Patents Assigned to Administration
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Patent number: 5149932Abstract: A gas/arc electrode for use under vacuum conditions wherein a first housing encloses a second housing, with an end of the second housing extending through an opening in the first housing and having therein an outlet orifice. Provisions are made for circulating a coolant through the first housing to surround and cool the second housing. An electrical current and a gas, such as argon, as passed through the second housing, with the current flowing through a narrow stream of the ionized gas flowing through the outlet orifice to a workpiece to be treated. The second housing forms a chamber which has a cross sectional area, in a plane perpendicular to the direction of gas flow, of at least ten times the cross sectional area of the outlet orifice such that a gas pressure can be maintained in the chamber to reduce erosion of the chamber walls.Type: GrantFiled: March 29, 1991Date of Patent: September 22, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Richard M. Poorman, Jack L. Weeks
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Patent number: 5150228Abstract: Edge enhancement of an input image by four-wave mixing a first write beam with a second write beam in a photorefractive crystal, e.g., GaAs, achieved for VanderLugt optical correlation with an edge enhanced reference image by optimizing the power ratio of a second write beam to the first write beam, e.g., 70:1, and optimizing the power ratio of a read beam, which carries the reference image to the first write beam, e.g., 100:701. Liquid crystal TV panels are employed as spatial light modulators in order to change the input and reference images in real time.Type: GrantFiled: November 25, 1991Date of Patent: September 22, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Tsuen-Hsi Liu, Li-Jen Cheng
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Patent number: 5149387Abstract: Flush mounting of a sensor on a surface is provided by first forming a recessed area on the surface. Next an adhesive bonding mixture is introduced into the recessed area. The adhesive bonding mixture is chosen to provide thermal expansion matching with the surface surrounding the recessed area. A strip of high performance polymeric tape is provided, with the sensor attached to the underside thereof, and the tape is positioned over the recessed area so that it acts as a carrier of the sensor. A shim having a flexibility so that it will conform to the surface surrounding the recessed area is placed over the tape, and a vacuum pad is placed over the shim. The area above the surface is then evacuated while holding the sensor flush with the surface during curing of the adhesive bonding mixture. After such curing, the pad, shim, and tape are removed from the sensor, electrical connections for the sensor are provided, after which the remaining space in the recessed area is filled with a polymeric foam.Type: GrantFiled: May 6, 1991Date of Patent: September 22, 1992Assignee: Administrator of the National Aeronautics and Space AdministrationInventor: Thomas C. Moore, Sr.
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Patent number: 5150026Abstract: A redundant robot control scheme is provided for avoiding obstacles in a workspace during motion of an end effector along a preselected trajectory by stopping motion of the critical point on the robot closest to the obstacle when the distance therebetween is reduced to a predetermined sphere of influence surrounding the obstacle. Algorithms are provided for conveniently determining the critical point and critical distance.Type: GrantFiled: November 19, 1990Date of Patent: September 22, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Homayoun Seraji, Richard D. Colbaugh, Kristin L. Glass
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Patent number: 5149046Abstract: A device for holding reading materials for use by readers without arm mobility adapted to hold the reading materials in position for reading with the pages displayed to enable turning by use of a rubber tipped stick held in the mouth having a pair of rectangular frames for holding and positioning the reading material opened in reading posture with the pages displayed at a substantially unobstructed sighting position for reading with the pair of rectangular frames connected to one another by a hinge so the angle between the frames may be varied thereby varying the inclination of the reading materials.Type: GrantFiled: December 24, 1991Date of Patent: September 22, 1992Assignee: The United States of America as represented by the Administrator, National Aeronautics & Space AdministrationInventors: James J. Kerley, Wayne D. Eklund
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Patent number: 5149746Abstract: This invention is a process for making a semi-interpenetrating polymer network which includes a high performance thermosetting polyimide having a nadic end group acting as a crosslinking site and a high performance linear thermoplastic polyimide having the following repeating unit: ##STR1## Provided is an improved high temperature matrix resin which is capable of performing at 316.degree. C. in air for several hundreds of hours. This resin has significantly improved toughness and microcracking resistance, excellent processability and mechanical performance, and cost effectiveness.Type: GrantFiled: March 6, 1991Date of Patent: September 22, 1992Assignee: The United States of America as represented by The National Aeronautics and Space AdministrationInventor: Ruth H. Pater
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Patent number: 5146803Abstract: A rolling joint is provided for obtaining slewing maneuvers for various apparatuses including space structures, space vehicles, robotic manipulators and simulators. Two noncircular cylinders, namely a drive and a driven cylinder, are provided in driving contact with one another. This contact is maintained by two pairs of generally S-shaped bands, each pair forming a generally 8-shaped coupling tightly about the circumferential periphery of the noncircular drive and driven cylinders. A stationarily fixed arm extends between and is rotatably journalled with a drive axle and a spindle axle respectively extending through selected rotational points of the drive cylinder and of the driven cylinder. The noncircular cylinders are profiled to obtain the desired varying gear ratio.Type: GrantFiled: March 28, 1991Date of Patent: September 15, 1992Assignee: Administrator of the National Aeronautics and Space AdministrationInventors: Meng-Sang Chew, Jer-Nan Juang, Li-Farn Yang
