Patents Assigned to Space
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Patent number: 10166724Abstract: A method for providing spacers on a construction component to be adhered involves applying a planar formation, including passages, on the construction component to be adhered, and inserting a setting liquid in the passages of the planar formation, so that the liquid forms spacer on the construction component to be adhered after setting and peeling off the planar formation. The spacer ensures a predetermined minimum bondline when adhering the construction component.Type: GrantFiled: April 3, 2015Date of Patent: January 1, 2019Assignee: Airbus Defence and Space GmbHInventor: Thomas Koerwien
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Publication number: 20180374982Abstract: An optocoupler having a transmitter unit and a receiver unit being electrically isolated from each other and optically coupled with each other and integrated into a shared housing. The receiver unit includes an energy source that has a first electrical contact and a second electrical contact. The transmitter unit includes at least one first transmitter diode having a first optical wavelength and a second transmitter diode having a second optical wavelength. The first optical wavelength differing from the second optical wavelength by a difference wavelength, and the energy source of the receiving unit including two partial sources. The energy source being designed as a current source or as a voltage source, and the first partial source including a first semiconductor diode, and the second partial source including a second semiconductor diode. Each partial source having multiple semiconductor layers for each partial source being arranged in the shape of a stack.Type: ApplicationFiled: August 9, 2018Publication date: December 27, 2018Applicant: AZUR SPACE SOLAR POWER GMBHInventors: Wolfgang KOESTLER, Daniel FUHRMANN, Wolfgang GUTER, Clemens WAECHTER, Christoph PEPER
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Publication number: 20180374973Abstract: Solar cell stack comprising III-V semiconductor layers, which includes a first subcell having a first band gap and a first lattice constant and which includes a second subcell having a second band gap and a second lattice constant, and which includes an intermediate layer sequence disposed between the two solar cells. The intermediate layer sequence including a first barrier layer and a first tunnel diode and a second barrier layer, and the layers being arranged in the specified order. The tunnel diode includes a degenerate n+ layer having a third lattice constant and a degenerate p+ layer having a fourth lattice constant, the fourth lattice constant being smaller than the third lattice constant, and the first band gap being smaller than the second band gap, and the p+ layer having a different material composition than the n+ layer.Type: ApplicationFiled: June 21, 2018Publication date: December 27, 2018Applicant: AZUR SPACE Solar Power GmbHInventors: Lars EBEL, Wolfgang GUTER
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Patent number: 10161690Abstract: A multi-layer heat exchanger includes a fluid layer defined by a first sheet and a second sheet, the fluid layer configured to route a fluid in a predominant flow direction. Also included is a fluid inlet port disposed proximate an inlet end region of the fluid layer, wherein the fluid inlet port is oriented to introduce the fluid into the fluid layer in a direction substantially perpendicular to the predominant flow direction, wherein the inlet end region of the fluid layer comprises a non-linear geometry. Further included is at least one fin segment disposed between the first sheet and the second sheet, wherein the at least one fin segment includes a first plurality of apertures proximate the inlet end region.Type: GrantFiled: September 22, 2014Date of Patent: December 25, 2018Assignee: HAMILTON SUNDSTRAND SPACE SYSTEMS INTERNATIONAL, INC.Inventors: Mark A. Zaffetti, Jeremy M. Strange, Dale T. Cooke
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Patent number: 10164139Abstract: A solar cell unit having a semiconductor body formed as a solar cell and having a front side and a back side, a carrier with a top side enclosed by at least four edges, a bottom side, and a first contact surface, formed on the top side and connected to the first terminal contact, and a second contact surface, connected to the second terminal contact and spaced apart from the first contact surface, and a secondary optical element. A back side of the semiconductor body is non-positively connected to a part of the top side of the carrier. The secondary optical element guides light to the front side of the semiconductor body and at least parts of the bottom side of the secondary optical element are non-positively connected to the front side of the semiconductor body and/or to the top side of the carrier by a polymer adhesive layer.Type: GrantFiled: March 24, 2017Date of Patent: December 25, 2018Assignee: Azur Space Solar Power GmbHInventor: Ruediger Loeckenhoff
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Publication number: 20180360233Abstract: 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: ApplicationFiled: July 21, 2016Publication date: December 20, 2018Applicant: Retail Space Solutions LLCInventors: Christopher J. Turner, Craig A. Fluegge
