Patents Assigned to and Space Administration
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Patent number: 8938377Abstract: An improved model for simulating atmospheric disturbances is disclosed. A scale Kolmogorov spectral may be scaled to convert the Kolmogorov spectral into a finite energy von Karman spectral and a fractional order pole-zero transfer function (TF) may be derived from the von Karman spectral. Fractional order atmospheric turbulence may be approximated with an integer order pole-zero TF fit, and the approximation may be stored in memory.Type: GrantFiled: May 18, 2012Date of Patent: January 20, 2015Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: George Kopasakis
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Patent number: 8936395Abstract: Systems and methods that are capable of measuring temperature via spectrophotometry principles are discussed herein. These systems and methods are based on the temperature dependence of the reflection spectrum of hematite. Light reflected from these sensors can be measured to determine a temperature, based on changes in the reflection spectrum discussed herein.Type: GrantFiled: September 28, 2011Date of Patent: January 20, 2015Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Timothy J Bencic
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Patent number: 8932683Abstract: Method and apparatus for enhancing the durability as well as the strength and stiffness of prepreg fiber tows of the sort used in composite materials are disclosed. The method involves adhering electrospun fibers onto the surface of such composite materials as filament-wound composite objects and the surface of prepreg fiber tows of the sort that are subsequently used in the production of composite materials of the filament-wound, woven, and braided sorts. The apparatus performs the methods described herein.Type: GrantFiled: June 14, 2013Date of Patent: January 13, 2015Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Lee W. Kohlman, Gary D. Roberts
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Patent number: 8933789Abstract: Methods, apparatuses and systems for radio frequency identification (RFID)-enabled information collection are disclosed, including an enclosure, a collector coupled to the enclosure, an interrogator, a processor, and one or more RFID field sensors, each having an individual identification, disposed within the enclosure. In operation, the interrogator transmits an incident signal to the collector, causing the collector to generate an electromagnetic field within the enclosure. The electromagnetic field is affected by one or more influences. RFID sensors respond to the electromagnetic field by transmitting reflected signals containing the individual identifications of the responding RFID sensors to the interrogator. The interrogator receives the reflected signals, measures one or more returned signal strength indications (“RSSI”) of the reflected signals and sends the RSSI measurements and identification of the responding RFID sensors to the processor to determine one or more facts about the influences.Type: GrantFiled: March 8, 2013Date of Patent: January 13, 2015Assignee: The United States of America as represented by the Administrator of the National Aeronauties and Space AdministrationInventors: Patrick W. Fink, Gregory Y. Lin, Timothy F. Kennedy, Phong H. Ngo, Diane Byerly
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Patent number: 8920730Abstract: A chemochromic sensor for detecting a combustible gas, such as hydrogen, includes a chemochromic pigment mechanically mixed with a polymer and molded into a rigid or pliable shape. In a preferred embodiment, the chemochromic detector is within the material which is molded into a manufactured part, said part becoming the detector itself. The detector is robust and easily modifiable for a variety of applications and environmental conditions, such as atmospheres of inert gas, hydrogen gas, or mixtures of gases, or in environments that have variable temperature, including high temperatures such as above 100° C. and low temperatures such as below ?196° C.Type: GrantFiled: September 12, 2012Date of Patent: December 30, 2014Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Luke B. Roberson, Janine E. Captain, Martha K. Williams, Trent M. Smith, LaNetra Clayton Tate
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Patent number: 8922041Abstract: A kite system includes a kite and a ground station. The ground station includes a sensor that can be utilized to determine an angular position and velocity of the kite relative to the ground station. A controller utilizes a fuzzy logic control system to autonomously fly the kite. The system may include a ground station having powered winding units that generate power as the lines to the kite are unreeled. The control system may be configured to fly the kite in a crosswind trajectory to increase line tension for power generation. The sensors for determining the position of the kite are preferably ground-based.Type: GrantFiled: February 13, 2013Date of Patent: December 30, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: David D. North, Mark J. Aull
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Patent number: 8924069Abstract: A method and system for control of a first aircraft relative to a second aircraft. A desired location and desired orientation are estimated for the first aircraft, relative to the second aircraft, at a subsequent time, t=t2, subsequent to the present time, t=t1, where the second aircraft continues its present velocity during a subsequent time interval, t1?t?t2, or takes evasive action. Action command sequences are examined, and an optimal sequence is chosen to bring the first aircraft to the desired location and desired orientation relative to the second aircraft at time t=t2. The method applies to control of combat aircraft and/or of aircraft in a congested airspace.Type: GrantFiled: April 9, 2008Date of Patent: December 30, 2014Assignee: The United States of America as Represented by the Administrator of the National Aeronautics & Space Administration (NASA)Inventors: John T. Kaneshige, Kalmanje S. Krishnakumar
