Patents Assigned to THE U.S.A. AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
  • Publication number: 20120192407
    Abstract: A process and apparatus for collecting data for nondestructive evaluation of the quality of a crimped wire connector are provided. The process involves providing a crimping tool having an anvil and opposing jaw for crimping a terminal onto a stranded wire, moving the jaw relative to the anvil to close the distance between the jaw and the anvil and thereby compress the terminal against the wire, while transmitting ultrasonic waves that are propagated through the terminal-wire combination and received at a receiving ultrasonic transducer as the jaw is moved relative to the anvil, and detecting and recording the position of the jaw relative to the anvil as a function of time and detecting and recording the amplitude of the ultrasonic wave that is received at the receiving ultrasonic transducer as a function of time as the jaw is moved relative to the anvil.
    Type: Application
    Filed: February 1, 2012
    Publication date: August 2, 2012
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William T. Yost, Karl E. Cramer, Daniel F. Perey, Keith A. Williams
  • Publication number: 20120194120
    Abstract: A tendon tensioning system includes a tendon having a proximal end and a distal end, an actuator, and a motor controller. The actuator may include a drive screw and a motor, and may be coupled with the proximal end of the tendon and configured to apply a tension through the tendon in response to an electrical current. The motor controller may be electrically coupled with the actuator, and configured to provide an electrical current having a first amplitude to the actuator until a stall tension is achieved through the tendon; provide a pulse current to the actuator following the achievement of the stall tension, where the amplitude of the pulse current is greater than the first amplitude, and return the motor to a steady state holding current following the conclusion of the pulse current.
    Type: Application
    Filed: January 27, 2011
    Publication date: August 2, 2012
    Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS LLC
    Inventors: Matthew J. Reiland, Myron A. Diftler
  • Publication number: 20120177892
    Abstract: A method for manufacturing a thin film structural system including a thin film structure includes depositing a reinforcing material in a liquid form in a predefined pattern on a thin film membrane, and transforming the reinforcing material in the predefined pattern to form a reinforcing element connected to the thin film membrane. The reinforcing material may be deposited in a melted form and solidified by cooling, may be transformed by a light or laser induced chemical reaction, or may be deposited and solidified such that the reinforcing element is at least partially embedded in the thin film membrane. The predefined pattern may redistribute loads around a damaged portion of the thin film structure, or define a hinge, a folding line, a stiffening feature. The reinforcing element may be electrically, optically or thermally conductive, to communicate with a device included in the system. The system may be a space structure.
    Type: Application
    Filed: October 14, 2011
    Publication date: July 12, 2012
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Wendell Keith Belvin, David W. Sleight, John W. Connell, Thomas J. Burns, Nancy M.H. Holloway, Frank L. Palmieri, Gary A. Wainwright, Robert C. Andrews, Martin Eckhard Zander
  • Publication number: 20120175171
    Abstract: An amorphous robot includes a compartmented bladder containing fluid, a valve assembly, and an outer layer encapsulating the bladder and valve assembly. The valve assembly draws fluid from a compartment(s) and discharges the drawn fluid into a designated compartment to displace the designated compartment with respect to the surface. Another embodiment includes elements each having a variable property, an outer layer that encapsulates the elements, and a control unit. The control unit energizes a designated element to change its variable property, thereby moving the designated element. The elements may be electromagnetic spheres with a variable polarity or shape memory polymers with changing shape and/or size. Yet another embodiment includes an elongated flexible tube filled with ferrofluid, a moveable electromagnet, an actuator, and a control unit. The control unit energizes the electromagnet and moves the electromagnet via the actuator to magnetize the ferrofluid and lengthen the flexible tube.
    Type: Application
    Filed: January 3, 2012
    Publication date: July 12, 2012
    Applicant: U.S.A as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Arthur T. Bradley
  • Publication number: 20120107594
    Abstract: Disclosed is a single wall carbon nanotube (SWCNT) film electrode (FE), all-organic electroactive device systems fabricated with the SWNT-FE, and methods for making same. The SWCNT can be replaced by other types of nanotubes. The SWCNT film can be obtained by filtering SWCNT solution onto the surface of an anodized alumina membrane. A freestanding flexible SWCNT film can be collected by breaking up this brittle membrane. The conductivity of this SWCNT film can advantageously be higher than 280 S/cm. An electroactive polymer (EAP) actuator layered with the SWNT-FE shows a higher electric field-induced strain than an EAP layered with metal electrodes because the flexible SWNT-FE relieves the restraint of the displacement of the polymeric active layer as compared to the metal electrode. In addition, if thin enough, the SWNT-FE is transparent in the visible light range, thus making it suitable for use in actuators used in optical devices.
    Type: Application
    Filed: October 28, 2011
    Publication date: May 3, 2012
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Jin Ho Kang, Cheol Park, Joycelyn S. Harrison
  • Publication number: 20120109379
    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: Application
    Filed: November 1, 2010
    Publication date: May 3, 2012
    Applicants: The U.S.A. As Represented by the Administrator of The National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS, INC.
