Patents by Inventor Kenneth W. Cowan

Kenneth W. Cowan has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 11154073
    Abstract: Versatile temperature control systems adaptable to many different applications employ different states and proportions of a pressurized dual phase medium in direct contact with a thermal load. In one aspect of the invention, thermal energy generated by pressurization of a gaseous medium is stored at a selected temperature level so that it is later readily accessible. In addition, in accordance with the invention temperature control of a two-phase medium can be exercised across selectable dynamic ranges and with different resolutions. In accordance with such features, the control can be exerted by varying the input flow rate of a mixture applied to a thermal load, or by controlling the back pressure of the flow through the thermal load. In accordance with another feature of the invention, substantial energy conservation can be effected by employing an ambient temperature evaporator configuration between the thermal load and the input to the compressor.
    Type: Grant
    Filed: May 28, 2019
    Date of Patent: October 26, 2021
    Assignee: B/E Aerospace, Inc.
    Inventors: Kenneth W. Cowans, William W. Cowans, Glenn Zubillaga
  • Patent number: 10386101
    Abstract: In a temperature control system using a controlled mix of high temperature pressurized gas and a cooled vapor/liquid flow of the same medium to cool a thermal load to a target temperature in a high energy environment, particular advantages are obtained in precision and efficiency by passing at least a substantial percentage of the cooled vapor/liquid flow through the thermal load directly, and thereafter mixing the output with a portion of the pressurized gas flow. This “post load mixing” approach increases the thermal transfer coefficient, improves control and facilities target temperature change. Ad added mixing between the cooled expanded flow and a lesser flow of pressurized gas also is used prior to the input to the thermal load. A further feature, termed a remote “Line Box”, enables transport of the separate flows of the two phase medium through a substantial spacing from pressurizing and condensing units without undesired liquefaction in the transport lines.
    Type: Grant
    Filed: June 8, 2016
    Date of Patent: August 20, 2019
    Assignee: B/E Aerospace, Inc.
    Inventors: Kenneth W. Cowans, William W. Cowans, Glenn Zubillaga
  • Patent number: 10342241
    Abstract: A temperature control system is disclosed where thermal energy generated by pressurization of a gaseous medium is stored at a selected temperature level so that it is later readily accessible. Temperature control of a two-phase medium is exercised across selectable dynamic ranges and with different resolutions and the control can be exerted by varying the input flow rate of a mixture applied to a thermal load, or by controlling the back pressure of the flow through the thermal load.
    Type: Grant
    Filed: May 25, 2016
    Date of Patent: July 9, 2019
    Assignee: B/E Aerospace, Inc.
    Inventors: Kenneth W. Cowans, William W. Cowans, Glenn Zubillaga
  • Patent number: 10168086
    Abstract: A temperature control system employing a two-phase refrigerant and a compressor/condenser loop is disclosed wherein a two phase refrigerant condenses within the load, the system including a thermo-expansion valve that simultaneously allows refrigerant flow through the thermo-expansion valve and regulates a temperature of the refrigerant in its two phase state ahead of the thermo-expansion valve, and wherein a flow through the thermo-expansion valve occurs only after a pressure and temperature upstream of the thermo-expansion valve reaches a final temperature and pressure.
    Type: Grant
    Filed: July 9, 2014
    Date of Patent: January 1, 2019
    Assignee: B/E Aerospace, Inc.
    Inventor: Kenneth W. Cowans
  • Publication number: 20160282024
    Abstract: In a temperature control system using a controlled mix of high temperature pressurized gas and a cooled vapor/liquid flow of the same medium to cool a thermal load to a target temperature in a high energy environment, particular advantages are obtained in precision and efficiency by passing at least a substantial percentage of the cooled vapor/liquid flow through the thermal load directly, and thereafter mixing the output with a portion of the pressurized gas flow. This “post load mixing” approach increases the thermal transfer coefficient, improves control and facilities target temperature change. Ad added mixing between the cooled expanded flow and a lesser flow of pressurized gas also is used prior to the input to the thermal load. A further feature, termed a remote “Line Box”, enables transport of the separate flows of the two phase medium through a substantial spacing from pressurizing and condensing units without undesired liquefaction in the transport lines.
