Patents Assigned to and Space Administration
  • Patent number: 8518291
    Abstract: Piezoelectric ceramics that can be used in high temperature actuators. The piezoelectric ceramics have various desirable properties, for example the materials do not depole up to about 400° C. and have large piezoelectric coefficients >400 pm/V. In addition the thickness mode electromechanical coupling coefficient is large, increasing from 0.5 to 0.65 with temperature. The planar electromechanical coefficient is around 0.40 and does not show a significant dependence on temperature. These materials are highly polarizable with remnant polarization around 50 ?C/cm2 and are electrically hard with coercive field above 20 kV/cm. They exhibit single crystal like ferroelectric behavior with square hysteresis loops. Such properties make these materials a piezoelectric ceramic that can be used in stack actuators at high temperatures. Methods for preparing the piezoelectric ceramics are also disclosed.
    Type: Grant
    Filed: July 24, 2012
    Date of Patent: August 27, 2013
    Assignees: Case Western Reserve University, The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Alp Sehirlioglu, Ali Sayir, Fred Dynys
  • Patent number: 8511964
    Abstract: A humanoid robot includes a torso, a pair of arms, two hands, a neck, and a head. The torso extends along a primary axis and presents a pair of shoulders. The pair of arms movably extend from a respective one of the pair of shoulders. Each of the arms has a plurality of arm joints. The neck movably extends from the torso along the primary axis. The neck has at least one neck joint. The head movably extends from the neck along the primary axis. The head has at least one head joint. The shoulders are canted toward one another at a shrug angle that is defined between each of the shoulders such that a workspace is defined between the shoulders.
    Type: Grant
    Filed: September 22, 2009
    Date of Patent: August 20, 2013
    Assignees: GM Global Technology Operations LLC, The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Douglas Martin Linn, Robert O. Ambrose, Myron A. Diftler, Scott R. Askew, Robert Platt, Joshua S. Mehling, Nicolaus A. Radford, Phillip A. Strawser, Lyndon Bridgwater, Charles W. Wampler, II, Muhammad E. Abdallah, Chris A. Ihrke, Matthew J. Reiland, Adam M. Sanders, David M. Reich, Brian Hargrave, Adam H. Parsons, Frank Noble Permenter, Donald R. Davis
  • Patent number: 8511396
    Abstract: Aqueous droplets encapsulated in a flame retardant polymer are useful in suppressing combustion. Upon exposure to a flame, the encapsulated aqueous droplets rupture and vaporize, removing heat and displacing oxygen to retard the combustion process. The polymer encapsulant, through decomposition, may further add free radicals to the combustion atmosphere, thereby further retarding the combustion process. The encapsulated aqueous droplets may be used as a replacement to halon, water mist and dry powder flame suppression systems.
    Type: Grant
    Filed: May 20, 2002
    Date of Patent: August 20, 2013
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Clyde F. Parrish
  • Patent number: 8508413
    Abstract: An antenna includes a ground plane, a dielectric disposed on the ground plane, and an electrically-conductive radiator disposed on the dielectric. The dielectric includes at least one layer of a first dielectric material and a second dielectric material that collectively define a dielectric geometric pattern, which may comprise a fractal geometry. The radiator defines a radiator geometric pattern, and the dielectric geometric pattern is geometrically identical, or substantially geometrically identical, to the radiator geometric pattern.
    Type: Grant
    Filed: April 8, 2011
    Date of Patent: August 13, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Kenneth L. Dudley, Holly A. Elliott, Robin L. Cravey, John W. Connell, Sayata Ghose, Kent A. Watson, Joseph G. Smith, Jr.
  • Patent number: 8499779
    Abstract: Systems, methods and apparatus are provided through which in some embodiments a non-pyrotechnic valve includes an inlet piece, an actuator comprising a shape-memory metal, and an outlet attached to the inlet piece. In some examples, the shape-memory metal includes Nitinol.
