发明名称 System of attaching an injection system to a turbojet combustion chamber base
摘要 A system of attaching an injection system to a turbojet combustion chamber base. It comprises a deflector welded onto the chamber base. The deflector comprises an annular portion having an edge forming a retaining shoulder directed toward the front of the turbojet and the injection system comprises a collar on which is formed a retaining shoulder directed toward the rear of the turbojet and pressing against the retaining shoulder of the deflector.
申请公布号 US7673460(B2) 申请公布日期 2010.03.09
申请号 US20060422177 申请日期 2006.06.05
申请人 SNECMA 发明人 HERNANDEZ DIDIER HIPPOLYTE;LUNEL ROMAIN NICOLAS;PIEUSSERGUES CHRISTOPHE;PINCHON DAVID;SEVI GUILLAUME
分类号 F23R3/60 主分类号 F23R3/60
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