Patents Assigned to Space
  • Patent number: 10998606
    Abstract: In embodiments, a power splitter/combiner includes a first electrically conductive trace included in a first layer; second and third electrically conductive traces included in a second layer; a first via electrically coupled to the first and second electrically conductive traces; and a second via electrically coupled to the first and third electrically conductive traces. A first portion of the first electrically conductive trace comprises a first port of the power splitter/combiner. A second portion of the first electrically conductive trace, the first via, and the second electrically conductive trace comprises a second port of the power splitter/combiner. A third portion of the first electrically conductive trace, the second via, and the third electrically conductive trace comprises a third port of the power splitter/combiner.
    Type: Grant
    Filed: February 14, 2019
    Date of Patent: May 4, 2021
    Assignee: Space Exploration Technologies Corp.
    Inventors: Souren Shamsinejad, Javier Rodriguez De Luis, Nil Apaydin, Alireza Mahanfar
  • Patent number: 10995737
    Abstract: A method of producing a charge separation in a plasma having a low particle density which comprises a plurality of electrons and a plurality of positive ions. The method includes generating a magnetic field and passing the plasma having a low particle density along a first axis through the magnetic field. The magnetic field is generated having a component which is perpendicular to the first axis and is configured so as to deflect the plurality of electrons from the first axis and allow the plurality of positive ions to travel substantially undeflected along the first axis. Also provided is a magnetohydrodynamic generator and a low earth orbit thruster making use of the charge separation mechanism.
    Type: Grant
    Filed: May 12, 2016
    Date of Patent: May 4, 2021
    Assignee: AIRBUS DEFENCE AND SPACE LIMITED
    Inventors: Aaron Knoll, Paolo Bianco
  • Patent number: 10995406
    Abstract: Systems and methods for highly reproducible and focused plasma jet printing and patterning of materials using appropriate ink containing aerosol through nozzles with narrow orifice and tubes with controlled dielectric constant connected to high voltage power supply, in the presence of electric field and plasma, that enables morphological and/or bulk chemical modification and/or surface chemical modification of the material in the aerosol and/or the substrate prior to printing, during printing and post printing.
    Type: Grant
    Filed: April 3, 2017
    Date of Patent: May 4, 2021
    Assignee: UNIVERSITIES SPACE RESEARCH ASSOCIATION
    Inventors: Ramprasad Gandhiraman, Meyya Meyyappan, Jessica E. Koehne
  • Patent number: 10996136
    Abstract: An air to air refueling hose for an aircraft comprises an internal structure suitable for transporting fuel inside, an intermediate structure arranged around the internal structure, and an external structure arranged around the intermediate structure such that the intermediate structure is located between the internal structure and the external structure, and a sensing arrangement comprising electric conductors arranged along the air to air refueling hose and embedded inside of the external structure.
    Type: Grant
    Filed: June 18, 2019
    Date of Patent: May 4, 2021
    Assignee: AIRBUS DEFENCE AND SPACE, S.A.U.
    Inventor: Gonzalo Martín Gómez
  • Patent number: 10994861
    Abstract: A refueling system, comprising a drum rotatable to wind and unwind a hose, a carriage guiding the hose and lineally displaceable along a shaft parallel to the longitudinal direction of the drum so as to follow the movement of the hose along the drum. The shaft allows the displacement of the carriage along its length. A motor is coupled to the carriage and displaces the carriage along the shaft. A first position sensor communicates with the carriage to obtain its position. A second position sensor communicates with the drum to obtain the position of the hose. A control system is coupled to the first and the second sensor, to compare their obtained positions and to operate the motor.
    Type: Grant
    Filed: November 29, 2018
    Date of Patent: May 4, 2021
    Assignee: AIRBUS DEFENCE AND SPACE SAU
    Inventors: Martin Espinosa-Sanchez, Javier Valedeolmos Traba
  • Patent number: 10995780
    Abstract: An assembly for arrangement to the surface of an aerodynamic profile comprises an array of actuators, which are designed as piezo actuators and plasma actuators.
