Patents Represented by Attorney Wilfred Grifka
  • Patent number: 4044821
    Abstract: One embodiment of a low to high temperature energy conversion system includes a decomposition chamber in which ammonia (NH.sub.3) is decomposed into hydrogen and nitrogen by absorbing heat of decomposition from a low temperature, e.g., 300.degree. C energy source. The separated hydrogen and nitrogen are then supplied to a recombination chamber wherein they recombine to produce ammonia. The recombination process is associated with a significant increase in temperature, used to increase the temperature of a fluid to temperatures on the order of 500.degree. C.
    Type: Grant
    Filed: December 27, 1974
    Date of Patent: August 30, 1977
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Charles G. Miller
  • Patent number: 4045315
    Abstract: Hydrogen is produced by the solar photolysis of water in a first photo-oxidation vessel with a transparent wall in the presence of a water soluble photo-oxidizable reagent and an insoluble hydrogen recombination catalyst. Simultaneously oxygen is produced in a second photo-reduction reactor with a transparent wall in the presence of an insoluble photo-reduction reagent catalyst. When spent, the solution from the first reactor is fed into the second reactor. A reaction occurs in the dark in which the redox reagents are regenerated, and the regenerated photo-oxidation reagent solution is recycled to the first reactor. The photo-oxidation reagent is preferably a europium salt, and the first reactor also contains a hydrogen recombination catalyst such as platinum supported on glass beads.
    Type: Grant
    Filed: February 13, 1976
    Date of Patent: August 30, 1977
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Porter R. Ryason
  • Patent number: 4045359
    Abstract: The yield of photonically excited gas phase reactions is increased by extracting excess energy from unstable, excited species by contacting the species with the surface of a finely divided solid.
    Type: Grant
    Filed: January 29, 1976
    Date of Patent: August 30, 1977
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Melvin M. Saffren
  • Patent number: 4041233
    Abstract: A novel aldehyde-containing polymer (ACP) is prepared by reaction of a polysaccharide with periodate to introduce aldehyde groups onto the C.sub.2 - C.sub.3 carbon atoms and by introduction of ether and ester groups onto the pendant primary hydroxyl to modify solubility characteristics. The ACP is utilized to absorb nitrogen bases such as urea in vitro or in vivo.
    Type: Grant
    Filed: March 15, 1976
    Date of Patent: August 9, 1977
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, William A. Mueller, George C. Hsu, Harold E. Marsh, Jr.
  • Patent number: 4039489
    Abstract: A polymer system and resulting method useful for absorbing fats or oils which comprises forming a solid, network polymer having a minimal amount of cross-linking. The polymer that remains solid at a swelling ratio in oil or fat of at least ten and thus provides an oil absorption greater than 900 weight percent.
    Type: Grant
    Filed: April 7, 1976
    Date of Patent: August 2, 1977
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Harold E. Marsh, Jr.
  • Patent number: 4035065
    Abstract: An inexpensive, lightweight reflective assembly member having good optical quality is provided. The reflective assembly is particularly adaptable to accommodating temperature variations without providing destructive thermal stresses and reflective slope errors. The reflective assembly may consist of a thin lamina reflective surface member and a lightweight substrate member of cellular structure. The respective materials may be chosen so that the coefficient of thermal expansion will be approximately the same. The substrate can comprise a cellular glass block while the reflective lamina member can be a thin sheet of glass with appropriate reflective coating. The lamina and cellular substrate member can be bonded together to form the reflective assembly. The method of fabrication includes abrading the cellular substrate with an abrasive master die to form an appropriate concave surface.
    Type: Grant
    Filed: September 24, 1975
    Date of Patent: July 12, 1977
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Maurice J. Argoud, Jack Jolley, Walter L. Walker
  • Patent number: 4030348
    Abstract: An improved machine for use in determining the fatigue life for elastomeric specimens. The machine is characterized by a plurality of juxtaposed test stations, specimen support means located at each of the test stations for supporting a plurality of specimens of elastomeric material and means for subjecting the specimens at each of said stations to sinusoidal strain at a strain rate unique with respect to the strain rate at which the specimens at each of the other stations is subjected to sinusoidal strain.
    Type: Grant
    Filed: January 29, 1976
    Date of Patent: June 21, 1977
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, George E. Fitzer
  • Patent number: 4007430
    Abstract: A method and apparatus for producing intense, coherent, monochromatic light from a low temperature plasma are disclosed. The apparatus includes a housing for confining a gas at subatmospheric pressure and including a set of reflectors defining an optical cavity. At least one anode and cathode are positioned within the gas. First control means control the voltage applied to the anode and second control means independently control the temperature of the cathode. The pressure of the gas is controlled by a third control means. An intense monochromatic output is achieved by confining the gas in the housing at a controlled pre-determined reduced pressure, independently controlling the temperature of the electron emitting cathode and applying a predetermined controlled low voltage to the anode. An intermediate mode current is drawn from the cathode and produces in the confined gas, a region having a high density of metastable atomic states leading to a population inversion.
