Patents Assigned to The United States of America as represented by the United States National Aeronautics and Space Administration
  • Patent number: 6447266
    Abstract: A blood pump preferably has a magnetically suspended rotor that rotates within a housing. The rotor may rotate about a stator disposed within the housing. Radial magnetic bearings may be defined within the stator and the rotor in order to suspend the rotor. The radial magnetic bearings may be passive magnetic bearings that include permanent magnets disposed within the stator and the rotor or active magnetic bearings. The pump may further include an axial magnetic bearing that may be either a passive or an active magnetic bearing. A motor that drives the rotor may be disposed within the housing in order to more easily dissipate heat generated by the motor. A primary flow path is defined between the rotor and the stator, and a secondary flow path is defined between the stator and the rotor. Preferably, a substantial majority of blood passes through the primary flow path.
    Type: Grant
    Filed: April 24, 2001
    Date of Patent: September 10, 2002
    Assignees: University of Pittsburgh, The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: James F. Antaki, Bradley Paden, Gregory Burgreen, Nelson J. Groom
  • Patent number: 6446979
    Abstract: A thermal barrier for extremely high temperature applications consists of a carbon fiber core and one or more layers of braided carbon fibers surrounding the core. The thermal barrier is preferably a large diameter ring, having a relatively small cross-section. The thermal barrier is particularly suited for use as part of a joint structure in solid rocket motor casings to protect low temperature elements such as the primary and secondary elastomeric O-ring seals therein from high temperature gases of the rocket motor. The thermal barrier exhibits adequate porosity to allow pressure to reach the radially outward disposed O-ring seals allowing them to seat and perform the primary sealing function. The thermal barrier is disposed in a cavity or groove in the casing joint, between the hot propulsion gases interior of the rocket motor and primary and secondary O-ring seals.
    Type: Grant
    Filed: June 27, 2000
    Date of Patent: September 10, 2002
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: Bruce M. Steinetz, Patrick H. Dunlap, Jr.
  • Patent number: 6350817
    Abstract: Phenylethynyl containing reactive additives were prepared from aromatic diamines containing phenylethynyl groups and various ratios of phthalic anhydride and 4-phenylethynylphthalic anhydride in glacial acetic acid to form the imide in one step or in N-methyl-2-pyrrolidinone to form the amide acid intermediate. The reactive additives were mixed in various amounts (10% to 90%) with oligomers containing either terminal or pendent phenylethynyl groups (or both) to reduce the melt viscosity and thereby enhance processability. Upon thermal cure, the additives react and become chemically incorporated into the matrix and effect an increase in crosslink density relative to that of the host resin. This resultant increase in crosslink density has advantageous consequences on the cured resin properties such as higher glass transition temperature and higher modulus as compared to that of the host resin.
    Type: Grant
    Filed: April 13, 1999
    Date of Patent: February 26, 2002
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: John W. Connell, Joseph G. Smith, Jr., Paul M. Hergenrother
  • Patent number: 6308113
    Abstract: An assembly for moving a robotic device along selected axes includes a programmable logic controller (PLC) for controlling movement of the device along selected axes to effect movement of the device to a selected disposition. The PLC includes a plurality of single axis motion control modules, and a central processing unit (CPU) in communication with the motion control modules. A human-machine interface is provided for operator selection of configurations of device movements and is in communication with the CPU. A motor drive is in communication with each of the motion control modules and is operable to effect movement of the device along the selected axes to obtain movement of the device to the selected disposition.
    Type: Grant
    Filed: June 9, 2000
    Date of Patent: October 23, 2001
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: Brentley Craig Nowlin, Lisa Danielle Koch
  • Patent number: 6284325
    Abstract: A barrier layer for a silicon containing substrate which inhibits the formation of gaseous species of silicon when exposed to a high temperature aqueous environment comprises a calcium alumino silicate.