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Patent number: 8919842Abstract: A robotic system includes a tendon-driven end effector, a linear actuator, a flexible tendon, and a plate assembly. The linear actuator assembly has a servo motor and a drive mechanism, the latter of which translates linearly with respect to a drive axis of the servo motor in response to output torque from the servo motor. The tendon connects to the end effector and drive mechanism. The plate assembly is disposed between the linear actuator assembly and the tendon-driven end effector and includes first and second plates. The first plate has a first side that defines a boss with a center opening. The second plate defines an arcuate through-slot having tendon guide channels. The first plate defines a through passage for the tendon between the center opening and a second side of the first plate. A looped end of the flexible tendon is received within the tendon guide channels.Type: GrantFiled: February 7, 2014Date of Patent: December 30, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Chris A. Ihrke, Myron A. Diftler, Lyndon Bridgwater, Vienny Nguyen, Alexander Millerman
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Patent number: 8924736Abstract: A method of authenticating or declining to authenticate an asserted identity of a candidate-person. In an enrollment phase, a reference PQRST heart action graph is provided or constructed from information obtained from a plurality of graphs that resemble each other for a known reference person, using a first graph comparison metric. In a verification phase, a candidate-person asserts his/her identity and presents a plurality of his/her heart cycle graphs. If a sufficient number of the candidate-person's measured graphs resemble each other, a representative composite graph is constructed from the candidate-person's graphs and is compared with a composite reference graph, for the person whose identity is asserted, using a second graph comparison metric. When the second metric value lies in a selected range, the candidate-person's assertion of identity is accepted.Type: GrantFiled: March 11, 2013Date of Patent: December 30, 2014Assignee: The United States of America as Represented by the Administrator of the National Aeronautics & Space Administration (NASA)Inventors: Sorin V. Dusan, Charles C. Jorgensen
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Patent number: 8913844Abstract: An improved method for correcting for noise in the digital domain is disclosed. Reference pixel fast-varying components are extracted using a Hilbert-Huang Transform Real-Time Data Processing System (HHT-DPS-RT). The reference pixels are non-photon-detecting pixels in a sensor array. The fast-varying components of the reference pixels are processed in addition to the average over the remaining trend, facilitating additional noise correction for active pixels.Type: GrantFiled: June 5, 2012Date of Patent: December 16, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space AdministrationInventors: Katherine R. Heinzen, Semion Kizhner, Maxime Pinchinat, Thomas P. Flatley, Dominic J. Benford
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Patent number: 8912494Abstract: An apparatus for ultrasensitive long-wave imaging cameras is provided. In one embodiment, the apparatus includes a filter configured to allow high frequencies of interest to pass through the filter. The apparatus also includes an antenna that is configured to receive the high frequencies of interest. The apparatus further includes a plurality of bolometers that are configured to measure data regarding the high frequencies of interest.Type: GrantFiled: August 17, 2011Date of Patent: December 16, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space AdministrationInventors: James A. Chervenak, Ari D. Brown, Edward J. Wollack, Dominic J. Benford
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Patent number: 8913124Abstract: A lock-in imaging system is configured for detecting a disturbance in air. The system includes an airplane, an interferometer, and a telescopic imaging camera. The airplane includes a fuselage and a pair of wings. The airplane is configured for flight in air. The interferometer is operatively disposed on the airplane and configured for producing an interference pattern by splitting a beam of light into two beams along two paths and recombining the two beams at a junction point in a front flight path of the airplane during flight. The telescopic imaging camera is configured for capturing an image of the beams at the junction point. The telescopic imaging camera is configured for detecting the disturbance in air in an optical path, based on an index of refraction of the image, as detected at the junction point.Type: GrantFiled: February 3, 2011Date of Patent: December 16, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Yeonjoon Park, Sang Hyouk Choi, Glen C. King, James R. Elliott, Albert L. Dimarcantonio
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Patent number: 8912974Abstract: Disclosed herein is an antenna feed design for transmitting or receiving a circularly polarized microwave signal, and a communication device using that antenna feed design. Resonating disks are bowl-shaped to balance E-plane and H-plane magnetic field patterns, decreasing cross-polarization, and providing mechanical rigidity. A non-planar circuit replaces planar microstrip transmission lines for transmitting the signal, with 90° phase shifts, from an input point to excitation points. This non-planar circuit overcomes some of the layout problems encountered in planar circuits. It maintains impedance matching from the input point to the excitation points by progressively tapering down the characteristic transmission line impedance of each successive section. The non-planar circuit has sufficient mechanical strength and rigidity to allow it to be supported at only two anchor points. Similarly, the non-planar disks are also of sufficient strength to require only a single anchor point each.Type: GrantFiled: August 31, 2011Date of Patent: December 16, 2014Assignee: The United State of America as represented by the Administrator of the National Aeronautics Space AdministrationInventors: David Green, Cornelis Frederik Du Toit