    Type: Grant
    Filed: November 30, 2017
    Date of Patent: May 4, 2021
    Assignees: Airbus Defence and Space GmbH, Airbus Operations GmbH
    Inventors: Ralf Caspari, Robert Weichwald, Emanuel Ermann, Gerd Heller, Detlev Konigorski, Stefan Schnäubelt, Nicole Jordan
  • Publication number: 20210126704
    Abstract: The present teachings is generally directed to facilitating satellite and terrestrial internet communications. In some embodiments, configuration information for configuring a communications device may be retrieved. The configuration information may be provided to the communications device, and the communications device may be caused to be configured based on the configuration information. Responsive to receiving a first data signal from a first satellite, the communications device may be configured to generate and output a second data signal based on the first data signal, the first data signal including first data encoded using one or more space-based communication protocols, and the second data including second data encoded using one or more terrestrial-based communication protocols.
    Type: Application
    Filed: October 25, 2019
    Publication date: April 29, 2021
    Applicant: ATLAS Space Operations, Inc.
    Inventor: Sean McDaniel
  • Patent number: 10991548
    Abstract: Described herein are apparatus and methods of printing in the presence of plasma. The apparatus includes a modular print head comprising an inlet module, a plasma module with movable electrode configurations, and a nozzle module. The modular design of the print head allows for printing on and treatment of surfaces in many different applications.
    Type: Grant
    Filed: July 7, 2020
    Date of Patent: April 27, 2021
    Assignee: Space Foundry Inc.
    Inventors: Ramprasad Gandhiraman, Fergal John O'Moore, Lief Niklas Dennis Nordlund, Arlene Lynette Lopez
  • Patent number: 10987755
    Abstract: The invention provides a method and apparatus for forming a freeform metal structure by wire feed additive manufacturing. In accordance with the method, a holding structure is moved in at least one moving direction, the holding structure holding the metal structure. A metal wire end is fed along an area of deposition on the metal structure in the at least one moving direction. The metal wire end is heated to a melting temperature using a heat source, with the metal wire end as melted being deposited on the metal structure as a metallic build-up material. The metallic build-up material after heating and during the cooling is subjected in the at least one moving direction behind the area of deposition to at least one pulsed magnetic field using a magnetic coil arranged after the heat source, the at least one pulsed magnetic field effecting plastic deformation of the build-up material.
    Type: Grant
    Filed: December 11, 2015
    Date of Patent: April 27, 2021
    Assignees: AIRBUS DEFENCE AND SPACE GMBH, AIRBUS OPERATIONS LIMITED
    Inventors: Claudio Dalle Donne, Christian Karch, Jonathan Meyer
  • Patent number: 10991840
    Abstract: A stacked multi-junction solar cell having a first subcell and second subcell, the second subcell having a larger band gap than the first subcell. A third subcell has a larger band gap than the second subcell, and each of the subcells include an emitter and a base. The second subcell has a layer which includes a compound formed at least the elements GaInAsP, and a thickness of the layer is greater than 100 nm, and the layer is formed as part of the emitter and/or as part of the base and/or as part of the space-charge zone situated between the emitter and the base. The third subcell has a layer including a compound formed of at least the elements GaInP, and the thickness of the layer is greater than 100 nm.
    Type: Grant
    Filed: December 12, 2016
    Date of Patent: April 27, 2021
    Assignee: AZUR SPACE Solar Power GmbH
    Inventors: Lars Ebel, Wolfgang Guter, Matthias Meusel
  • Publication number: 20210119419
    Abstract: A semiconductor layer stack, a component made therefrom, a component module, and a production method is provided. The semiconductor layer stack has at least two layers (A, B), which, as individual layers, each have an energy position of the Fermi level in the semiconductor band gap, E F - E V < E G 2 applying to the layer (A) and E L - E F < E G 2 applying to the layer (B), with EF the energy position of the Fermi level, EV the energy position of the valence band, EL the energy position of a conduction band and EL?EV the energy difference of the semiconductor band gap EG, the thickness of the layers (A, B) being selected in such a way that a continuous space charge zone region over the layers (A, B) results.
