Patents by Inventor U.S.A., as represented by the Administrator of the National Aeronautics and Space Administration
U.S.A., as represented by the Administrator of the National Aeronautics and Space Administration has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Publication number: 20160049885Abstract: A generator for producing an electric field for use with an inspection technology system is provided. The generator provides the required variable magnitude quasi-static electric fields for the “illumination” of objects, areas and volumes to be inspected by the system, and produces human-safe electric fields that are only visible to the system. The generator includes a casing, a driven, non-conducting and triboelectrically neutral rotation shaft mounted therein, an ungrounded electrostatic dipole element which works in the quasi-static range, and a non-conducting support for mounting the dipole element to the shaft. The dipole element has a wireless motor system and a charging system which are wholly contained within the dipole element and the support that uses an electrostatic approach to charge the dipole element.Type: ApplicationFiled: March 13, 2013Publication date: February 18, 2016Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20150376069Abstract: Multifunctional Boron Nitride nanotube-Boron Nitride (BN—BN) nanocomposites for energy transducers, thermal conductors, anti-penetrator/wear resistance coatings, and radiation hardened materials for harsh environments. An all boron-nitride structured BN—BN composite is synthesized. A boron nitride containing precursor is synthesized, then mixed with boron nitride nanotubes (BNNTs) to produce a composite solution which is used to make green bodies of different forms including, for example, fibers, mats, films, and plates. The green bodies are pyrolized to facilitate transformation into BN—BN composite ceramics. The pyrolysis temperature, pressure, atmosphere and time are controlled to produce a desired BN crystalline structure. The wholly BN structured materials exhibit excellent thermal stability, high thermal conductivity, piezoelectricity as well as enhanced toughness, hardness, and radiation shielding properties.Type: ApplicationFiled: March 29, 2013Publication date: December 31, 2015Inventors: National Institute of Aerospace Associates, U.S.A., as represented by the Administrator of the National Aeronautics and Space Administration
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Height Control and Deposition Measurement for the Electron Beam Free Form Fabrication (EBF3) Process
Publication number: 20150258626Abstract: A method of controlling a height of an electron beam gun and wire feeder during an electron freeform fabrication process includes utilizing a camera to generate an image of the molten pool of material. The image generated by the camera is utilized to determine a measured height of the electron beam gun relative to the surface of the molten pool. The method further includes ensuring that the measured height is within the range of acceptable heights of the electron beam gun relative to the surface of the molten pool. The present invention also provides for measuring a height of a solid metal deposit formed upon cooling of a molten pool. The height of a single point can be measured, or a plurality of points can be measured to provide 2D or 3D surface height measurements.Type: ApplicationFiled: March 15, 2013Publication date: September 17, 2015Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration -
Publication number: 20150259060Abstract: An orthotropic lattice structure interconnects porous surfaces of the flap with internal lattice structured perforations to equalize the steady pressure field on the flap surfaces adjacent to the end and to reduce the amplitude of the fluctuations in the flow field near the flap end. The global communication that exists within all of the perforations provides the mechanism to lessen the pressure gradients experienced by the end portion of the flap. In addition to having diffusive effects (diffusing the incoming flow), the three-dimensional orthogonal lattice structure is also reactive (acoustic wave phase distortion) due to the interconnection of the perforations.Type: ApplicationFiled: February 11, 2013Publication date: September 17, 2015Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20150264498Abstract: The present invention is an extremely low frequency (ELF) microphone and acoustic measurement system capable of infrasound detection in a portable and easily deployable form factor. In one embodiment of the invention, an extremely low frequency electret microphone comprises a membrane, a backplate, and a backchamber. The backchamber is sealed to allow substantially no air exchange between the backchamber and outside the microphone. Compliance of the membrane may be less than ambient air compliance. The backplate may define a plurality of holes and a slot may be defined between an outer diameter of the backplate and an inner wall of the microphone. The locations and sizes of the holes, the size of the slot, and the volume of the backchamber may be selected such that membrane motion is substantially critically damped.Type: ApplicationFiled: February 20, 2013Publication date: September 17, 2015Inventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20150260685Abstract: An electrical conductor and antenna are positioned in a fixed relationship to one another. Relative lateral movement is generated between the electrical conductor and a homogenous material while maintaining the electrical conductor at a fixed distance from the homogenous material. The antenna supplies a time-varying magnetic field that causes the electrical conductor to resonate and generate harmonic electric and magnetic field responses. Disruptions in at least one of the electric and magnetic field responses during this lateral movement are indicative of a lateral location of a subsurface anomaly. Next, relative out--of-plane movement is generated between the electrical conductor and the homogenous material in the vicinity of the anomaly's lateral location. Disruptions in at least one of the electric and magnetic field responses during this out-of-plane movement are indicative of a depth location of the subsurface anomaly. A recording of the disruptions provides a mapping of the anomaly.Type: ApplicationFiled: March 12, 2013Publication date: September 17, 2015Inventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20150253911Abstract: An interactive liner design and impedance modeling tool comprises software utilized to design acoustic liners for use in constrained spaces, both regularly and irregularly shaped. A graphical user interface allows the acoustic channel geometry to be drawn in a liner volume while the surface impedance calculations are updated and displayed in real-time. A one-dimensional transmission line model may be used as the basis for the impedance calculations.Type: ApplicationFiled: February 20, 2013Publication date: September 10, 2015Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20150254075Abstract: A processing device for high-speed execution of a computer program is provided. A memory module may store one or more computer programs. A sequencer may select one of the computer programs and controls execution of the selected program. A register module may store intermediate values associated with a current