发明授权
US07673460B2 System of attaching an injection system to a turbojet combustion chamber base 有权
将喷射系统附接到涡轮喷气燃烧室基座的系统

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.
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