• Patent Title: Atomizer for gas turbine engine
  • Application No.: US17791232
    Application Date: 2021-01-07
  • Publication No.: US11892167B2
    Publication Date: 2024-02-06
  • Inventor: Michael Levitsky
  • Applicant: Turbogen Ltd.
  • Applicant Address: IL Ramat Gan
  • Assignee: Turbogen Ltd.
  • Current Assignee: Turbogen Ltd.
  • Current Assignee Address: IL Ramat Gan
  • Agent Mark M. Friedman
  • International Application: PCT/IB2021/050087 2021.01.07
  • International Announcement: WO2021/148896A 2021.07.29
  • Date entered country: 2022-07-07
  • Main IPC: F23R3/12
  • IPC: F23R3/12 F23R3/28 F23R3/30
Atomizer for gas turbine engine
Abstract:
An atomizer provides a high-quality fuel-air mixture to a gas turbine engine, by combining air input from an engine compressor and fuel input from a single low-pressure fuel supply pump. The atomizer includes an atomizer body, a main vortex chamber, a secondary vortex chamber for improving quality of the fuel-air mixture, and a fuel sleeve providing fuel to the secondary vortex chamber. The main vortex chamber includes a main outlet nozzle in fluid communication with a combustion chamber inlet of the gas turbine engine. The secondary vortex chamber includes a secondary outlet nozzle in fluid communication with the main vortex chamber. The fuel sleeve has a blind channel with a longitudinal axis and a fuel tip. The same atomizer may be used for startup mode and for all operational modes of the gas turbine engine.
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