calculation set, a set of output values associated with a previous calculation set, and a set of input values associated with a subsequent calculation set. An external interface may receive the set of input values from a computing device and provides the set of output values to the computing device. A computation interface may provide a set of operands for computation during processing of the current calculation set. The set of input values are loaded into the register and the set of output values are unloaded from the register in parallel with processing of the current calculation set.Type: ApplicationFiled: March 11, 2013Publication date: September 10, 2015Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20150238982Abstract: A fluidic oscillator having independent frequency and amplitude control includes a fluidic-oscillator main flow channel having a main flow inlet, a main flow outlet, and first and second control ports disposed at opposing, sides thereof. A fluidic-oscillator controller has an inlet and outlet. A volume defined by the main flow channel is greater than the volume defined by the controller. A flow diverter coupled to the outlet of the controller defines a first fluid flow path from the controller's outlet to the first control port and defines a second fluid flow path from the controller's outlet to the second control port.Type: ApplicationFiled: March 6, 2013Publication date: August 27, 2015Applicant: U.S.A as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: U.S.A as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20150238983Abstract: A fluidic oscillator array includes a plurality of fluidic-oscillator main flow channels. Each main flow channel has an inlet and an outlet. Each main flow channel has first and second control ports disposed at opposing sides thereof, and has a first and a second feedback ports disposed at opposing sides thereof. The feedback ports are located downstream of the control ports with respect to a direction of a fluid flow through the main flow channel. The system also includes a first fluid accumulator in fluid communication with each first control port and each first feedback port, and a second fluid accumulator in fluid communication with each second control port and each second feedback port.Type: ApplicationFiled: March 6, 2013Publication date: August 27, 2015Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20140262498Abstract: An interconnect device forms an electrical and mechanical connection between electrical connections pads on an integrated circuit and those on a printed circuit board. The device is a coil with a first portion of its turns at one axial end of the coil having at least two turns in axial contact with one another, a second portion of its turns at an opposing axial end of the coil having at least two turns in axial contact with one another, and a third portion of the turns disposed between and contiguous with the first and second portions. The third portion is defined by at least two of the turns in a spaced apart axial relationship. The coil is made from a spring material and is electrically conductive. Each of the coil's first portion and second portion is coated with a solder material.Type: ApplicationFiled: March 13, 2013Publication date: September 18, 2014Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20140066553Abstract: A composite comprising a combination of a self-healing polymer matrix and a carbon fiber reinforcement is described. In one embodiment, the matrix is a polybutadiene graft copolymer matrix, such as polybutadiene graft copolymer comprising poly(butadiene)-graft-poly(methyl acrylate-co-acrylonitrile). A method of fabricating the composite is also described, comprising the steps of manufacturing a pre-impregnated unidirectional carbon fiber preform by wetting a plurality of carbon fibers with a solution, the solution comprising a self-healing polymer and a solvent, and curing the preform. A method of repairing a structure made from the composite of the invention is described. A novel prepreg material used to manufacture the composite of the invention is described.Type: ApplicationFiled: February 22, 2013Publication date: March 6, 2014Inventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20130315816Abstract: A scalable method allows preparation of bulk quantities of holey carbon allotropes with holes ranging from a few to over 100 nm in diameter. Carbon oxidation catalyst nanoparticles are first deposited onto a carbon allotrope surface in a facile, controllable, and solvent-free process. The catalyst-loaded carbons are then subjected to thermal treatment in air. The carbons in contact with the carbon oxidation catalyst nanoparticles are selectively oxidized into gaseous byproducts such as CO or CO2, leaving the surface with holes. The catalyst is then removed via refluxing in diluted nitric acid to obtain the final holey carbon allotropes. The average size of the holes correlates strongly with the size of the catalyst nanoparticles and is controlled by adjusting the catalyst precursor concentration. The temperature and time of the air oxidation step, and the catalyst removal treatment conditions, strongly affect the morphology of the holes.Type: ApplicationFiled: April 1, 2013Publication date: November 28, 2013Inventors: National Institute of Aerospace Associates, U.S.A., as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20130193704Abstract: A robotic hand includes a finger with first, second, and third phalanges. A first joint rotatably connects the first phalange to a base structure. A second joint rotatably connects the first phalange to the second phalange. A third joint rotatably connects the third phalange to the second phalange. The second joint and the third joint are kinematically linked such that the position of the third phalange with respect to the second phalange is determined by the position of the second phalange with respect to the first phalange.Type: ApplicationFiled: March 14, 2013Publication date: August 1, 2013Applicants: The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration, GM GLOBAL TECHNOLOGY OPERATIONS, INC.Inventors: GM GLOBAL TECHNOLOGY OPERATIONS, INC., The U.S.A. As Represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20130157079Abstract: A first material with a known maximum temperature of operation is coated with a second material on at Least one surface of the first material. The coating has a melting temperature that is greater than the maximum temperature of operation of the first material. The coating is heated to its melting temperature until the coating flows into any cracks in the first material's surface.Type: ApplicationFiled: December 19, 2012Publication date: June 20, 2013Applicant: U.S.A. as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration
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Publication number: 20130152727Abstract: A touchdown bearing system is provided to safely spin down a magnetically suspended flywheel rotor from full speed when the magnetic suspension system fails. In one embodiment, a plurality of touchdown wheels are mounted on a rigid support ring in a planetary arrangement.Type: ApplicationFiled: December 14, 2012Publication date: June 20, 2013Applicant: U.S.A., as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: U.S.A., as represented by the Administrator of the National Aeronautics and Space Administration