Patents Assigned to Space
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Patent number: 11356639Abstract: This invention is directed to improving communication among people at remote locations, accomplished at low cost, by communication schemes involving “portal” structures, “channels” and “phonos.” The portal structures are mobile and easily deployed to the remote locations, for quick assembly and use, creating an audio-visual immersive communication experience for its users. A portal network architecture includes a plurality of portals located in different remote locations, configured to provide identical spaces that facilitate audio-video, immersive conferencing among users at the various portal sites. The portal interiors include favorable lighting and camera configurations to facilitate display of life-size, realistic, and planar images of the users while maintaining eye contact between them.Type: GrantFiled: June 22, 2020Date of Patent: June 7, 2022Assignee: Shared Space Studios LLCInventor: Amar Chopra Bakshi
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Patent number: 11353314Abstract: A method for determining a distance between components has the steps of providing a first conductive section in or on the first component in a region directed toward the second component, providing a second conductive section in or on the second component in a region directed toward the first conductive section, feeding a first voltage pulse into a first connection of the first conductive section, capturing a reflection voltage pulse in response to the first voltage pulse at the first connection, determining an impedance profile along the first conductive section by evaluating the reflection voltage pulse, and determining a distance between the components along the first conductive section by calculating a corresponding local distance, associated with the determined impedance profile, between the first conductive section and the second conductive section.Type: GrantFiled: June 7, 2018Date of Patent: June 7, 2022Assignees: Airbus Defence and Space GmbH, Airbus Operations GmbHInventors: Christopher Buchmann, Alois Friedberger, Thomas Kruse, Thomas Körwien
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Patent number: 11346138Abstract: A system for monitoring the state of a hook-keeper unit of an aeronautical structure. The hook-keeper unit is movable between a latched state and in a non-latched state, a mechanical warning element is movable between an exposed state and an unexposed state, and a connecting mechanism comprises a first end coupled to the hook-keeper unit, and a second end coupled to the mechanical warning element. The connecting mechanism is configured to automatically transmit the state of the hook-keeper unit to the mechanical warning element. The hook-keeper unit and the mechanical warning element are coupled between them by the connecting mechanism in an automatic bijective relationship, so that when the hook-keeper unit is in the latched state, the mechanical warning element is automatically in the unexposed state, and when the hook-keeper unit is in the non-latched state, the mechanical warning element is automatically in the exposed state.Type: GrantFiled: November 2, 2018Date of Patent: May 31, 2022Assignee: AIRBUS DEFENCE AND SPACE S.A.U.Inventors: Francisco Romero Galan, Carlos Manuel Escribano Serrano, Isabel Romero Molina, Jesús De Gracia Maqueda
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Patent number: 11347437Abstract: A processor system comprises a memory having at least two interleaved memory banks, at least two multiplexers which are respectively coupled to one of the at least two interleaved memory banks via a respective memory bank bus, a first processor or processor core which is coupled to first multiplexer inputs of the at least two multiplexers via a first data bus, a second processor or processor core which is coupled to second multiplexer inputs of the at least two multiplexers via a second data bus, and at least two queue buffers which are arranged in the second data bus between the second processor or processor core and the second multiplexer inputs of the at least two multiplexers. The first processor or processor core is configured to have read access or write access only to one of the at least two interleaved memory banks within one clock cycle.Type: GrantFiled: September 11, 2020Date of Patent: May 31, 2022Assignee: Airbus Defence and Space GmbHInventors: Sascha Uhrig, Johannes Freitag
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Patent number: 11347610Abstract: A system and a method for assisting with troubleshooting a complex system is disclosed in which the troubleshooting procedure can be modeled by a Markov decision process. Combining the fault tree technique with a Markov decision process, in order to determine in an optimal manner the sequence of troubleshooting actions will quickly address the consequences of a failure and ensure maintainability of the complex system.Type: GrantFiled: December 20, 2018Date of Patent: May 31, 2022Assignees: AIRBUS DEFENCE AND SPACE SAS, AIRBUSInventors: Jean-Luc Marty, David Canu, Alexandre Arnold
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Publication number: 20220160786Abstract: In an embodiment, an object of the present invention is to provide a therapeutic and/or preventive agent for a fibrosis such as pulmonary fibrosis, an inflammatory disease and/or an aging disease. In an embodiment, the present invention relates to a therapeutic and/or preventive agent for at least one disease of a fibrosis, an inflammatory disease and an aging disease, comprising extracellular vesicle derived from cell of a tissue or a surrounding tissue thereof where disease can occur, in which the cell is differentiated cell, and relates to a pharmaceutical composition containing the therapeutic and/or preventive agent.Type: ApplicationFiled: April 8, 2020Publication date: May 26, 2022Applicant: INTERNATIONAL SPACE MEDICAL CO., LTD.Inventors: Takahiro OCHIYA, Kazuyoshi KUWANO, Yu FUJITA, Tsukasa KADOTA