    Type: Grant
    Filed: November 16, 2000
    Date of Patent: September 4, 2001
    Assignees: General Electric Company, United Technologies Corporation, The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: Harry Edwin Eaton, Jr., William Patrick Allen, Robert Alden Miller, Nathan S. Jacobson, James L. Smialek, Elizabeth J. Opila, Kang N. Lee, Bangalore A. Nagaraj, Hongyu Wang, Peter Joel Meschter, Krishan Lal Luthra
  • Patent number: 6278404
    Abstract: The satellite selection method as utilized by the spaceborne Global Positioning System receiver provides navigational solutions and is designed for use in low Earth orbit. The satellite selection method is a robust algorithm that can be used a GPS receiver to select appropriate GPS satellites for use in calculating point solutions or attitude solutions. The method is takes into account the difficulty of finding a particular GPS satellite phase code, especially when the search range in greatly increased due to Doppler shifts introduced into the carrier frequency. The method starts with an update of the antenna pointing and spacecraft vectors to determine the antenna backplane direction. Next, the GPS satellites that will potentially be in view of the antenna are ranked on a list, whereby the list is generated based on the estimated attitude and position of each GPS satellite. Satellites blocked by the Earth are not entered on this list.
    Type: Grant
    Filed: July 7, 1999
    Date of Patent: August 21, 2001
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventor: Frederick A. Niles
  • Patent number: 6125297
    Abstract: Method and apparatus are described for determining volumes of body fluids in a subject using bioelectrical response spectroscopy. The human body is represented using an electrical circuit. Intra-cellular water is represented by a resistor in series with a capacitor; extra-cellular water is represented by a resistor in series with two parallel inductors. The parallel inductors represent the resistance due to vascular fluids. An alternating, low amperage, multi-frequency signal is applied to determine a subject's impedance and resistance. From these data, statistical regression is used to determine a 1% impedance where the subject's impedance changes by no more than 1% over a 25 kHz interval. Circuit components of the human body circuit are determined based on the 1% impedance. Equations for calculating total body water, extra-cellular water, total blood volume, and plasma volume are developed based on the circuit components.
    Type: Grant
    Filed: February 6, 1998
    Date of Patent: September 26, 2000
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventor: Steven F. Siconolfi
  • Patent number: 6098579
    Abstract: Carbon fiber reinforced carbon composite rotary, sleeve, and disc valves for internal combustion engines and the like are disclosed. The valves are formed from knitted or braided or warp-locked carbon fiber shapes. Also disclosed are valves fabricated from woven carbon fibers and from molded carbon matrix material. The valves of the present invention with their very low coefficient of thermal expansion and excellent thermal and self-lubrication properties, do not present the sealing and lubrication problems that have prevented rotary, sleeve, and disc valves from operating efficiently and reliably in the past. Also disclosed are a sealing tang to further improve sealing capabilities and anti-oxidation treatments.
    Type: Grant
    Filed: May 27, 1999
    Date of Patent: August 8, 2000
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: G. Burton Northam, Philip O. Ransone, H. Kevin Rivers
  • Patent number: 6060811
    Abstract: The present invention relates to the mounting of pre-stressed electroactive material in such a manner that large displacement actuators or sensors result. The invention comprises mounting the pre-stressed electroactive material to a support layer. This combination of a pre-stressed electroactive material and support layer may in turn be attached to a mounting surface. The pre-stressed electroactive material may be a ferroelectric, pyroelectric, piezoelectric, or magnetostrictive material. The size, stiffness, mass, and material of the support layer is selected to result in the electroactive device having dynamic response properties, environmental capability characteristics, and the required resilience optimized for a given application. The capacity to connect the support layer to a surface expands the arenas in which the pre-stressed electroactive device may be used.
    Type: Grant
    Filed: July 25, 1997
    Date of Patent: May 9, 2000
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: Robert L. Fox, Richard F. Hellbaum, Robert G. Bryant, Benjamin M. Copeland, Jr.
  • Patent number: 6055048
    Abstract: An optical-to-tactile translator provides an aid for the visually impaired by translating a near-field scene to a tactile signal corresponding to said near-field scene. An optical sensor using a plurality of active pixel sensors (APS) converts the optical image within the near-field scene to a digital signal. The digital signal is then processed by a microprocessor and a simple shape signal is generated based on the digital signal. The shape signal is then communicated to a tactile transmitter where the shape signal is converted into a tactile signal using a series of contacts. The shape signal may be an outline of the significant shapes determined in the near-field scene, or the shape signal may comprise a simple symbolic representation of common items encountered repeatedly. The user is thus made aware of the unseen near-field scene, including potential obstacles and dangers, through a series of tactile contacts.
