Login| Sign Up| Help| Contact|

Patent Searching and Data


Title:
【発明の名称】航空機の垂直安定板及び方向舵
Document Type and Number:
Japanese Patent JP3364720
Kind Code:
B2
Abstract:
The fin 12 has an end plate 16 mounted at its upper end and the end plate covers the upper end of the rudder, so that the rudder 14 seals against the end plate at all rudder deflections. The fin and rudder lift curved slopes are increased by the effect of the end plate 16.

Inventors:
Hyde, Leslie Ray
Application Number:
JP55892299A
Publication Date:
January 08, 2003
Filing Date:
August 03, 1999
Export Citation:
Click for automatic bibliography generation   Help
Assignee:
Airbus UK Limited
International Classes:
B64C5/06; B64C9/00; B64C5/02; (IPC1-7): B64C5/02; B64C9/00
Other References:
【文献】航空情報 臨時増刊 第2次大戦 ドイツ軍用機の全貌、[88](昭33)株式会社 酣燈社 p70
Attorney, Agent or Firm:
Takehiko Suzue (4 outside)