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Patent number: 11338896Abstract: A balloon system, preferably including a balloon and a payload. A balloon, preferably including a plurality of gores, a plurality of load members, and an apex fitting. A method of balloon system operation, preferably including deflating a balloon, and optionally including operating the balloon system in flight and/or landing the balloon system.Type: GrantFiled: January 29, 2021Date of Patent: May 24, 2022Assignee: Space Perspective Inc.Inventor: Taber MacCallum
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Patent number: 11339463Abstract: A local phase transformation strengthened nickel-base superalloy includes at least 8.0 wt % eta phase formers; at least 7.0 wt % of chi phase formers; less than 12 wt % chromium; at least 18 wt % cobalt; and aluminum. A ratio of eta phase formers:aluminum is (3.2-3.4):1. The eta phase formers can include titanium, tantalum, hafnium, and niobium. The chi phase formers include tungsten and molybdenum. When the superalloy is subjected to elevated temperatures, these levels of components promote eta and chi phase formation along superlattice stacking faults, thereby resulting in a local phase transformation at the stacking faults, which strengthens the superalloy and inhibits creep deformation.Type: GrantFiled: January 31, 2020Date of Patent: May 24, 2022Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Timothy M. Smith, Robert W. Carter
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Publication number: 20220147777Abstract: This disclosure relates to a system and method for separating partial discharge and noise signals from digital signals. The system comprises a data collecting module configured to recording and translating electromagnetic signals measured from a sensor to digital signals and a data processing module configured to: receive digital signals from the data collecting module; generate a feature from a time domain for each of the digital signals; generate a plurality of features from a frequency domain for each of the digital signals; apply clustering algorithm on the generated features for all the digital signals to identify a plurality of distinct clusters; and display each distinct cluster on a Phase-Resolved Partial Discharge (PRPD) chart.Type: ApplicationFiled: November 10, 2021Publication date: May 12, 2022Applicant: SPACE PTE. LTD.Inventors: Tian Tian Guo, Elissa Yanting Lim
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Publication number: 20220148441Abstract: A device is specified for producing a flight plan for lightweight aircraft. The device includes a first interface, a second interface, and a processing unit. The first interface is configured to receive aircraft data relating to the lightweight aircraft, wherein the aircraft data at least contain flight properties and functions of the lightweight aircraft. The second interface is configured to receive weather data from a weather information source, wherein the weather data contain at least weather data from the past and contain at least air movements in an altitude profile between a maximum altitude of the lightweight aircraft and the Earth's surface. The processing unit is configured to compare the aircraft data to the weather data and to ascertain whether the lightweight aircraft is manoeuvrable in the case of the received weather data and on the basis of the aircraft data.Type: ApplicationFiled: February 26, 2020Publication date: May 12, 2022Applicant: Airbus Defence and Space GmbHInventors: Fabian Klüßendorf, Paul Stevens, Steve Tate
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Patent number: 11327261Abstract: A composite fiber braid arrangement includes at least one fiber optic sensor embedded in a polymer resin. The polymer resin encloses a tow formed from an untwisted bundle of graphite fibers, and the untwisted bundle, together with the polymer resin, is enclosed by an outer jacket comprised of relatively dry, non-resin-impregnated, graphite fibers. Techniques for controlling alignment of an assembly of structural members, each structural member including such a fiber braid arrangement are also disclosed.Type: GrantFiled: April 22, 2020Date of Patent: May 10, 2022Assignee: Space Systems/Loral, LLCInventors: Maxwell Perham, Kevin Ziemann, Michael Freestone
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Patent number: 11329653Abstract: In an embodiment, an apparatus includes a first integrated circuit (IC) chip configured to receive a timing signal and a reference clock signal; and a second IC chip configured to receive the timing signal and the reference clock signal. The first and second IC chips are configured to generate respective first and second reference time signals based on the timing signal and the reference clock signal. The first and second IC chips include a respective first phase lock loop (PLL) and second PLL. The first PLL and the second PLL are synchronized to each other based on the first reference time signal and the second reference time signal.Type: GrantFiled: August 12, 2021Date of Patent: May 10, 2022Assignee: Space Exploration Technologies Corp.Inventors: David Francois Jacquet, Mostafa Ghazali, Masoud Kahrizi, Andras Tantos
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Patent number: 11324340Abstract: A product display merchandiser includes a tray having a top product-supporting surface with a longitudinally extending channel defined therein. A first sidewall has a vertical portion and a horizontal portion, and at least a laterally inner part of the horizontal portion can slide laterally with respect to the tray between a bottom of the tray and a base plate below the tray. A front end of the tray has a fitting received in a socket in the base plate. At a rear end of the tray, the channel receives a support assembly that connects the tray to a support structure.Type: GrantFiled: February 6, 2020Date of Patent: May 10, 2022Assignee: Retail Space Solutions LLCInventors: Matthew Wills, Julia Padvoiskis
