VERTICAL TAKE-OFF AND LANDING DEVICE

申请号 EP13761380 申请日 2013-03-12 公开(公告)号 EP2826710A4 公开(公告)日 2015-11-11
申请人 IHI CORP; 发明人 TSUNEKAWA MASAYOSHI; TAMURA TETSUYA;
摘要 There is provided a vertical take-off and landing aircraft including: a propulsion mechanism 2 for generating lift and thrust; a power supply unit (e.g. an engine 3 as a power source) for supplying power to the propulsion mechanism 2; a main frame 4 for supporting the engine 3, a seat, and a landing undercarriage; a sub-frame 5 for supporting the propulsion mechanism 2; a frame coupling unit 6 for rotatably coupling the main frame 4 and the sub-frame 5; and a control stick 7 connected to the sub-frame 5, so that an occupant sitting on a seat 41 operates a control stick 7 thereby to move the sub-frame 5 relative to the main frame 4 so as to change the orientation of the propulsion mechanism 2.
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