Invention Grant
- Patent Title: Fuel injector for a turbine engine
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Application No.: US14506914Application Date: 2014-10-06
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Publication No.: US09857080B2Publication Date: 2018-01-02
- Inventor: Christophe Chabaille , Sebastien Christophe Loval
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1359730 20131008
- Main IPC: F23R3/28
- IPC: F23R3/28 ; F02C7/232 ; F23K5/14

Abstract:
A fuel injector for a turbine engine is provided. The fuel injector includes a body including an admissions chamber for admitting fuel under pressure, a stop valve mounted in the body downstream from the admission chamber and designed to open at a first determined fuel pressure and to remain open beyond that first pressure in order to feed a primary fuel circuit, and a metering valve mounted in the body downstream from the stop valve and designed to open above a second determined fuel pressure, greater than the first pressure, and to remain open above the second pressure in order to feed a secondary fuel circuit. The stop valve and the metering valve form a common movable assembly.
Public/Granted literature
- US20150096301A1 FUEL INJECTOR FOR A TURBINE ENGINE Public/Granted day:2015-04-09
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