    Inventors: Muhammad E. Abdallah, Robert J. Platt, JR., Matthew J. Reiland, Brian Hargrave, Myron A. Diftler, Philip A. Strawser, Chris A. Ihrke
  • Publication number: 20120097791
    Abstract: A slat cove filler is utilized to reduce airframe noise resulting from deployment of a leading edge slat of an aircraft wing. The slat cove filler is preferably made of a super elastic shape memory alloy, and the slat cove filler shifts between stowed and deployed shapes as the slat is deployed. The slat cove filler may be configured such that a separate powered actuator is not required to change the shape of the slat cove filler from its deployed shape to its stowed shape and vice-versa. The outer contour of the slat cove filler preferably follows a profile designed to maintain accelerating flow in the gap between the slat cove filler and wing leading edge to provide for noise reduction.
    Type: Application
    Filed: October 20, 2011
    Publication date: April 26, 2012
    Applicant: U.S.A as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Travis L. Turner, Reggie T. Kidd, David P. Lockard, Mehdi R. Khorrami, Craig L. Streett, Douglas Leo Weber
  • Publication number: 20120068011
    Abstract: An active pylon noise control system for an aircraft includes a pylon structure connecting an engine system with an airframe surface of the aircraft and having at least one aperture to supply a gas or fluid therethrough, an intake portion attached to the pylon structure to intake a gas or fluid, a regulator connected with the intake portion via a plurality of pipes, to regulate a pressure of the gas or fluid, a plenum chamber formed within the pylon structure and connected with the regulator, and configured to receive the gas or fluid as regulated by the regulator, and a plurality of injectors in communication with the plenum chamber to actively inject the gas or fluid through the plurality of apertures of the pylon structure.
    Type: Application
    Filed: August 22, 2011
    Publication date: March 22, 2012
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Russell H. Thomas, Michael J. Czech, Alaa A. Elmiliqui
  • Publication number: 20120061525
    Abstract: An aircraft system includes a wing and a trailing edge device coupled to the wing. The trailing edge device is movable relative to the wing, and includes a leading edge and a trailing edge having a center flap portion and a plurality of outer edge portions integrally combined with the center flap portion such that the center flap portion is shorter in width than that of outer edge portions.
    Type: Application
    Filed: August 22, 2011
    Publication date: March 15, 2012
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Michael J. Czech, Russell H. Thomas
  • Publication number: 20120061510
    Abstract: The aircraft exhaust engine nozzle system includes a fan nozzle to receive a fan flow from a fan disposed adjacent to an engine disposed above an airframe surface of the aircraft, a core nozzle disposed within the fan nozzle and receiving an engine core flow, and a pylon structure connected to the core nozzle and structurally attached with the airframe surface to secure the engine to the aircraft.
    Type: Application
    Filed: August 22, 2011
    Publication date: March 15, 2012
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Russell H. Thomas, Michael J. Czech, Ronen Elkoby
  • Publication number: 20120059515
    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: Application
    Filed: September 3, 2010
    Publication date: March 8, 2012
    Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS, INC.
    Inventors: Muhammad E. Abdallah, Brian Hargrave, John D. Yamokoski, Philip A. Strawser
  • Publication number: 20110317147
    Abstract: A continuous wave Light Detection and Ranging (CW LiDAR) system utilizes two or more laser frequencies and time or range shifted pseudorandom noise (PN) codes to discriminate between the laser frequencies. The performance of these codes can be improved by subtracting out the bias before processing. The CW LiDAR system may be mounted to an artificial satellite orbiting the earth, and the relative strength of the return signal for each frequency can be utilized to determine the concentration of selected gases or other substances in the atmosphere.
    Type: Application
    Filed: June 23, 2011
    Publication date: December 29, 2011
    Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Joel F. Campbell, Narasimha S. Prasad, Fenton W. Harrison, Michael A. Flood
  • Publication number: 20110300523
    Abstract: Disclosed are methods and apparatuses provided for modifying the effect of an operator controlled input device on an interactive device to encourage the self-regulation of at least one physiological activity by a person different than the operator. The interactive device comprises a display area which depicts images and apparatus for receiving at least one input from the operator controlled input device to thus peiiiiit the operator to control and interact with at least some of the depicted images. One effect modification comprises measurement of the physiological activity of a person different from the operator, while modifying the ability of the operator to control and interact with at least some of the depicted images by modifying the input from the operator controlled input device in response to changes in the measured physiological signal.
