Patents Assigned to United States of America as represented by the National Aeronautics and Space Administration
  • Patent number: 7513546
    Abstract: The present invention relates to a conformal gripping device. In an embodiment of the present invention a conformal gripper device may be disclosed comprising a frame that includes an array of movable pins. The device may also include a roller locking and unlocking system within the frame. The system may comprise a pair of locking rollers for each row of gripper pins to facilitate locking and unlocking the array of gripper pins on a column-by-column basis. The system may also include a striker element that may force the locking rollers to roll along an angled roll surface to facilitate unlocking of the array of pins on a column-by-column basis. The system may further include an electromagnetic actuator or solenoid and permanent magnets to facilitate movement of the striker element and the locking rollers.
    Type: Grant
    Filed: March 21, 2007
    Date of Patent: April 7, 2009
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventor: John M. Vranish
  • Patent number: 7509774
    Abstract: For an inflatable structure having a flexible outer shell or wall structure having a flexible restraint layer comprising interwoven, load-bearing straps, apparatus for integrating one or more substantially rigid members into the flexible shell. For each rigid member, a corresponding opening is formed through the flexible shell for receiving the rigid member. A plurality of connection devices are mounted on the rigid member for receiving respective ones of the load-bearing straps.
    Type: Grant
    Filed: December 13, 2006
    Date of Patent: March 31, 2009
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: Christopher J. Johnson, Ross M. Patterson, Gary R. Spexarth
  • Patent number: 7506541
    Abstract: A system and method are provided for determining the volume of a fluid in a container. Sensors are positioned at distinct locations in a container of a fluid. Each sensor is sensitive to an interface defined by the top surface of the fluid. Interfaces associated with at least three of the sensors are determined and used to find the volume of the fluid in the container in a geometric process.
    Type: Grant
    Filed: January 9, 2006
    Date of Patent: March 24, 2009
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: Stanley E. Woodard, Bryant D. Taylor
  • Patent number: 7389675
    Abstract: A miniaturized Schottky diode hydrogen and hydrocarbon sensor and the method of making same is disclosed and claimed. The sensor comprises a catalytic metal layer, such as palladium, a silicon carbide substrate layer and a thin barrier layer in between the catalytic and substrate layers made of palladium oxide (PdOx). This highly stable device provides sensitive gas detection at temperatures ranging from at least 450 to 600° C. The barrier layer prevents reactions between the catalytic metal layer and the substrate layer. Conventional semiconductor fabrication techniques are used to fabricate the small-sized sensors. The use of a thicker palladium oxide barrier layer for other semiconductor structures such as a capacitor and transistor structures is also disclosed.
    Type: Grant
    Filed: May 12, 2006
    Date of Patent: June 24, 2008
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: Gary W. Hunter, Jennifer C. Xu, Dorothy Lukco
  • Patent number: 7040319
    Abstract: Method and apparatus are disclosed for monitoring an oxygen partial pressure in an air mask and providing a tactile warning to the user. The oxygen partial pressure in the air mask is detected using an electrochemical sensor, the output signal from which is provided to a comparator. The comparator compares the output signal with a preset reference value or range of values representing acceptable oxygen partial pressures. If the output signal is different than the reference value or outside the range of values, the air mask is vibrated by a vibrating motor to alert the user to a potentially hypoxic condition.
    Type: Grant
    Filed: February 22, 2002
    Date of Patent: May 9, 2006
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: Mark E. Kelly, Donald R. Pettit
  • Patent number: 6997637
    Abstract: Roadway barrier system and method are disclosed for decelerating a moving vehicle in a controlled manner and for retaining the decelerated vehicle. A net or mesh of the roadway barrier system receives and captures the moving vehicle. The net or mesh is secured to anchors by energy absorbing straps. The energy absorbing straps deploy under a tensional load to decelerate the moving vehicle, the straps providing a controlled resistance to the tensional load over a predefined displacement or stroke to bring the moving vehicle to rest. Additional features include a sacrificial panel or sheet in front of the net that holds up the net or mesh while deflecting vehicles that collide only tangentially with the roadway barrier system.
