceramic fibers. The fibers of the ceramic preform are coated with an organic resin film. The organic resin can be a thermoplastic resin or a cured thermosetting resin. In one embodiment, the resin is uniformly distributed within the ceramic article. In a second embodiment, the resin is distributed so as to provide a density gradient along at least one direction of the ceramic article. The resin impregnated ceramic article is prepared by providing a fired preform of ceramic fibers; immersing the preform of ceramic fibers in a solution of a solvent and an organic resin infiltrant; and removing the solvent to form a resin film on the ceramic fibers.
    Type: Grant
    Filed: March 14, 1994
    Date of Patent: July 16, 1996
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Huy K. Tran, William D. Henline, Ming-ta S. Hsu, Daniel J. Rasky, Salvatore R. Riccitiello
  • Patent number: 5526109
    Abstract: A laser doppler velocimeter uses frequency shifting of a laser beam to provide signal information for each velocity component. A composite electrical signal generated by a light detector is digitized and a processor produces a discrete Fourier transform based on the digitized electrical signal. The transform includes two peak frequencies corresponding to the two velocity components.
    Type: Grant
    Filed: June 27, 1991
    Date of Patent: June 11, 1996
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Dennis A. Johnson
  • Patent number: 5523959
    Abstract: An ice detector and deicing fluid effectiveness monitoring system for an aircraft is disclosed. The ice detection portion is particularly suited for use in flight to notify the flight crew of an accumulation of ice on an aircraft lifting and control surfaces, or helicopter rotors, whereas the deicing fluid effectiveness monitoring portion is particularly suited for use on the ground to notify the flight crew of the possible loss of the effectiveness of the deicing fluid. The ice detection portion comprises a temperature sensor and a parallel arrangement of electrodes whose coefficient of coupling is indicative of the formation of the ice, as well as the thickness of the formed ice. The fluid effectiveness monitoring portion comprises a temperature sensor and an ionic-conduction cell array that measures the conductivity of the deicing fluid which is indicative of its concentration and, thus, its freezing point.
    Type: Grant
    Filed: April 25, 1994
    Date of Patent: June 4, 1996
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: H. Lee B. Seegmiller
  • Patent number: 5515158
    Abstract: A retroreflective type focusing schlieren system which permits the light source to be positioned on the optic side of the system. The system includes an extended light source, as opposed to a point source, located adjacent a beam splitter which projects light through the flow field onto a reflecting grating in the form of a grid which generates sheets of light that are directed back through the flow field and the beam splitter onto a primary lens behind which is located a cut-off grid having a grid pattern which corresponds to the grid pattern of the reflecting grating. The cut-off grid is adjustably positioned behind the primary lens and an image plane for imaging the turbulence is adjustably located behind the cut-off grid.
    Type: Grant
    Filed: February 1, 1994
    Date of Patent: May 7, 1996
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: James T. Heineck
  • Patent number: 5499609
    Abstract: An animal feeder for use in a metabolic cage. The feeder includes a confined passageway and an adjustable notched gate proceeding a food cup. The gate is adjusted so that the entry area to the food cup approximates the cross sectional head area of the animal. Food ejected from the food cup by a caged animal is dropped through a grate into a spill tray.
    Type: Grant
    Filed: March 25, 1994
    Date of Patent: March 19, 1996
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: JuliAnn Evans, Daniel P. Gundo, Jennifer S. Harper, Gerald M. Mulenburg, Thomas L. Skundberg
  • Patent number: 5491738
    Abstract: An x-ray diffraction apparatus for use in analyzing the x-ray diffraction pattern of a sample. The apparatus includes a beam source for generating a collimated x-ray beam having one or more discrete x-ray energies, a holder for holding the sample to be analyzed in the path of the beam, and a charge-coupled device having an array of pixels for detecting, in one or more selected photon energy ranges, x-ray diffraction photons produced by irradiating such a sample with said beam. The CCD is coupled to an output unit which receives input information relating to the energies of photons striking each pixel in the CCD, and constructs the diffraction pattern of photons within a selected energy range striking the CCD.
