Patents Assigned to Space
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Patent number: 11083425Abstract: A wheel alignment guide that provides a visual indication of the desired placement of an apparatus. The wheel alignment guide includes a body having an opening disposed therein. The wheel alignment guide is configured to surround a portion of the apparatus, such as a wheel, via the opening. In addition, the wheel alignment guide is adapted to rest on a ground surface, being held in place via a charge, such as an electrostatic charge created by static cling vinyl. A wheel of a medical device is disposed within the opening of the wheel alignment guide after a desired position of the medical device is selected. If the medical device is moved during a medical procedure, the medical device may be repositioned due to the placement of the wheel alignment guide. Accordingly, the wheel alignment guide eliminates the need for inefficient markers and potentially-dangerous adhesives, particularly in an operating room.Type: GrantFiled: June 28, 2018Date of Patent: August 10, 2021Assignee: The Parking Space, LLCInventors: Graig Thomas O'Brien, Jon Kimball
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Patent number: 11079568Abstract: A payload module (1) of a stratospheric drone including: a casing (10), and a piece of optical equipment (20) comprising an optical axis, mounted in the casing, wherein the module being includes a mirror (40) positioned on the optical axis facing the optical equipment, the mirror being swivelable about at least one axis, within an angular range, wherein the casing has a through-opening (11) shaped so that any light ray received or emitted by the optical equipment parallel to the optical axis and reflected by the mirror passes through the through-opening, over the entire angular range of the mirror.Type: GrantFiled: November 20, 2018Date of Patent: August 3, 2021Assignee: Airbus Defence and Space SASInventors: Pierre-Luc Georgy, Pere Roca
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Patent number: 11081615Abstract: A protection method for through-holes of a semiconductor wafer having the steps: providing a semiconductor wafer, and comprising a plurality of solar cell stacks, wherein each solar cell stack has a Ge substrate forming a bottom side of the semiconductor wafer, a Ge subcell, and at least two III-V subcells in the order mentioned, as well as at least one through-hole, extending from the top side to the bottom side of the semiconductor wafer, with a continuous side wall and a circumference that is oval in cross section; applying a photoresist layer to a top side of the semiconductor wafer and to at least one region of the side wall of the through-hole, said region adjoining the top side, and applying an organic filler material by means of a printing process to a region of the top side, said region comprising the through-hole, and into the through-hole.Type: GrantFiled: August 31, 2020Date of Patent: August 3, 2021Assignee: AZUR SPACE Solar Power GmbHInventors: Alexander Frey, Benjamin Hagedorn
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Patent number: 11077607Abstract: Additive manufacturing devices operable in various external force environments are disclosed. In an aspect, an additive manufacturing device operable in microgravity is disclosed. In other aspects, devices which are operable in high-vibration environments or varying external force environments are disclosed. Additive manufacturing devices herein may produce parts from metal, polymer, or other feedstocks.Type: GrantFiled: July 15, 2014Date of Patent: August 3, 2021Assignee: MADE IN SPACE, INC.Inventors: Michael Snyder, Jason Dunn, Michael Chen, Aaron Kemmer, Noah Paul-Gin, Matthew Napoli, Eddie Gonzalez, Michael Pless
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Patent number: 11081775Abstract: A deployable structure includes a plurality of interconnected elongated support members, deployed from a stowed state to an expanded state in which the support members are arranged in a ring. Each support member is provided with a connector (28) for longitudinal movement during deployment with respect to the support member. An actuating support member (27) has a drive member (50) for longitudinal movement with respect to the actuating support member, and an electromagnetic device arranged to drive the drive member in one direction with respect to the actuating support member. The drive member is connected to the connector by a lost motion connector, thus the connector is capable of moving in said one direction even if the drive member is not moved by the electromechanical device.Type: GrantFiled: January 30, 2018Date of Patent: August 3, 2021Assignee: OXFORD SPACE SYSTEMS LIMITEDInventors: Juan Reveles-Wilson, Vincent Fraux, Martin Humphries
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Patent number: 11075384Abstract: A battery cell includes an anode, a cathode, and a separator between the anode and the cathode, wherein at least one of the anode or the cathode includes at least a carbon fiber ply comprising carbon fibers, the carbon fiber ply having a thickness of less than 90 micrometers. Also disclosed are a battery and an aircraft including such battery cell, and a method for manufacturing such battery cell.Type: GrantFiled: November 20, 2018Date of Patent: July 27, 2021Assignees: Airbus Defence and Space GmbH, Airbus Operations GmbHInventors: Peter Linde, Leif Asp, Dan Zenkert, Maciej Wysocki, Fredrik Ohlsson, Christian Metzner
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Patent number: 11073306Abstract: A lens, a solar cell unit including the lens and a joining method for the solar cell unit, wherein the lens has a main body with a substantially planar base, a receiving surface opposite the base, a side surface area connecting the base and the receiving surface and an optical axis extending perpendicular to the base and at least one bulge is arranged on the main body of the lens at a first height above the base on the side surface area.Type: GrantFiled: March 21, 2019Date of Patent: July 27, 2021Assignee: AZUR SPACE Solar Power GmbHInventor: Ruediger Loeckenhoff
