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Patent Searching and Data


Title:
ELECTRIC REMOTE CONTROL AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2001/008777
Kind Code:
A1
Abstract:
An electric remote-control aircraft comprises a tail which is formed V-shape. An automatic compensation mechanism of a steering aerodynamic lift is arranged on each of the left and right sides of the tail, respectively. The automatic compensation mechanism is comprised of a left rudder surface, a right rudder-surface, a left compensation rudder-surface, and a right compensation rudder-surface. A frame is provided on each of the left and right compensation rudder-surfaces, respectively. Above the left half of the tail is provided with an arm of a wishbone, which connected to the left frame, and under the right half of the tail is provided with another arm of the wishbone, which is connected to the right frame. The wishbone is connected to a remote-control device through a steel-cable. An apron is provided on each of the stabilizers of the left and right halves of the tail and on each of the left and right rudder surfaces, respectively. A reset mechanism is arranged on each of the left and right compensation rudder surfaces, respectively.

Inventors:
TIAN YU (CN)
Application Number:
PCT/CN2000/000193
Publication Date:
February 08, 2001
Filing Date:
July 11, 2000
Export Citation:
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Assignee:
TIAN YU (CN)
International Classes:
A63H27/18; B64C5/02; B64C9/12; B64C39/02; A63H30/04; (IPC1-7): A63H27/18
Foreign References:
US4381091A1983-04-26
GB2055729A1981-03-11
DE3934840A11991-04-25
CN2253239Y1997-04-30
CN1052084A1991-06-12
CN1169935A1998-01-14
Attorney, Agent or Firm:
SHANGHAI ZHI XIN PATENT AGENT LTD. (Italy Building 446 Zhao Jia Bang Road, Shanghai 1, CN)
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