    Type: Grant
    Filed: January 16, 2008
    Date of Patent: August 6, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space Administration
    Inventor: Rebecca A. Gillespie
  • Patent number: 8502987
    Abstract: Disclosed herein is a method of determining the near angle scattering of a sample reflective surface comprising the steps of: a) splitting a beam of light having a coherence length of greater than or equal to about 2 meters into a sample beam and a reference beam; b) frequency shifting both the sample beam and the reference beam to produce a fixed beat frequency between the sample beam and the reference beam; c) directing the sample beam through a focusing lens and onto the sample reflective surface, d) reflecting the sample beam from the sample reflective surface through a detection restriction disposed on a movable stage; e) recombining the sample beam with the reference beam to form a recombined beam, followed by f) directing the recombined beam to a detector and performing heterodyne analysis on the recombined beam to measure the near-angle scattering of the sample reflective surface, wherein the position of the detection restriction relative to the sample beam is varied to occlude at least a portion of t
    Type: Grant
    Filed: February 1, 2011
    Date of Patent: August 6, 2013
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Russell A. Chipman, Brian J. Daugherty, Stephen C. McClain, Steven A. Macenka
  • Publication number: 20130193704
    Abstract: A robotic hand includes a finger with first, second, and third phalanges. A first joint rotatably connects the first phalange to a base structure. A second joint rotatably connects the first phalange to the second phalange. A third joint rotatably connects the third phalange to the second phalange. The second joint and the third joint are kinematically linked such that the position of the third phalange with respect to the second phalange is determined by the position of the second phalange with respect to the first phalange.
    Type: Application
    Filed: March 14, 2013
    Publication date: August 1, 2013
    Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS, INC.
    Inventors: GM GLOBAL TECHNOLOGY OPERATIONS, INC., The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration
  • Patent number: 8498741
    Abstract: A humanoid robot includes a torso, a pair of arms, a neck, a head, a wrist joint assembly, and a control system. The arms and the neck movably extend from the torso. Each of the arms includes a lower arm and a hand that is rotatable relative to the lower arm. The wrist joint assembly is operatively defined between the lower arm and the hand. The wrist joint assembly includes a yaw axis and a pitch axis. The pitch axis is disposed in a spaced relationship to the yaw axis such that the axes are generally perpendicular. The pitch axis extends between the yaw axis and the lower arm. The hand is rotatable relative to the lower arm about each of the yaw axis and the pitch axis. The control system is configured for determining a yaw angle and a pitch angle of the wrist joint assembly.
    Type: Grant
    Filed: September 22, 2009
    Date of Patent: July 30, 2013
    Assignees: GM Global Technology Operations, The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Chris A. Ihrke, Lyndon Bridgwater, David M. Reich, Charles W. Wampler, II, Scott R. Askew, Myron A. Diftler, Vienny Nguyen
  • Patent number: 8498756
    Abstract: A reusable space flight launch system is configured to eliminate complex descent and landing systems from the space flight hardware and move them to maneuverable ground based systems. Precision landing of the reusable space flight hardware is enabled using a simple, light weight aerodynamic device on board the flight hardware such as a parachute, and one or more translating ground based vehicles such as a hovercraft that include active speed, orientation and directional control. The ground based vehicle maneuvers itself into position beneath the descending flight hardware, matching its speed and direction and captures the flight hardware. The ground based vehicle will contain propulsion, command and GN&C functionality as well as space flight hardware landing cushioning and retaining hardware. The ground based vehicle propulsion system enables longitudinal and transverse maneuverability independent of its physical heading.
    Type: Grant
    Filed: August 18, 2011
    Date of Patent: July 30, 2013
    Assignee: The United States of America as Represented by the Adminstrator of the National Aeronautics & Space Administration (NASA)
    Inventor: George L. Sarver
  • Patent number: 8492160
    Abstract: The invention is a device including array of aciive regions for use in reacting one or more species in at least two of the active regions in a sequential process, e.g., sequential reactions. The device has a transparent substrate member, which has a surface region and a silane material overlying the surface region. A first active region overlies a first portion of the silane material. The first region has a first dimension of less than 1 micron in size and has first molecules capable of binding to the first portion of the silane material. A second active region overlies a second portion of the silane material. The second region has a second dimension of less than 1 micron in size, second molecules capable of binding to the second portion of the active region, and a spatial distance separates the first active region and the second active region.
