Patents Assigned to Administration
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Patent number: 4932777Abstract: An electro-optical spin measurement system for a spin model in a spin tunnel includes a radio controlled receiver/transmitter, targets located on the spin model, optical receivers mounted around the perimeter of the spin tunnel and the base of the spin tunnel for receiving data from the targets, and a control system for accumulating data from the radio controlled receiver and receivers. Six targets are employed. The spin model includes a fuselage, wings, nose and tail. Two targets are located under the fuselage of the spin model at the nose tip and tail, two targets are located on the side of the fuselage at the nose tip and tail, and a target is located under each wing tip. The targets under the fuselage at the nose tip and tail measure spin rate of the spin model, targets on the side of the fuselage at the nose tip and tail measure angle of attack of the spin model, and the targets under the wing tips measure roll angle of the spin model. Optical receivers are mounted at 90.degree.Type: GrantFiled: September 30, 1988Date of Patent: June 12, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert Fodale, Herbert R. Hampton
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Patent number: 4933551Abstract: An in-line reversal electron, high-current ionizer capable of focusing a beam of electrons to a reversal region and executing a reversal of said electrons, such that the electrons possess zero kinetic energy at the point of reversal, may be used to produce both negative and positive ions. A sample gas is introduced at the point of electron reversal for low energy electron-(sample gas) molecule attachment with high efficiency. The attachment process produces negative ions from the sample gas, which includes species present in trace (minute) amounts. These ions are extracted efficiently and directed to a mass analyzer where they may be detected and identified. The generation and detection of positive ions is accomplished in a similar fashion with minimal adjustment to potentials applied to the apparatus.Type: GrantFiled: June 5, 1989Date of Patent: June 12, 1990Assignee: The United State of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Mark T. Bernius, Ara Chutjian
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Patent number: 4932098Abstract: A device composed of a clear plastic cover, supported by a ribbed framework which is attached to a collar all of which define a cavity. The collar has at least one large aperture for receiving an appendage to be groomed within the cavity. The cover is provided with slits for receiving the hands of an individual conducting a grooming service. A vacuum hose for collecting unwanted material produced during grooming is also included within the cavity.Type: GrantFiled: August 29, 1988Date of Patent: June 12, 1990Assignee: The United States of America as Represented by the United States National Aeronautics and Space AdministrationInventor: Richard F. Haines
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Patent number: 4932610Abstract: The invention is a boundary flow control system and method which comprises heating elements 24 to trigger boundary layer transition and audio speakers 83 to provide acoustic suppression 51 of boundary layer turbulence 52. The trigger and suppression control are activated by a feedback amplifier 82 which reads boundary layer flow conditions using an anemometer probe 81. The active control of the boundary layer permits delay of flow separation and a reduction in skin friction drag as compared to natural flow conditions.Type: GrantFiled: March 11, 1986Date of Patent: June 12, 1990Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventor: Lucio Maestrello
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Patent number: 4932688Abstract: A system for mating fluid transfer couplings is constructed having a male connector 32 which is provided with a pair of opposed rollers 54 mounted to an exterior region thereof. A male half 30 of a fluid transfer coupling is rotatably supported in an opening 36 in an end 38 of connector 32 and is equipped with an outwardly extending forward portion 20. Forward portion 20 locks into an engagement and locking region 16 of a female half 60 of the fluid transfer coupling, with female half 60 being rotatably supported in a receptacle 62. Receptacle 62 has an opening 70 aligned with locking region 16, with this opening having a pair of concentric, annularly disposed ramps 74 extending around an interior portion of opening 70. These ramps are inclined toward interior 78 of receptacle 62 and are provided with slots 76 through which rollers 54 of connector 32 pass.Type: GrantFiled: February 29, 1988Date of Patent: June 12, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Joseph C. Cody, Paul R. Matthews
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Patent number: 4933936Abstract: This is a distributed computing system providing flexible fault tolerance; ease of software design and concurrency specification; and dynamic balance of the loads. The system comprises a plurality of computers each having a first input/output interface and a second input/output interface for interfacing to communications networks each second input/output interface including a bypass for bypassing the associated computer. A global communications network interconnects the first input/output interfaces for providing each computer the ability to broadcast messages simultaneously to the remainder of the computers. A meshwork communications network interconnects the second input/output interfaces providing each computer with the ability to establish a communications link with another of the computers bypassing the remainder of computers. Each computer is controlled by a resident copy of a common operating system.Type: GrantFiled: August 17, 1987Date of Patent: June 12, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert D. Rasmussen, Robert M. Manning, Blair F. Lewis, Gary S. Bolotin, Richard S. Ward
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Patent number: 4933558Abstract: A radiation sensitive area detection device is disclosed which comprises a phosphor-containing film capable of receiving and storing an image formed by a pattern of incoming X-rays, UV, or other radiation falling on the film and capable of fluorescing in response to stimulation by a light source in a manner directly proportional to the stored radiation pattern; a light source capable of projecting light or other appropriate electromagnetic wave on the film so as to cause it to fluoresce; means, such as a lens, to focus the fluoresced light coming from the phosphor-containing film after light stimulation; and at least one charged coupled detector or other detecting element capable of receiving and digitizing the pattern of fluoresced light coming from the phosphor-containing film.Type: GrantFiled: January 31, 1989Date of Patent: June 12, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Daniel C. Carter, William K. Witherow, Marc L. Pusey, Vaughn H. Yost