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Patent number: 8909040Abstract: A method and system for multiplexing a network of parallel fiber Bragg grating (FBG) sensor-fibers to a single acquisition channel of a closed Michelson interferometer system via a fiber splitter by distinguishing each branch of fiber sensors in the spatial domain. On each branch of the splitter, the fibers have a specific pre-determined length, effectively separating each branch of fiber sensors spatially. In the spatial domain the fiber branches are seen as part of one acquisition channel on the interrogation system. However, the FBG-reference arm beat frequency information for each fiber is retained. Since the beat frequency is generated between the reference arm, the effective fiber length of each successive branch includes the entire length of the preceding branch. The multiple branches are seen as one fiber having three segments where the segments can be resolved.Type: GrantFiled: February 5, 2013Date of Patent: December 9, 2014Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Allen R Parker, Jr., Hon Man Chan, Anthony (Nino) Piazza, William Lance Richards
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Patent number: 8899563Abstract: A flexible volumetric structure has a first spring that defines a three-dimensional volume and includes a serpentine structure elongatable and compressible along a length thereof. A second spring is coupled to at least one outboard edge region of the first spring. The second spring is a sheet-like structure capable of elongation along an in-plane dimension thereof. The second spring is oriented such that its in-plane dimension is aligned with the length of the first spring's serpentine structure.Type: GrantFiled: June 11, 2009Date of Patent: December 2, 2014Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Christopher M. Cagle, Robin W. Schlecht
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Patent number: 8899467Abstract: A welding head assembly has a work piece disposed between its containment plates' opposing surfaces with the work piece being maintained in a plastic state thereof at least in a vicinity of the welding head assembly's stir rod as the rod is rotated about its longitudinal axis. The welding head assembly and the work piece experience relative movement therebetween in a direction perpendicular to the rod's longitudinal axis as the work piece is subjected to a compressive force applied by the containment plates. A first source coupled to the first containment plate applies a first ultrasonic wave thereto such that the first ultrasonic wave propagates parallel to the direction of relative movement. A second source coupled to the second containment plate applies a second ultrasonic wave thereto such that the second ultrasonic wave propagates parallel to the direction of relative movement.Type: GrantFiled: September 23, 2011Date of Patent: December 2, 2014Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventor: R. Jeffrey Ding
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Patent number: 8902015Abstract: A radio frequency power load and associated method. A radio frequency power load apparatus may include a container with an ionized fluid therein. The apparatus may include one conductor immersed in a fluid and another conductor electrically connected to the container. A radio frequency transmission system may include a radio frequency transmitter, a radio frequency amplifier connected to the transmitter and a radio frequency power load apparatus connected to the amplifier. The apparatus may include a fluid having an ion source therein, one conductor immersed in a fluid, and another conductor electrically connected to the container. A method of dissipating power generated by a radio frequency transmission system may include constructing a waveguide with ionized fluid in a container and connecting the waveguide to an amplifier of the transmission system.Type: GrantFiled: November 18, 2011Date of Patent: December 2, 2014Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Karthik Srinivasan, V, Todd M. Freestone, William Herbert Sims, III
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Patent number: 8896315Abstract: A battery cell balancing system is operable to utilize a relatively small number of transformers interconnected with a battery having a plurality of battery cells to selectively charge the battery cells. Windings of the transformers are simultaneously driven with a plurality of waveforms whereupon selected battery cells or groups of cells are selected and charged. A transformer drive circuit is operable to selectively vary the waveforms to thereby vary a weighted voltage associated with each of the battery cells.Type: GrantFiled: January 20, 2012Date of Patent: November 25, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Francis J. Davies
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Patent number: 8898479Abstract: Apparatuses, systems, computer programs and methods for implementing a genomics-based security solution are discussed herein. In an encryption process, plaintext may be converted to DNAtext and DNAtext may be converted to a ciphergene. The ciphergene may then be converted into a pre-transcriptional complex. The pre-transcriptional complex, in turn, may then be converted into a cipherprotein. The decryption process operates in the reverse of the encryption process to obtain plaintext.Type: GrantFiled: June 27, 2012Date of Patent: November 25, 2014Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space AdministrationInventor: Harry C. Shaw
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Patent number: 8894918Abstract: Methods are disclosed for producing architectural preforms and high-temperature composite structures containing high-strength ceramic fibers with reduced preforming stresses within each fiber, with an in-situ grown coating on each fiber surface, with reduced boron within the bulk of each fiber, and with improved tensile creep and rupture resistance properties tier each fiber. The methods include the steps of preparing an original sample of a preform formed from a pre-selected high-strength silicon carbide ceramic fiber type, placing the original sample in a processing furnace under a pre-selected preforming stress state and thermally treating the sample in the processing furnace at a pre-selected processing temperature and hold time in a processing gas having a pre-selected composition, pressure, and flow rate.Type: GrantFiled: February 19, 2010Date of Patent: November 25, 2014Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: James A. DiCarlo, Hee-Mann Yun