    Type: Application
    Filed: June 8, 2016
    Publication date: September 29, 2016
    Inventors: Kenneth W. Cowans, William W. Cowans, Glenn Zubillaga
  • Publication number: 20160262419
    Abstract: A temperature control system is disclosed where thermal energy generated by pressurization of a gaseous medium is stored at a selected temperature level so that it is later readily accessible. Temperature control of a two-phase medium is exercised across selectable dynamic ranges and with different resolutions and the control can be exerted by varying the input flow rate of a mixture applied to a thermal load, or by controlling the back pressure of the flow through the thermal load.
    Type: Application
    Filed: May 25, 2016
    Publication date: September 15, 2016
    Inventors: Kenneth W. Cowans, William W. Cowans, Glenn Zubillaga
  • Patent number: 9435255
    Abstract: One of the two combustion chambers of an internal combustion engine using variable compression ratio and fuel charge, VCRC engine, is improved. These improvements involve adding another, second combustion chamber for mixing products of the first combustion with engine air and refining the insulation of engine heat in the engine process.
    Type: Grant
    Filed: April 8, 2014
    Date of Patent: September 6, 2016
    Inventor: Kenneth W. Cowans
  • Patent number: 9416723
    Abstract: The air supply to internal combustion engines using variable compression ratio and variable fuel supply VCRC, is improved. The improvements involve increasing thermal efficiency and/or reducing production of pollutants by this engine. The improvements can also be used with other engines that are regulated by fuel supply such as two-stroke diesel engines. These improvements are directed to engines in two basic categories; those with mechanical blowers only and those with turbo charging.
    Type: Grant
    Filed: April 7, 2014
    Date of Patent: August 16, 2016
    Inventor: Kenneth W. Cowans
  • Patent number: 9372020
    Abstract: In a temperature control system using a controlled mix of high temperature pressurized gas and a cooled vapor/liquid flow of the same medium to cool a thermal load to a target temperature in a high energy environment, particular advantages are obtained in precision and efficiency by passing at least a substantial percentage of the cooled vapor/liquid flow through the thermal load directly, and thereafter mixing the output with a portion of the pressurized gas flow. This “post load mixing” approach increases the thermal transfer coefficient, improves control and facilities target temperature change. Ad added mixing between the cooled expanded flow and a lesser flow of pressurized gas also is used prior to the input to the thermal load. A further feature, termed a remote “Line Box”, enables transport of the separate flows of the two phase medium through a substantial spacing from pressurizing and condensing units without undesired liquefaction in the transport lines.
    Type: Grant
    Filed: August 23, 2013
    Date of Patent: June 21, 2016
    Assignee: B/E AEROSPACE, INC.
    Inventors: Kenneth W. Cowans, William W. Cowans, Glenn Zubillaga
  • Patent number: 9360243
    Abstract: Versatile temperature control systems adaptable to many different applications employ different states and proportions of a pressurized dual phase medium in direct contact with a thermal load. In one aspect of the invention, thermal energy generated by pressurization of a gaseous medium is stored at a selected temperature level so that it is later readily accessible. In addition, in accordance with the invention temperature control of a two-phase medium can be exercised across selectable dynamic ranges and with different resolutions. In accordance with such features, the control can be exerted by varying the input flow rate of a mixture applied to a thermal load, or by controlling the back pressure of the flow through the thermal load. In accordance with another feature of the invention, substantial energy conservation can be effected by employing an ambient temperature evaporator configuration between the thermal load and the input to the compressor.
    Type: Grant
    Filed: July 13, 2011
    Date of Patent: June 7, 2016
    Assignee: B/E Aerospace, Inc.
    Inventors: Kenneth W. Cowans, William W. Cowans, Glenn Zubillaga
  • Publication number: 20160061161
    Abstract: The air supply to internal combustion engines using variable compression ratio and variable fuel supply VCRC, is improved. The improvements involve increasing thermal efficiency and/or reducing production of pollutants by this engine. The improvements can also be used with other engines that are regulated by fuel supply such as two-stroke diesel engines. These improvements are directed to engines in two basic categories; those with mechanical blowers only and those with turbo charging.
