Patents Assigned to Administrator of the National Aeronautics and Space Administration
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Patent number: 11004802Abstract: An integrated circuit chip includes a wide bandgap semiconductor substrate, a plurality of semiconductor electronic components disposed on the semiconductor substrate, an overlying insulating layer disposed on the plurality of semiconductor devices, and a crack barrier laterally displaced from all of the plurality of semiconductor components. The crack barrier is configured to prevent propagation of cracks in the overlying insulating layer. The crack barrier does not conductively connect to any of the plurality of semiconductor electronic components.Type: GrantFiled: October 12, 2018Date of Patent: May 11, 2021Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: David J. Spry, Philip G. Neudeck
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Patent number: 10977776Abstract: A method includes placing an imaging device in contact with a sample, irradiating the sample via an illuminator such that radiation scatters off of the structure, and providing the scattered radiation to a detector to generate a digital video signal. A processor then performs various operations including subtracting a sum of a black state value and a user-defined black level clamping value from the digital video signal to create subtracted image data, substituting negative values in the subtracted image data with a reference value to create modified image data, and amplifying the modified image data by a user-defined gain to create contrast enhanced image data.Type: GrantFiled: August 7, 2018Date of Patent: April 13, 2021Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Michael J. Krasowski, Joseph M. Flatico, Phillip P. Jenkins, Lawrence C. Greer
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Patent number: 10966809Abstract: A method and a device for treating dental caries using microwave energy applied directly to teeth at frequencies that are lethal to the bacteria in caries, without being destructive to tooth tissues. The method and a device will have a significant economic and health impact, leading to a reduction in traditional surgical interventions, as well by improving access to care for those with health disparities.Type: GrantFiled: February 3, 2014Date of Patent: April 6, 2021Assignee: THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONInventors: Ivan Stangel, Marguerite A. Sognier, George D. Arndt, Diane L. Byerly, John Dusl
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Patent number: 10962166Abstract: Calibration of a hexapod structure includes measuring a head pose of the hexapod structure relative to a base of the hexapod structure. Calibration of the hexapod structure also includes for each strut, independently increasing a length of each strut by a predefined amount from an original length and repeating the measuring of the head pose relative to the base. Calibration of the hexapod structure further includes for each strut, independently decreasing a length of each strut by a predefined amount from the original length and repeating the measuring of the head pose relative to the base. Additionally, calibration of the hexapod structure includes moving each strut back to the original length, and estimating joint errors for each strut prior to calibrating of the hexapod structure.Type: GrantFiled: August 2, 2018Date of Patent: March 30, 2021Assignee: United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Yong Liu
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Patent number: 10954152Abstract: A supercritical water oxidation-flame piloted vortex reactor has a hydrothermal flame produced within the interior of the reactor fed by a fuel including a waste water stream, and has a subcritical wash stream, including water below its critical point, that creates an upward helical flow in the material within the reactor. The hydrothermal flame and upward helical flow produce within the reactor a supercritical core region, a subcritical outer region around the core region, and a transcritical intermediate region between them. The upward helical flow serves to transfer precipitated ionic compounds out of the supercritical core region, through the transcritical intermediate region, and into the subcritical outer region where they re-dissolve. A processed flow, including purified water, is removed from an upper portion of the supercritical core region by an aspirator.Type: GrantFiled: March 4, 2020Date of Patent: March 23, 2021Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Michael C. Hicks, Uday G. Hegde
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Patent number: 10934028Abstract: A lightweight flexible BNNT mat or fabric provides improved thermal stability and shielding capabilities under a hypersonic thermal flux. The BNNT mat reduces the stagnation temperature and maintains a low regression rate. An in-situ passivation layer may be formed on the BNNT mat or fabric under high thermal flux. The passivation layer minimizes or prevents penetration of the atmosphere (air or gas) as well as heat and radiation through the thickness of the BNNT material, and it effectively diffuses heat throughout the mat or fabric laterally and radially to minimize localized excessive heat. A BNNT mat according to the present disclosure may also efficiently transfer heat from the BNNT material via radiation due to the high thermal emissivity (0.92) of the BNNT material.Type: GrantFiled: November 15, 2017Date of Patent: March 2, 2021Assignee: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: John-Andrew S. Hocker, Cheol Park, Sang-Hyon Chu, Jin Ho Kang, Catharine C. Fay
