发明名称 Multi-role aircraft with interchangeable mission modules
摘要 A flight-operable, truly modular aircraft has an aircraft core to which one or more of outer wings members, fuselage, cockpit, leading and trailing edge couplings, and empennage and tail sections can be removably coupled and/or replaced during the operating life span of the aircraft. In preferred embodiments the aircraft core houses the propulsive engines, avionics, at least 80% of the fuel, and all of the landing gear. The aircraft core is preferably constructed with curved forward and aft composite spars, that transfer loads across the center section, while accommodating a mid-wing configuration. The aircraft core preferably has a large central cavity dimensioned to interchangeably carry an ordnance launcher, a surveillance payload, electronic countermeasures, and other types of cargo. Contemplated aircraft can be quite large, for example having a wing span of at least 80 ft.
申请公布号 US9221532(B2) 申请公布日期 2015.12.29
申请号 US201414205156 申请日期 2014.03.11
申请人 发明人 Karem Abe
分类号 B64C1/00;B64C3/56;B64C1/06;B64C39/10;B64C39/02;B64D37/00;B64C1/26 主分类号 B64C1/00
代理机构 Fish & Tsang, LLP 代理人 Fish & Tsang, LLP
主权项 1. A flight-operable, modular aircraft comprising: a center section having a cargo bay, and fore and aft spars positioned fore and aft of the cargo bay, respectively; and left and right wings that are structurally coupled together at least predominantly through the fore and aft spars; wherein the center section provides a least 25% of the lift of the aircraft during at least some portion of cruise flight the aircraft has a wing span of at least 80 ft, and has left and right wings having sufficient stiffness to produce a natural frequency of no less than 6 Hz.
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