Patents Assigned to and Space Administration
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Patent number: 9446851Abstract: Landing hazard avoidance displays can provide rapidly understood visual indications of where it is safe to land a vehicle and where it is unsafe to land a vehicle. Color coded maps can indicate zones in two dimensions relative to the vehicles position where it is safe to land. The map can be simply green (safe) and red (unsafe) areas with an indication of scale or can be a color coding of another map such as a surface map. The color coding can be determined in real time based on topological measurements and safety criteria to thereby adapt to dynamic, unknown, or partially known environments.Type: GrantFiled: November 18, 2014Date of Patent: September 20, 2016Assignees: Rapid Imaging Software, Inc., National Aeronautics and Space AdministrationInventors: Michael Franklin Abernathy, Robert L. Hirsh
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Patent number: 9449818Abstract: One aspect of the present invention is a double sided hybrid crystal structure including a trigonal Sapphire wafer containing a (0001) C-plane and having front and rear sides. The Sapphire wafer is substantially transparent to light in the visible and infrared spectra, and also provides insulation with respect to electromagnetic radio frequency noise. A layer of crystalline Si material having a cubic diamond structure aligned with the cubic <111> direction on the (0001) C-plane and strained as rhombohedron to thereby enable continuous integration of a selected (SiGe) device onto the rear side of the Sapphire wafer. The double sided hybrid crystal structure further includes an integrated III-Nitride crystalline layer on the front side of the Sapphire wafer that enables continuous integration of a selected III-Nitride device on the front side of the Sapphire wafer.Type: GrantFiled: March 11, 2014Date of Patent: September 20, 2016Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Yeonjoon Park, Sang Hyouk Choi
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Patent number: 9447260Abstract: High quality thermoplastic composites and composite laminates containing nanoparticles and/or nanofibers, and methods of producing such composites and laminates are disclosed. The composites comprise a thermoplastic polymer and a plurality of nanoparticles, and may include a fibrous structural reinforcement. The composite laminates are formed from a plurality of nanoparticle-containing composite layers and may be fused to one another via an automated process.Type: GrantFiled: December 18, 2009Date of Patent: September 20, 2016Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Mark B. Gruber, Brian J. Jensen, Roberto J. Cano
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Patent number: 9449723Abstract: Methods for making a neutron converter layer are provided. The various embodiment methods enable the formation of a single layer neutron converter material. The single layer neutron converter material formed according to the various embodiments may have a high neutron absorption cross section, tailored resistivity providing a good electric field penetration with submicron particles, and a high secondary electron emission coefficient. In an embodiment method a neutron converter layer may be formed by sequential supercritical fluid metallization of a porous nanostructure aerogel or polyimide film. In another embodiment method a neutron converter layer may be formed by simultaneous supercritical fluid metallization of a porous nanostructure aerogel or polyimide film. In a further embodiment method a neutron converter layer may be formed by in-situ metalized aerogel nanostructure development.Type: GrantFiled: March 10, 2014Date of Patent: September 20, 2016Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Cheol Park, Godfrey Sauti, Jin Ho Kang, Sharon E. Lowther, Sheila A. Thibeault, Robert G. Bryant
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Patent number: 9440752Abstract: A method for increasing density of a region of a porous, phenolic bonded (“PPB”) body adjacent to a selected surface to increase failure tensile strength of the adjacent region and/or to decrease surface recession at elevated temperatures. When the surface-densified PPB body is brought together with a substrate, having a higher failure tensile strength, to form a composite body with a PPB body/substrate interface, the location of tensile failure is moved to a location spaced apart from the interface, the failure tensile strength of the PPB body is increased, and surface recession of the material at elevated temperature is reduced. The method deposits and allows diffusion of a phenolic substance on the selected surface. The PPB body and the substrate may be heated and brought together to form the composite body. The phenolic substance is allowed to diffuse into the PPB body, to volatilize and to cure, to provide a processed body with an increased surface density.Type: GrantFiled: November 26, 2013Date of Patent: September 13, 2016Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventors: Margaret M. Stackpoole, Christian Espinoza
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Patent number: 9444548Abstract: The present invention is an improved method of processing conglomerate data. The method employs a Triband Wavelet Transform that decomposes and decimates the conglomerate signal to obtain a final result. The invention may be employed to improve performance of Optical Frequency Domain Reflectometry systems.Type: GrantFiled: October 15, 2014Date of Patent: September 13, 2016Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Philip J Hamory, Allen R Parker, Jr.
