Patents Assigned to Aerojet Rocketdyne of DE, Inc.
  • Patent number: 8925543
    Abstract: 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: Grant
    Filed: January 13, 2009
    Date of Patent: January 6, 2015
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventors: Andrew J. Zillmer, Alfred Little
  • Patent number: 8904752
    Abstract: 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: Grant
    Filed: February 16, 2011
    Date of Patent: December 9, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventors: Bradley C. Johnson, Randolph T. Lyda, Ryan W. Brandt, Mark J. Ricciardo
  • Patent number: 8893878
    Abstract: 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: Grant
    Filed: June 29, 2011
    Date of Patent: November 25, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventor: Kenneth M. Sprouse
  • Patent number: 8887503
    Abstract: 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: Grant
    Filed: December 13, 2011
    Date of Patent: November 18, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc
    Inventors: Chandrashekhar Sonwane, Kenneth M. Sprouse, Ganesan Subbaraman, George M. O'Connor, Gregory A. Johnson
  • Patent number: 8883007
    Abstract: A fluid separation system includes a separation membrane having a pattern of features thereon.
    Type: Grant
    Filed: December 13, 2009
    Date of Patent: November 11, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventors: Mark F. Buser, Alan B. Minick
  • Patent number: 8875510
    Abstract: 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: Grant
    Filed: May 16, 2012
    Date of Patent: November 4, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventors: Bryan William McEnerney, Andrew J. Zillmer, Charles Thomas Kudija, Jr.
  • Patent number: 8859882
    Abstract: 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: Grant
    Filed: September 30, 2008
    Date of Patent: October 14, 2014
    Assignee: 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
  • Patent number: 8858869
    Abstract: 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: Grant
    Filed: February 4, 2011
    Date of Patent: October 14, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventor: Clifford C. Bampton
  • Patent number: 8851406
    Abstract: 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: Grant
    Filed: July 31, 2012
    Date of Patent: October 7, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventors: Chandrashekhar Sonwane, Timothy Saunders, Mark Andrew Fitzsimmons
  • Publication number: 20140294695
    Abstract: 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: Application
    Filed: May 31, 2011
    Publication date: October 2, 2014
    Applicant: Aerojet Rocketdyne of DE, Inc.
    Inventors: Chandrashekhar Sonwane, Kenneth M. Sprouse
  • Patent number: 8839761
    Abstract: 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: Grant
    Filed: July 6, 2010
    Date of Patent: September 23, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventors: Alan B. Minick, Alfred Little
  • Patent number: 8835762
    Abstract: 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: Grant
    Filed: June 10, 2011
    Date of Patent: September 16, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc
    Inventors: Leo Gard, Karl Wefers
  • Patent number: 8836169
    Abstract: 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: Grant
    Filed: December 15, 2010
    Date of Patent: September 16, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventors: Cheng-Yi Lu, Kenneth John Metcalf
  • Patent number: 8833076
    Abstract: 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: Grant
    Filed: June 24, 2010
    Date of Patent: September 16, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventor: Chandrashekhar Sonwane
  • Patent number: 8814562
    Abstract: An ignition system and method of igniting the ignition system includes a main catalyst section in a staged relationship with a pilot-catalyst section to stage a decomposition though the pilot-catalyst section which preheats the main catalyst section.
    Type: Grant
    Filed: June 2, 2008
    Date of Patent: August 26, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventors: Jeff Jensen, Scott Claflin
  • Patent number: 8816639
    Abstract: A rechargeable battery assembly provides load balancing for individual battery cells making up a battery assembly. The battery assembly includes a plurality of series-connected battery cell assemblies. Each battery cell assembly includes a battery cell and a charge bypass load connected in parallel with the battery cell. A cell supervisory circuits (CSCs) and battery interface unit (BUI) interface between the battery cell assembly and a battery charge/discharge circuit to provide load balancing by comparing the voltages monitored with respect to each battery cell assembly to an end of charge voltage (EOCV) threshold and in response to the monitored voltage equaling the EOCV threshold issues a charge bypass command to the CSC to activate the charge bypass load.
    Type: Grant
    Filed: June 2, 2011
    Date of Patent: August 26, 2014
    Assignee: AeroJet Rocketdyne of DE, Inc.
    Inventors: Cheng-Yi Lu, Erich H. Soendker
  • Patent number: 8787516
    Abstract: An apparatus is provided and includes a reactor core, a boom and a shield assembly supportively interposed between the reactor core and the boom, a heat pipe disposed in thermal communication with the reactor core, a thermoelectric power converter operably coupled to the heat pipe, struts supportively coupled to the heat pipe at opposite ends of the power converter and hinge joints to rotatably couple the struts to the boom, at least one of the hinge joints being spring-loaded.
    Type: Grant
    Filed: May 5, 2011
    Date of Patent: July 22, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventors: Cheng-Yi Lu, William Determan
  • Patent number: 8783246
    Abstract: A solar receiver device includes a metal conduit and a glass container disposed around the metal conduit such that there is a space between the glass container and the conduit. A coating is disposed on the metal conduit and has a composition that includes at least one element from silicon, titanium, aluminum, barium, and samarium.
    Type: Grant
    Filed: December 14, 2009
    Date of Patent: July 22, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventors: Cheng-Yi Lu, William Determan, David Grimmett, Gregory A. Johnson
  • Patent number: 8784998
    Abstract: A structure includes a nanophase titanium node and a plurality of nanophase aluminum struts. Each of the plurality of nanophase aluminum struts is bonded to the nanophase titanium node at a weld joint.
    Type: Grant
    Filed: August 31, 2010
    Date of Patent: July 22, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventors: Daniel P. Cap, Arunabh Bhattacharya
  • Patent number: 8771604
    Abstract: A liner for use within a gasifier vessel includes a plurality of elongated channels and a plurality of ceramic sheaths. The elongated channels pass coolant through the gasifier. The ceramic sheaths surround the elongated channels.
    Type: Grant
    Filed: February 6, 2007
    Date of Patent: July 8, 2014
    Assignee: Aerojet Rocketdyne of DE, Inc.
    Inventors: Mark A. Fitzsimmons, Stephen Arthur Yows, Steven P. Fusselman