    Type: Grant
    Filed: December 4, 2001
    Date of Patent: February 14, 2006
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: William C. Schneider, P. James Locke
  • Patent number: 6903685
    Abstract: System and methods are disclosed for passively determining the location of a moveable transmitter utilizing a pair of phase shifts at a receiver for extracting a direction vector from a receiver to the transmitter. In a preferred embodiment, a phase difference between the transmitter and receiver is extracted utilizing a noncoherent demodulator in the receiver. The receiver includes antenna array with three antenna elements, which preferably are patch antenna elements aced apart by one-half wavelength. Three receiver channels are preferably utilized for simultaneously processing the received signal from each of the three antenna elements. Multipath transmission paths for each of the three receiver channels are indexed so that comparisons of the same multipath component are made for each of the three receiver channels. The phase difference for each received signal is determined by comparing only the magnitudes of received and stored modulation signals to determine a winning modulation symbol.
    Type: Grant
    Filed: July 1, 2003
    Date of Patent: June 7, 2005
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: G. Dickey Arndt, Phong H. Ngo, Henry A. Chen, Chau T. Phan, Brian A. Bourgeois, John Dusl, Brent W. Hill
  • Patent number: 6866098
    Abstract: System and methods for transmitting and receiving electromagnetic pulses through a geological formation. A preferably programmable transmitter having an all-digital portion in a preferred embodiment may be operated at frequencies below 1 MHz without loss of target resolution by transmitting and over sampling received long PN codes. A gated and stored portion of the received signal may be correlated with the PN code to determine distances of interfaces within the geological formation, such as the distance of a water interfaces from a wellbore. The received signal is oversampled preferably at rates such as five to fifty times as high as a carrier frequency. In one method of the invention, an oil well with multiple production zones may be kept in production by detecting an approaching water front in one of the production zones and shutting down that particular production zone thereby permitting the remaining production zones to continue operating.
    Type: Grant
    Filed: October 30, 2002
    Date of Patent: March 15, 2005
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: G. Dickey Arndt, James R. Carl, Kent A. Byerly, B. Jon Amini
  • Patent number: 6818259
    Abstract: Porous organic articles having no surface functionality may be treated by remote plasma discharge to thereby introduce functionality to the surface of the article. The functionality is introduced throughout the article's surface, including the exterior surface and the surfaces of the pores. Little or no degradation of the porous organic article occurs as a result of the functionalization. Amino, hydroxyl, carbonyl and carboxyl groups may be introduced to the article. In this way, an essentially inert hydrophobic porous article, made from, for example, polyethylene, can have its surface modified so that the surface becomes hydrophilic. The remote plasma discharge process causes essentially no change in the bulk properties of the organic article. The remote plasma discharge process is preferably conducted so that no photons, and particularly no ultraviolet radiation, is transmitted from the plasma glow to the porous article.
    Type: Grant
    Filed: November 23, 1998
    Date of Patent: November 16, 2004
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventor: Steven L. Koontz
  • Patent number: 6802444
    Abstract: A method for treating alloy before and after friction stir welding, the method comprising the following steps. First solution heat treating a multiplicity of aluminum-zinc alloy engineered components for a first time period at a first temperature. First air cooling the components in ambient air at room temperature until the components are cooled to room temperature. Friction stir welding the components to form an assembly. Second solution heat treating the assembly for a second time period at a second temperature. Additional steps and embodiments are considered.
    Type: Grant
    Filed: March 17, 2003
    Date of Patent: October 12, 2004
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: George E. Petter, John D. Figert, Daniel J. Rybicki, Timothy H. Burns
  • Patent number: 6734603
    Abstract: A method for forming ferroelectric wafers is provided. A prestress layer is placed on the desired mold. A ferroelectric wafer is placed on top of the prestress layer. The layers are heated and then cooled, causing the ferroelectric wafer to become prestressed. The prestress layer may include reinforcing material and the ferroelectric wafer may include electrodes or electrode layers may be placed on either side of the ferroelectric layer. Wafers produced using this method have greatly improved output motion.
