Patents Assigned to Administration
  • Patent number: 5174772
    Abstract: A mechanical coupling system wherein a spline screw system is used to connect two bodies, a work attachment mechanism and a work attachment fixture. A kinematic clamp first guides and mates the attachment mechanism to the attachment fixture. The kinematic clamp includes three round roller members equidistantly located around the periphery of the bodies and three correspondingly located V-shaped grooves located on the periphery of the other body. A motor driven spline screw in the attachment mechanism then engages a spline bolt head in the attachment fixture and includes a threaded shank upon which is mounted a translatable nut which is adapted to translate up and down the shank but not rotate. The nut carries one or more electrical connectors which travel upwardly during a connecting sequence and cams open a set of dust covers which operate to engage an opposing set of dust covers adjacent complementary type electrical connectors on the attachment mechanism.
    Type: Grant
    Filed: January 22, 1992
    Date of Patent: December 29, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space Administration
    Inventor: John M. Vranish
  • Patent number: 5174694
    Abstract: A retractable tool bit assembly utilized in conenction with a robotic gripper type and end-effector. The apparatus includes one or more spring loaded nestable or telescoping tubular sections together with a catch mechanism for capturing and holding the tool, such as an allen key, in its retracted position. The innermost tubular section includes a threshold cap and engages and holds the tool. The catch mechanism consists of a slider type mechanism located adjacent a relatively larger outer base sction and includes means for engaging a conically or mushroom shaped rear end portion of the tool when the telescoping sections are moved to a retracted or parked position. The catch mechanism is released upon actuation of a rotary tool drive motor coupled to a circular mount and which holds the base section. When released all the telescoping sections including the tool extends fully outward to a use position.
    Type: Grant
    Filed: September 24, 1991
    Date of Patent: December 29, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space Administration
    Inventor: George M. Voellmer
  • Patent number: 5174590
    Abstract: A compliant walker for humans having limited use of their legs and lower back includes an upright wheeled frame which at least partially surrounds an upright user wearing a partial body harness which is attached to the frame by means of cable compliant apparatus consisting of sets of cable segments and angle bracket members connected between opposite side members of the frame and adjacent side portions of the harness. The type of partial body harness utilized takes two forms, the first being a torso harness which encircles the waist or rib cage of the user, while the second type of harness is a hip harness which fits around the hips and buttocks. The frame itself lends itself to several embodiments, one of which completely surrounds the user, while the other consists of a frame open at the front end including a pair of upright side members which attach to the cable support apparatus and which is vertically adjustable to accommodate the user's height.
    Type: Grant
    Filed: July 3, 1991
    Date of Patent: December 29, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space Administration
    Inventors: James J. Kerley, Wayne D. Eklund, J. Allen A. Crane
  • Patent number: 5173944
    Abstract: An apparatus for producing pseudo-stereophonic sound from a monaural signal including a monaural source having a first speaker disposed in an anechoic room and having a sound output generated by the monaural signal. Second, third, fourth and fifth speaker disposed in the anechoic room (substantially) symmetrically about a listener having two ears. The monaural signal from the source is processed to output processed signals to each of the second, third, fourth and fifth speakers, each speaker producing a sound output corresponding to the received processed signal. A pair of microphones are disposed in the ears of the listener for receiving the sound outputs of the first, second, third, fourth and fifth speakers and producing two differentiated audio channels.
    Type: Grant
    Filed: January 29, 1992
    Date of Patent: December 22, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Durand R. Begault
  • Patent number: 5173873
    Abstract: A high speed read MRAM memory element is configured from a sandwich of magnetizable, ferromagnetic films surrounding a magento-resistive film which may be ferromagnetic or not. One outer ferromagnetic film has a higher coercive force than the other and therefore remains magnetized in one sense while the other may be switched in sense by a switching magnetic field. The magneto-resistive film is therefore sensitive to the amplitude of the resultant field between the outer ferromagnetic films and may be constructed of a high resistivity, high magneto-resistive material capable of higher sensing currents. This permits higher read voltages and therefore faster read operations. Alternate embodiments with perpendicular anisotropy, and in-plane anisotropy are shown, including an embodiment which uses high permeability guides to direct the closing flux path through the magneto-resistive material. High density, high speed, radiation hard, memory matrices may be constructed from these memory elements.