    Type: Grant
    Filed: August 10, 1971
    Date of Patent: February 8, 1977
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Willard F. Libby, Carl A. Jensen, Lowell L. Wood
  • Patent number: 3996070
    Abstract: A thermocouple assembly which includes a plug having a pair of small diameter holes near one end thereof which are spaced a small distance apart to leave a thin quantity of plug material between the holes, and a pair of thermocouple wires extending through the different holes and with the outer ends of the wires joined to the thin quantity of plug material which lies between the holes to form a thermocouple junction.
    Type: Grant
    Filed: November 22, 1974
    Date of Patent: December 7, 1976
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Walter B. Powell, Lee R. Potter, Kenton S. MacDavid
  • Patent number: 3996464
    Abstract: A mass spectrometer (MS) with unique magnetic pole pieces which provide a homogenous magnetic field across the gap of the MS magnetic sector as well as the magnetic field across an ion-type vacuum pump is disclosed. The pole pieces form the top and bottom sides of a housing. The housing is positioned so that portions of the pole pieces form part of the magnetic sector with the space between them defining the gap region of the magnetic sector, through which an ion beam passes. The pole pieces extend beyond the magnetic sector with the space between them being large enough to accommodate the electrical parts of an ion-type vacuum pump. The pole pieces which provide the magnetic field for the pump, together with the housing form the vacuum pump enclosure or housing.
    Type: Grant
    Filed: November 21, 1975
    Date of Patent: December 7, 1976
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Leonard M. Sieradski, Charles E. Giffin, Alfred O. Nier
  • Patent number: 3990860
    Abstract: Cermet composition having high temperature oxidation resistance, high abrasion and corrosion resistances, and good thermal shock resistance, and particularly adapted for production of high temperature resistant cermet insulator bodies, comprising a sintered body of particles of stainless steel or molybdenum, in a ceramic phase comprised of a ceramic oxide, particularly a ceramic mixture of chromium oxide and aluminum oxide, and forming a coating of chromium oxide as an oxidation barrier around the metal particles, to provide oxidation resistance for the metal particles.The cermet compositions are designed particularly to provide high temperature resistant refractory coatings on stainless steel or molybdenum substrates.
    Type: Grant
    Filed: November 20, 1975
    Date of Patent: November 9, 1976
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Wayne M. Phillips
  • Patent number: 3983749
    Abstract: An annular arc accelerator shock tube employs a cold gas driver to flow a stream of gas from an expansion section through a high voltage electrode section to a test section, thus driving a shock wave in front of it. A glow discharge detects the shock wave and actuates a trigger generator which in turn fires spark-gap switches to discharge a bank of capacitors across a centered cathode and an annular anode in tandem electrode sections as the initial shock wave passes through the anode section from the cathode section thereby depositing energy into the flow gas without the necessity of any diaphragm opening in the gas flow from the expansion section through the electrode sections.
    Type: Grant
    Filed: November 6, 1974
    Date of Patent: October 5, 1976
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Lewis P. Leibowitz
  • Patent number: 3983714
    Abstract: A cryostat system for cooling a device to a temperature on the order of 2.degree.K or less includes a dewar, in which helium, in other than the superfluid state, is stored. Helium flows from the dewar through a heat exchanger tube and a restrictor tube, which controls the helium flow rate, into the cavity of a heat exchanger, to whose outer wall the device to be cooled is attached. A pressure regulator valve controls the pressure in the cavity to be very low, e.g., on the order of 30 Torr. As the helium exits the restrictor tube into the cavity, due to low pressure cavity, it becomes an aerosol mixture of helium gas and superfluid helium droplets at the desired temperature. The latter form a thin layer or film of superfluid helium on the inner side of the heat exchanger wall and thereby cool the device, which is attached to the wall to the desired temperature.
    Type: Grant
    Filed: July 24, 1975
    Date of Patent: October 5, 1976
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Charles G. Miller, James B. Stephens
  • Patent number: 3982910
    Abstract: A process and apparatus are described for producing hydrogen-rich product gases by mixing a spray of liquid hydrocarbon with a stream of air in a startup procedure and the mixture is ignited for partial oxidation, then the stream of air is heated by the resulting combustion to reach a temperature such that a signal is produced. The signal triggers a two way valve which directs liquid hydrocarbon from a spraying mechanism to a vaporizing mechanism with which a vaporized hydrocarbon is formed. The vaporized hydrocarbon is subsequently mixed with the heated air in the combustion chamber where partial oxidation takes place and hydrogen-rich product gases are produced.