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Patent number: 10931480Abstract: A wireless flight sensor system that incorporates a network of wireless sensors all in communication with a sensor gateway, the gateway in turn being in communication with a flight network. The sensor gateway includes a software defined radio (SDR) by which sensors communicate. The SDR is easily reconfigurable to accommodate new wireless technology. The flight network software (FNS) comprises a modular software architecture with a management repository, a traffic manager, a wireless interface controller, and a sensor database. The resulting system is both scalable and easily reprogrammable to accommodate a wide variety of current and future wireless sensing capability.Type: GrantFiled: June 13, 2018Date of Patent: February 23, 2021Assignee: United States of America as Represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Matthew R Waldersen
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Patent number: 10907025Abstract: An aerogel and method of making the aerogel is disclosed. The aerogel is a polyimide/polyamide hybrid with a cross-linking agent that induces gelation.Type: GrantFiled: August 24, 2018Date of Patent: February 2, 2021Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Jarrod C. Williams, Mary Ann B. Meador
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Patent number: 10899045Abstract: A soft lithography template or stamp is made by casting a polydimethysiloxane (PDMS) or other suitable elastomeric precursor onto a master pattern. The master pattern may be formed utilizing known micro-fabrication techniques. The PDMS template includes an inverse copy of the micro-structures on the master pattern, and can be placed into a mold used to prepare a carbon-fiber reinforced polymer composite part or other polymer molding systems where a matrix material passes through a fluid state during the cure process. The liquid resin material flows into the structures on the surface of the PDMS template and hardens during the curing cycle. After the part is released from the mold, the PDMS template can be peeled from the surface of the part to reveal the free standing micro structures which are a replica of the master pattern.Type: GrantFiled: March 12, 2014Date of Patent: January 26, 2021Assignee: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Frank L. Palmieri, Vincent B. Cruz, Christopher J. Wohl, Jr.
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Patent number: 10899937Abstract: Various embodiments provide ice mitigating surface coatings and methods for applying ice mitigating surface coatings. Various embodiment ice mitigating surface coatings may be formed by hydrolysis of one or more substituted n-alkyldimethylalkoxysilanes terminated with functionalities having the following characteristics with respect to water: 1) non-polar interactions; 2) hydrogen bonding through donor and acceptor interactions; or 3) hydrogen bonding through acceptor interactions only. The substituted n-alkyldimethylalkoxysilanes of the various embodiments may include methyl terminated species, hydroxyl terminated species, ethylene glycol terminated species, and methoxyethylene glycol terminated species. Various embodiment ice mitigating surface coatings may be applied to metal surfaces, such as aluminum surfaces. Various embodiment substituted n-alkyldimethylalkoxysilanes may have an aliphatic chain that is saturated and liner or branched or that is partially unsaturated and liner or branched.Type: GrantFiled: December 21, 2015Date of Patent: January 26, 2021Assignee: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Joseph G. Smith, Jr., Christopher J. Wohl, Jr.
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Patent number: 10888487Abstract: A grasp assist system includes a glove having a glove palm and fingers, with the glove worn on a user's hand. A sensor measures flexion of the glove fingers, and thus a change of position and/or attitude of the fingers is determined. Finger saddles at least partially surround a phalange of a respective one of the user's fingers. The system uses one or more tendon actuators to pull on flexible tendons. Each tendon connects to a respective finger saddle. A controller is in communication with the actuators and sensor(s). The glove may use feedback from optional contact sensors to adjust tension, and may have a built-in restorative force. In executing a control method, the controller selectively applies tension to the tendons in response to finger flexion, via the tendon actuators, at a level sufficient for moving the user's fingers when the user executes a hand maneuver.Type: GrantFiled: April 5, 2018Date of Patent: January 12, 2021Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Jonathan M. Rogers, Benjamin J. Peters, Evan Laske, Emily R. McBryan
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Patent number: 10884012Abstract: The embodiments described herein include a method and system for determining velocity and a motor controller implementing such velocity determination. In one embodiment, a rotatable element has a digital encoder coupled thereto for determining discrete angular positions of the rotatable element. An amount of time for the rotatable element to rotate between two successive ones of the discrete angular positions is measured. The amount of time is converted to a rotational velocity determination of the rotatable element.Type: GrantFiled: December 6, 2016Date of Patent: January 5, 2021Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Aaron M. Hulse, Harrison D. Pham, Stanley Lewis
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Patent number: 10876024Abstract: A material that facilitates dissipation of heat is provided and includes hexagonal boron nitride and alumina.Type: GrantFiled: October 4, 2017Date of Patent: December 29, 2020Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Ching-Cheh Hung, Janet B. Hurst
