Patents Assigned to and Space Administration
  • Patent number: 10787569
    Abstract: 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: Grant
    Filed: May 14, 2018
    Date of Patent: September 29, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Mary Ann B. Meador, Jarrod C. Williams
  • Patent number: 10784593
    Abstract: 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: Grant
    Filed: August 2, 2018
    Date of Patent: September 22, 2020
    Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: William Herbert Sims, III
  • Patent number: 10780514
    Abstract: 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: Grant
    Filed: November 3, 2016
    Date of Patent: September 22, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Jeffrey J. DeMange, Frank J. Ritzert, Michael V. Nathal, Patrick H. Dunlap, Jr., Bruce M. Steinetz
  • Patent number: 10774682
    Abstract: 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: Grant
    Filed: June 21, 2013
    Date of Patent: September 15, 2020
    Assignee: The United States of America as Represented by the Administrator of National Aeromautics and Space Administration
    Inventors: Dongming Zhu, Janet B. Hurst
  • Patent number: 10759140
    Abstract: A polymer matrix composite includes layers that alternate between a thin carbon fiber veil layer and a thicker base carbon fiber reinforcement layer. Each veil is coated with conductive carbon nanotubes (CNTs) prior to being added as a laminate layer. Epoxy resin fixes CNTs extended into adjacent reinforcement layers, which results in a composite improved in interlaminar strength, fracture toughness, and impact resistance. Thermal and electrical conductivity are also improved due to the conductive CNTs bridging the resin-insulating interlayer region. As the fuzzy fiber veil is not relied on to provide strength or stiffness to the composite structure, any damage to the veil will not affect composite integrity. Also, as the CNT growth is not on a replacement section of reinforcement layer, the composite avoids pitfalls of strength degradation, reinforcing phase continuity disruption, and residual stress introduction.
    Type: Grant
    Filed: May 12, 2014
    Date of Patent: September 1, 2020
    Assignee: United States of America as Represented by the Admin of the National Aeronautics and Space Administration
    Inventor: Sandi Miller
  • Patent number: 10738373
    Abstract: An apparatus and method for creating shapes (e.g., letters, numbers, characters, symbols, or a combination thereof) using shape memory alloy (SMAs) component. The SMA components shaped into formed shapes that can then be distorted to obscure the original formed shaped. The original formed shape can be restored upon exposure to a heat source, magnetic field, or upon load removal.
    Type: Grant
    Filed: September 26, 2017
    Date of Patent: August 11, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Othmane Benafan, Eunice E. Arvizu
  • Patent number: 10732161
    Abstract: Systems, methods, and other embodiments associated with gas detecting sensors. According to one embodiment, a gas sensor includes a metal layer, a barrier interlayer, a substrate layer, a first insulating layer, a conduction path, a contact pad, and a second insulating layer. The conduction path connects the metal layer to the contact pad. The second insulating layer prevents diffusion through the contact pad, the conduction path, or the metal layer. The sensor includes a wire bonded electrical connection to the contact pad such that voltage can be determined and/or applied.
    Type: Grant
    Filed: May 4, 2018
    Date of Patent: August 4, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Jennifer Xu, Gary W. Hunter
  • Patent number: 10732073
    Abstract: The invention is a method for obtaining the curved displacement of a flexible structure by using strain measurements obtained by strain sensors. By obtaining the displacement of structures in this manner, one may accurately construct the deformed shape of the structure under large geometric nonlinear deformations and display said deformed shape in real-time, enabling active control of the structure shape if desired.
    Type: Grant
    Filed: October 4, 2017
    Date of Patent: August 4, 2020
    Assignee: U.S.A. as Represented by the Administration of the National Aeronautics and Space Administration
    Inventors: William L Ko, Van T Fleischer, Shun-Fat Lung
  • Patent number: 10731237
    Abstract: Advanced ultra high temperature ceramic (UHTC) systems with higher temperature capabilities, particularly an integrated ceramic coating and ceramic matrix composite (ICC-CMC). Also disclosed are coating and/or ceramic matrix composites and architecture arrangements to achieve ultra-high temperature and heat flux capability, resistance to oxidation, combustion, and a wide range of spectrum wavelength and charged particle radiation environments.
    Type: Grant
    Filed: September 25, 2017
    Date of Patent: August 4, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Dongming Zhu, Janet B. Hurst
  • Patent number: 10724030
    Abstract: The present invention provides a system for delivering a time-varying stimulation field to a subject. In the system, a power source, a control component and a transmission component operate as a stimulation field generator to provide a predetermined time-varying stimulation field to up-regulate or down-regulate an expression level of human genes. The present invention also provides a wearable apparatus for delivering the time-varying magnetic field to mammalian cells associated with bone formation in a subject. The wearable apparatus contains the stimulation field generator in a housing. The resulted modification on gene regulation of these genes and mammalian cells promotes the retention, repair of and reduction of compromised mammalian cartilage, bone, and associated tissue.
    Type: Grant
    Filed: February 19, 2018
    Date of Patent: July 28, 2020
    Assignee: United States of America as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Thomas J. Goodwin, Linda C. Shackelford
  • Patent number: 10728426
    Abstract: Methods and systems for analyzing and processing digital data comprising a plurality of infra-red (IR) video images acquired by a pulse thermography system are used to compute video data from the raw and smoothed video data acquired for the performance of non-destructive evaluation. New video data types computed may include but are not limited to contrast evolution data such as normalized contrast, converted contrast and normalized temperature contrast. Additionally, video data types computed comprise surface temperature, surface temperature rise and temperature simple contrast.