    Type: Application
    Filed: April 7, 2014
    Publication date: March 3, 2016
    Inventor: Kenneth W. COWANS
  • Publication number: 20160053669
    Abstract: One of the two combustion chambers of an internal combustion engine using variable compression ratio and fuel charge, VCRC engine, is improved. These improvements involve adding another, second combustion chamber for mixing products of the first combustion with engine air and refining the insulation of engine heat in the engine process.
    Type: Application
    Filed: April 8, 2014
    Publication date: February 25, 2016
    Inventor: Kenneth W. COWANS
  • Patent number: 8980044
    Abstract: A plasma reactor having a reactor chamber and an electrostatic chuck having a surface for holding a workpiece inside the chamber includes inner and outer zone backside gas pressure sources coupled to the electrostatic chuck for applying a thermally conductive gas under respective pressures to respective inner and outer zones of a workpiece-surface interface formed whenever a workpiece is held on the surface, and inner and outer evaporators inside respective inner and outer zones of the electrostatic chuck and a refrigeration loop having respective inner and cuter expansion valves for controlling flow of coolant through the inner and outer evaporators respectively. The reactor further includes inner and outer zone temperature sensors in inner and outer zones of the electrostatic chuck and a thermal model capable of simulating heat transfer through the inner and outer zones, respectively, between the evaporator and the surface based upon measurements from the inner and outer temperature sensors, respectively.
    Type: Grant
    Filed: August 12, 2010
    Date of Patent: March 17, 2015
    Assignee: BE Aerospace, Inc.
    Inventors: Paul Lukas Brillhart, Richard Fovell, Hamid Tavassoli, Douglas A. Buchberger, Jr., Douglas H. Burns, Kallol Bera, Daniel J. Hoffman, Kenneth W. Cowans, William W. Cowans, Glenn W. Zubillaga, Isaac Millan
  • Publication number: 20150040586
    Abstract: In a temperature control system using a controlled mix of high temperature pressurized gas and a cooled vapor/liquid flow of the same medium to cool a thermal load to a target temperature in a high energy environment, particular advantages are obtained in precision and efficiency by passing at least a substantial percentage of the cooled vapor/liquid flow through the thermal load directly, and thereafter mixing the output with a portion of the pressurized gas flow. This “post load mixing” approach increases the thermal transfer coefficient, improves control and facilities target temperature change. Ad added mixing between the cooled expanded flow and a lesser flow of pressurized gas also is used prior to the input to the thermal load. A further feature, termed a remote “Line Box”, enables transport of the separate flows of the two phase medium through a substantial spacing from pressurizing and condensing units without undesired liquefaction in the transport lines.
    Type: Application
    Filed: August 23, 2013
    Publication date: February 12, 2015
    Applicant: BE Aerospace
    Inventors: Kenneth W. Cowans, William W. Cowans, Glenn Zubillaga
  • Publication number: 20150013366
    Abstract: A temperature control system employing a two-phase refrigerant and a compressor/condenser loop is disclosed wherein a two phase refrigerant condenses within the load, the system including a thermo-expansion valve that simultaneously allows refrigerant flow through the thermo-expansion valve and regulates a temperature of the refrigerant in its two phase state ahead of the thermo-expansion valve, and wherein a flow through the thermo-expansion valve occurs only after a pressure and temperature upstream of the thermo-expansion valve reaches a final temperature and pressure.
    Type: Application
    Filed: July 9, 2014
    Publication date: January 15, 2015
    Inventor: Kenneth W. Cowans
  • Patent number: 8801893
    Abstract: A method of transferring heat from or to a workpiece support in an RF coupled plasma reactor includes placing coolant in an internal flow channel that is located inside the workpiece support and transferring heat from or to the coolant by circulating the coolant through a refrigeration loop in which the internal flow channel of the workpiece support constitutes an evaporator of the refrigeration loop. The method further includes maintaining thermal conditions of the coolant inside the evaporator within a range in which heat exchange between the workpiece support and the coolant is primarily or exclusively through the latent heat of vaporization of the coolant.