    Type: Application
    Filed: December 28, 2020
    Publication date: April 22, 2021
    Applicants: OTTO-VON-GUERICKE-UNIVERSITAET MAGDEBURG, AZUR SPACE SOLAR POWER GMBH
    Inventors: Armin DADGAR, André STRITTMATTER
  • Publication number: 20210119693
    Abstract: A system for electromagnetic wave data transmission, including a ground main information node, a communication satellite, a relay satellite, an uplink control carrier, and a relay satellite antenna unit. The ground main information node is connected to an external network by a broadband cable; and the ground main information node is connected to the communication satellite by the relay satellite. The communication satellite includes a service range of the communication satellite, and the communication satellite is separately connected to a plurality of mobile terminals and a ground data collection node. The mobile terminals and the ground data collection node are arranged within the service range of the communication satellite. The mobile terminals include data collection nodes; additionally, the ground data collection node is arranged within a service range of the ground data collection node.
    Type: Application
    Filed: August 23, 2019
    Publication date: April 22, 2021
    Applicant: XUZHOU SPACE-TIME THOUGHT INTELLIGENT TECHNOLOGY CO., LTD
    Inventor: Lianke ZHANG
  • Publication number: 20210119570
    Abstract: A method of a solar cell array arranged on the surface of a support by providing and utilizing an assembly fixture having a smooth, concave surface. An uncured supporting film composed of a composite material (such as a carbon fiber composite) is mounted directly on the back side of the solar cells; and the film of composite material is co-cured on the assembly fixture so that the array of interconnected solar cells is bonded to the supporting film. The bonded and cured film of composite material and an array of interconnected solar cells is then removed from the assembly fixture.
    Type: Application
    Filed: December 16, 2020
    Publication date: April 22, 2021
    Applicant: Vanguard Space Technologies, Inc.
    Inventors: Matthew Wrosch, Eric McNaul, Theodore Stern, Fadel Hernandez
  • Patent number: 10986636
    Abstract: A wireless communication system includes frequency reuse between terminals in common coverage regions using a multiple satellite architecture with spatial diversity. Different terminals may be associated with different ones of the satellites such that a common frequency can be reused by the different terminals. A gateway may communicate with a first satellite using a feeder beam having an overlapping geographic coverage region with a user beam used for communication between a set of user terminals and a second satellite. Spatial diversity is provided between the satellites, and the feeder beam and the user beam operate at common frequencies within the overlapping coverage region. In this manner, the bandwidth of both satellites at the common coverage region is used to increase the available capacity.
    Type: Grant
    Filed: July 9, 2019
    Date of Patent: April 20, 2021
    Assignee: Maxar Space LLC
    Inventor: Kirby Chung
  • Patent number: 10983043
    Abstract: A method for categorizing a fracture surface of a component. A digital image of the fracture surface is generated. The digital image or one or more segments of the digital image is/are analyzed, wherein a category of a fracture pattern is assigned to one or more regions of the digital image or of one or more segments based on detection and statistical evaluation of spatial distribution of the smallest homogeneous image units (pixels) or image elements, and, provided that multiple regions and/or multiple segments of the digital image were analyzed, information about the regions and/or details of the digital image and categories of fracture patterns determined and assigned to them are linked to each other, and a category is assigned to the fracture surface based on this link. The method permits automatic, self-learning-categorization of fracture surfaces, for example for series tests carried out for joining technologies.
