Patents Assigned to Aerojet Rocketdyne of DE, Inc.
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Patent number: 9586702Abstract: A multi-function nitrous oxide system is disclosed for producing breathing air. The system includes a nitrous oxide storage container and a nitrous oxide conversion element connected with the nitrous oxide storage container. The nitrous oxide conversion element is downstream from the nitrous oxide storage container and produces hot fluid. The system includes a breathing air storage container connected with the nitrous oxide conversion element downstream from the nitrous oxide conversion element.Type: GrantFiled: November 29, 2011Date of Patent: March 7, 2017Assignee: Aerojet Rocketdyne of DE, Inc.Inventor: Brian W. Lariviere
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Patent number: 9022742Abstract: The disclosed fluid elements include radial blades extending to trailing edges and that are integral with front and rear shrouds to provide a fluid exit. Fillets adjoin the trailing edge and the front and rear shrouds at the exit. The front and rear shrouds respectively have first and second perimeter thicknesses at the impeller outer perimeter. The first perimeter thickness is greater than the second perimeter thickness at the trailing edge and adjacent to the exit, which provides greater high cycle fatigue in the area of the fillets.Type: GrantFiled: January 4, 2012Date of Patent: May 5, 2015Assignee: Aerojet Rocketdyne of DE, Inc.Inventors: Jeff H. Miller, Kelvin Sorensen, John Fung, Thaddeus Pearce Chilcoat, Fabian Bitar
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Patent number: 8992149Abstract: Anti-rotation keys are typically used in applications where an end of a threaded stud is received in a housing, and where the opposite end of the stud projects from the housing to allow attachment of another component to the housing. Once partially received in the housing, further rotation of the stud is prevented by an anti-rotation key. The disclosed anti-rotation key is self-retaining, in that it prevents itself from “backing out” of the channel due to vibration or thermal expansion of the housing, etc., while also being removable from the channel if desired.Type: GrantFiled: September 1, 2011Date of Patent: March 31, 2015Assignee: Aerojet Rocketdyne of DE, Inc.Inventor: Alan Benjamin Christopher Dixon
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Patent number: 8987579Abstract: A power converter is provided and includes a heat collector surface, n- and p-legs formed of n- and p-type thermoelectric materials, respectively, which are each disposed in thermal communication with the heat collector surface, parallel electric busses electrically coupled to the n- and p-legs and a housing, which is electrically decoupled from the busses, to support the heat collector surface at a predefined distance from a heat pipe.Type: GrantFiled: May 5, 2011Date of Patent: March 24, 2015Assignee: Aerojet Rocketdyne of DE, Inc.Inventor: Cheng-Yi Lu
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Patent number: 8981232Abstract: A multi-layer substrate includes a ground structure, a plurality of dielectric layers on the ground structure and a plurality of conductive layers separating the plurality of dielectric layers. The conductive layers include a first conductive layer and a second conductive layer and a connection electrically coupling the first conductive layer and the second conductive layer. The first conductive layer and the ground structure are configured to define a first parasitic capacitance there between and the first conductive layer and the second conductive layer are configured to define a second, negating parasitic capacitance there between.Type: GrantFiled: June 1, 2012Date of Patent: March 17, 2015Assignee: Aerojet Rocketdyne of DE, Inc.Inventors: Thomas A. Hertel, Erich H. Soendker, Horacio Saldivar
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Patent number: 8939278Abstract: A deconsolidation device defines a flow path with an inlet which defines a first cross-section generally equivalent to a passageway cross-section of a particulate material extrusion pump and an outlet that defines a second cross-section different than the first cross-section.Type: GrantFiled: April 13, 2010Date of Patent: January 27, 2015Assignee: Aerojet Rocketdyne of DE, Inc.Inventor: Mark Andrew Fitzsimmons
