Vertical take-off and landing aircraft

Title:

Vertical take-off and landing aircraft

Document Type and Number:

Japanese Patent JP6037100

Kind Code:

B2

Abstract:

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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Inventors:

Tsunekawa Masayoshi
Remo-con Tetsuya

Application Number:

JP2012057270A

Publication Date:

November 30, 2016

Filing Date:

March 14, 2012

Export Citation:

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Assignee:

Ihi Co., Ltd.

International Classes:

B64C29/00

Domestic Patent References:

JP59501202A

Foreign References:

DE2021043A1
US20020003188
US1551834

Attorney, Agent or Firm:

Koji Nagato
Echizen Masahiro

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