Invention Grant
- Patent Title: Fairing for a combustion chamber end wall
- Patent Title (中): 用于燃烧室端壁的整流罩
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Application No.: US12053091Application Date: 2008-03-21
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Publication No.: US07861531B2Publication Date: 2011-01-04
- Inventor: Jacques Marcel Arthur Bunel , Mario Cesar De Sousa , Stephane Henri Guy Touchaud
- Applicant: Jacques Marcel Arthur Bunel , Mario Cesar De Sousa , Stephane Henri Guy Touchaud
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0754051 20070327
- Main IPC: F02C1/00
- IPC: F02C1/00

Abstract:
An annular fairing for covering the annular chamber end wall of a turbomachine combustion chamber, and in particular of an airplane turbojet. The fairing presents openings for passing fuel injectors that are supported by the chamber end wall. The fairing is subdivided into a plurality of adjacent sectors, each sector presenting inner and outer fastener edges capable of being fastened on either side of said chamber end wall. Each sector includes a lip on one of its side edges, which lip is connected to the remainder of the sector by a step, said lip being designed to over the side edge of the adjacent sector.
Public/Granted literature
- US20080236164A1 FAIRING FOR A COMBUSTION CHAMBER END WALL Public/Granted day:2008-10-02
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