    Type: Grant
    Filed: August 7, 1998
    Date of Patent: April 25, 2000
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: Maurice L. Langevin, Philip I Moynihan
  • Patent number: 6033510
    Abstract: A method for fabricating composite structures at a low-cost, moderate-to-high production rate. A first embodiment of the method includes employing a continuous press forming fabrication process. A second embodiment of the method includes employing a pultrusion process for obtaining composite structures. The methods include coating yarns with matrix material, weaving the yarn into fabric to produce a continuous fabric supply and feeding multiple layers of net-shaped fabrics having optimally oriented fibers into a debulking tool to form an undebulked preform. The continuous press forming fabrication process includes partially debulking the preform, cutting the partially debulked preform and debulking the partially debulked preform to form a netshape. An electron-beam or similar technique then cures the structure. The pultrusion fabric process includes feeding the undebulked preform into a heated die and gradually debulking the undebulked preform.
    Type: Grant
    Filed: September 23, 1997
    Date of Patent: March 7, 2000
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventor: Gary L. Farley
  • Patent number: 6018861
    Abstract: A device for measuring turbulence in high-speed flows is provided which includes a micro-sensor thin-film probe. The probe is formed from a single crystal of aluminum oxide having a 14.degree. half-wedge shaped portion. The tip of the half-wedge is rounded and has a thin-film sensor attached along the stagnation line. The bottom surface of the half-wedge is tilted upward to relieve shock induced disturbances created by the curved tip of the half-wedge. The sensor is applied using a microphotolithography technique.
    Type: Grant
    Filed: August 15, 1996
    Date of Patent: February 1, 2000
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: Mark Sheplak, Catherine B. McGinley, Eric F. Spina, Ralph M. Stephens, Purnell Hopson, Jr., Vincent B. Cruz
  • Patent number: 5948977
    Abstract: A soft-sided air displacement volumometer includes a soft-sided bag, an air injector, a pressure transducer, and a recording device. The soft-sided volumometer is used to measure the total body volume of a person or the volume of one limb of a person. After the person enters the soft-sided bag, the bag is sealed and pressurized to a predetermined level using the air injector. The pressure inside the soft-sided bag is continuously monitored using the pressure transducer and recording device while the volume of the soft-side bag is incrementally reduced. The elasticity of the soft-sided bag is eliminated from the volume calculations by operating the soft-sided air displacement volumometer over a relatively small range of volumes and pressures in which the elasticity is substantially constant. The volume of the person inside the soft-sided bag is calculated as the volume of the empty bag (i.e. without a person) minus the initial volume of the bag with the person pressurized to an initial pressure level.
    Type: Grant
    Filed: March 31, 1998
    Date of Patent: September 7, 1999
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventor: Steven F. Siconolfi
  • Patent number: 5919387
    Abstract: A method for bonding or joining plastic or metallic pipe using induced energy is provided. A susceptor is placed between the two pipes to be joined and a magnetic flux is induced onto the susceptor. The second pipe may be a coupling device. The magnetic flux may be induced by a tank circuit or an induction heating gun. The induction heating gun may be formed with a hinged heating head. The susceptor may be a perforated metal ring or a wire coil. The susceptor is coated with a material compatible with the pipes, for example, a plastic adhesive material, magnetic flux is an induction heating gun having a hinged heating head.
    Type: Grant
    Filed: April 3, 1997
    Date of Patent: July 6, 1999
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: John D. Buckley, Robert L. Fox, Samuel D. Johnson, Carl E. Copeland, Robert H. Coultrip
  • Patent number: 5866676
    Abstract: Polyimide copolymers were prepared by reacting different ratios of 3,4'-oxydianiline (ODA) and 1,3-bis(3-aminophenoxy)benzene (APB) with 3,3',4,4'-biphenylcarboxylic dianhydride (BPDA) and endcapping with an effective amount of a non-reactive endcapper. Within a narrow ratio of diamines, from .sup..about. 50% ODA/50% APB to .sup..about. 95% ODA/5% APB, the copolyimides prepared with BPDA have a unique combination of properties that make them very attractive for various applications. This unique combination of properties includes low pressure processing (200 psi and below), long term melt stability (several hours at 390.degree. C.), improved toughness, improved solvent resistance, improved adhesive properties, and improved composite mechanical properties.
