Patents by Inventor Avi PONCHEK

Avi PONCHEK 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: 11629666
    Abstract: A method for converting a turbofan engine including providing a turbofan engine and converting the turbofan engine. The turbofan engine includes a core engine (including at least one high pressure spool assembly and a combustion chamber), and an unmodified fan configured for providing at least a bypass flow bypassing the core engine, the fan being mechanically coupled to a low pressure turbine that is in turn driven by the core engine. The conversion includes modifying or replacing the unmodified fan to provide a modified fan, the modified fan configured for generating a reduced bypass flow with respect to said fan bypass flow during operation of the converted turbofan engine corresponding to at least one set of engine conditions, enabling said low pressure turbine to generate an excess shaft power above a baseline shaft power required for driving the modified fan during operation of the converted turbofan engine.
    Type: Grant
    Filed: February 25, 2021
    Date of Patent: April 18, 2023
    Assignee: ISRAEL AEROSPACE INDUSTRIES LTD.
    Inventors: Aviad Brandstein, Avi Ponchek
  • Publication number: 20210270209
    Abstract: A method for converting a turbofan engine including providing a turbofan engine and converting the turbofan engine. The turbofan engine includes a core engine (including at least one high pressure spool assembly and a combustion chamber), and an unmodified fan configured for providing at least a bypass flow bypassing the core engine, the fan being mechanically coupled to a low pressure turbine that is in turn driven by the core engine. The conversion includes modifying or replacing the unmodified fan to provide a modified fan, the modified fan configured for generating a reduced bypass flow with respect to said fan bypass flow during operation of the converted turbofan engine corresponding to at least one set of engine conditions, enabling said low pressure turbine to generate an excess shaft power above a baseline shaft power required for driving the modified fan during operation of the converted turbofan engine.
    Type: Application
    Filed: February 25, 2021
    Publication date: September 2, 2021
    Inventors: Aviad BRANDSTEIN, Avi PONCHEK
  • Patent number: 11053891
    Abstract: There is provided a method for converting a turbofan engine, including the step of providing a turbofan engine and the step of converting the turbofan engine to provide a converted turbofan engine. The turbofan engine includes a core engine (including at least one high pressure spool assembly and a combustion chamber), and an unmodified fan configured for providing at least a bypass flow bypassing the core engine, the fan being mechanically coupled to a low pressure turbine that is in turn driven by the core engine.
    Type: Grant
    Filed: August 31, 2014
    Date of Patent: July 6, 2021
    Assignee: ISRAEL AEROSPACE INDUSTRIES LTD.
    Inventors: Aviad Brandstein, Avi Ponchek
  • Publication number: 20160201605
    Abstract: There is provided a method for converting a turbofan engine, including the step of providing a turbofan engine and the step of converting the turbofan engine to provide a converted turbofan engine. The turbofan engine includes a core engine (including at least one high pressure spool assembly and a combustion chamber), and an unmodified fan configured for providing at least a bypass flow bypassing the core engine, the fan being mechanically coupled to a low pressure turbine that is in turn driven by the core engine.
    Type: Application
    Filed: August 31, 2014
    Publication date: July 14, 2016
    Inventors: Aviad BRANDSTEIN, Avi PONCHEK