发明名称 |
REDUNDANT FUEL MANIFOLD SEALING ARRANGEMENT |
摘要 |
A fuel manifold of gas turbine engines comprises a tube for fluid communication with a fuel source and for connection with at least one fuel nozzle tip to thereby define a fuel conveying passage. There is a means for providing a redundant seal around the tube and covering substantially an entire length thereof to reduce a risk of fuel leakage of the fuel conveying passage.
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申请公布号 |
CA2558897(C) |
申请公布日期 |
2013.06.25 |
申请号 |
CA20062558897 |
申请日期 |
2006.09.07 |
申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
SHAFIQUE, HARRIS;PROCIW, LEV ALEXANDER |
分类号 |
F02C7/22;B23P15/00;F02C7/28;F23R3/28 |
主分类号 |
F02C7/22 |
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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