    Type: Grant
    Filed: June 28, 1990
    Date of Patent: December 22, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Jiin-Chuan Wu, Henry L. Stadler, Romney R. Katti
  • Patent number: 5173087
    Abstract: Gravitational phenomena, including convection, sedimentation, and interactions of materials with their containers all affect the crystal growth process. If they are not taken into consideration they can have adverse effects on the quantity and quality of crystals produced. As a practical matter, convection and sedimentation can be completely eliminated only under conditions of low gravity attained during orbital flight. There is, then, an advantage to effecting crystallization in space. But in the absence of of convection in a microgravity environment cooling proceeds by thermal diffusion from the walls to the center of the solution chamber. This renders control of nucleation difficult. Accordingly there is a need for a new and improved nucleation process in space. Herein crystals are nucleated by creating a small localized region of high relative supersaturation in a host solution at a lower degree of supersaturation.
    Type: Grant
    Filed: June 19, 1991
    Date of Patent: December 22, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Roger L. Kroes, Donald A. Reiss, Sandor L. Lehoczky
  • Patent number: 5173696
    Abstract: The invention herein disclosed is a digital circuit which emulates a synchro signal in a synchro-resolver follower system for precise control of shaft position and rotation at very low rotational rates. The subject invention replaces the synchro and drive motor in a synchro-resolver follower system with a digital and analog synchro emulation circuit for generating the resolver control signal. The synchro emulation circuit includes amplitude modulation means to provide relatively high frequency resolver excitation signals for accurate resolver response even with very low shaft rotation rates.
    Type: Grant
    Filed: June 3, 1991
    Date of Patent: December 22, 1992
    Assignee: The United States of America as represented by the Adminstrator of the National Aeronautics and Space Administration
    Inventors: David E. Howard, Dennis A. Smith
  • Patent number: 5173930
    Abstract: An x-ray monochromator, wherein a housing supports a plurality of mirrors forming a plurality of opposed mirror faces in parallel with each other and having thereon multilayer coatings, with each of said pairs of mirror faces being provided with identical coatings which are different from the coatings on the other pairs of mirror faces such that each pair of mirror faces has a peak x-ray reflection at a different wavelength regime. The housing is moveable to bring into a polychromatic x-ray beam that pair of mirror faces having the best x-ray reflection for the desired wavelength, with the mirrors being pivotable to move the mirror faces to that angle of incidence at which the peak reflectivity of the desired wavelength x-rays occurs.
    Type: Grant
    Filed: November 22, 1991
    Date of Patent: December 22, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Richard B. Hoover
  • Patent number: 5171822
    Abstract: An improved low toxicity polymerization of monomer reactants (PMR) system has 3,4'-oxydianiline as the key monomer reactant. One variation of this system, LaRC-RP46, is prepared by reacting together monomethyl ester or 5-norbornene-2,3-dicarboxylic acid (NE), 3,4'-oxydianiline (3,4'-ODA), and dimethyl ester of 3,3',4,4'-benzophenonetetracarboxylic acid (BTDE); this combination is then treated with heat. This new matrix resin is readily processed into a high quality graphite fiber reinforced composite with excellent reproducibility. The flexibility of the ether linkage in 3,4'-ODA provides high toughness. The composite retains excellent mechanical properties both at 316.degree. C. and at 371.degree. C. The development of LaRC-RP46 will significantly extend the applications of PMR type polyimides.