    Type: Grant
    Filed: July 7, 2017
    Date of Patent: April 20, 2021
    Assignee: Airbus Defence and Space GmbH
    Inventors: Hauke Brüning, Robert Meissner, André Homeyer, Thomas Körwien
  • Patent number: 10981748
    Abstract: A frictionless service carriage system including: a shaft 1 having a first 2 and a second 3 helix-shaped guide in its surface, each helix shaped-guide 2, 3 defining a linear movement along the longitudinal axis of the shaft 1 of a carriage 4 in opposite directions and both helix shaped-guides 2, 3 crossing each other 2, 3 along the longitudinal axis of the shaft 1, wherein the carriage 4 includes a movable element 5 located successively in each of the helix-shaped guides 2, 3 and movable along the guides 2, 3, the movable element 5 comprising a set of rolling elements 6 along the first or second helix-shaped guide 2, 3 of the shaft 1 and configured such that in a crossing with the other helix-shaped guide 2, 3, the set of rolling elements 6 has at least two contact points with the helix-shaped guide 2, 3 for which it rolls.
    Type: Grant
    Filed: November 14, 2018
    Date of Patent: April 20, 2021
    Assignee: AIRBUS DEFENCE AND SPACE S.A.U.
    Inventors: Martin Espinosa-Sanchez, Javier Valdeolmos Traba
  • Patent number: 10986294
    Abstract: A sensing module includes a linear image sensor and an optical unit. The unit includes an optical element having a curved, outward surface and a covering on the outward surface. The covering has a slit formed therein. The optical unit faces the sensor with the slit perpendicular to a longitudinal axis of the sensor and images a wide field of view onto a single pixel of the linear sensor, wherein light impinging normal to the slit, at any location along the slit, is imaged on a central pixel of the sensor while light impinging one of a plurality of non-normal angles to the slit is imaged on an associated one of a plurality of non-central pixels of the sensor.
    Type: Grant
    Filed: September 26, 2019
    Date of Patent: April 20, 2021
    Assignee: Six Degrees Space Ltd
    Inventors: Klonymus Sholom Lieberman, Daniel Greenspan
  • Patent number: 10985288
    Abstract: 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: Grant
    Filed: September 15, 2017
    Date of Patent: April 20, 2021
    Assignee: AZUR SPACE Solar Power GmbH
    Inventors: Matthias Meusel, Gerhard Strobl, Frank Dimroth, Andreas Bett
  • Patent number: 10986641
    Abstract: A wireless communication platform utilizes flexible bandwidth assignment to re-allocate bandwidth between spot beams. The platform may assign a first combination of frequency and polarization (FP) to a first spot beam and a second combination of frequency and polarization to a second spot beam that is adjacent and at least partially overlapping the first spot beam. The platform may assign to the first spot beam a reserved combination of frequency and polarization during a first time period, and at second time, assign the reserved combination to the second spot beam. The platform may also assign the reserved combination simultaneously to adjacent spot beams by managing user of the reserved combination by geographically isolated terminals in the spot beams. The platform may further assign different portions of the reserved combination to adjacent spot beams without geographical limitations.
    Type: Grant
    Filed: October 17, 2018
    Date of Patent: April 20, 2021
    Assignee: Maxar Space LLC
    Inventor: Hampton Chan
  • Patent number: 10983139
    Abstract: A system includes a vacuum chamber to receive a laser beam and a charged nanoparticle. The nanoparticle oscillates at a trapping frequency in a focus of the laser beam. Resonant oscillation of the nanoparticle is driven by a presence of an ambient electric field adjacent to the vacuum chamber. The system also includes a controller to tune the trapping frequency of an oscillating nanoparticle to be in resonance with the ambient electric field causing on-resonant enhancement of the system; a detector to detect positional changes of the oscillating nanoparticle; and a processor to calculate an electromagnetic force of the ambient electric field based on the positional changes of the oscillating nanoparticle.
    Type: Grant
    Filed: March 5, 2020
    Date of Patent: April 20, 2021
    Assignees: Government of the United States, as represented by the Secretary of the Air Force, Utah State University Space Dynamics Laboratory
    Inventors: Sean Krzyzewski, Maxwell D. Gregoire, Brian L. Kasch