    Type: Grant
    Filed: January 24, 1997
    Date of Patent: May 11, 2004
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: Richard F. Hellbaum, Robert G. Bryant, Robert L. Fox, Antony Jalink, Jr., Wayne W. Rohrbach, Joycelyn O. Simpson
  • Patent number: 6718196
    Abstract: A system with multimodality instrument for tissue identification includes a computer-controlled motor driven heuristic probe with a multisensory tip. For neurosurgical applications, the instrument is mounted on a stereotactic frame for the probe to penetrate the brain in a precisely controlled fashion. The resistance of the brain tissue being penetrated is continually monitored by a miniaturized strain gauge attached to the probe tip. Other modality sensors may be mounted near the probe tip to provide real-time tissue characterizations and the ability to detect the proximity of blood vessels, thus eliminating errors normally associated with registration of pre-operative scans, tissue swelling, elastic tissue deformation, human judgement, etc., and rendering surgical procedures safer, more accurate, and efficient. A neural network program adaptively learns the information on resistance and other characteristic features of normal brain tissue during the surgery and provides near real-time modeling.
    Type: Grant
    Filed: August 28, 2000
    Date of Patent: April 6, 2004
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: Robert W. Mah, Russell J. Andrews
  • Patent number: 6680797
    Abstract: A polarization-independent optical switch is disclosed for switching at least one incoming beam from at least one input source to at least one output drain.
    Type: Grant
    Filed: June 21, 2001
    Date of Patent: January 20, 2004
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventor: Richard D. Juday
  • Patent number: 6676964
    Abstract: Microcapsules prepared by encapsulating an aqueous solution of a protein, drug or other bioactive substance inside a semi-permeable membrane by are disclosed. The microcapsules are formed by interfacial coacervation under conditions where the shear forces are limited to 0-100 dynes/cm2 at the interface. By placing the microcapsules in a high osmotic dewatering solution, the protein solution is gradually made saturated and then supersaturated, and the controlled nucleation and crystallization of the protein is achieved. The crystal-filled microcapsules prepared by this method can be conveniently harvested and stored while keeping the encapsulated crystals in essentially pristine condition due to the rugged, protective membrane. Because the membrane components themselves are x-ray transparent, large crystal-containing microcapsules can be individually selected, mounted in x-ray capillary tubes and subjected to high energy x-ray diffraction studies to determine the 3-D structure of the protein molecules.
    Type: Grant
    Filed: January 26, 2001
    Date of Patent: January 13, 2004
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: Dennis R. Morrison, Benjamin Mosier
  • Patent number: 6592687
    Abstract: A cast article from an aluminum alloy, which has improved mechanical properties at elevated temperatures, has the following composition in weight percent: Silicon 14-25.0, Copper 5.5-8.0, Iron 0.05-1.2, Magnesium 0.5-1.5, Nickel 0.05-0.9, Manganese 0.05-1.0, Titanium 0.05-1.2, Zirconium 0.05-1.2, Vanadium 0.05-1.2, Zinc 0.05-0.9, Phosphorus 0.001-0.1, and the balance is Aluminum, wherein the silicon-to-magnesium ratio is 10-25, and the copper-to-magnesium ratio is 4-15. The aluminum alloy contains a simultaneous dispersion of three types of Al3X compound particles (X═Ti, V, Zr) having a L12 crystal structure, and their lattice parameters are coherent to the aluminum matrix lattice. A process for producing this cast article is also disclosed, as well as a metal matrix composite, which includes the aluminum alloy serving as a matrix and containing up to about 60% by volume of a secondary filler material.
