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
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