发明名称 |
STABILIZER SACRIFICIAL SURFACES |
摘要 |
<p>An aircraft assembly is disclosed and includes a fuselage including a turbine engine mounted within the aft fuselage. A burst zone is defined about the turbine engine and a tail is disposed at least partially with the burst zone. The tail includes primary control surfaces and sacrificial control surfaces. The sacrificial control surfaces can break away in a defined manner to maintain integrity of the primary control surfaces outside of the burst zone.</p> |
申请公布号 |
WO2014074149(A1) |
申请公布日期 |
2014.05.15 |
申请号 |
WO2013US32028 |
申请日期 |
2013.03.15 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
CHANDLER, JESSE M.;SUCIU, GABRIEL L. |
分类号 |
B64C5/02 |
主分类号 |
B64C5/02 |
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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