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Patent number: 10862189Abstract: An apparatus that combines an antenna and telescope to minimize system mass without compromising performance of either the antenna or telescope. The apparatus includes a sub-reflector placed before a prime focus feed of a hybrid reflector system. The apparatus also includes a radio frequency (RF) reflector is rigidly attached to a body of a spacecraft and an optical section is attached to a vibration isolation platform.Type: GrantFiled: November 6, 2017Date of Patent: December 8, 2020Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventor: Robert R. Romanofsky
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Patent number: 10816420Abstract: A tension-measurement device configured to determine a tension in a line includes a body. The body includes a first portion, a second portion extending from the first portion of the body, and a third portion extending from the first portion of the body. The line is configured to extend at least partially through the second and third portions of the body. A first sensor is coupled to the body and is configured to measure a strain on the body when a first portion of the line is placed under tension. The tension in the first portion of the line is configured to be determined based at least partially upon the strain.Type: GrantFiled: April 5, 2018Date of Patent: October 27, 2020Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Douglas A Litteken, Jared S Daum
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Patent number: 10807912Abstract: Advanced environmental barrier coating bond coat systems with higher temperature capabilities and environmental resistance are disclosed. These bond coat systems can be applied to ceramic substrates such as SiC/SiC ceramic matrix composite substrates, and can provide protection from extreme temperature, mechanical loading and environmental conditions, such as in high temperature gas turbines. Example bond coat systems can include either an advanced silicon/silicide component, an oxide/silicate component, or a combination thereof.Type: GrantFiled: May 1, 2017Date of Patent: October 20, 2020Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Dongming Zhu, Janet B. Hurst
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Patent number: 10800883Abstract: Processes and precursors may be used to produce a highly porous, extremely large surface area polyimide aerogel with optical translucency and diminished heat transfer. The resulting material maintains or exceeds structural integrity and low thermal conductivity seen in the high opacity polyimide aerogels of similar porosity and density. The formulations used for fabrication of aerogels may include combinations of fluorinated dianhydride and diamine fractions and non-fluorinated dianhydrides and diamines with various aliphatic and aromatic bridgehead components as precursors to the condensation polymerization of polyimide aerogels with polyamide crosslinks.Type: GrantFiled: October 19, 2017Date of Patent: October 13, 2020Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Stephanie L. Vivod, Mary Ann B. Meador, Andrew Shinko, Sadan C. Jana, Coleen Pugh
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Patent number: 10787569Abstract: Polyamide aerogels and methods of making the same are discussed. One example method can include the act of creating a mixture of at least one diamine with at least one diacid chloride in a first solvent. The mixture can comprise a plurality of amine capped polyamide oligomers. Such a method can also include the acts of adding a cross-linking agent to the mixture to create a gel and performing one or more solvent exchanges to remove the first solvent. Additionally, such a method can include the act of subjecting the gel to supercritical drying to polyamide aerogel.Type: GrantFiled: May 14, 2018Date of Patent: September 29, 2020Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Mary Ann B. Meador, Jarrod C. Williams
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Patent number: 10784593Abstract: A dual-band patch antenna includes a first patch antenna for operation at a first frequency and a second patch antenna for operation at a second frequency that is an integer multiple of the first frequency. A dielectric support is provided on which the first and second patch antennas are mounted. A nearest distance defined between the first and second patch antennas is a function of the second frequency and a dielectric constant of the dielectric support. The dielectric support has a feed point adapted to have a transmission line electrically coupled thereto. Electrically-conducting paths are coupled to the dielectric support for electrically coupling the feed point to the first and second patch antennas where at least one such electrically-conducting path has an insertion loss that is greater than 0 dB and less than or equal to 3 dB.Type: GrantFiled: August 2, 2018Date of Patent: September 22, 2020Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: William Herbert Sims, III
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Patent number: 10780514Abstract: A process for forming a single crystal superalloy wave spring is provided. In one embodiment, the process may include machining a wave spring from a single crystal superalloy slab after optimizing its orientation using diffraction techniques so that the wave spring will exhibit optimal spring properties.Type: GrantFiled: November 3, 2016Date of Patent: September 22, 2020Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Jeffrey J. DeMange, Frank J. Ritzert, Michael V. Nathal, Patrick H. Dunlap, Jr., Bruce M. Steinetz