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Patent number: 8925543Abstract: A heating system for heating a fluid pipe in an industrial process system includes at least one gas tank fluidically connected to a first catalyst via a gas supply pipe. A first pipe heating zone is fluidically connected to the first catalyst via a first hot gas pipe. The first pipe heating zone has at least one passage extending along a first portion of the fluid pipe, in thermal contact with the fluid pipe.Type: GrantFiled: January 13, 2009Date of Patent: January 6, 2015Assignee: Aerojet Rocketdyne of DE, Inc.Inventors: Andrew J. Zillmer, Alfred Little
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Patent number: 8904752Abstract: A cap for a liquid propellant injection assembly of a rocket engine includes a cap body and a valve assembly. The cap body extends between first and second ends. The cap body has a bore that fluidly connects one or more inlets to an outlet. The inlets are disposed in a tubular sidewall of the cap body. The outlet is disposed in the second end of the cap body. The valve assembly includes a valve cap disposed around the first end of the cap body. The valve assembly is adapted to selectively regulate flow of a propellant through the inlets in the cap body as a function of pressure exerted by the propellant against the valve assembly.Type: GrantFiled: February 16, 2011Date of Patent: December 9, 2014Assignee: Aerojet Rocketdyne of DE, Inc.Inventors: Bradley C. Johnson, Randolph T. Lyda, Ryan W. Brandt, Mark J. Ricciardo
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Patent number: 8893878Abstract: A pump system includes a pump that includes a first belt and a second belt that are spaced apart from each other to provide generally straight sides of a passage there between. There is an inlet at one end of the passage and an outlet at an opposite end of the passage, with a passage length that extends between the inlet and the outlet. The passage defines a gap distance in a width direction between the straight sides at the passage inlet. A hopper includes an interior space that terminates at a mouth at the passage inlet. At least one screw is located within the interior space of the hopper and includes a screw diameter in the width direction that is less than or equal to the gap distance.Type: GrantFiled: June 29, 2011Date of Patent: November 25, 2014Assignee: Aerojet Rocketdyne of DE, Inc.Inventor: Kenneth M. Sprouse
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Patent number: 8887503Abstract: A power plant includes a closed loop, supercritical carbon dioxide system (CLS-CO2 system). The CLS-CO2 system includes a turbine-generator and a high temperature recuperator (HTR) that is arranged to receive expanded carbon dioxide from the turbine-generator. The HTR includes a plurality of heat exchangers that define respective heat exchange areas. At least two of the heat exchangers have different heat exchange areas.Type: GrantFiled: December 13, 2011Date of Patent: November 18, 2014Assignee: Aerojet Rocketdyne of DE, IncInventors: Chandrashekhar Sonwane, Kenneth M. Sprouse, Ganesan Subbaraman, George M. O'Connor, Gregory A. Johnson
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Patent number: 8883007Abstract: A fluid separation system includes a separation membrane having a pattern of features thereon.Type: GrantFiled: December 13, 2009Date of Patent: November 11, 2014Assignee: Aerojet Rocketdyne of DE, Inc.Inventors: Mark F. Buser, Alan B. Minick
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Patent number: 8875510Abstract: A solar receiver includes a cavity that is operable to receive concentrated solar energy and a heat exchanger in thermal-receiving communication with the cavity. The heat exchanger includes a plurality of thermal capacitors. Each of the plurality of thermal capacitors has a regular geometry. The plurality of thermal capacitors defines open flow passages there between and at least two of the plurality of thermal capacitors have a different size. The plurality of thermal capacitors has a packing factor of greater than 74% with regard to the volume of the heat exchanger.Type: GrantFiled: May 16, 2012Date of Patent: November 4, 2014Assignee: Aerojet Rocketdyne of DE, Inc.Inventors: Bryan William McEnerney, Andrew J. Zillmer, Charles Thomas Kudija, Jr.
