Patents by Inventor Metin Talan

Metin Talan 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).

  • Two-shaft engine for aircraft with high electric power demand
    Patent number: 8522526
    Abstract: With an engine for aircraft with high electric power demand, the power of the low-pressure shaft (7) operating in a lower speed range is transmitted to the high-pressure shaft (6) by an electromagnetic clutch (10). In the clutch element (14) on the side of the low-pressure shaft a frequency-controllable rotary field is generated, which drives a magnet (13) connected to the high-pressure shaft.
    Type: Grant
    Filed: June 1, 2007
    Date of Patent: September 3, 2013
    Assignee: Rolls-Royce Deutschland Ltd & Co.
    Inventor: Metin Talan
  • Gas turbine with at least one multi-stage compressor unit including several compressor modules
    Patent number: 8251639
    Abstract: A gas turbine includes at least one multi-stage compressor unit 2, with the compressor unit 2 including several, independent compressor modules 3-5, which, independently of each other, are rotatably borne on a drive shaft 1 and are each engageable with the drive shaft 1 by at least one clutch unit 9-11.
    Type: Grant
    Filed: June 17, 2009
    Date of Patent: August 28, 2012
    Assignee: Rolls-Royce Deutchland Ltd Co KG
    Inventor: Metin Talan
  • GAS TURBINE WITH AT LEAST ONE MULTI-STAGE COMPRESSOR UNIT INCLUDING SEVERAL COMPRESSOR MODULES
    Publication number: 20100000198
    Abstract: A gas turbine includes at least one multi-stage compressor unit 2, with the compressor unit 2 including several, independent compressor modules 3-5 which, independently of each other, are rotatably borne on a drive shaft 1 and are each engageable with the drive shaft 1 by variable transmission 9-11.
    Type: Application
    Filed: July 6, 2009
    Publication date: January 7, 2010
    Applicant: Rolls-Royce Deutschland Ltd & Co KG
    Inventor: Metin TALAN
  • GAS TURBINE WITH AT LEAST ONE MULTI-STAGE COMPRESSOR UNIT INCLUDING SEVERAL COMPRESSOR MODULES
    Publication number: 20090314003
    Abstract: A gas turbine includes at least one multi-stage compressor unit 2, with the compressor unit 2 including several, independent compressor modules 3-5, which, independently of each other, are rotatably borne on a drive shaft 1 and are each engageable with the drive shaft 1 by at least one clutch unit 9-11.
    Type: Application
    Filed: June 17, 2009
    Publication date: December 24, 2009
    Inventor: Metin TALAN
  • Two-shaft engine for aircraft with high electric power demand
    Publication number: 20070277532
    Abstract: With an engine for aircraft with high electric power demand, the power of the low-pressure shaft (7) operating in a lower speed range is transmitted to the high-pressure shaft (6) by an electromagnetic clutch (10). In the clutch element (14) on the side of the low-pressure shaft a frequency-controllable rotary field is generated, which drives a magnet (13) connected to the high-pressure shaft.
    Type: Application
    Filed: June 1, 2007
    Publication date: December 6, 2007
    Inventor: Metin Talan