Patents Represented by Attorney Gene E. Shook
  • Patent number: 4990739
    Abstract: An improved plasma gun coaxially injects particles of ceramic materials having high melting temperatures into the central portion of a plasma jet. This results in a more uniform and higher temperature and velocity distribution of the sprayed particles. The position of the cathode is adjustable to facilitate optimization of the performance of the gun wherein grains of the ceramic material are melted at lower power input labels.
    Type: Grant
    Filed: July 7, 1989
    Date of Patent: February 5, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Isidor Zaplatynsky
  • Patent number: 4986132
    Abstract: A fully articulated four-point-bend loading fixture for MOR and fracture toughness specimens utilizes an upper loading plate in combination with a lower loading plate. The lower plate has a pair of spring loaded ball bearings which seat in V-shaped grooves located in the upper plate. The ball bearings are carried in the arms of the lower plate. A load is applied to the specimen through steel rollers, one large roller and one smaller roller each located on both the upper and lower plates. The large rollers have needle roller bearings which enable a single loading roller to rotate relative to the plate to which it is attached.
    Type: Grant
    Filed: December 28, 1989
    Date of Patent: January 22, 1991
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Anthony M. Calomino
  • Patent number: 4980636
    Abstract: An MMIC test fixture includes a bias module having spring-loaded contacts which electrically engage pads on a chip carrier disposed in a recess of a base member. RF energy is applied to and passed from the chip carrier by chamfered edges of ridges in the waveguide passages of housings which are removably attached to the base member. "Thru", "Delay" and "Short" calibration standards having dimensions identical to those of the chip carrier assure accuracy and reliability of the test. The MMIC chip fits in an opening in the chip carrier with the boundaries of the MMIC lying on movable reference planes thereby establishing accuracy and flexibility.
    Type: Grant
    Filed: August 10, 1989
    Date of Patent: December 25, 1990
    Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space Administration
    Inventors: Robert R. Romanofsky, Kurt A. Shalkhauser
  • Patent number: 4957661
    Abstract: Improved graphite fluoride fibers are produced by contact reaction between highly graphitized fibers and fluorine gas. It is preferable to intercalate the fibers with bromine or fluorine and metal fluoride prior to fluorination.These graphite fluoride fibers are bound by an epoxy. The resulting composites have high thermal conductivity, high electric resistivity, and high emissivity.
    Type: Grant
    Filed: September 30, 1988
    Date of Patent: September 18, 1990
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventor: Ching-Cheh Hung
  • Patent number: 4946122
    Abstract: A pair of spaced collars are mounted at right angles on a clamp body by retaining rings which enable the collars to rotate with respect to the clamp body. Mounting posts extend through aligned holes in the collars and clamp body. Each collar can be clamped onto the inserted post while the clamp body remains free to rotate about the post and collar. The clamp body is selectively clamped onto each post.
    Type: Grant
    Filed: September 29, 1989
    Date of Patent: August 7, 1990
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: John K. Ramsey, Erwin H. Meyn
  • Patent number: 4946890
    Abstract: A processable, high temperature polymer derived from 1,4,5,8-tetrahydro-1,4;5,8-diepoxyanthracene and a bis-diene, particularly an anthracene end-capped polyimide oligomer and a method for the preparation thereof. Also provided is a fabricated, electrically conducting, void-free composite comprising said polymer.
    Type: Grant
    Filed: August 11, 1988
    Date of Patent: August 7, 1990
    Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space Administration
    Inventor: Mary Ann Meador
  • Patent number: 4916954
    Abstract: Apparatus is provided for obtaining a single crack in fatigue loading which emanates from a predetermined starting notch in a test specimen. This crack propagates in a direction in line with that of the applied Mode II load. The loading may be performed either monotonically or in a cyclic fatigue.
    Type: Grant
    Filed: August 21, 1989
    Date of Patent: April 17, 1990
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventor: Robert J. Buzzard
  • Patent number: 4917302
    Abstract: This device is concerned with sealing the sliding interfaces between structural panels that are roughly perpendicular to each other or whose edges are butted against one another. The gap which the seal element must seal is not uniform along the seal length requiring significant seal flexibility.The seal 10 is mounted in a rectangular groove 14 in a moveable structural panel 16. The seal comprises a plurality of rectangular shaped wafers 12 stacked next to one another and preloaded in the axial direction to minimize leakage between wafers. The wafers are laterally preloaded to maintain sealing contact along the wafer faces which engage the adjacent wall of a sidewall 18 using one of several approaches, such as the pressurized linear bellows 22. The seal accomodates distortions in the adjacent panel by relative sliding between adjacent wafers.Leakage between wafers is further minimized with good wafer surface finishes.
    Type: Grant
    Filed: December 30, 1988
    Date of Patent: April 17, 1990
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: Bruce M. Steinetz, Paul J. Sirocky
  • Patent number: 4913225
    Abstract: An external flow, liquid sheet radiator apparatus adapted for space applications has as its radiating surface a thin stable liquid sheet formed by fluid flow through a very narrow slit affixed to the sheet generator.