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Patent number: 5147966Abstract: The invention is a novel polyimide prepared from 3,4'-oxydianiline (3,4'-ODA) and 4,4'-oxydiphthalic anhydride (ODPA), in 2-methoxyethyl ether (diglyme). The polymer has been prepared in ultra high molecular weight and in a controlled molecular weight form which has a 2.5 percent offset is stoichiometry (excess diamine) with a 5.0 percent level of phthalic anhydride as an endcap. This controlled molecular weight form allows for greatly improved processing of the polymer for moldings, adhesive bonding, and composite fabrication. The higher molecular weight version affords tougher films and coatings. The overall polymer structure groups in the dianhydride, the diamine, and a metal linkage in the diamine affords adequate flow properties for making this polymer useful as a molding powder, adhesive, and matrix resin.Type: GrantFiled: July 31, 1990Date of Patent: September 15, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Terry L. St. Clair, Donald J. Progar
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Patent number: 5146780Abstract: A vacuum-isolation vessel for measurement of thermal noise in microphones s an outer vessel and an inner vessel suspended within the outer vessel. A high vacuum is created between the inner and outer vessels to provide acoustical isolation. The suspension assembly coupled between the inner and outer vessels provides a substantially vibration-free environment. Thus, thermal noise in a microphone mounted within the inner vessel is accurately measured, especially at low thermal noise levels and at low frequencies.Type: GrantFiled: October 7, 1991Date of Patent: September 15, 1992Assignee: The Administrator of the National Aeronautics and Space AdministrationInventors: Allan J. Zuckerwar, Kim Chi T. Ngo
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Patent number: 5147562Abstract: A method and apparatus are provided for acoustophoresis, i.e., the separation of species via acoustic waves. An ultrasonic transducer applies an acoustic wave to one end of a sample container containing at least two species having different acoustic absorptions. The wave has a frequency tuned to or harmonized with the point of resonance of the species to be separated. This wave causes the species to be driven to an opposite end of the sample container for removal. A second ultrasonic transducer may be provided to apply a second, oppositely directed acoustic wave to prevent undesired streaming. In addition, a radio frequency tuned to the mechanical resonance and coupled with a magnetic field can serve to identify a species in a medium comprising species with similar absorption coefficients, whereby an acoustic wave having a frequency corresponding to this gyrational rate can then be applied to sweep the identified species to one end of the container for removal.Type: GrantFiled: December 17, 1990Date of Patent: September 15, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Joseph S. Heyman
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Patent number: 5145937Abstract: New polyimides have been prepared from the reaction of aromatic dianhydrides with novel aromatic diamines containing carbonyl and ether connecting groups between the aromatic rings. Several of these polyimides were shown to be semi-crystalline as evidenced by wide angle x-ray diffraction and differential scanning calorimetry. Most of the polyimides form tough solvent resistant films with high tensile properties. Several of these materials can be thermally processed to form solvent and base resistant moldings.Type: GrantFiled: November 9, 1989Date of Patent: September 8, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Paul M. Hergenrother, Stephen J. Havens
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Patent number: 5146293Abstract: A projected fringe interferometer for measuring the topography of an object periodically steps the phase angle between a pair of light beams emanating from a common source. The steps are .pi./2 radians (90.degree.) apart and at each step a video image of the fringes is recorded and stored. Photodetectors measure either the phase angle .theta. of the beams or 2.theta. either of which is used to control one of the light beams so the 90.degree. .theta. is accurately maintained. A camera, a computer, a phase controller and a phase modulator established closed-loop control of .theta.. Measuring the phase map of a flat surface establishes a calibration reference.Type: GrantFiled: May 13, 1991Date of Patent: September 8, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Carolyn R. Mercer, Glenn Beheim
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Patent number: 5146482Abstract: A multispectral variable magnification glancing incidence x-ray telescope capable of broadband, high resolution imaging of solar and stellar x-ray and extreme ultraviolet radiation sources includes a primary optical system which focuses the incoming radiation to a primary focus. Two or more rotatable mirror carriers each providing a different magnification are positioned behind the primary focus at an inclination to the optical axis, each carrier carrying a series of ellipsoidal mirrors each having a concave surface coated with a multilayer (layered synthetic microstructure) coating to reflect a different desired wavelength. The mirrors of both carriers are segments of ellipsoids having a common first focus coincident with the primary focus. A detector such as an x-ray sensitive photographic film is positioned at the second respective focus of each mirror so that each mirror may reflect the image at the first focus to the detector at the second focus.Type: GrantFiled: June 28, 1990Date of Patent: September 8, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Richard B. Hoover
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Patent number: 5145063Abstract: A Sharps container constructed from lightweight alodined non-magnetic metal material with a cup member having an elongated tapered shape and a length greater than its transverse dimensions. A magnet in the cup member provides for metal retention in the container. A non-magnetic lid member has an opening and spring biased closure flap member. The flap member is constructed from stainless steel. A Velcro patch on the container permits selective attachment at desired locations.Type: GrantFiled: October 7, 1991Date of Patent: September 8, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Angelene M. Lee
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Patent number: 5146083Abstract: A fiber optic microphone is provided for measuring fluctuating pressures. An optical fiber probe having at least one transmitting fiber for transmitting light to a pressure-sensing membrane and at least one receiving fiber for receiving light reflected from a stretched membrane is provided. The pressure-sensing membrane may be stretched for high frequency response. Further, a reflecting surface of the pressure-sensing membrane may have dimensions which substantially correspond to dimensions of a cross section of the optical fiber probe. Further, the fiber optic microphone can be made of materials for use in high temperature environments, for example greater than 1000.degree. F. A fiber optic probe is also provided with a backplate for damping membrane motion. The backplate further provides a means for on-line calibration of the microphone.Type: GrantFiled: September 21, 1990Date of Patent: September 8, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Allan J. Zuckerwar, Frank W. Cuomo, William E. Robbins, Purnell Hopson, Jr.