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Patent number: 8859882Abstract: A heat rejection system includes a plurality of panel subassemblies and a solid state heat pipe flex joint. Each panel subassembly includes a fin, a solid state heat pipe manifold, a first solid state heat pipe tube operatively connected to the solid state heat pipe manifold and secured to the fin, a second solid state heat pipe tube operatively connected to the solid state heat pipe manifold adjacent to the first solid state heat pipe and secured to the fin. The solid state heat pipe flex joint operably connects the solid state heat pipe manifolds of two of the plurality of panel subassemblies in a hermetically sealed configuration, and is configured to permit repositioning of the two panel subassemblies relative to each other.Type: GrantFiled: September 30, 2008Date of Patent: October 14, 2014Assignee: Aerojet Rocketdyne of DE, Inc.Inventors: Cheng-Yi Lu, James A. McClanahan, Joseph P. Carroll, William Determan, Patrick E. Frye, Charles Thomas Kudija, Rick L. Howerton, Kenneth John Metcalf, Andrew J. Zillmer
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Patent number: 8858869Abstract: A method of treating a porous work piece includes infiltrating a liquid metallic alloy into surface porosity of a work piece and isothermally solidifying the liquid metallic alloy to at least partially fill the surface porosity.Type: GrantFiled: February 4, 2011Date of Patent: October 14, 2014Assignee: Aerojet Rocketdyne of DE, Inc.Inventor: Clifford C. Bampton
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Patent number: 8851406Abstract: A pump apparatus includes a particulate pump that defines a passage that extends from an inlet to an outlet. A duct is in flow communication with the outlet. The duct includes a deconsolidator configured to fragment particle agglomerates received from the passage.Type: GrantFiled: July 31, 2012Date of Patent: October 7, 2014Assignee: Aerojet Rocketdyne of DE, Inc.Inventors: Chandrashekhar Sonwane, Timothy Saunders, Mark Andrew Fitzsimmons
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Publication number: 20140294695Abstract: An injector mixer for a gasification reactor system that utilizes reactants includes an injector body that extends between a first face and a second face. The injector body includes a first passage that extends between the first face and the second face and has a first central axis. At least one second, impinging passage extends between the first face and second face and has an associated second central axis that has an angle with the first axis. The angle satisfies mixing efficiency Equation (I) disclosed herein.Type: ApplicationFiled: May 31, 2011Publication date: October 2, 2014Applicant: Aerojet Rocketdyne of DE, Inc.Inventors: Chandrashekhar Sonwane, Kenneth M. Sprouse
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Patent number: 8839761Abstract: A rotary engine includes a first rotary unit operable to provides a first phase of compression to a fresh air charge drawn in through an inlet port to the first rotary unit. A second rotary unit in communication with the first rotary unit through a first passage, the second rotary unit operable to provide a second phase of compression to the first phase of compression, a combustion phase and a first phase of expansion, the second rotary unit in communication with the first rotary unit through a second passage such that the first rotary unit provides a second phase of expansion to the first phase of expansion and an exhaust phase that exhausts the first rotary unit via an exhaust port. A first fuel injector is in communication with the second rotary unit operable to initiate the combustion phase and a second fuel injector is in communication with the first rotary unit operable to selectively initiate augmented operation.Type: GrantFiled: July 6, 2010Date of Patent: September 23, 2014Assignee: Aerojet Rocketdyne of DE, Inc.Inventors: Alan B. Minick, Alfred Little
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Patent number: 8835762Abstract: An apparatus for electrical isolation of metallic hardware is provided and includes an item of hardware and an isolation sheet disposed in contact with the item of hardware. The isolation sheet includes first and second opposing sides at least one of which is anodized.Type: GrantFiled: June 10, 2011Date of Patent: September 16, 2014Assignee: Aerojet Rocketdyne of DE, IncInventors: Leo Gard, Karl Wefers
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Patent number: 8836169Abstract: A center-tapped solar array includes a plurality of series-connected solar cells connected between a positive terminal and a negative terminal for generating an output voltage. A center-tapped terminal connected to ground is connected to the plurality of series-connected solar cells at a midpoint between the positive and negative terminals. As a result, the positive terminal of the solar array has a positive voltage relative to ground greater than the center-tapped terminal and the negative terminal has a negative voltage relative to ground less than the center-tapped terminal.Type: GrantFiled: December 15, 2010Date of Patent: September 16, 2014Assignee: Aerojet Rocketdyne of DE, Inc.Inventors: Cheng-Yi Lu, Kenneth John Metcalf
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Patent number: 8833076Abstract: A thermal storage system includes a first tank and a second tank thermally interfaced with the first tank. A pump is connected between the first tank and the second tank to move a fluid from the first tank to the second tank. A first heat exchanger includes a heat-exchanging portion that is located within the first tank. A second heat exchanger includes another heat-exchanging portion that is located within the second tank.Type: GrantFiled: June 24, 2010Date of Patent: September 16, 2014Assignee: Aerojet Rocketdyne of DE, Inc.Inventor: Chandrashekhar Sonwane