发明名称 |
FAIRING FOR A GAS TURBINE ENGINE |
摘要 |
Gas turbine engine systems involving fairings with locating data are provided. In this regard, a representative a fairing assembly for a gas turbine engine includes: a first locating component having a leading edge, first and second sides extending from the leading edge, and a recess oriented parallel to the leading edge, the recess having a first datum surface, the first locating component being operative to be positioned between a portion of a strut and a portion of an interior surface of a fairing sheath such that the first datum surface establishes a desired orientation of the fairing sheath relative to the strut. |
申请公布号 |
EP2271830(A2) |
申请公布日期 |
2011.01.12 |
申请号 |
EP20090752535 |
申请日期 |
2009.03.18 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
LYDERS, DAVID;KLINETOB, CARL BRIAN;ALEXANDER, PHILLIP |
分类号 |
F02C7/20;F01D9/04;F01D25/28 |
主分类号 |
F02C7/20 |
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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