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Patent number: 4932270Abstract: Piezoelectric sensor devices are attached across pairs of circularly arranged spokes arrayed on the periphery of an annular ring. The sensor devices each include a preloaded steel ball mounting arrangement for mounting a piezoelectric sensor element. A first circular interface plate on one side of the sensor structure attaches to alternate ones of the spokes, and a circular interface plate on the opposite side of the same diameter as the first interface plate attaches to the remaining spokes.Type: GrantFiled: March 21, 1989Date of Patent: June 12, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Boris J. Lurie, J. Alan Schier, Michael M. Socha
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Patent number: 4932807Abstract: A zero-play pin clevis joint for deployable space structures includes a tapered pin and tapered bores extending through a shackle and through a tang such that the tapered pin is received in the tapered bores. Spring washers urge the tapered pin into the tapered bores of the shackle and also urge the tang onto the tapered pin. Deployable truss structures use a plurality of the aforementioned zero play pin clevis joints to connect a plurality of truss tubes. The angle of taper for the various components is preferably about 12.degree. included angle.Type: GrantFiled: July 28, 1988Date of Patent: June 12, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Marvin D. Rhodes
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Patent number: 4932806Abstract: A compliant joint is provided for prosthetic and robotic devices which permits rotation in three different planes. The joint provides for the controlled use of cable under motion. Perpendicular outer mounting frames are joined by swaged cables that interlock at a center block. Ball bearings allow for the free rotation of the second mounting frame relative to the first mounting frame within a predetermined angular rotation that is controlled by two stop devices. The cables allow for compliance at the stops and the cables allow for compliance in six degrees of freedom enabling the duplication or simulation of the rotational movement and flexibility of a natural hip or knee joint, as well as the simulation of a joint designed for a specific robotic component for predetermined design parameters.Type: GrantFiled: March 21, 1989Date of Patent: June 12, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Wayne D. Eklund, James J. Kerley
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Patent number: 4932491Abstract: A rough terrain vehicle is described which includes auxiliary wheels that can be deployed to avoid overturning the vehicle when turning while traversing a slope, to climb an embankment or the like, and to right the vehicle when it is overturned. The vehicle includes a pair of front and rear primary wheels, and a pair of auxiliary arms having inner ends pivotally mounted on the front wheel axes and outer ends that carry auxiliary wheels. A motor can turn the arms to move the auxiliary wheels from a stowed position about halfway between the front and rear wheels and above the ground, to a second position against the ground to stabilize the vehicle. The arms can be turned more than 180.degree. to move the auxiliary wheels in front of the front primary wheels to help climb an embankment. The primary wheels can be mounted at the end of primary arms, so when the primary arms are turned they not only move the primary front wheels but also the inner ends of the auxiliary arms.Type: GrantFiled: March 21, 1989Date of Patent: June 12, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Earl R. Collins, Jr.
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Patent number: 4926694Abstract: A delamination test apparatus and method uses a single beam to simultaneously apply opening and shear stresses to a test specimen. A fulcrum extending downwardly from the beam produces shear stress in the specimen by downward movement, and opening stress by pivotal upward movement of the beam, which results by virtue of the fact that the applied load is on one side of the fulcrum while the test specimen is connected to the beam on the opposite side of the fulcrum.Type: GrantFiled: July 28, 1989Date of Patent: May 22, 1990Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: John H. Crews, Jr., James R. Reeder
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Patent number: 4927326Abstract: Damping seals, damping bearings and a support sleeve for the ball bearings of a high speed rotor, the ball bearings being a duplex set having the outer races packaged tightly within the sleeve while the sleeve provides a gap with a support member so that the bearings may float with the sleeve. The sleeve has a web extending radially between the pair of outer races and acts in conjunction with one or more springs to apply an axial preload to the outer races. The sleeves have a series of slits which provide the sleeve with a spring-like quality so that the spring acts to center the rotor upon which the bearings are mounted during start up and shut down. A damping seal or a damping bearing may be used in conjunction with the ball bearings and supporting sleeve, the damping seal and damping bearing having rotor portions including rigid outer surfaces mounted within the bore of a stator portion triangular shaped pockets on the surface facing the rotor.Type: GrantFiled: May 26, 1989Date of Patent: May 22, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: George L. von Pragenau
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Patent number: 4928027Abstract: A radiation type heat dissipator for use in a plasma engine is formed of a refractory metal layer upon which there is deposited a radiation emissive coating made of a high emissivity material such as zirconium diboride. The radiation emissive coating has a surface emissivity coefficient substantially greater than the emissivility coefficient of the refractory metal and thereby enhances the optical radiating efficiency of the heat dissipator.Type: GrantFiled: August 20, 1987Date of Patent: May 22, 1990Assignee: The United States of America as represented by the administrator of the National Aeronautics and Space AdministrationInventors: William D. Deininger, David Q. King
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Patent number: 4926481Abstract: A security code system for controlling access to computer and computer-controlled entry situations comprises a plurality of subsets of alpha-numeric charcters disposed in random order in matrices of at least two dimensions forming theoretical rectangles, cubes, etc., such that when access is desired, at least one pair of previously unused character subsets not found in the same row or column of the matrix is chosen at random and transmitted by the computer. The proper response to gain access is transmittal of subsets which complete the rectangle, and/or a parallelepiped whose opposite corners were defined by first groups of code. Once used, subsets are not used again to absolutely defeat unauthorized access by eavesdropping, and the like.Type: GrantFiled: December 5, 1988Date of Patent: May 15, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Earl R. Collins, Jr.