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Patent number: 10154739Abstract: A universal front-facing merchandiser is described having a front rail having a first mating structure and a plurality of integrated pusher and divider assemblies. Each divider assembly includes a second mating structure that corresponds to and mates with the first mating structure to couple the integrated pusher and divider assemblies to the front rail. The mating structures of each pusher and divider assembly and the front rail are movable between a first position where the integrated pusher and divider assembly is coupled to and laterally movable about the front rail and is not removable from the front rail without force being applied to the integrated pusher and divider assembly and a second position where the integrated pusher and divider assembly is secured to the front rail in a desired position in a manner that hinders lateral movement of the integrated pusher and divider assembly.Type: GrantFiled: December 2, 2014Date of Patent: December 18, 2018Assignee: Retail Space Solutions LLCInventors: Christopher J. Turner, Craig A. Fluegge
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Patent number: 10155597Abstract: Disclosed is an artificial satellite including one face from the North face and the South face supporting at least one main radiator having an outer face turned towards space and an inner face opposite the outer face. The satellite includes a bearing structure carrying the North face, the South face, the East face and the West face. At least one part of the at least one main radiator protrudes from at least one face from the East face and the West face. The inner face of the at least one protruding part is covered with a high infrared emissivity material. The value of the dimension of the at least one protruding part is between 19% and 50% of the value of the distance between the East and West faces.Type: GrantFiled: August 10, 2016Date of Patent: December 18, 2018Assignee: AIRBUS DEFENCE AND SPACE SASInventors: Philippe Cael, Andrew Walker, Fabrice Mena
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Patent number: 10158335Abstract: A Gated CDS Integrator (GCI) may amplify low-level signals without introducing excessive offset and noise. The GCI may also amplify the low level signals with accurate and variable gain. The GCI may include a modulator preceding an amplifier such that offset or noise present in a signal path between the modulator and a demodulator input is translated to a higher out of band frequency, and thereafter reduced by a double sampled discrete time integrator which also reduces thermal noise. The thermal noise may also be reduced by averaging the output of the discrete time integrator.Type: GrantFiled: September 27, 2016Date of Patent: December 18, 2018Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Gerard T. Quilligan, Shahid Aslam
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Patent number: 10156094Abstract: A window covering can be configured as roll-up shade. The window covering can have a plurality of clips that are configured to be moveable from a first position in which the clips engage window covering material and a second position at which the clips do not engage the window covering material. When the clips are in the second position, the window covering material is manually adjustable from between a fully extended position to a retracted position. When the window covering material is moved to a retracted position, the lower portion of the window covering material may be rolled up upon height adjustment to form a roll of the window covering material. After the adjustment of the window covering material, the clips can be moved to their first position to engage the unrolled material to maintain a position of the rolled up material.Type: GrantFiled: January 11, 2017Date of Patent: December 18, 2018Assignee: Whole Space Industries LTDInventor: Tzu-Yen Lin
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Publication number: 20180359670Abstract: A satellite network comprises networks nodes including multiple satellites, multiple gateways, additional servers and a mobile vehicle (e.g., an aircraft). All of (or a subset) of the network nodes include switches. The network implements a software defined network that includes a mobility manager as part of the management plane, a network controller as part of the control plane, and the switches on the network nodes as the data plane. In one embodiment, the switches communicate using an Open Flow communications protocol and make routing decisions based on flow tables. The mobility manager communicates with, and manages, the switches via the network controller. The mobility manager proactively generate updates to flow tables based on satellite ephemeris data for the multiple satellites and itinerary data for the aircraft, and pushes the updates to the switches in response to determining that the aircraft needs to be handed off between satellites.Type: ApplicationFiled: June 9, 2017Publication date: December 13, 2018Applicant: SPACE SYSTEMS/LORAL, LLCInventor: Jun Fang
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Patent number: 10150263Abstract: A testing arrangement serves for controlling the manufacturing of a fiber reinforced component. The testing arrangement includes an inspection device with a sensor system, with the inspection device being configured to move on and/or above one or more material layer(s) and/or a surface of the component and to examine the material layer(s) or the surface with the sensor system. A device serves for automated manufacturing of a fiber reinforced plastic laminate. The device includes a forming tool, a laying head for automated laying of material layers in the forming tool as well as a testing arrangement.Type: GrantFiled: July 12, 2016Date of Patent: December 11, 2018Assignee: Airbus Defence and Space GmbHInventors: Daniel Bauer, Franz Engel, Tilman Orth, Christian Weimer
