Invention Grant
- Patent Title: Atomizer for gas turbine engine
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Application No.: US17791232Application Date: 2021-01-07
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Publication No.: US11892167B2Publication 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

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.
Public/Granted literature
- US20220364731A1 ATOMIZER FOR GAS TURBINE ENGINE Public/Granted day:2022-11-17
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