    Type: Grant
    Filed: March 9, 2010
    Date of Patent: July 23, 2013
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Lawrence A. Wade, Charles Patrick Collier
  • Patent number: 8490463
    Abstract: A method is provided for calibrating ultrasonic signals passed through a crimp formed with respect to a deformable body via an ultrasonically-equipped crimp tool (UECT). The UECT verifies a crimp quality using the ultrasonic signals. The method includes forming the crimp, transmitting a first signal, e.g., a pulse, to a first transducer of the UECT, and converting the first signal, using the first transducer, into a second signal which defines an ultrasonic pulse. This pulse is transmitted through the UECT into the crimp. A second transducer converts the second signal into a third signal, which may be further conditioned, and the ultrasonic signals are calibrated using the third signal or its conditioned variant. An apparatus for calibrating the ultrasonic signals includes a pulse module (PM) electrically connected to the first and second transducers, and an oscilloscope or display electrically connected to the PM for analyzing an electrical output signal therefrom.
    Type: Grant
    Filed: September 14, 2010
    Date of Patent: July 23, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William T. Yost, Daniel F. Perey, K. Elliott Cramer
  • Patent number: 8490470
    Abstract: A parallel-plate system collects data used to determine viscosity. A first plate is coupled to a translator so that the first plate can be moved along a first direction. A second plate has a pendulum device coupled thereto such that the second plate is suspended above and parallel to the first plate. The pendulum device constrains movement of the second plate to a second direction that is aligned with the first direction and is substantially parallel thereto. A force measuring device is coupled to the second plate for measuring force along the second direction caused by movement of the second plate.
    Type: Grant
    Filed: September 29, 2009
    Date of Patent: July 23, 2013
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William Kaukler, Edwin C. Ethridge
  • Patent number: 8494687
    Abstract: A method for enhancing a three dimensional image from frames of flash LIDAR data includes generating a first distance Ri from a first detector i to a first point on a surface Si. After defining a map with a mesh ? having cells k, a first array S(k), a second array M(k), and a third array D(k) are initialized. The first array corresponds to the surface, the second array corresponds to the elevation map, and the third array D(k) receives an output for the DEM. The surface is projected onto the mesh ?, so that a second distance Rk from a second point on the mesh ? to the detector can be found. From this, a height may be calculated, which permits the generation of a digital elevation map. Also, using sequential frames of flash LIDAR data, vehicle control is possible using an offset between successive frames.
    Type: Grant
    Filed: June 22, 2011
    Date of Patent: July 23, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Michael D. Vanek, Farzin Amzajerdian, Alexander Bulyshev
  • Patent number: 8494782
    Abstract: Method and system for rapid and accurate determination of each of a sequence of unknown polymer components, such as nucleic acid components. A self-assembling monolayer of a selected substance is optionally provided on an interior surface of a pipette tip, and the interior surface is immersed in a selected liquid. A selected electrical field is impressed in a longitudinal direction, or in a transverse direction, in the tip region, a polymer sequence is passed through the tip region, and a change in an electrical current signal is measured as each polymer component passes through the tip region. Each of the measured changes in electrical current signals is compared with a database of reference electrical change signals, with each reference signal corresponding to an identified polymer component, to identify the unknown polymer component with a reference polymer component.
    Type: Grant
    Filed: April 21, 2011
    Date of Patent: July 23, 2013
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics & Space Administration (NASA)
    Inventors: Viktor Stolc, Matthew W Brock
  • Patent number: 8489181
    Abstract: A method and associated system for use of statistical parameters based on peak amplitudes and/or time interval lengths and/or depolarization-repolarization vector angles and/or depolarization-repolarization vector lengths for PQRST electrical signals associated with heart waves, to identify a person. The statistical parameters, estimated to be at least 192, serve as biometric indicia, to authenticate, or to decline to authenticate, an asserted identity of a candidate person.
    Type: Grant
    Filed: January 2, 2009
    Date of Patent: July 16, 2013
    Assignee: The United States of America as Represented by the Administrator of the National Aeronautics & Space Administration (NASA)
    Inventors: John F. Schipper, Sorin V. Dusan, Charles C. Jorgensen, Eugene Belousof
  • Patent number: 8484980
    Abstract: A new dual-mode ramjet combustor used for operation over a wide flight Mach number range is described. Subsonic combustion mode is usable to lower flight Mach numbers than current dual-mode scramjets. High speed mode is characterized by supersonic combustion in a free-jet that traverses the subsonic combustion chamber to a variable nozzle throat. Although a variable combustor exit aperture is required, the need for fuel staging to accommodate the combustion process is eliminated. Local heating from shock-boundary-layer interactions on combustor walls is also eliminated.
