Patents by Inventor Peter John Baron

Peter John Baron 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: 8474241
    Abstract: A gas turbine engine system includes a gas turbine engine using vaporized liquefied gas as fuel. The gas turbine engine is configured to ingest intake air from an intake port and direct exhaust gases to an exhaust port. The gas turbine engine system also includes a heat exchanger with a heat transfer fluid therein. The heat exchanger is configured to create at least a part of the fuel by heating the liquefied gas. The gas turbine engine system also includes an intake air temperature control circuit. The intake air temperature control circuit includes conduits configured to direct the heat transfer fluid to the intake port and the exhaust port. The gas turbine engine system also includes a control system configured to selectively direct the heat transfer fluid to one of the intake port and the exhaust port.
    Type: Grant
    Filed: February 29, 2008
    Date of Patent: July 2, 2013
    Assignee: Solar Turbines Inc.
    Inventors: Peter John Baron, David Anthony Pocengal, Rainer Kurz
  • Publication number: 20090321607
    Abstract: A mounting system for supporting a power system is disclosed. The mounting system may have a support structure including a first end spaced from a second end of the support structure. The mounting system may further have a first mounting assembly attached near the first end of the support structure. The first mounting assembly may have a first mounting support and a second mounting support for supporting the support structure, each of the first mounting support and the second mounting support attached to the support structure offset to a side of a longitudinal axis. The mounting system may also have a second mounting assembly attached near the second end of the support structure. The second mounting assembly may have a third mounting support attached to the support structure below the longitudinal axis for supporting the support structure. The second mounting assembly may have at least one shock absorber mounted near the third mounting support.
    Type: Application
    Filed: June 30, 2008
    Publication date: December 31, 2009
    Inventors: Peter John Baron, Martin Regis Habel
  • Publication number: 20090060725
    Abstract: A gas turbine engine system includes a gas turbine engine using vaporized liquefied gas as fuel. The gas turbine engine is configured to ingest intake air from an intake port and direct exhaust gases to an exhaust port. The gas turbine engine system also includes a heat exchanger with a heat transfer fluid therein. The heat exchanger is configured to create at least a part of the fuel by heating the liquefied gas. The gas turbine engine system also includes an intake air temperature control circuit. The intake air temperature control circuit includes conduits configured to direct the heat transfer fluid to the intake port and the exhaust port. The gas turbine engine system also includes a control system configured to selectively direct the heat transfer fluid to one of the intake port and the exhaust port.
    Type: Application
    Filed: February 29, 2008
    Publication date: March 5, 2009
    Inventors: Peter John Baron, David Anthony Pocengal, Rainer Kurz