    Type: Grant
    Filed: August 16, 2017
    Date of Patent: July 28, 2020
    Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Ajay M. Koshti
  • Patent number: 10723857
    Abstract: A polyimide aerogel and method of making the aerogel is disclosed. The polymer backbone of the aerogel includes a cardo-diamine. The disclosed polyimide aerogel is less susceptible to temperature induced shrinkage than a polyimide aerogel that does not include a cardo-diamine.
    Type: Grant
    Filed: April 13, 2017
    Date of Patent: July 28, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Rocco P. Viggiano, Mary Ann B. Meador
  • Patent number: 10689986
    Abstract: A film cooled component is provided that includes a body having a cavity defined therein, wherein a coolant is supplied to the cavity cooling apertures having at least one channel defined on an inside surface. The coolant exits the cavity through the plurality of cooling apertures thereby providing a cooling effect to the body and the channel creates an air flow such that the air coolant moves towards the body upon exiting the plurality of cooling apertures. The film cooled component may include cooling apertures configured to reverse blow coolant air.
    Type: Grant
    Filed: October 10, 2017
    Date of Patent: June 23, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Ali A. Ameri, Vikram Shyam
  • Patent number: 10675781
    Abstract: Shape memory alloys (SMAs) may be used for static rock splitting. The SMAs may be used as high-energy multifunctional materials, which have a unique ability to recover large deformations and generate high stresses in response to thermal loads.
    Type: Grant
    Filed: April 4, 2017
    Date of Patent: June 9, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Othmane Benafan, Ronald D. Noebe
  • Patent number: 10673146
    Abstract: A communications system includes a radio frequency (“RF”) antenna. The RF antenna includes a RF reflector and a RF feed axially spaced from the RF reflector. The communications system also includes an optical telescope sharing an axis with the RF antenna. The optical telescope includes primary and secondary reflectors centered at the axis. A mounting structure mechanically couples a housing of the primary reflector to the secondary optical reflector. The mounting structure includes a plurality of truss struts extending the entirety of an axial distance between the primary and secondary optical reflectors and a plurality of support rings interconnecting the plurality of truss struts at various locations on the central axis at or between the primary and secondary optical reflectors. Each of the plurality of support rings and truss struts is structured to minimize the cross section of the support rings along radials originating at the RF feed.
    Type: Grant
    Filed: July 30, 2018
    Date of Patent: June 2, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventor: Adam Wroblewski
  • Patent number: 10663376
    Abstract: An apparatus includes a motor having a first shaft extending therefrom. The motor is configured to apply energy to the first shaft. A particle cartridge mechanically is coupled to the motor via the first shaft. The particle cartridge includes a screen separating an internal volume of the particle cartridge from an environment of the apparatus, and a plurality of particles disposed within the internal volume. A particle manipulation element is mechanically coupled to the first shaft and in contact with the plurality of particles. The particle manipulation element moves in response to the energy being applied to the first shaft to force some of the particles through the screen and into the environment of the apparatus.
    Type: Grant
    Filed: September 17, 2018
    Date of Patent: May 26, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Juan H. Agui, Rajagopal Vijayakumar
  • Patent number: 10654756
    Abstract: An engineered ceramic matrix is provided to blunt and self-heal matrix cracks to reduce oxygen ingress into a fiber reinforced composite.
    Type: Grant
    Filed: January 19, 2018
    Date of Patent: May 19, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventor: Sai V. Raj
  • Patent number: 10647439
    Abstract: A hybrid propulsion system for an aircraft is provided that includes a turbine engine, a first electric machine assembly connected to the turbine engine, a second electric machine assembly driven by the first electric machine assembly, and multiple third electric machine assemblies driven by the first electric machine assembly, wherein the multiple third electric machines provide a thrust output to propel the aircraft.
    Type: Grant
    Filed: September 9, 2019
    Date of Patent: May 12, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventor: Raymond F. Beach
  • Patent number: 10632828
    Abstract: A prime mover is combined with a flywheel storage device and a control system to implement a flywheel pulse and glide system in a vehicle. In one embodiment, the control system is configured to cycle power delivery between the prime mover and the flywheel storage device to power the vehicle. The prime mover, when activated by the control system, is configured to power the vehicle and spin up the flywheel storage device to capture a sufficient amount of energy.
    Type: Grant
    Filed: March 29, 2013
    Date of Patent: April 28, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Larry M. Trase, Ralph H. Jansen, Peter E. Kascak
  • Patent number: 10633256
    Abstract: Aerogels, aerogel composites and methods of making the same are discussed. One example method can include the act of creating a Boehmite colloid and adding a hydrolyzed silicon precursor to form a sol. A reinforcement can be infused with the sol, gelled to form a gel, then dried to form an aerogel composite. Such a method can also include the acts of performing one or more solvent exchanges and subjecting the gel composite to subcritical drying. Additionally, such a method can include the act of heat treating the aerogel composite. The aerogel composite can be used in high temperature, flexible seals capable of withstanding temperatures, pressures, and compression levels associated with aerodynamic heating generated during flight and in aerospace applications. The aerogel composite also can be used in thermal protection systems designed for fire protection for structures or in personnel fire protective equipment.
    Type: Grant
    Filed: April 19, 2017
    Date of Patent: April 28, 2020
    Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
    Inventors: Haiquan Guo, Frances I. Hurwitz