    Type: Grant
    Filed: March 15, 1993
    Date of Patent: February 13, 1996
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: David F. Blake, Charles Bryson, Friedemann Freund
  • Patent number: 5483168
    Abstract: The present invention relates to an optical system for creating a potential field map of a bounded two dimensional region containing a goal location and an arbitrary number of obstacles. The potential field mapping system has an imaging device and a processor. Two image writing modes are used by the imaging device, electron deposition and electron depletion. Patterns written in electron deposition mode appear black and expand. Patterns written in electron depletion mode are sharp and appear white. The generated image represents a robot's workspace. The imaging device under processor control then writes a goal location in the workspace using the electron deposition mode. The black image of the goal expands in the workspace. The processor stores the generated images, and uses them to generate a feedback pattern. The feedback pattern is written in the workspace by the imaging device in the electron deposition mode to enhance the expansion of the original goal pattern.
    Type: Grant
    Filed: March 1, 1993
    Date of Patent: January 9, 1996
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Max B. Reid
  • Patent number: 5478029
    Abstract: Blade-vortex interaction noises, sometimes referred to as "blade slap", are avoided by increasing the absolute value of inflow to the rotor system of a rotorcraft. This is accomplished by creating a drag force which causes the angle of the tip-path plane of the rotor system to become more negative or more positive.
    Type: Grant
    Filed: May 12, 1995
    Date of Patent: December 26, 1995
    Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space Administration
    Inventor: Fredric H. Schmitz
  • Patent number: 5477506
    Abstract: An acoustic sensor for measuring acoustic waves contained in fluid flow flowing over the sensor. The acoustic sensor reduces any unwanted self-noise associated with the flowing fluid by providing a nose cone having proper aerodynamic properties and by positioning the diaphragm of a microphone of the sensor at a location where any unwanted noise is at a relatively low level. The nose cone has a rounded, blunt or even sharp tip neither of which creates any major disturbances in the flowing fluid which it intercepts.
    Type: Grant
    Filed: November 10, 1993
    Date of Patent: December 19, 1995
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Christopher S. Allen
  • Patent number: 5459566
    Abstract: A method and apparatus for passing light bundles through a multiple pass sampling cell. The multiple pass sampling cell includes a sampling chamber having first and second ends positioned along a longitudinal axis of the sampling cell. The sampling cell further includes an entrance opening, located adjacent the first end of the sampling cell at a first azimuthal angular position. The entrance opening permits a light bundle to pass into the sampling cell. The sampling cell also includes an exit opening at a second azimuthal angular position. The light exit permits a light bundle to pass out of the sampling cell after the light bundle has followed a predetermined path.
    Type: Grant
    Filed: April 22, 1994
    Date of Patent: October 17, 1995
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Richard Pearson, Dana H. Lynch, William D. Gunter
  • Patent number: 5451448
    Abstract: Sewn, quilted ceramic blankets (AFRSI) and integrally woven core insulation systems (TABI) were examined in a 170 decibel aeroacoustic environment under oscillating air loads. Preconditioning in a radiant heat source was done at both 2000.degree. F. and 2500.degree. F. before testing. A multi-layer ceramic weave construction based on an angle interlock weave architecture is superior over all other TPS systems examined. These configurations do not require a surface coating to enhance survivability. Single-ply TABI fabric surfaces using an insulated integrally woven core structure survive up to 2000.degree. F. without the use of a ceramic coating to toughen the surface to the aeroacoustic noise level. AFRSI blankets of the art require a ceramic coating in order to demonstrate comparable performance after exposure to a 2000.degree. F. radiant heat temperature.
    Type: Grant
    Filed: July 1, 1993
    Date of Patent: September 19, 1995
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: Paul M. Sawko, Dominic P. Calamito, Anthony Jong
  • Patent number: 5447730
    Abstract: A novel rehydration beverage containing sodium chloride, sodium citrate and aspartame useful for rapid restoration of hydration homeostasis. The beverage is particularly useful for restoration of normal body fluid volumes and their intracellular and extracellular distribution during a hypohydration state observed in astronauts and air passengers.
    Type: Grant
    Filed: January 21, 1992
    Date of Patent: September 5, 1995
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: John E. Greenleaf
  • Patent number: 5438879
    Abstract: A method is provided for determining surface shear magnitude and direction at every point on a surface. The surface is covered with a shear stress-sensitive liquid crystal coating and illuminated by white light from a normal direction. A video camera is positioned at an oblique angle above the surface to observe the color of the liquid crystal at that angle. The shear magnitude and direction are derived from the color information. A method of calibrating the device is also provided.
    Type: Grant
    Filed: October 20, 1994
    Date of Patent: August 8, 1995
    Assignee: The United States of America represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Daniel C. Reda