发明名称 |
BOX WING WITH ANGLED GAS TURBINE ENGINE CORES |
摘要 |
An aircraft including a fuselage having a forward portion and an aft portion with a propulsion system mounted within the aft portion of the fuselage. A burst zone is defined that extends outward from the propulsion system. The aircraft includes a box wing extending from the aft portion of the fuselage to a forward portion of the fuselage that is disposed outside of the burst zone. |
申请公布号 |
WO2014074146(A1) |
申请公布日期 |
2014.05.15 |
申请号 |
WO2013US31211 |
申请日期 |
2013.03.14 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
CHANDLER, JESSE M.;SUCIU, GABRIEL L. |
分类号 |
B64D27/14;B64C1/00;B64C5/06 |
主分类号 |
B64D27/14 |
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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