    Type: Grant
    Filed: July 11, 2002
    Date of Patent: July 15, 2003
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: Jonathan A. Lee, Po-Shou Chen
  • Patent number: 6578851
    Abstract: A pair of substantially opposed mating surfaces are joined to each other and sealed in place by means of an electrically-conductive member which is placed in proximity to the mating surfaces. The electrically-conductive member has at least one element secured thereto which is positioned to contact the mating surfaces, and which softens when the electrically-conductive member is heated by passing an electric current therethrough. The softened element conforms to the mating surfaces, and upon cooling of the softened element the mating surfaces are joined together in an effective seal. Of particular significance is an embodiment of the electrically-conductive member which is a gasket having an electrically-conductive gasket base and a pair of the elements secured to opposite sides of the gasket base. This embodiment is positioned between the opposed mating surfaces to be joined to each other.
    Type: Grant
    Filed: October 16, 2000
    Date of Patent: June 17, 2003
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventor: Melvin A. Bryant, III
  • Patent number: 6513730
    Abstract: A nozzle body and assembly for delivering atomized fuel to a combustion chamber. The nozzle body is rotatably mounted onto a substrate. One or more curvilinear fuel delivery channels are in flow communication with an internal fuel distribution cavity formed in the nozzle body. Passage of pressurized fuel through the nozzle body causes the nozzle body to rotate. Components of the nozzle assembly are formed of silicon carbide having surfaces etched by deep reactive ion etching utilizing MEMS technology. A fuel premix chamber is carried on the substrate in flow communication with a supply passage in the nozzle body.
    Type: Grant
    Filed: March 21, 2001
    Date of Patent: February 4, 2003
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventor: Robert S. Okojie
  • Patent number: 6487866
    Abstract: A multi-purpose thermal insulation test apparatus is used for testing insulation materials, or other components. The test apparatus is a fluid boil-off calorimeter system for calibrated measurement of the apparent thermal conductivity (k-value) of a specimen material at a fixed vacuum level. The apparatus includes an inner vessel for receiving a fluid with a normal boiling point below ambient temperature, such as liquid nitrogen, enclosed within a vacuum chamber. A cold mass assembly, including the inner vessel and thermal guards, is suspended from the top of the vacuum chamber. Handling tools attach to the cold mass assembly for convenient manipulation of the assembly and for the installation or wrapping of insulation test materials. Liquid nitrogen is typically supplied to the inner vessel using a fill tube with funnel. A single port through the top of the vacuum chamber facilitates both filling and venting.
    Type: Grant
    Filed: July 9, 2001
    Date of Patent: December 3, 2002
    Assignee: The United States of America as represented by the National Aeronautics & Space Administration
    Inventors: James E. Fesmire, Stanislaw D. Augustynowicz
  • Patent number: 6361961
    Abstract: A method and apparatus for sensing gravity using an NADH oxidase of the plasma membrane which has been found to respond to unit gravity and low centrifugal g forces. The oxidation rate of NADH supplied to the NADH oxidase is measured and translated to represent the relative gravitational force exerted on the protein. The NADH oxidase of the plasma membrane may be obtained from plant or animal sources or may be produced recombinantly.
    Type: Grant
    Filed: April 25, 2000
    Date of Patent: March 26, 2002
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventor: D. James Morre′
  • Patent number: 6311107
    Abstract: The present invention is a two-part wind advisory system comprising a ground station at an airfield and an airborne unit placed inside an aircraft. The ground station monitors wind conditions (wind speed, wind direction, and wind gust) at the airfield and transmits the wind conditions and an airfield ID to the airborne unit. The airborne unit identifies the airfield by comparing the received airfield ID with airfield IDs stored in a database. The airborne unit also calculates the headwind and crosswind for each runway in both directions at the airfield using the received wind conditions and runway information stored in the database. The airborne unit then determines a recommended runway for takeoff and landing operations of the aircraft based on the runway having the greatest headwind value and displays the airfield ID, wind conditions, and recommended runway to the pilot.
    Type: Grant
    Filed: June 23, 2000
    Date of Patent: October 30, 2001
    Assignee: The United States of America as represented by the National Aeronautics and Space Administration
    Inventors: Paul A. Curto, Gerald E. Brown, Jan A. Zysko