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Patent number: 9435821Abstract: A single-axis accelerometer includes a housing defining a sleeve. An object/mass is disposed in the sleeve for sliding movement therein in a direction aligned with the sleeve's longitudinal axis. A first piezoelectric strip, attached to a first side of the object and to the housing, is longitudinally aligned with the sleeve's longitudinal axis. The first piezoelectric strip includes a first strip of a piezoelectric material with carbon nanotubes substantially aligned along a length thereof. A second piezoelectric strip, attached to a second side of the object and to the housing, is longitudinally aligned with the sleeve's longitudinal axis. The second piezoelectric strip includes a second strip of the piezoelectric material with carbon nanotubes substantially aligned along a length thereof. A voltage sensor is electrically coupled to at least one of the first and second piezoelectric strips.Type: GrantFiled: December 12, 2013Date of Patent: September 6, 2016Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Dennis Stephen Tucker, Pedro A. Capó-Lugo
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Patent number: 9434486Abstract: A frictionless satellite constraint system is provided. The constraint system includes at least one clamp bar configured to restrain a satellite within the constraint system in an axial direction. The constraint system also includes a plurality of pins configured to restrain the satellite within the constraint system in a lateral direction.Type: GrantFiled: February 28, 2013Date of Patent: September 6, 2016Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Luis H. Santos, John D. Hudeck
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Patent number: 9434832Abstract: An aerogel and process of making the aerogel is provided. The aerogel is a polyimide aerogel having polyamide cross-links formed using a triacid chloride cross-linker.Type: GrantFiled: March 17, 2015Date of Patent: September 6, 2016Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Mary Ann B. Meador
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Patent number: 9431778Abstract: Methods and systems may provide for debris exclusion and removal apparatuses for connectors which have inverting end caps with a multi-axis lever configuration, inverting end caps with enlarged handle and/or side rail configurations, rotating end cap configurations, poppet valve configurations, O-ring configurations, filament barrier configurations, retractable cover configurations, clamshell end cap configurations, or any combination thereof. Apparatuses may also provide for an intelligent electrical connector system capable of detecting damage to or faults within a plurality of conductors and then rerouting the energy through a non-damaged spare conductor.Type: GrantFiled: March 12, 2014Date of Patent: August 30, 2016Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert P. Mueller, Mark E. Lewis, Gary L. Bastin, Matthew C. Branch, Jeffrey W. Carlson, Adam G. Dokos, Kevin A. Murtland, Matthew W. Nugent, Gabor J. Tamasy, Ivan I. Townsend, III
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Patent number: 9423426Abstract: A circuit board that serves as a control and sampling interface to an inertial measurement unit (“IMU”) is provided. The circuit board is also configured to interface with a local oscillator and an external trigger pulse. The circuit board is further configured to receive the external trigger pulse from an external source that time aligns the local oscillator and initiates sampling of the inertial measurement device for data at precise time intervals based on pulses from the local oscillator. The sampled data may be synchronized by the circuit board with other sensors of a navigation system via the trigger pulse.Type: GrantFiled: August 3, 2012Date of Patent: August 23, 2016Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: David T Chelmins, Richard T. Powis, Jr., Obed Sands
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Patent number: 9424654Abstract: Analog circuits for detecting edges in pixel arrays are disclosed. A comparator may be configured to receive an all pass signal and a low pass signal for a pixel intensity in an array of pixels. A latch may be configured to receive a counter signal and a latching signal from the comparator. The comparator may be configured to send the latching signal to the latch when the all pass signal is below the low pass signal minus an offset. The latch may be configured to hold a last negative edge location when the latching signal is received from the comparator.Type: GrantFiled: July 31, 2015Date of Patent: August 23, 2016Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Norman F Prokop
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Patent number: 9423799Abstract: An information processing system and method for adaptively selecting an aircraft descent flight path for an aircraft, are provided. The system receives flight adaptation parameters, including aircraft flight descent time period, aircraft flight descent airspace region, and aircraft flight descent flyability constraints. The system queries a plurality of flight data sources and retrieves flight information including any of winds and temperatures aloft data, airspace/navigation constraints, airspace traffic demand, and airspace arrival delay model. The system calculates a set of candidate descent profiles, each defined by at least one of a flight path angle and a descent rate, and each including an aggregated total fuel consumption value for the aircraft following a calculated trajectory, and a flyability constraints metric for the calculated trajectory.Type: GrantFiled: August 11, 2014Date of Patent: August 23, 2016Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space Administration (NASA)Inventors: Minghong G. Wu, Steven M. Green