    Type: Grant
    Filed: February 5, 1991
    Date of Patent: December 15, 1992
    Assignee: The United States of America as represented by the Administrator of National Aeronautics and Space Administration
    Inventor: Ruth H. Pater
  • Patent number: 5171835
    Abstract: Disclosed herein are analogues of the luteinizing hormone-releasing hormone (LH-RH), which are potent antagonists of LH-RH. These peptides inhibit the release of gonadotropins from the pituitary in mammals, including humans and possess antitumor activity.Formula I represents peptides which are within the scope of this invention:X--R.sup.1 --R.sup.2 --R.sup.3 --Ser--R.sup.5 --R.sup.6 (AY.sub.2)--Leu--Arg--Pro--D--Ala--NH.sub.2 Iand the pharmaceutically acceptable salts thereof, whereinR.sup.1 is D-Phe, D-Phe(4Cl), D-Nal(1) or D-Nal(2),R.sup.2 is D-Phe or D-Phe(4HI),R.sup.3 is D-Trp, D-Phe, D-Phe(4HI), D-Nal(1), D-Nal(2) or D-Pal(3),R.sup.5 is Tyr or Arg,R.sup.6 is D-Lys or D-Orn,HI is fluoro, chloro or bromoX is a lower alkanoyl group of 2-5 carbon atoms,A is a diaminoacyl residue having the formula ##STR1## where m is 0 or 1,n is 0 or 1,Y is Y.sup.1 or Y.sup.2, whereinY.sup.
    Type: Grant
    Filed: January 30, 1991
    Date of Patent: December 15, 1992
    Assignee: The Administrators of the Tulane Educational Fund
    Inventors: Tamas Janaky, Atilla Juhasz, Andrew V. Schally
  • Patent number: 5169674
    Abstract: A metallic "close-out" layer is applied to the surface of a thermal barrier coating system to seal the ceramic material in the coating. The "close-out" layer is glass-bead preened to densify the surface.
    Type: Grant
    Filed: May 23, 1991
    Date of Patent: December 8, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Robert A. Miller
  • Patent number: 5167464
    Abstract: A robot-friendly coupling device for an Orbital Replacement Unit (ORU). The invention will provide a coupling that is detached and attached remotely by a robot. The design of the coupling must allow for slight misalignments, over torque protection, and precision placement. This is accomplished by using of a triangular interface having three components. A base plate assembly is located on an attachment surface, such as a satellite. The base plate assembly has a cup member, a slotted member, and a post member. The ORU that the robot attaches to the base plate assembly has an ORU plate assembly with two cone members and a post member which mate to the base plate assembly. As the two plates approach one another, one cone member of the ORU plate assembly only has to be placed accurately enough to fall into the cup member of the base plate assembly. The cup forces alignment until a second cone falls into a slotted member which provides final alignment. A single bolt is used to attach the two plates.
    Type: Grant
    Filed: October 7, 1991
    Date of Patent: December 1, 1992
    Assignee: The United States of America as represented by the Administrator of the Natoinal Aeronautics and Space Administration
    Inventor: George M. Voellmer
  • Patent number: 5165229
    Abstract: A thruster nozzle sealing system and apparatus is provided for protection of spacecraft thruster motors. The system includes a sealing plug, a sealing plug insertion tool, an outer cover, an outer cover attachment, a ferry flight attachment, and a test stand. The sealing plug provents moisture from entering the thruster engine so as to prevent valve failure. The attachments are interchangeably connectable with the sealing plug. The ferry flight attachment is used during air transportation of the spacecraft, and the outer cover attachment is used during storage and service of the spacecraft. The outer cover provides protection to the thruster nozzle from mechanical damage. The test stand provides a means for testing and certifying the operating condition of each component of the system.
    Type: Grant
    Filed: October 22, 1991
    Date of Patent: November 24, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Paul A. Svejkovsky
  • Patent number: 5165169
    Abstract: A tool for removing and/or replacing bearings in situ comprises a brace having a first end adapted to engage a first end of the bearing housing, and a second end adapted to engage a second end of the bearing housing. If the two ends of the bearing housing are different in configuration, the respective ends of the brace are correspondingly configured. An elongate guide member integral with the brace has two parts, each projecting endwise from a respective end of the brace. A pressure plate is alternatively removable mountable on either part of the guide member for longitudinal movement therealong, and has first and second ends of different configurations adapted to engage first and second ends respectively of the bearing. A threaded-type drive is cooperative between the guide and the pressure plate to move the pressure plate longitudinally along the guide and apply a force to the bearing, either to remove the bearing from its housing, or to emplace a new bearing in the housing.