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Patent number: 5145130Abstract: A robot serviced space facility includes multiple modules which are identical in physical structure, but selectively differing in function and purpose. Each module includes multiple like attachment points which are identically placed on each module so as to permit interconnection with immediately adjacent modules. Connection is made through like outwardly extending flange assemblies having identical male and female configurations for interconnecting to and locking to a complementary side of another flange. Multiple rows of interconnected modules permit force, fluid, data and power transfer to be accomplished by redundant circuit paths. Redundant modules of critical subsystems are included. Redundancy of modules and of interconnections results in a space complex with any module being removable upon demand, either for module replacement or facility reconfiguration, without eliminating any vital functions of the complex.Type: GrantFiled: October 23, 1991Date of Patent: September 8, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space AdministrationInventor: Lloyd R. Purves
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Patent number: 5145942Abstract: Novel polyimides have been prepared from the reaction of aromatic diahydrides with novel aromatic diamines having carbonyl and ether groups connecting aromatic rings containing pendant methyl groups. The methyl substituent polyimides exhibit good solubility and form tough, strong films. Upon exposure to ultraviolet irradiation and/or heat, the methyl substituted polyimides crosslink to become insoluble.Type: GrantFiled: September 28, 1990Date of Patent: September 8, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Paul M. Hergenrother, Stephen J. Havens
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Patent number: 5145227Abstract: An electromagnetic attachment mechanism for use as an end effector of a remote manipulator system. A pair of electromagnets 15A, 15B, each with a U-shaped magnetic core with a pull-in coil 34 and two holding coils 35,36 are mounted by a spring suspension system 38,47 on a base plate 25 of the mechanism housing 30 with end pole pieces 21,22 adapted to move through openings in the base plate when the attractive force of the electromagnets is exerted on a strike plate 65 of a grapple fixture 20 affixed to a target object 14. The pole pieces are spaced by an air gap from the strike plate when the mechanism first contacts the grapple fixture. An individual control circuit and power source is provided for the pull-in coil and one holding coil of each electromagnet. A back-up control circuit connected to the two power sources and a third power source is provided for the remaining holding coils.Type: GrantFiled: December 31, 1990Date of Patent: September 8, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Leo G. Monford, Jr.
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Patent number: 5142932Abstract: A plurality of identical modules are serially connected together with each module including a base plate and a top plate interconnected by a universal joint assembly so that the top plate is adapted to pivotally nutate around the base plate to describe a cone in space. An array of twenty-four electromagnets, sequentially energized in sets of three, are arranged in a ring around the periphery of the base plate. Selective energization of the eight sets of electromagnets causes the rim of the top plate to be magnetically attracted to the energized electromagnets. The tilt of the top pivot plate is detected and controlled over a range of 360.degree., thus permitting a series string of modules to assume any desired elongated configuration.Type: GrantFiled: September 4, 1991Date of Patent: September 1, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Israel A. Moya, Philip A. Studer
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Patent number: 5143327Abstract: A heavy launch vehicle for placing a payload into a spatial Earth orbit including an expendable, multi-container, propellant tank having a plurality of winged booster propulsion modules releasably disposed about one end thereof; and a payload supported by adapter structure at the other end. The preferred payload is an entry module adapted to be docked to a space station and used as a return vehicle for the space station crew, as scheduled, or in emergency situations. Alternately, the payload may include communication satellites, supplies, equipment and/or structural elements for the space station. The winged propulsion modules are released from the expendable propellant tank in pairs and return to Earth in a controlled glide, for safe landing at or near the launch site and prepared for reuse. The rocket engines for each propulsion module are dual-fuel, dual-mode engines and use methane-oxygen and hydrogen-oxygen, respectively, from the multi-containers of the propellant tank.Type: GrantFiled: August 31, 1990Date of Patent: September 1, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: James A. Martin