    Type: Grant
    Filed: February 14, 1995
    Date of Patent: February 2, 1999
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventor: Brian J. Jensen
  • Patent number: 5818057
    Abstract: A simultaneous luminescence pressure and temperature mapping system is developed including improved dye application techniques for surface temperature and pressure measurements from 5 torr to 1000 torr with possible upgrade to from 0.5 torr to several atmospheres with improved camera resolution. Adsorbed perylene dye on slip-cast silica is pressure (oxygen) sensitive and reusable to relatively high temperatures (.about.150.degree. C.). Adsorbed luminescence has an approximately linear color shift with temperature, which can be used for independent temperature mapping and brightness pressure calibration with temperature.
    Type: Grant
    Filed: October 7, 1996
    Date of Patent: October 6, 1998
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventor: Gregory M. Buck
  • Patent number: 5814259
    Abstract: This invention improves upon a method for molding structural parts from preform material. Preform material to be used for the part is provided. A silicone rubber composition containing entrained air voids is prepared. The silicone rubber and preform material assembly is situated within a rigid mold cavity used to shape the preform material to the desired shape. The entire assembly is heated in a standard heating device so that the thermal expansion of the silicone rubber exerts the pressure necessary to force the preform material into contact with the mold container. The introduction of discrete air voids into the silicone rubber allows for accurately controlled pressure application on the preform material at the cure temperature.
    Type: Grant
    Filed: March 25, 1997
    Date of Patent: September 29, 1998
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: Erik S. Weiser, Robert M. Baucom, John J. Snoha
  • Patent number: 5756892
    Abstract: The invention as disclosed herein teaches apparatus whereby the instantaneous dynamic static pressure and the steady-state static pressure may be simultaneously measured within a supersonic or subsonic gaseous fluid flow field. The dynamic static pressure is measured by an electronic transducer and the steady-state static pressure is measured by pneumatic means.
    Type: Grant
    Filed: February 27, 1997
    Date of Patent: May 26, 1998
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: A. Robert Porro, Michael A. Ernst
  • Patent number: 5723923
    Abstract: A torque reaction/momentum wheel device for attitude control of a body, such as a spacecraft, having a motor driven flywheel with the flywheel at one end of a shaft and cantilevered with respect to at least two bearings which support the shaft which is common to the motor and flywheel, all having substantially the same spin axis. A housing which supports the motor and bearings is located all on one side of the flywheel which allows the flywheel to be balanced while mounted onto the shaft thus reducing dynamic unbalance forces. A cover is placed over the flywheel, motor, and housing so that the torque reaction/momentum wheel device can be pressurized which is necessary to prevent the bearing lubricant from migrating or evaporating out of the bearings. The bearings are lubricated by a grease which has low drag torque characteristics. This grease is a diester based oil with a lithium soap additive and filtered so that all particles are less than 10 microns in size.
    Type: Grant
    Filed: February 21, 1995
    Date of Patent: March 3, 1998
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventor: Charles E. Clagett
  • Patent number: 5698771
    Abstract: A hydrocarbon gas detection device operates by dissociating or electro-chemically oxidizing hydrocarbons adsorbed to a silicon carbide detection layer. Dissociation or oxidation are driven by a varying potential applied to the detection layer. Different hydrocarbon species undergo reaction at different applied potentials so that the device is able to discriminate among various hydrocarbon species. The device can operate at temperatures between 100.degree. C. and at least 650.degree. C., allowing hydrocarbon detection in hot exhaust gases. The dissociation reaction is detected either as a change in a capacitor or, preferably, as a change of current flow through an FET which incorporates the silicon carbide detection layers. The silicon carbide detection layer can be augmented with a pad of catalytic material which provides a signal without an applied potential. Comparisons between the catalytically produced signal and the varying potential produced signal may further help identify the hydrocarbon present.
    Type: Grant
    Filed: March 30, 1995
    Date of Patent: December 16, 1997
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: Virgil B. Shields, Margaret A. Ryan, Roger M. Williams