Patents by Inventor Larry C. George

Larry C. George 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).

  • Flow sleeve impingement cooling baffles
    Patent number: 8794006
    Abstract: A combustor assembly for a turbine engine includes a combustor liner, a flow sleeve and a baffle ring. The flow sleeve surrounds the combustor liner. An annulus is formed between the flow sleeve and the combustor liner. A plurality of row of cooling holes are formed in the flow sleeve. The baffle ring radially surrounds the combustor liner and is located in the annulus.
    Type: Grant
    Filed: July 19, 2012
    Date of Patent: August 5, 2014
    Assignee: United Technologies Corporation
    Inventors: Jaisukhlal V. Chokshi, Craig F. Smith, Carlos G. Figueroa, Larry C. George
  • FLOW SLEEVE IMPINGEMENT COOLING BAFFLES
    Publication number: 20130000310
    Abstract: A combustor assembly for a turbine engine includes a combustor liner, a flow sleeve and a baffle ring. The flow sleeve surrounds the combustor liner. An annulus is formed between the flow sleeve and the combustor liner. A plurality of row of cooling holes are formed in the flow sleeve. The baffle ring radially surrounds the combustor liner and is located in the annulus.
    Type: Application
    Filed: July 19, 2012
    Publication date: January 3, 2013
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: Jaisukhlal V. Chokshi, Craig F. Smith, Carlos G. Figueroa, Larry C. George
  • Flow sleeve impingement cooling baffles
    Patent number: 8291711
    Abstract: A combustor assembly for a turbine engine includes a combustor liner, a flow sleeve and a baffle ring. The flow sleeve surrounds the combustor liner. An annulus is formed between the flow sleeve and the combustor liner. A plurality of row of cooling holes are formed in the flow sleeve. The baffle ring radially surrounds the combustor liner and is located in the annulus.
    Type: Grant
    Filed: July 25, 2008
    Date of Patent: October 23, 2012
    Assignee: United Technologies Corporation
    Inventors: Jaisukhlal V. Chokshi, Craig F. Smith, Carlos G. Figueroa, Larry C. George
  • FLOW SLEEVE IMPINGEMENT COOLILNG BAFFLES
    Publication number: 20100031666
    Abstract: A combustor assembly for a turbine engine includes a combustor liner, a flow sleeve and a baffle ring. The flow sleeve surrounds the combustor liner. An annulus is formed between the flow sleeve and the combustor liner. A plurality of row of cooling holes are formed in the flow sleeve. The baffle ring radially surrounds the combustor liner and is located in the annulus.
    Type: Application
    Filed: July 25, 2008
    Publication date: February 11, 2010
    Applicant: UNITED TECHNOLOGIES CORPORATION
    Inventors: Jaisukhlal V. Chokshi, Craig F. Smith, Carlos G. Figueroa, Larry C. George