    Type: Grant
    Filed: July 10, 1974
    Date of Patent: September 28, 1976
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: John Houseman, Donald J. Cerini
  • Patent number: 3978490
    Abstract: An improved furlable antenna particularly suited for use in a celestial space environment. The antenna is characterized by an actuator comprising an elastomeric member of an annular configuration, an annular array of uniformly spaced antenna ribs rigidly affixed at the base ends thereof to said actuator and supported thereby for pivotal displacement from a deployed configuration, wherein the ribs are substantially radially extended from said actuator to a furled configuration wherein the ribs are extended in substantial parallelism with the axis of the actuator, a flexible reflecting web affixed to the ribs, and a plurality of angularly spaced bearing blocks supporting every radially extended section of the member for rotation about its own centroid.
    Type: Grant
    Filed: September 24, 1975
    Date of Patent: August 31, 1976
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Morris A. Barnett
  • Patent number: 3978187
    Abstract: Annular elastomeric bodies having intricate shapes are cast by dipping a heated, rotating mandrel into a solution of the elastomer, permitting the elastomer to creep into sharp recesses, dryng the coated mandrel and repeating the operation until the desired thickness has been achieved. A bladder for a heart assist pump in which a cylindrical body terminating in flat, sharp horizontal flanges fabricated by this procedure has been subjected to over 2,500 hours of simulated life conditions with no visible signs of degradation.
    Type: Grant
    Filed: March 28, 1975
    Date of Patent: August 31, 1976
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Howard F. Broyles, Jovan Moacanin, Edward F. Cuddihy
  • Patent number: 3972651
    Abstract: A solar-powered pump particularly suited for intermittently delivering a stream of water. The pump is characterized by a housing adapted to be seated in a source of water having a water discharge port disposed above the water line of the source, a sump including a valved inlet port through which water is introduced to the sump, disposed beneath the water line, a displacer supported for vertical reciprocation in said housing, an air passageway extended between the vertically spaced faces of the displacer, a tipple disposed adjacent to the water discharge port adapted to be filled in response to a discharge of water from the housing, and a line so interconnecting the tipple and the displacer that the displacer is moved upwardly in response to a filling of the tipple and moved downwardly once water is discharged from the tipple.
    Type: Grant
    Filed: April 9, 1975
    Date of Patent: August 3, 1976
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Charles C. Kirsten
  • Patent number: 3971847
    Abstract: A process and apparatus is described for producing a hydrogen rich gas by introducing a liquid hydrocarbon fuel in the form of a spray into a partial oxidation region and mixing with a mixture of steam and air that is preheated by indirect heat exchange with the formed hydrogen rich gas, igniting the hydrocarbon fuel spray mixed with the preheated mixture of steam and air within the partial oxidation region to form a hydrogen rich gas. The apparatus for performing the process is in the form of a bell-shaped chamber which consists of an open cylinder wherein a partial oxidation reaction takes place. An air pasageway and a pipe for injecting water into the passageway are provided for forming a steam-air mixture. The air is preheated indirectly by the heat generated as a result of igniting a hydrocarbon fuel spray and thus the water is converted into steam when injected into the preheated air.
    Type: Grant
    Filed: February 27, 1975
    Date of Patent: July 27, 1976
    Assignee: The United States of America as represented by the Adminstrator of the National Aeronautics and Space Administration
    Inventor: John Houseman
  • Patent number: 3971364
    Abstract: A force transducer for measuring dynamic force activity within the heart of a subject essentially consists of a U-shaped beam of low elastic compliance material. Two tines extend from the beam's legs and a long coil spring is attached to the beam. A strain gauge is coupled to one of the beam's legs to sense deflections thereof. The beam with the tines and most of the spring are surrounded by a flexible tube, defining a catheter, which is insertable into a subject's heart through an appropriate artery. The tines are extractable from the catheter for implantation into the myocardium by pushing on the end of the spring which extends beyond the external end of the catheter. The tines are retractable back into the catheter, prior to catheter removal from the subject, by pulling on the externally exposed spring end.
    Type: Grant
    Filed: May 16, 1975
    Date of Patent: July 27, 1976
    Inventors: James C. Administrator of the National Aeronautics and Space Administration Fletcher, Cyril Feldstein, Gilbert W. Lewis, Robert H. Silver, Virgil H. Culler
  • Patent number: 3971230
    Abstract: A Stirling cycle heat engine is disclosed in which displacer motion is controlled as a function of the working fluid pressure P.sub.1 and a substantially constant pressure P.sub.0. The heat engine includes an auxiliary chamber at the constant pressure P.sub.0. An end surface of a displacer piston is disposed in the auxiliary chamber. During the compression portion of the engine cycle when P.sub.1 rises above P.sub.0 the displacer forces the working fluid to pass from the cold chamber to the hot chamber of the engine. During the expansion portion of the engine cycle the heated working fluid in the hot chamber does work by pushing down on the engine's drive piston. As the working fluid pressure P.sub.1 drops below P.sub.0 the displacer forces most of the working fluid in the hot chamber to pass through the regenerator to the cold chamber.
    Type: Grant
    Filed: May 5, 1975
    Date of Patent: July 27, 1976
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Walter H. Higa