Title:
VERTICAL TAKEOFF AND LANDING AIRPLANE
Document Type and Number:
WIPO Patent Application WO/2009/149592
Kind Code:
A1
Abstract:
A vertical takeoff and landing airplane comprises a driving cabin (1), a fuselage (16), an aero-engine (10), a wing (9), a horizontal tail (7), a vertical tail (6), a reducer (13) and a control system. The aero-engine (10) is connected with the reducer (13) through a driving shaft (11) and a clutch (12). Steering vector tail propelling nozzle (8) is assembled on the back part of the aero-engine (10). A rotor wing (5) is assembled on the top of the fuselage (6), and the said rotor wing (5) is connected with a rotor wing shaft (3). The vertical takeoff and landing airplane has a retracting device (14) of the rotor wing shaft (3) and an open-close rotor wing cabin (2) which can contain the furled rotor wing (5). The said open-close rotor wing cabin (2) is located on the top of the fuselage (6). The rotor wing shaft (3) is connected with the reducer (13) and the retracting device (14) of the rotor wing shaft (3). An automatic positioning device (4) is assembled on the rotor wing (5), and an automatic positioning device (4) of the rotor wing shaft (3) is assembled on the rotor wing shaft (3).
Inventors:
ZHANG QINGLIU (CN)
Application Number:
PCT/CN2008/002094
Publication Date:
December 17, 2009
Filing Date:
December 26, 2008
Export Citation:
Assignee:
ZHANG QINGLIU (CN)
International Classes:
B64C29/00; B64C27/22
Foreign References:
| DE10241732A1 | 2004-03-25 | |||
| US6622962B1 | 2003-09-23 | |||
| US3370809A | 1968-02-27 | |||
| US2953319A | 1960-09-20 | |||
| CN1281409A | 2001-01-24 |
Attorney, Agent or Firm:
CCPIT PATENT AND TRADEMARK LAW OFFICE (Vantone New World Plaza2 Fuchengmenwai Street, Beijing 7, CN)
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