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Patent Searching and Data


Title:
遠隔調整飛行体において速くて安定的な旋回が可能な水平尾翼の構造
Document Type and Number:
Japanese Patent JP2006518246
Kind Code:
A
Abstract:
The present invention provides a horizontal rear wing structure of a remote controlled flight assuring fast and stable turning. The horizontal rear wing structure 1000 includes a servomotor facing the upper side of the flight body D, a rotating member 220 mounted on the servomotor and a connecting part 300 mounted on the top side of the rotating member, the connecting part being combined with the horizontal rear wing. Accordingly, the horizontal rear wing 400 rotates with respect to the plane of the flight body.

Inventors:
Kim Sun-Woo
Jean Yi-Hyun
Application Number:
JP2006502704A
Publication Date:
August 10, 2006
Filing Date:
February 09, 2004
Export Citation:
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Assignee:
Nuros Company Limited
International Classes:
A63H27/28; A63H27/00; A63H27/18; A63H27/24; B64C5/02; B64C33/00; A63H30/00
Foreign References:
US2687858A1954-08-31
US1721598A1929-07-23
US1396459A1921-11-08
US1118124A1914-11-24
US3009670A1961-11-21
Attorney, Agent or Firm:
Masatsugu Suzuki
Kenichi Wakui
Norihiro Yamamoto
Kazunaga Suzuki