Patents Assigned to and Space Administration
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Patent number: 8518291Abstract: 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: GrantFiled: July 24, 2012Date of Patent: August 27, 2013Assignees: Case Western Reserve University, The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Alp Sehirlioglu, Ali Sayir, Fred Dynys
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Patent number: 8511964Abstract: 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: GrantFiled: September 22, 2009Date of Patent: August 20, 2013Assignees: GM Global Technology Operations LLC, The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: 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
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Patent number: 8511396Abstract: 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: GrantFiled: May 20, 2002Date of Patent: August 20, 2013Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Clyde F. Parrish
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Patent number: 8508413Abstract: 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: GrantFiled: April 8, 2011Date of Patent: August 13, 2013Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Kenneth L. Dudley, Holly A. Elliott, Robin L. Cravey, John W. Connell, Sayata Ghose, Kent A. Watson, Joseph G. Smith, Jr.
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Patent number: 8499779Abstract: 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: GrantFiled: January 16, 2008Date of Patent: August 6, 2013Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space AdministrationInventor: Rebecca A. Gillespie
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Patent number: 8502987Abstract: 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 tType: GrantFiled: February 1, 2011Date of Patent: August 6, 2013Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Russell A. Chipman, Brian J. Daugherty, Stephen C. McClain, Steven A. Macenka
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Publication number: 20130193704Abstract: 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: ApplicationFiled: March 14, 2013Publication date: August 1, 2013Applicants: 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
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Patent number: 8498741Abstract: 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: GrantFiled: September 22, 2009Date of Patent: July 30, 2013Assignees: GM Global Technology Operations, The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Chris A. Ihrke, Lyndon Bridgwater, David M. Reich, Charles W. Wampler, II, Scott R. Askew, Myron A. Diftler, Vienny Nguyen
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Patent number: 8498756Abstract: 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: GrantFiled: August 18, 2011Date of Patent: July 30, 2013Assignee: The United States of America as Represented by the Adminstrator of the National Aeronautics & Space Administration (NASA)Inventor: George L. Sarver
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Patent number: 8492160Abstract: 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: GrantFiled: March 9, 2010Date of Patent: July 23, 2013Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Lawrence A. Wade, Charles Patrick Collier
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Patent number: 8490463Abstract: 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: GrantFiled: September 14, 2010Date of Patent: July 23, 2013Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William T. Yost, Daniel F. Perey, K. Elliott Cramer
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Patent number: 8490470Abstract: 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: GrantFiled: September 29, 2009Date of Patent: July 23, 2013Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William Kaukler, Edwin C. Ethridge
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Patent number: 8494687Abstract: 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: GrantFiled: June 22, 2011Date of Patent: July 23, 2013Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Michael D. Vanek, Farzin Amzajerdian, Alexander Bulyshev
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Patent number: 8494782Abstract: 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: GrantFiled: April 21, 2011Date of Patent: July 23, 2013Assignee: The United States of America as Represented by the Administrator of the National Aeronautics & Space Administration (NASA)Inventors: Viktor Stolc, Matthew W Brock
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Patent number: 8489181Abstract: 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: GrantFiled: January 2, 2009Date of Patent: July 16, 2013Assignee: 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
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Patent number: 8484980Abstract: 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: GrantFiled: September 30, 2010Date of Patent: July 16, 2013Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Charles J Trefny, Vance F Dippold
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Patent number: 8489239Abstract: 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: GrantFiled: November 1, 2010Date of Patent: July 16, 2013Assignees: GM Global Technology Operations LLC, The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Muhammad E Abdallah, Robert J. Platt, Jr., Matthew J Reiland, Brian Hargrave, Myron A Diftler, Philip A Strawser, Chris A. Ihrke
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Patent number: 8484509Abstract: 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: GrantFiled: August 11, 2010Date of Patent: July 9, 2013Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space AdministrationInventors: Daniel C. Espinosa, Alessandro Geist, David J. Petrick, Thomas P. Flatley, Jeffrey C. Hosler, Gary A. Crum, Manuel Buenfil
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Patent number: 8480826Abstract: 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: GrantFiled: April 18, 2007Date of Patent: July 9, 2013Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space AdministrationInventors: Kenneth N. Segal, James M. Lohr, Russell Rowles, Wanda Peters, Robert Kiwak
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Patent number: 8483877Abstract: 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: GrantFiled: September 3, 2010Date of Patent: July 9, 2013Assignees: GM Global Technology Operations LLC, The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Muhammad E. Abdallah, Brian Hargrave, John D. Yamokoski, Philip A. Strawser