    Type: Application
    Filed: June 22, 2011
    Publication date: December 8, 2011
    Applicant: U. S.A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Alan T. Pope, Olafur S. Palsson
  • Publication number: 20110295419
    Abstract: A robotic system includes a robotic mechanism responsive to velocity control signals, and a permissible workspace defined by a convex-polygon boundary. A host machine determines a position of a reference point on the mechanism with respect to the boundary, and includes an algorithm for enforcing the boundary by automatically shaping the velocity control signals as a function of the position, thereby providing smooth and unperturbed operation of the mechanism along the edges and corners of the boundary. The algorithm is suited for application with higher speeds and/or external forces. A host machine includes an algorithm for enforcing the boundary by shaping the velocity control signals as a function of the reference point position, and a hardware module for executing the algorithm. A method for enforcing the convex-polygon boundary is also provided that shapes a velocity control signal via a host machine as a function of the reference point position.
    Type: Application
    Filed: May 26, 2010
    Publication date: December 1, 2011
    Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS, INC.
    Inventors: Muhammad E. Abdallah, Brian Hargrave, Robert J. Platt, JR.
  • Publication number: 20110254739
    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: Application
    Filed: April 8, 2011
    Publication date: October 20, 2011
    Applicant: U. S. A. 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
  • Publication number: 20110257784
    Abstract: A robotic system includes a dexterous robot having robotic joints, angle sensors adapted for measuring joint angles at a corresponding one of the joints, load cells for measuring a set of strain values imparted to a corresponding one of the load cells during a predetermined pose of the robot, and a host machine. The host machine is electrically connected to the load cells and angle sensors, and receives the joint angle values and strain values during the predetermined pose. The robot presses together mating pairs of load cells to form the poses. The host machine executes an algorithm to process the joint angles and strain values, and from the set of all calibration matrices that minimize error in force balance equations, selects the set of calibration matrices that is closest in a value to a pre-specified value. A method for calibrating the load cells via the algorithm is also provided.
    Type: Application
    Filed: April 15, 2010
    Publication date: October 20, 2011
    Applicants: The U.S.A. as Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS, INC.
    Inventors: Charles W. Wampler, II, Robert J. Platt, JR.
  • Publication number: 20110224840
    Abstract: A method for creating a digital elevation map (“DEM”) 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: Application
    Filed: March 11, 2011
    Publication date: September 15, 2011
    Applicant: U.S.A as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Michael D. Vanek
  • Publication number: 20110203288
    Abstract: A jet engine exhaust nozzle flow effector is a chevron formed with a radius of curvature with surfaces of the flow effector being defined and opposing one another. At least one shape memory alloy (SMA) member is embedded in the chevron closer to one of the chevron's opposing surfaces and substantially spanning from at least a portion of the chevron's root to the chevron's tip.
    Type: Application
    Filed: April 28, 2011
    Publication date: August 25, 2011
    Applicant: U. S. A. as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Travis L. Turner, Roberto J. Cano, Richard J. Silox, Ralph D. Buehrle, Christopher M. Cagle, Randolph H. Cabell, George C. Hilton
  • Publication number: 20110071675
    Abstract: A robotic system includes a humanoid robot with robotic joints each moveable using an actuator(s), and a distributed controller for controlling the movement of each of the robotic joints. The controller includes a visual perception module (VPM) for visually identifying and tracking an object in the field of view of the robot under threshold lighting conditions. The VPM includes optical devices for collecting an image of the object, a positional extraction device, and a host machine having an algorithm for processing the image and positional information. The algorithm visually identifies and tracks the object, and automatically adapts an exposure time of the optical devices to prevent feature data loss of the image under the threshold lighting conditions. A method of identifying and tracking the object includes collecting the image, extracting positional information of the object, and automatically adapting the exposure time to thereby prevent feature data loss of the image.
    Type: Application
    Filed: September 22, 2009
    Publication date: March 24, 2011
    Applicants: GM GLOBAL TECHNOLOGY OPERATIONS, INC., The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, HRL Laboratories, LLC
    Inventors: James W. Wells, Neil David Mc Kay, Suhas E. Chelian, Douglas Martin Linn, Charles W. Wampler, II, Lyndon Bridgwater
  • Publication number: 20110067517
    Abstract: A rotary actuator assembly is provided for actuation of an upper arm assembly for a dexterous humanoid robot. The upper arm assembly for the humanoid robot includes a plurality of arm support frames each defining an axis. A plurality of rotary actuator assemblies are each mounted to one of the plurality of arm support frames about the respective axes. Each rotary actuator assembly includes a motor mounted about the respective axis, a gear drive rotatably connected to the motor, and a torsion spring. The torsion spring has a spring input that is rotatably connected to an output of the gear drive and a spring output that is connected to an output for the joint.
    Type: Application
    Filed: September 22, 2009
    Publication date: March 24, 2011
    Applicants: GM GLOBAL TECHNOLOGY OPERATIONS,INC., The U.S.A .As Represented by the Administrator of the National Aeronautics and Space Administration, Oceaneering International, Inc.
    Inventors: Chris A. Ihrke, Joshua S. Mehling, Adam H. Parsons, Bryan Kristian Griffith, Nicolaus A. Radford, Frank Noble Permenter, Donald R. Davis, Robert O. Ambrose, Lucien Q. Junkin