    Type: Grant
    Filed: September 30, 2010
    Date of Patent: July 16, 2013
    Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Charles J Trefny, Vance F Dippold
  • Patent number: 8489239
    Abstract: A robotic system includes a tendon-driven finger and a control system. The system controls the finger via a force-based control law when a tension sensor is available, and via a position-based control law when a sensor is not available. Multiple tendons may each have a corresponding sensor. The system selectively injects a compliance value into the position-based control law when only some sensors are available. A control system includes a host machine and a non-transitory computer-readable medium having a control process, which is executed by the host machine to control the finger via the force- or position-based control law. A method for controlling the finger includes determining the availability of a tension sensor(s), and selectively controlling the finger, using the control system, via the force or position-based control law. The position control law allows the control system to resist disturbances while nominally maintaining the initial state of internal tendon tensions.
    Type: Grant
    Filed: November 1, 2010
    Date of Patent: July 16, 2013
    Assignees: GM Global Technology Operations LLC, The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Muhammad E Abdallah, Robert J. Platt, Jr., Matthew J Reiland, Brian Hargrave, Myron A Diftler, Philip A Strawser, Chris A. Ihrke
  • Patent number: 8484509
    Abstract: A processing system including an FPGA having a dual port RAM and for use in hostile environments. The FPGA includes three portions: a C&DH portion; a first scratch pad portion receiving a first set of data, processing the first set of data, and outputting a first set of processed data to a first location of the RAM; and a second scratch pad portion receiving a second set of data identical to the first set of data, processing the second set of data in the same way that the first set of data is processed, and outputting a second set of processed data to a second location of the RAM. The C&DH portion compares the first set of processed data to the second set of processed data and, if the first set of processed data is the same as the second set of processed data, outputs one set of processed data.
    Type: Grant
    Filed: August 11, 2010
    Date of Patent: July 9, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space Administration
    Inventors: Daniel C. Espinosa, Alessandro Geist, David J. Petrick, Thomas P. Flatley, Jeffrey C. Hosler, Gary A. Crum, Manuel Buenfil
  • Patent number: 8480826
    Abstract: Disclosed herein is a method for bonding dissimilar materials using an elastic adhesive to permit the bond to withstand variations in temperature and pressure. The use of elastic adhesive accommodates previous problems associated with large differences in thermal expansion coefficient between dissimilar materials, and provides a thermally and chemically stable materials combination that withstands large thermal shock loads, such as may be experienced in a space environment. Also disclosed herein is a method for attaching a coating to a structure. In particular applications, the coating may be (1) specular (greater than 98% specularity); or (2) RF reflective for use in applications including but not limited to high frequency satellite communications.
    Type: Grant
    Filed: April 18, 2007
    Date of Patent: July 9, 2013
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space Administration
    Inventors: Kenneth N. Segal, James M. Lohr, Russell Rowles, Wanda Peters, Robert Kiwak
  • Patent number: 8483877
    Abstract: A method of controlling a robotic manipulator of a force- or impedance-controlled robot within an unstructured workspace includes imposing a saturation limit on a static force applied by the manipulator to its surrounding environment, and may include determining a contact force between the manipulator and an object in the unstructured workspace, and executing a dynamic reflex when the contact force exceeds a threshold to thereby alleviate an inertial impulse not addressed by the saturation limited static force. The method may include calculating a required reflex torque to be imparted by a joint actuator to a robotic joint. A robotic system includes a robotic manipulator having an unstructured workspace and a controller that is electrically connected to the manipulator, and which controls the manipulator using force- or impedance-based commands. The controller, which is also disclosed herein, automatically imposes the saturation limit and may execute the dynamic reflex noted above.
    Type: Grant
    Filed: September 3, 2010
    Date of Patent: July 9, 2013
    Assignees: GM Global Technology Operations LLC, The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Muhammad E. Abdallah, Brian Hargrave, John D. Yamokoski, Philip A. Strawser