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Patent number: 11329182Abstract: A monolithic multiple solar cell includes at least three partial cells, with a semiconductor mirror placed between two partial cells. The aim of the invention is to improve the radiation stability of said solar cell. For this purpose, the semiconductor mirror has a high degree of reflection in at least one part of a spectral absorption area of the partial cell which is arranged above the semiconductor mirror and a high degree of transmission within the spectral absorption range of the partial cell arranged below the semiconductor mirror.Type: GrantFiled: March 23, 2021Date of Patent: May 10, 2022Assignee: AZUR SPACE Solar Power GmbHInventors: Matthias Meusel, Gerhard Strobl, Frank Dimroth, Andreas Bett
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Patent number: 11325869Abstract: Slurry EBC systems and method for fabricating slurry EBC systems for protecting component substrates and extending the longevity of such components are disclosed. The slurry EBC systems include a bond coat having a temperature capability of up to 1482° C. (2700° F.). Example bond coats include a mullite-based bond coat and a rare earth disilicate-based bond coat.Type: GrantFiled: October 22, 2018Date of Patent: May 10, 2022Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space AdministrationInventors: Kang N. Lee, Deborah L. Waters
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Publication number: 20220134655Abstract: A three-dimensional print head apparatus may include a securing mechanism, a hopper, a nozzle, a heating system, and a fume extraction system. The securing mechanism may be adapted to secure to a wrist joint of a robotic arm. The hopper may have a cavity and a lower aperture and may be secured to the securing mechanism. The nozzle may have an upper aperture and a lower aperture. The heating system may be positioned along the barrel.Type: ApplicationFiled: January 14, 2022Publication date: May 5, 2022Applicant: Sidus Space, Inc.Inventors: Ivan Townsend, Robert Mueller, Nathan Gelino, Jonathan Smith, Matthew Nugent, Andrew Nick, Jason Schuler, Bradley Buckles
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Publication number: 20220140088Abstract: A stacked, high-blocking III-V semiconductor power diode having a first metallic terminal contact layer, formed at least in regions, and a highly doped semiconductor contact region of a first conductivity type and a first lattice constant. A drift layer of a second conductivity type and having a first lattice constant is furthermore provided. A semiconductor contact layer of a second conductivity, which includes an upper side and an underside, and a second metallic terminal contact layer are formed, and the second metallic terminal contact layer being integrally connected to the underside of the semiconductor contact layer, and the semiconductor contact layer having a second lattice constant at least on the underside, and the second lattice constant being the lattice constant of InP, and the drift layer and the highly doped semiconductor contact region each comprising an InGaAs compound or being made up of InGaAs.Type: ApplicationFiled: January 19, 2022Publication date: May 5, 2022Applicants: AZUR SPACE Solar Power GmbH, 3-5 Power Electronics GmbHInventors: Daniel FUHRMANN, Gregor KELLER, Clemens WAECHTER, Volker DUDEK
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Publication number: 20220139236Abstract: A device is specified for ascertaining a movement corridor for lightweight aircraft. The device includes a first interface, a second interface, and a processing unit. The first interface is configured to receive aircraft data relating to the lightweight aircraft, wherein the aircraft data at least contain flight properties and functions of the lightweight aircraft. The second interface is configured to receive weather data from a weather information source, wherein the weather data contain weather predictions and also current weather data and contain at least air movements in an altitude profile between a maximum altitude of the lightweight aircraft and the Earth's surface. The processing unit is configured to compare the aircraft data to the weather data and to ascertain a probable movement corridor of the aircraft.Type: ApplicationFiled: February 24, 2020Publication date: May 5, 2022Applicant: Airbus Defence and Space GmbHInventors: Fabian Klüßendorf, Paul Stevens, Steve Tate
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Patent number: 11322833Abstract: In one embodiment of the present disclosure, a housing assembly for an antenna apparatus includes a radome portion, a lower enclosure portion, and a fastener system configured for coupling the radome portion and the lower enclosure portion couplable to form an inner compartment for antenna components of an antenna assembly.Type: GrantFiled: June 3, 2020Date of Patent: May 3, 2022Assignee: Space Exploration Technologies Corp.Inventors: David Milroy, Victor Q. Dang, Michael J. Conte
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Patent number: 11319092Abstract: A spacecraft is disclosed having at least three flat side walls, at least one main communication antenna, including a radiating element having a central axis of radiation (AC-AC), a movable arm configured to move between a deployed position and a folded position, a reflector suitable for reflecting or receiving radiofrequency waves in a direction of emission (DE). The radiating element is fixed to a side wall so that the central axis of radiation (AC-AC) is arranged perpendicularly to the side wall, and the movable arm is shaped so that an offset angle (?) of between 25° and 65° is formed between the side wall and the direction of emission (DE), when the movable arm is in a deployed position.Type: GrantFiled: August 12, 2019Date of Patent: May 3, 2022Assignee: AIRBUS DEFENCE AND SPACE SASInventor: Philippe Cael