Title:
【発明の名称】高運動性航空機とその飛行方法
Document Type and Number:
Japanese Patent JP2534666
Kind Code:
B2
Abstract:
A superagile tactical fighter aircraft has articulatable air inlets (13), articulatable exhaust nozzles (14), highly deflectable canard surfaces (19), and control thruster jets (22) located around the nose (11) of the fuselage, on the top and bottom surfaces of the propulsion system near the exhaust nozzles, and on both sides of at least one vertical tail (20). The superagile aircraft attains supernormal flight by articulating the air inlets and exhaust nozzles, deflecting the canard surfaces, and vectoring the thruster jets. Supernormal flight may be defined as flight at which the superagile aircraft operates at an angle of attack much greater than the angle of attack which produces maximum lift. In supernormal flight, the superagile aircraft is capable of almost vertical ascents, sharp turns, and very steep descents without losing control.
Inventors:
TOOMASU EICHI SUTOROOMU
Application Number:
JP8196286A
Publication Date:
September 18, 1996
Filing Date:
April 09, 1986
Export Citation:
Assignee:
DAINAMITSUKU ENG INC
International Classes:
B64C5/04; B64C5/16; B64C15/02; B64C13/00; B64C15/00; B64C15/14; B64C39/12; F02K1/00; (IPC1-7): B64C15/00; B64C39/12
Domestic Patent References:
| JP5973395A | ||||
| JP51127915A | ||||
| JP51130715A | ||||
| JP4918397B1 |
Attorney, Agent or Firm:
Takehiko Suzue (2 outside)