Invention Grant
- Patent Title: Fuel injector for a turbine engine
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Application No.: US15026082Application Date: 2014-09-24
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Publication No.: US10563586B2Publication Date: 2020-02-18
- Inventor: Christophe Chabaille , Sébastien Loval
- Applicant: Snecma
- Applicant Address: FR Paris
- Assignee: Safran Aircraft Engines
- Current Assignee: Safran Aircraft Engines
- Current Assignee Address: FR Paris
- Agency: Blank Rome LLP
- Priority: FR1359516 20131001
- International Application: PCT/FR2014/052385 WO 20140924
- International Announcement: WO2015/049438 WO 20150409
- Main IPC: F02C7/22
- IPC: F02C7/22 ; F23R3/28

Abstract:
A fuel injector (10) such as an injector for an annular combustion chamber of a turbine engine, comprising a downstream head (16) having a central outlet (22) and an annular peripheral outlet (24) surrounding the central outlet (22), and an injector arm (12) upstream of the head (16) comprising coaxial central channel (18) and annular channel (20), characterised in that the central channel (18) is in fluid communication with the peripheral outlet (24) and the annular channel (20) is in fluid communication with the central outlet (22).
Public/Granted literature
- US20160237911A1 FUEL INJECTOR FOR A TURBINE ENGINE Public/Granted day:2016-08-18
Information query
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