Patents by Inventor Jason F. Joel

Jason F. Joel 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: 11473527
    Abstract: Systems and methods are provided for an aircraft propulsor with a fan cowl with one or more tangential restraints. The tangential restraints may be configured to enter respective tangential receiving portions of a fixed portion of the aircraft propulsor. The fan cowl may receive a load that may include a bending load. The tangential restraints may be configured to convert the bending load to membrane tension and thus decrease deflection of the fan cowl. The fan cowl may be a translating sleeve used for a reverse thrust.
    Type: Grant
    Filed: March 16, 2020
    Date of Patent: October 18, 2022
    Assignee: The Boeing Company
    Inventor: Jason F. Joel
  • Publication number: 20200284221
    Abstract: Systems and methods are provided for an aircraft propulsor with a fan cowl with one or more tangential restraints. The tangential restraints may be configured to enter respective tangential receiving portions of a fixed portion of the aircraft propulsor. The fan cowl may receive a load that may include a bending load. The tangential restraints may be configured to convert the bending load to membrane tension and thus decrease deflection of the fan cowl. The fan cowl may be a translating sleeve used for a reverse thrust.
    Type: Application
    Filed: March 16, 2020
    Publication date: September 10, 2020
    Inventor: Jason F. Joel
  • Patent number: 10589868
    Abstract: Systems and methods are provided for an aircraft propulsor with a fan cowl with one or more tangential restraints. The tangential restraints may be configured to contact one or more tangential receiving portions of a fixed portion of the aircraft propulsor. The fan cowl may receive a load that may include a bending load. The tangential restraints may be configured to convert the bending load to membrane tension and thus decrease deflection of the fan cowl.
    Type: Grant
    Filed: September 28, 2016
    Date of Patent: March 17, 2020
    Assignee: The Boeing Company
    Inventor: Jason F. Joel
  • Publication number: 20180086473
    Abstract: Systems and methods are provided for an aircraft propulsor with a fan cowl with one or more tangential restraints. The tangential restraints may be configured to contact one or more tangential receiving portions of a fixed portion of the aircraft propulsor. The fan cowl may receive a load that may include a bending load. The tangential restraints may be configured to convert the bending load to membrane tension and thus decrease deflection of the fan cowl.
    Type: Application
    Filed: September 28, 2016
    Publication date: March 29, 2018
    Inventor: Jason F. Joel
  • Patent number: 9623977
    Abstract: A hybrid structure comprises a metallic built-up sandwich structure, and a monolithic superplastic formed and diffusion bonded structure joined to the built-up sandwich structure.
    Type: Grant
    Filed: March 20, 2014
    Date of Patent: April 18, 2017
    Assignee: The Boeing Company
    Inventors: Max R. Runyan, Daniel G. Sanders, Jack W. Mauldin, Brent C. Ludwig, John M. Comfort, Larry D. Hefti, Jason F. Joel
  • Publication number: 20150266586
    Abstract: A hybrid structure comprises a metallic built-up sandwich structure, and a monolithic superplastic formed and diffusion bonded structure joined to the built-up sandwich structure.
    Type: Application
    Filed: March 20, 2014
    Publication date: September 24, 2015
    Applicant: The Boeing Company
    Inventors: Max R. Runyan, Daniel G. Sanders, Jack W. Mauldin, Brent C. Ludwig, John M. Comfort, Larry D. Hefti, Jason F. Joel