    Type: Grant
    Filed: August 12, 2010
    Date of Patent: August 12, 2014
    Assignee: BE Aerospace, Inc.
    Inventors: Paul Lukas Brillhart, Richard Fovell, Douglas A. Buchberger, Jr., Douglas H. Burns, Kallol Bera, Daniel J. Hoffman, Kenneth W. Cowans, William W. Cowans, Glenn W. Zubillaga, Isaac Millan
  • Patent number: 8689575
    Abstract: A system for improving the thermal efficiency of a thermal control loop in which refrigerant after compression and condensation is applied to an evaporator employs a subsidiary counter-current heat exchange intercepting refrigerant flow to maintain the quality of the refrigerant by exchanging thermal energy between the input flow and the output flow from the evaporator. The same principle is effective, with particular advantage when small connections have to be made, in systems using mixed phase media and using the concept of direct energy transfer with saturated fluid.
    Type: Grant
    Filed: October 15, 2012
    Date of Patent: April 8, 2014
    Assignee: B/E Aerospace, Inc.
    Inventors: William W. Cowans, Glenn W. Zubillaga, Kenneth W. Cowans
  • Patent number: 8546267
    Abstract: A method of controlling wafer temperature in a plasma reactor by obtaining the next scheduled change in RF heat load on the workpiece, and using thermal modeling to estimate respective changes in wafer backside gas pressure and in coolant flow through a wafer support pedestal that would compensate for the next scheduled change in RF heat load, and making the respective changes in the backside gas pressure or in the coolant flow prior to the time of the next scheduled change.
    Type: Grant
    Filed: November 24, 2010
    Date of Patent: October 1, 2013
    Assignees: B/E Aerospace, Inc., Applied Materials, Inc.
    Inventors: Paul Lukas Brillhart, Richard Fovell, Douglas A. Buchberger, Jr., Douglas H. Burns, Kallol Bera, Daniel J. Hoffman, Kenneth W. Cowans, William W. Cowans, Glenn W. Zubillaga, Isaac Millan
  • Patent number: 8532832
    Abstract: In a temperature control system using a controlled mix of high temperature pressurized gas and a cooled vapor/liquid flow of the same medium to cool a thermal load to a target temperature in a high energy environment, particular advantages are obtained in precision and efficiency by passing at least a substantial percentage of the cooled vapor/liquid flow through the thermal load directly, and thereafter mixing the output with a portion of the pressurized gas flow. This “post load mixing” approach increases the thermal transfer coefficient, improves control and facilities target temperature change. Ad added mixing between the cooled expanded flow and a lesser flow of pressurized gas also is used prior to the input to the thermal load. A further feature, termed a remote “Line Box”, enables transport of the separate flows of the two phase medium through a substantial spacing from pressurizing and condensing units without undesired liquefaction in the transport lines.
    Type: Grant
    Filed: September 14, 2009
    Date of Patent: September 10, 2013
    Assignee: BE Aerospace, Inc.
    Inventors: Kenneth W. Cowans, William W. Cowans, Glenn Zubillaga
  • Patent number: 8453468
    Abstract: A system and method for controlling cooling of a thermal load having different cooling requirements in different sections based on direct thermal exchange using a two-phase refrigerant employs the pressure/temperature characteristics of the refrigerant to particular benefit for this multi-level cooling system. The two-phase refrigerant is first adjusted to have temperature/enthalpy characteristics chosen as the starting level for different cooling demands at related temperatures. After appropriate generation of a mixture of two-phase refrigerant initial reference temperature and pressure are established. Thereafter, incremental changes in the comprising hot gas and expanded cooled liquid/vapor, an temperature cooling medium area made by lowering the pressure by predetermined amounts, or alternatively by bypassing the pressure drop and proceeding to the next stage.
    Type: Grant
    Filed: March 18, 2010
    Date of Patent: June 4, 2013
    Assignee: BE Aerospace, Inc.
    Inventors: Kenneth W. Cowans, William W. Cowans, Glenn Zubillaga