    Type: Grant
    Filed: September 15, 1988
    Date of Patent: April 3, 1990
    Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space Administration
    Inventor: Donald L. Chubb
  • Patent number: 4912238
    Abstract: Synthetic procedures to tetraalkyls, tetraacids and dianhydrides substituted 1,1,1-triaryl-2,2,2-trifluoroethanes which comprises: (1) 1,1-bis(dialkylaryl)-1-aryl-2,2,2-trifluoroethane, (2) 1,1-bis(dicarboxyaryl)-1-aryl-2,2,2-trifluoroethane or (3) cyclic dianhydride or diamine of 1,1-bis(dialkylaryl)-1-aryl-2,2,2-trifluoroethanes. The synthesis of (1) is accomplished by the condensation reaction of an aryltrifluoromethyl ketone with a dialkylaryl compound. The synthesis of (2) is accomplished by oxidation of (1). The synthesis dianhydride of (3) is accomplished by the conversion of (2) to its corresponding cyclic dianhydride. The synthesis of the diamine is accomplished by the similar reaction of an aryltrifluoromethyl ketone with aniline or alkyl substituted or disubstituted anilines. Also, other derivatives of the above are formed by nucleophilic displacement reactions.
    Type: Grant
    Filed: December 30, 1988
    Date of Patent: March 27, 1990
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: William B. Alston, Roy F. Gratz
  • Patent number: 4911738
    Abstract: The gaseous phase is detected and then separated from a liquid phase in a fluid. This is accomplished by centrifuging the liquid phase while the gaseous phase migrates to the axis. When the expected phase is detected at a predetermined port, a signal is generated to open the liquid or gas valve at the respective outlet ports and to modulate these valves in such a manner as to withdraw fluid at the same volume rate at which it is admitted.
    Type: Grant
    Filed: March 21, 1989
    Date of Patent: March 27, 1990
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventor: Steven J. Schneider
  • Patent number: 4904538
    Abstract: A single step is relied on in the canning process for hot isostatic pressing powder metallurgy composites. The binders are totally removed while the HIP can of compatible refractory metal is sealed at high vacuum and temperature. This eliminates out-gassing during hot isostatic pressing.
    Type: Grant
    Filed: March 21, 1989
    Date of Patent: February 27, 1990
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: John J. Juhas
  • Patent number: 4890036
    Abstract: It is an object of the invention to provide a miniature traveling wave tube which will have most of the advantages of solid state circuitry but with higher efficiency and without being highly sensitive to temperature and various types of electromagnetic radiation and subatomic particles as are solid state devices.The traveling wave tube which is about 2.5 cm in length includes a slow wave circuit (SWS) comprising apertured fins with a top cover which is insulated from the fins by strips or rungs of electrically insulating, dielectric material.Another object of the invention is to construct a SWS of extremely small size by employing various grooving or etching methods and by providing insulating strips or rungs by various deposition and masking techniques.
    Type: Grant
    Filed: December 8, 1987
    Date of Patent: December 26, 1989
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventor: Henry G. Kosmahl
  • Patent number: 4885116
    Abstract: Synthetic procedures to tetraalkyls, tetraacids and dianhydrides substituted 1,1,1-triaryl-2,2,2-trifluoroethanes which comprises: (1) 1,1-bis(dialkylaryl)-1-aryl-2,2,2-trifluoroethane, (2) 1,1-bis(dicarboxyaryl)-1-aryl-2,2,2-trifluoroethane or (3) cyclic dianhydride or diamine of 1,1-bis(dialkylaryl)-1-aryl-2,2,2-trifluoroethanes. The synthesis of (1) is accomplished by the condensation reaction of an aryltrifluoromethyl ketone with a dialkylaryl compound. The synthesis of (2) is accomplished by oxidation of (1). The synthesis dianhydride of (3) is accomplished by the conversion of (2) to its corresponding cyclic dianhydride. The synthesis of the diamine is accomplished by the similar reaction of an aryltrifluoromethyl ketone with aniline or alkyl substituted or disubstituted anilines. Also, other derivatives of the above are formed by nucleophilic displacement reactions.
    Type: Grant
    Filed: February 23, 1988
    Date of Patent: December 5, 1989
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William B. Alston, Roy F. Gratz
  • Patent number: 4845167
    Abstract: A condensation polyimide containing a 1,1,1-triaryl-2,2,2-trifluoroethane structure, other related condensation polyimides and process for their preparation, which comprises polymerization of a cyclic dianhydride with a diamine.
    Type: Grant
    Filed: October 29, 1986
    Date of Patent: July 4, 1989
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William B. Alston, Roy F. Gratz
  • Patent number: 4781993
    Abstract: 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: Grant
    Filed: April 15, 1987
    Date of Patent: November 1, 1988
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Ramakrishna T. Bhatt
  • Patent number: 4780276
    Abstract: 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: Grant
    Filed: October 14, 1987
    Date of Patent: October 25, 1988
    Assignee: The Unites States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Charles A. Barrett, William H. Holt
  • Patent number: 4770232
    Abstract: A gas particle radiator adapted to operate in a microgravity space environment having a transparent boundary which transmits energy in the infrared spectrum, and a gas particle mixture that yields high absorption and emittances.
    Type: Grant
    Filed: October 9, 1986
    Date of Patent: September 13, 1988
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Donald L. Chubb
  • Patent number: 4766724
    Abstract: A dc power supply for spacecraft arcjet thrusters has an integral automatic starting circuit and an output averaging inductor. The output averaging inductor, in series with the load, provides instantaneous current control, and ignition pulse and an isolated signal proportional to the arc voltage. A pulse width modulated converter, close loop configured, is also incorporated to give fast response output current control.
    Type: Grant
    Filed: June 10, 1987
    Date of Patent: August 30, 1988
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Robert P. Gruber
  • Patent number: 4728448
    Abstract: A self-lubricating, friction and wear reducing composite material for use over a wide temperature spectrum from cryogenic temperature to about 900.degree. C. in a chemically reactive environment comprising silver, barium fluoride/calcium fluoride eutectic, and metal bonded chromium carbide.
    Type: Grant
    Filed: May 28, 1987
    Date of Patent: March 1, 1988
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Harold E. Sliney