发明名称 |
Arrangement for a combustion chamber of a turbine engine |
摘要 |
The arrangement has an injection system associated with a circular passage hole (62) in a chamber base (16) of a combustion chamber and mounted so that the system slides diametrically with respect to the hole. A deflector has a fitting ring (64) bearing tenons (66) spaced circumferentially and projecting radially. A sleeve (48) is coaxial to the ring and bears other tenons (72) spaced circumferentially and projecting radially. The system is slidably mounted in the sleeve, and a tab is introduced in a notch (60) to prevent a rotation of the system with respect to the sleeve. Independent claims are also included for the following: (1) a sleeve forming part of a combustion chamber arrangement (2) an injection system forming part of a combustion chamber arrangement (3) a deflector forming part of a combustion chamber arrangement. |
申请公布号 |
EP1826492(B1) |
申请公布日期 |
2014.09.17 |
申请号 |
EP20070102863 |
申请日期 |
2007.02.22 |
申请人 |
SNECMA |
发明人 |
HERNANDEZ, DIDIER HIPPOLYTE;NOEL, THOMAS OLIVIER MARIE |
分类号 |
F23R3/28;F23R3/60 |
主分类号 |
F23R3/28 |
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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