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. A redundant seal is provided around the tube and covers substantially an entire length thereof to reduce a risk of fuel leakage of the fuel conveying passage.
|
申请公布号 |
US7559201(B2) |
申请公布日期 |
2009.07.14 |
申请号 |
US20050220849 |
申请日期 |
2005.09.08 |
申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
PROCIW LEV ALEXANDER;SHAFIQUE HARRIS |
分类号 |
F02C1/00 |
主分类号 |
F02C1/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|