    Type: Grant
    Filed: October 31, 1991
    Date of Patent: November 24, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Rex A. Boyce
  • Patent number: 5166679
    Abstract: A capacitive proximity sensing element, backed by a reflector driven at the same voltage as and in phase with the sensor, is used to reflect the field lines away from a grounded robot arm towards an intruding object, thus dramatically increasing the sensor's range and sensitivity.
    Type: Grant
    Filed: June 6, 1991
    Date of Patent: November 24, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space Administration
    Inventors: John M. Vranish, Robert L. McConnell
  • Patent number: 5163966
    Abstract: A prosthetic limb (10) for a below-the-elbow amputee is constructed having a removable effector (16) removably mounted in a mount (18) having semicircular bands (20) set by "hand lapped" construction in sides of a body (12) near a closed end (22) thereof. The effector (16) is offset from the body (12) and is provided with supports (60, 62), each having a C-shaped slot (64, 66) for receiving a horizontally oriented bar, such as that on a chainsaw. A pair of semi-circular gripping members (68, 70) are pivotally mounted by pins (72, 74) near a closed end of the slots (64, 66) and are biased closed by a C-shaped leaf spring (90) disposed about an outer periphery of the members (68, 70).
    Type: Grant
    Filed: April 15, 1992
    Date of Patent: November 17, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William E. Norton, Thomas W. Vest, Jewell G. Belcher, Jr., James R. Carden
  • Patent number: 5164669
    Abstract: The invention is a method and apparatus for characterizing residual uniaxial stress in a ferromagnetic test member by distinguishing between residual stresses resulting from positive (tension) forces and negative (compression) forces by using the distinct and known magnetoacoustic (MAC) and a novel magnetoacoustic emission (MAE) measurement circuit means. A switch permits the selective operation of the respective circuit means.
    Type: Grant
    Filed: July 23, 1990
    Date of Patent: November 17, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Min Namkung, Peter W. Kushnick, William T. Yost, John L. Grainger
  • Patent number: 5165051
    Abstract: This is a method and associated apparatus for accurately and quickly estimating the amplitude, frequency and phase of a signal of interest. The method comprises the steps of, inputting the signal of interest; generating a reference signal with adjustable amplitude, frequency and phase at an output thereof; mixing the signal of interest with the reference signal and a signal 90.degree. out of phase with the reference signal to provide a pair of quadrature sample signals comprising respectively a difference between the signal of interest and the reference signal and a difference between the signal of interest and the signal 90.degree.
    Type: Grant
    Filed: November 27, 1991
    Date of Patent: November 17, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Rajendra Kumar
  • Patent number: 5164956
    Abstract: Surface-emitting distributed feedback (DFB) lasers are disclosed with hybrid gratings. A first-order grating is provided at one or both ends of the active region of the laser for retroreflection of light back into the active region, and a second-order or nonresonant grating is provided at the opposite end for coupling light out perpendicular to the surface of the laser or in some other selected direction. The gratings may be curved to focus light retroreflected into the active region and to focus light coupled out to a point P. When so focused to a point, the DFB laser may be part of a monolithic read head for a laser recorded disk, or an optical coupler into an optical fiber.
    Type: Grant
    Filed: October 21, 1991
    Date of Patent: November 17, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Robert J. Lang
  • Patent number: 5162143
    Abstract: A uniformly flexible core, and method for manufacturing the same, for use between the face plates of a sandwich structure. The core is made of a plurality of thin corrugated strips, the corrugations being defined by a plurality of peaks and valleys connected to one another by a plurality of diagonal risers. The corrugated strips are orthogonally criss-crossed to form the core. The core is particualrly suitable for use with high accuracy spherically curved sandwich structures because undesirable stresses in the curved face plates are minimized due to the uniform flexibility characteristics of the core in both the X and Y directions. The core is self-venting because of the open geometry of the corrugations. The core can be made from any suitable composite, metal, or polymer. Thermal expansion problems in sandwich structures may be minimized by making the core from the same composite materials that are selected in the manufacture of the curved face plates because of their low coefficients of thermal expansion.
    Type: Grant
    Filed: March 30, 1990
    Date of Patent: November 10, 1992
    Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space Administration
    Inventors: Christopher C. Porter, Paul J. Jacoy, Wesley P. Schmitigal