Invention Grant
- Patent Title: Ring-shaped combustion chamber for a turbine engine
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Application No.: US15765823Application Date: 2016-10-04
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Publication No.: US10895383B2Publication Date: 2021-01-19
- Inventor: Stéphane Pascaud , Guillaume Taliercio
- Applicant: SAFRAN HELICOPTER ENGINES
- Applicant Address: FR Bordes
- Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee Address: FR Bordes
- Agency: Bookoff McAndrews, PLLC
- Priority: FR1559491 20151006
- International Application: PCT/FR2016/052539 WO 20161004
- International Announcement: WO2017/060605 WO 20170413
- Main IPC: F23R3/06
- IPC: F23R3/06 ; F23R3/50 ; F23R3/54 ; F23R3/26

Abstract:
An annular combustion chamber (10) having a first annular wall (12) and a second annular wall (13) that are coaxial about an axis (X), a chamber end wall (14) connecting together the first and second walls (12, 13), and a plurality of injectors (16), the first wall (12) including first air feed holes (18) downstream from the injectors (16), the combustion chamber (10) being characterized in that for at least a first one of said injectors (16), at least three of the first holes (18) sharing the first injector as their closest injector are situated at equal distances (D) from the first injector (16).
Public/Granted literature
- US20180299127A1 RING-SHAPED COMBUSTION CHAMBER FOR A TURBINE ENGINE Public/Granted day:2018-10-18
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