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Patent number: 9418844Abstract: A multi-junction solar cell is provided and includes multiple semiconducting layers and an interface layer disposed between the multiple semiconducting layers. The interface layer is made from an interface bonding material that has a refractive index such that a ratio of a refractive index of each of the multiple semiconducting layers to the refractive index of the interface bonding material is less than or equal to 1.5.Type: GrantFiled: July 31, 2015Date of Patent: August 16, 2016Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Geoffrey A. Landis
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Patent number: 9419319Abstract: A photonic waveguide choke includes a first waveguide flange member having periodic metal tiling pillars, a dissipative dielectric material positioned within an area between the periodic metal tiling pillars and a second waveguide flange member disposed to be coupled with the first waveguide flange member and in spaced-apart relationship separated by a gap. The first waveguide flange member has a substantially smooth surface, and the second waveguide flange member has an array of two-dimensional pillar structures formed therein.Type: GrantFiled: September 30, 2014Date of Patent: August 16, 2016Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Edward J. Wollack, Kongpop U-Yen, David T. Chuss
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Patent number: 9419558Abstract: Embodiments of the present invention describe an apparatus including an oscillator, a ramp generator, and an inverter. The oscillator is configured to generate a waveform comprising a low time and a high time. The inverter is configured to receive the waveform generated by the oscillator, and invert the waveform. The ramp generator is configured to increase a gate control voltage of a transistor connected to a solar cell, and rapidly decrease the gate control voltage of the transistor. During the low time, a measurement of a current and a voltage of the solar cell is performed. During the high time, a measurement of a current of a shorted cell and a voltage reference is performed.Type: GrantFiled: April 17, 2012Date of Patent: August 16, 2016Assignee: The United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Michael J. Krasowski, Norman F. Prokop
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Patent number: 9411569Abstract: A system, method and computer-readable storage devices for providing a climate data analytic services application programming interface distribution package. The example system can provide various components. The system provides a climate data analytic services application programming interface library that enables software applications running on a client device to invoke the capabilities of a climate data analytic service. The system provides a command-line interface that provides a means of interacting with a climate data analytic service by issuing commands directly to the system's server interface. The system provides sample programs that call on the capabilities of the application programming interface library and can be used as templates for the construction of new client applications. The system can also provide test utilities, build utilities, service integration utilities, and documentation.Type: GrantFiled: May 12, 2015Date of Patent: August 9, 2016Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: John L. Schnase, Daniel Q. Duffy, Glenn S. Tamkin
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Patent number: 9414072Abstract: Frequency-based, pixel-adaptive filtering using the JPEG-ESAP algorithm for low bit rate JPEG formatted color images may allow for more compressed images while maintaining equivalent quality at a smaller file size or bitrate. For RGB, an image is decomposed into three color bands—red, green, and blue. The JPEG-ESAP algorithm is then applied to each band (e.g., once for red, once for green, and once for blue) and the output of each application of the algorithm is rebuilt as a single color image. The ESAP algorithm may be repeatedly applied to MPEG-2 video frames to reduce their bit rate by a factor of 2 or 3, while maintaining equivalent video quality, both perceptually, and objectively, as recorded in the computed PSNR values.Type: GrantFiled: July 28, 2015Date of Patent: August 9, 2016Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Irving Linares
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Patent number: 9405005Abstract: The present invention proposes an automatic dependent surveillance broadcast (ADS-B) architecture and process, in which priority aircraft and ADS-B IN traffic information are included in the transmission of data through the telemetry communications to a remote ground control station. The present invention further proposes methods for displaying general aviation traffic information in three and/or four dimension trajectories using an industry standard Earth browser for increased situation awareness and enhanced visual acquisition of traffic for conflict detection. The present invention enable the applications of enhanced visual acquisition of traffic, traffic alerts, and en-route and terminal surveillance used to augment pilot situational awareness through ADS-B IN display and information in three or four dimensions for self-separation awareness.Type: GrantFiled: March 5, 2013Date of Patent: August 2, 2016Assignee: The United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Ricardo A. Arteaga
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Patent number: 9400237Abstract: An ultra-high temperature optical method incorporates speckle optics for sensing displacement and strain measurements well above conventional measurement techniques. High temperature pattern materials are used which can endure experimental high temperature environments while simultaneously having a minimum optical aberration. A purge medium is used to reduce or eliminate optical distortions and to reduce, and/or eliminate oxidation of the target specimen.Type: GrantFiled: March 17, 2014Date of Patent: July 26, 2016Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Russell W. Smith, H. Kevin Rivers, Joseph G. Sikora, Mark C. Roth, William M. Johnston