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Patent number: 4925297Abstract: A three-dimensional laser Doppler velocimeter (10) has laser optics (12) for a first channel positioned to create a probe volume (18) in space, and laser optics (14) and (16) for second and third channels, respectively, positioned to create entirely overlapping probe volumes (20) in space. The probe volumes (18) and (20) overlap partially in space. Photodetector (22) is positioned to receive light scattered by a particle present in the probe volume (18), while photodetectors (24) and (26)are positioned to receive light scattered by a particle present in the probe volume (20). The photodetector (22) for the first channel is directly connected to provide a first channel analog signal (23) to frequency measuring circuits 28. The first channel is therefore a primary channel for the system.Type: GrantFiled: October 14, 1988Date of Patent: May 15, 1990Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space AdministrationInventor: James L. Brown
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Patent number: 4922807Abstract: A ballast system for a glove box including a fixed platform on which is mounted an inflatable bag on top of which resides a cover and a weight. The variable gas volume of the inflatable bag communicates with that of the glove box via a valved tube. The weight and gas volume are selected to maintain a relatively constant pressure in the glove box despite variations in the glove box volume while avoiding the use of complicated valving apparatus.Type: GrantFiled: September 29, 1989Date of Patent: May 8, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Paul J. Shlichta
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Patent number: 4924053Abstract: A welding torch for gas tungsten arc welding apparatus has a hollow tungsten electrode including a ceramic liner and forms the filler metal wire guide. The wire is fed through the tungsten electrode thereby reducing the size of the torch to eliminate clearance problems which exist with external wire guides. Since the wire is pre-heated from the tungsten more wire may be fed into the weld puddle, and the wire will not oxidize because it is always within the shielding gas.Type: GrantFiled: December 5, 1988Date of Patent: May 8, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Gene E. Morgan, Gerald E. Dyer
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Patent number: 4924507Abstract: System for optically recognizing and tracking a plurality of objects within a field of vision. Laser (46) produces a coherent beam (48). Beam splitter (24) splits the beam into object (26) and reference (28) beams. Beam expanders (50) and collimators (52) transform the beams (26, 28) into coherent collimated light beams (26', 28'). A two-dimensional SLM (54), disposed in the object beam (26'), modulates the object beam with optical information as a function of signals from a first camera (16) which develops X and Y signals reflecting the contents of its field of vision. A hololens (38), positioned in the object beam (26') subsequent to the modulator (54), focuses the object beam at a plurality of focal points (42). A planar transparency-forming film (32), disposed with the focal points on an exposable surface, forms a multiple position interference filter (62) upon exposure of the surface and development processing of the film (32).Type: GrantFiled: February 11, 1988Date of Patent: May 8, 1990Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Tien-Hsin Chao, Hua-Kuang Liu
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Patent number: 4923741Abstract: A flexible multi-layered covering article 10 for protection against the hazards of exposure to the environment of outer space. The covering 10 includes an outer layer section 12 comprising an outermost lamina 14 of woven expanded tetrafluoroethylene yarns (Gore-Tex) for protecting against abrasion and tearing, an underlying weave 16 of meta-aramid yarns (Nomex) and para-aramid yarns (Kevlar) for particle impart protection, an electrostatic charge dissipation and control system 18 incorporated therein, and a chemical contaminants control barrier applied as a coating 19. A middle section includes a succession of thermal insulating layers 21 of polymeric thermoplastic or thermoforming material, each of which is coated with a metal deposit of high infra-red emissivity and low solar radiation absorption characteristics and separated from adjacent insulating layers 21 by a low thermal conductance material 26.Type: GrantFiled: June 30, 1988Date of Patent: May 8, 1990Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space AdministrationInventors: Joseph J. Kosmo, Frederic S. Dawn