Invention Grant
- Patent Title: Turbine engine combustion assembly with a variable air supply
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Application No.: US14432855Application Date: 2013-09-17
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Publication No.: US10054056B2Publication Date: 2018-08-21
- Inventor: Bernard Joseph Jean Pierre Carrere
- Applicant: SAFRAN HELICOPTER ENGINES
- Applicant Address: FR Bordes
- Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee Address: FR Bordes
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1259288 20121001
- International Application: PCT/FR2013/052125 WO 20130917
- International Announcement: WO2014/053724 WO 20140410
- Main IPC: F02C7/20
- IPC: F02C7/20 ; F23R3/04 ; F23R3/34 ; F02C3/04 ; F02C7/22 ; F02C7/26

Abstract:
A turbine engine combustion assembly including a casing, a combustion chamber, and at least one fuel injector. The combustion chamber includes an internal wall and an external wall extending one inside the other and connected by an annular chamber base wall. The external wall of the chamber is secured to an annular external wall of the casing. The injector is attached to the annular external wall of the casing and includes a fuel ignition enclosure extending inside the casing successively through openings in the casing wall and in the external wall before opening into the chamber. At least one wall of the ignition enclosure extending between the casing wall and the combustion chamber wall includes at least one air intake port. The external wall of the combustion chamber is solidly connected to a device for plugging the air intake port according to a thermal expansion state of the combustion chamber.
Public/Granted literature
- US20150247459A1 TURBINE ENGINE COMBUSTION ASSEMBLY WITH A VARIABLE AIR SUPPLY Public/Granted day:2015-09-03
Information query
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