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Patent number: 11072410Abstract: A balloon system including a balloon, and optionally including a payload and/or a safety module. A balloon, preferably including a balloon envelope and one or more passive vents, and optionally including one or more active valves. A method of balloon system operation, preferably including maintaining a zero-pressure balloon condition and sealing balloon vents, and optionally including ascending, descending, and/or otherwise operating the balloon system in flight.Type: GrantFiled: February 1, 2021Date of Patent: July 27, 2021Assignee: Space Perspective Inc.Inventor: Taber MacCallum
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Patent number: 11067341Abstract: A heat transfer device is disclosed having a housing including a first main wall and a second main wall, the housing having a sealed internal cavity, a liquid contained in the internal cavity, and a mixer able to set the liquid in motion, the heat transfer device being able to be switched between a first state and a second state in which the liquid is in motion and transfers heat by convection between the first main wall and the second main wall, the thermal conductance between the first main wall and the second main wall in the first state being four times less than the thermal conductance between the first main wall and the second main wall in the second state.Type: GrantFiled: March 13, 2018Date of Patent: July 20, 2021Assignee: AIRBUS DEFENCE AND SPACE SASInventor: Andrew Walker
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Patent number: 11064817Abstract: A product display tray is provided including one or more arms including engagement members. The product display tray can also include a base having one or more tracks receiving the one or more arms, wherein the base is slidable along the one or more arms from a first position to a second position. The product display tray can also include a handle. The product display tray can also include a latch, wherein the latch is operably connected to the handle, wherein the latch has an engaged position and a disengaged position, and wherein the latch is in the engaged position when the base is in the first position and the base is operable to enter the second position when the latch is in the disengaged position.Type: GrantFiled: July 21, 2016Date of Patent: July 20, 2021Assignee: Retail Space Solutions LLCInventors: Christopher J. Turner, Craig A. Fluegge
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Patent number: 11069087Abstract: A method for locating a three-dimensional target with respect to a vehicle is disclosed including capturing an image of the target, and from a three-dimensional mesh of the target, and from an estimation of the pose of the target, determining a set of projecting edges of the mesh of the target in the pose. The step of determining the projecting edges of the mesh of the target includes positioning the mesh of the target according to the pose, projecting in two dimensions the mesh so positioned, scanning the projection of the mesh in a plurality of scanning rows and, for each scanning row: defining a set of segments, each segment corresponding to the intersection of a face of the mesh with the scanning row and being defined by its ends, analyzing the relative depths of the ends of the segments, the depth being the position along a third dimension orthogonal to the two dimensions of the projection, in order to select a set of end points of segments corresponding to projecting edges of the mesh.Type: GrantFiled: December 19, 2018Date of Patent: July 20, 2021Assignee: AIRBUS DEFENCE AND SPACE SASInventors: Roland Brochard, Cyril Robin
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Publication number: 20210214081Abstract: A device for accommodating and deploying at least one payload on a flying machine includes at least one housing. The housing includes at least two opposite first side surfaces which extend over at least a portion of a length of a payload to be accommodated. The payload to be accommodated is releasably held between the two first side surfaces of the housing. The housing is at least partially arranged in a cavity on an outer surface of a flying machine. The cavity includes at least one outwardly open first opening, and the housing can be at least partially moved out of the cavity for deploying and/or receiving the payload to be accommodated.Type: ApplicationFiled: January 13, 2021Publication date: July 15, 2021Applicant: Airbus Defence and Space GmbHInventor: Ralf Schlüter
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Publication number: 20210214660Abstract: A system adapted for growing and harvesting algae and for obtaining products thereof adapted for domestic use, comprises a Photo-bioreactor adapted for use in a home environment, said Photo-bioreactor being controlled by a CPU control unit, said Photo-bioreactor being coupled to a Separation Harvesting and Extraction Unit (SEU), adapted to receive algae from said Photo-bioreactor as an input, and to generate therefrom an algal paste, said SEU being in turn coupled to an extraction unit adapted to receive said paste and to extract a desired material therefrom, said system being controlled and monitored by a CPU control unit.Type: ApplicationFiled: June 6, 2019Publication date: July 15, 2021Applicant: Shalem for Space Industries Ltd.Inventor: Jacob GURMAN
