Title:
【発明の名称】ジェットフラップ推進式航空機
Document Type and Number:
Japanese Patent JP2000506466
Kind Code:
A
Abstract:
PCT No. PCT/IB95/00818 Sec. 371 Date Mar. 23, 1998 Sec. 102(e) Date Mar. 23, 1998 PCT Filed Sep. 29, 1995 PCT Pub. No. WO97/12804 PCT Pub. Date Apr. 10, 1997In an aircraft (1) according to the invention the engine drives a blower and the compressed air is used to increase the lift of the wing (18) and the canard (22) using jet flap propulsion. The airfoil profile has maximum thickness just forward of the control surface device (12) which has large included trailing edge angle and large leading edge radius. The control surface device hinge (17) is positioned close to the mean line (19) of the plane, and air slots (10) in the plane are blowing the control surface device.
Inventors:
Arnason, Christian
Application Number:
JP51409197A
Publication Date:
May 30, 2000
Filing Date:
September 29, 1995
Export Citation:
Assignee:
Bergfredistofa Christians Arnasonard
International Classes:
B64C9/38; B64C21/04; B64C39/12; (IPC1-7): B64C9/38; B64C21/04; B64C39/12
Attorney, Agent or Firm:
Takashi Ishida (3 others)