Patents by Inventor Joseph J. Seydel

Joseph J. Seydel 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).

  • Enhanced temperature control anti-ice nozzle
    Patent number: 10138811
    Abstract: Systems, methods, and apparatus are disclosed for preventing formation of ice on an engine. Apparatus may include a nozzle housing coupled to a compression stage of the engine and further coupled to a leading edge housing of the engine. The nozzle housing may receive gases from the compression stage of the engine. The nozzle housing may include a first nozzle that may be configured to generate a first flow pattern and may be further configured to generate a first flow of a first portion of the gases into the leading edge housing based on the first flow pattern. The nozzle housing may also include a second nozzle that includes a concentric nozzle configured to generate a second flow pattern. The second nozzle may be configured to generate a second flow of a second portion of the gases into the leading edge housing based on the second flow pattern.
    Type: Grant
    Filed: March 13, 2014
    Date of Patent: November 27, 2018
    Assignee: The Boeing Company
    Inventors: Daniel H. Gally, Joseph J. Seydel, Nyi Nyi, Tristan Wit, Joseph G. Davidson
  • ENHANCED TEMPERATURE CONTROL ANTI-ICE NOZZLE
    Publication number: 20150260099
    Abstract: Systems, methods, and apparatus are disclosed for preventing formation of ice on an engine. Apparatus may include a nozzle housing coupled to a compression stage of the engine and further coupled to a leading edge housing of the engine. The nozzle housing may receive gases from the compression stage of the engine. The nozzle housing may include a first nozzle that may be configured to generate a first flow pattern and may be further configured to generate a first flow of a first portion of the gases into the leading edge housing based on the first flow pattern. The nozzle housing may also include a second nozzle that includes a concentric nozzle configured to generate a second flow pattern. The second nozzle may be configured to generate a second flow of a second portion of the gases into the leading edge housing based on the second flow pattern.
    Type: Application
    Filed: March 13, 2014
    Publication date: September 17, 2015
    Applicant: The Boeing Company
    Inventors: Daniel H. Gally, Joseph J. Seydel, Nyi Nyi, Tristan Wit, Joseph G. Davidson