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Patent number: 11062099Abstract: A system includes a plurality of radiofrequency identification (RFID) tags including a first RFID tag. The first RFID tag is configured to perform RFID tag operations that include acquiring one or more samples using a sensor of the first RFID tag. The RFID tag operations also include writing the one or more samples in a memory of the first RFID tag. The RFID tag operations also include transferring custody of the one or more samples to a first RFID reader on request. The system also includes a plurality of RFID readers including the first RFID reader. The first RFID reader is configured to perform RFID reader operations including reading an identifier from each of the plurality of RFID tags in view of the first RFID reader during an inventory management mode.Type: GrantFiled: October 29, 2020Date of Patent: July 13, 2021Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Raymond S Wagner, Patrick W Fink, David S. Hafermalz
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Patent number: 11060483Abstract: A rocket engine with an improved solid fuel segment mainly comprises a combustion chamber, a solid fuel segment installed in the combustion chamber, and an oxidizer injector installed at one end of the combustion chamber. The solid fuel segment surrounds and forms a trajectory to allow the oxidizer injector to inject oxidizer into the trajectory, in particular, on the solid fuel segment is formed with a plurality of protrusions, between the each two protrusions are defined a recess, a flame holding hot-gas region is formed between the protrusion and the recess, so as to produce eddy current in the flame holding hot-gas region when the propellant mixture is burned inside the trajectory, such that the whole solid fuel segment can produce even regression rate and high combustion efficiency.Type: GrantFiled: March 12, 2019Date of Patent: July 13, 2021Assignee: Taiwan Innovative Space, Inc.Inventor: Yen-Sen Chen
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Patent number: 11063170Abstract: A two-step hole etching method including: providing a semiconductor wafer which has a plurality of solar cell stacks and performing a first and a second processing step. In the first processing step, a first resist layer is applied to a top surface of the semiconductor wafer, at least a first opening is produced in the first resist layer and, via a first etching process, a hole which extends beyond a p/n junction of the Ge sub-cell into the semiconductor wafer is produced in the area of the first opening. In the second process step a second resist layer is applied to the top surface of the semiconductor wafer, a second opening greater than the first opening and surrounding the hole is produced in the second resist layer, and, the hole is widened in an area which extends to the Ge sub-cell serving as an etch stop layer.Type: GrantFiled: August 31, 2020Date of Patent: July 13, 2021Assignee: AZUR SPACE Solar Power GmbHInventor: Wolfgang Koestler
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Patent number: 11058990Abstract: A system and method for removing one or more predetermined gases from an environment is herein disclosed. An embodiment of the system and method will now be described. A means for conveying a fluid and a means for flowing the fluid is combined with adsorber and desorber sections. The fluid flows in the means for conveying the fluid by the means for flowing the fluid. Comparably, the fluid flows in the adsorber and desorber sections not by the means for flowing the fluid, but rather by capillary action. In the adsorber section, the environment is in direct contact with the fluid. The fluid is capable for adsorbing one or more gases from the environment. The fluid exits the adsorber section and subsequently flows into the desorber section. The desorber section is self-contained wherein an inner portion of the desorber section is not in direct contact with the environment. In the desorber section, the one or more gases are desorbed from the fluid into the inner portion of the desorber section.Type: GrantFiled: June 24, 2019Date of Patent: July 13, 2021Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Tanya K. Rogers, John Graf, Mark Weislogel
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Publication number: 20210210267Abstract: An electropermanent magnet array is provided. The electropermanent magnet array includes one or more of a plurality of electropermanent magnets, arranged in a parallel fashion, a plurality of switching circuits, each switching circuit coupled to a different electropermanent magnet of the plurality of electropermanent magnets, and a control circuit, coupled to the plurality of switching circuits. The control circuit is configured to receive commands to control the plurality of switching circuits to demagnetize the plurality of electropermanent magnets, magnetize the plurality of electropermanent magnets to produce a first magnetic field with a strength and an attraction distance and magnetize the plurality of electropermanent magnets to produce a second magnetic field with a lower strength and greater attraction distance than the first magnetic field.Type: ApplicationFiled: March 25, 2021Publication date: July 8, 2021Applicant: Altius Space Machines Inc.Inventor: Andreas Jochum
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Publication number: 20210210649Abstract: 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: ApplicationFiled: March 23, 2021Publication date: July 8, 2021Applicant: AZUR SPACE Solar Power GMBHInventors: Matthias MEUSEL, Gerhard STROBL, Frank DIMROTH, Andreas BETT
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Patent number: 11056801Abstract: Embodiments of present disclosure are directed to apparatuses, systems, and methods relating to antenna apertures in phased array antenna systems directed to configuring antenna lattices in a space tapered configuration and mapping from the antenna lattices, interspersing of antenna elements in an antenna aperture, and rotation of antenna element in the antenna aperture for purity polarization.Type: GrantFiled: February 14, 2019Date of Patent: July 6, 2021Assignee: Space Exploration Technologies Corp.Inventors: Alireza Mahanfar, Javier Rodriguez De Luis, Nil Apaydin, Ersin Yetisir, Shaya Karimkashi Arani