专利名称：Vertical takeoff and landing aircraft发明人：Hideharu Kawai申请号：US10284208申请日：20021031公开号：US06892980B2公开日：20050517
专利附图：
摘要：A vertical takeoff and landing (VTOL) aircraft is superior in maneuverability,safety, and mobility. The aircraft has turbofan engines with separate core engines havingfan engines used commonly for cruising and lifting up. The thrust from the fan enginescan be directed to all directions by supporting the fan engines of the turbofan engines
with separate core engines with biaxial support so that the fan engines are rotatable inthe direction of pitching and rolling. The fan engines are mounted on both sides of eachof front and rear sings. With this construction, the VTOL aircraft can cruise and hover bytilting the fan engines about the two axes while using the fan engines commonly forcruising and hovering.
申请人：Hideharu Kawai
地址：Nagoya JP
国籍：JP
代理机构：Wenderoth, Lind & Ponack, L.L.P.
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