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Shape-variable gap covering between control surfaces and adjacent structural components on aircrafts
Patent number: 10150557Abstract: A transition piece, which can be mounted in a recess, and which can form a continuous surface from a structural component of an airplane to a control surface, which is connected to the structural component in a pivotable manner is described. The transition piece can be mounted between an edge of the structural component and a lateral edge of the control surface such that the transition piece is fastened in a pivotable manner both to the edge of the structural component and to the lateral edge of the control surface. According to an example, the transition piece has a planar design and can be deformed within said plane, that is, the transition piece can be stretched or compressed within this plane.Type: GrantFiled: January 20, 2016Date of Patent: December 11, 2018Assignee: Airbus Defence and Space GmbHInventor: Luiz Da Rocha-Schmidt -
Patent number: 10151142Abstract: A window covering can be configured to facilitate height adjustment of window covering material. In some embodiments, a handle or clips may be utilized to help maintain the position of the window covering material so that the use of an operator cord and/or exposed lift cords can be avoided or minimized.Type: GrantFiled: January 11, 2017Date of Patent: December 11, 2018Assignee: Whole Space Industries LTDInventor: Tzu-Yen Lin
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Patent number: 10150277Abstract: A connection element includes a composite component with a cured epoxy resin, a first layer including a first thermoplastic polymer and an intermediate layer arranged between the composite component and the first layer, the first layer containing both the cured epoxy resin of the composite component and the first thermoplastic polymer of the first layer. The first thermoplastic polymer has a melting point above a curing temperature of the epoxy resin and is soluble at a temperature of at least 150° C. in the epoxy resin used for producing the composite component.Type: GrantFiled: December 7, 2016Date of Patent: December 11, 2018Assignee: Airbus Defence and Space GmbHInventor: Thomas Meer
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Publication number: 20180351026Abstract: A receiver component having a number of partial voltage sources implemented as semiconductor diodes connected to one another in series, so that the number of partial voltage sources generate a source voltage, and each of the partial voltage sources has a semiconductor diode with a p-n junction, and the semiconductor diode has a p-doped absorption layer. The p absorption layer is passivated by a p-doped passivation layer with a larger band gap than the band gap of the p absorption layer, and the semiconductor diode has an n absorption layer that is passivated by an n-doped passivation layer with a larger band gap than the band gap of the n absorption layer. The partial source voltages of the individual partial voltage sources have a deviation of less than 20% from one another, and a tunnel diode is formed between each sequential pair of partial voltage sources.Type: ApplicationFiled: August 9, 2018Publication date: December 6, 2018Applicant: AZUR SPACE SOLAR POWER GMBHInventors: Clemens Waechter, Daniel Fuhrmann, Wolfgang Guter, Christoph Peper
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Publication number: 20180351020Abstract: A stacked multi-junction solar cell having a first subcell with a first band gap and a first thickness, and an additional first subcell with an additional first band gap and an additional first thickness. Each of the subcells have an emitter and a base, and a tunnel diode formed between the subcells. Light radiation passes through the first subcell before the additional first subcell. The first band gap is larger than the additional first band gap by a maximum of 0.1 eV, or the first band gap is larger than the additional first band gap by a maximum of 0.07 eV, or the first band gap is larger than the additional first band gap by a maximum of 0.04 eV, or the first band gap is larger than the additional first band gap by a maximum of 0.02 eV, or the first band gap is equal in size to the additional first band gap.Type: ApplicationFiled: August 9, 2018Publication date: December 6, 2018Applicant: AZUR SPACE SOLAR POWER GMBHInventors: Wolfgang Guter, Christoph Peper
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Patent number: D835628Type: GrantFiled: November 10, 2016Date of Patent: December 11, 2018Assignee: AIRBUS DEFENCE AND SPACE OYInventors: Mika Myllymaki, Tuomas Talvitie
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Patent number: D835629Type: GrantFiled: November 10, 2016Date of Patent: December 11, 2018Assignee: AIRBUS DEFENCE AND SPACE OYInventors: Mika Myllymaki, Tuomas Talvitie
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Patent number: D836954Type: GrantFiled: March 2, 2016Date of Patent: January 1, 2019Assignee: Retail Space Solutions LLCInventors: Christopher J. Turner, Craig A. Fluegge