发明名称 |
COMBUSTION CHAMBER FOR AN AIRCRAFT ENGINE, AND METHOD FOR ATTACHING AN INJECTION SYSTEM IN A COMBUSTION CHAMBER OF AN AIRCRAFT ENGINE |
摘要 |
A combustion chamber in which the injection system is attached so as to prevent any axial motion of the injection system, the combustion chamber includes: a baffle including a tubular portion having a first upstream end surrounded by a first radially projecting collar; and an injection system including a bowl which includes a cylindrical portion inserted into the tubular portion, the cylindrical portion including a second upstream end surrounded by a second radially projecting collar, the second collar axially bearing against the first collar, wherein the combustion chamber includes a clamp which axially clamps the first and the second collars against one another, and a fastener which retains the clamp clamped on either side of the first and second collars.
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申请公布号 |
US2013152603(A1) |
申请公布日期 |
2013.06.20 |
申请号 |
US201113819113 |
申请日期 |
2011.08.12 |
申请人 |
BUNEL JACQUES MARCEL ARTHUR;DEMOULIN BRICE ARNAUD;DE SOUSA MARIO CESAR;SEVI GUILLAUME |
发明人 |
BUNEL JACQUES MARCEL ARTHUR;DEMOULIN BRICE ARNAUD;DE SOUSA MARIO CESAR;SEVI GUILLAUME |
分类号 |
F23R3/60;F23R3/28 |
主分类号 |
F23R3/60 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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