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Title:
DEVICE FOR INCREASING PITCHING MOMENT OF AIRCRAFT
Document Type and Number:
Japanese Patent JPH07251797
Kind Code:
A
Abstract:

PURPOSE: To keep the position of an airframe by providing at the nose of the aircraft a movable control board which is longitudinally movable and which when in a forwardly projected position generates pitching moments in a direction for lifting the nose.

CONSTITUTION: During normal flight, an aircraft flies with a movable control board 2 put in a nose part 1 by an actuator 4. During a takeoff and landing at which pitching moments are generated in a direction for lowering the nose, the movable control board 2 is moved onto a rail 3 by the actuator 4 and projected diagonally upwards. At this projected position the movable control board 2 generates vortices 5 even with a small elevation angle of the takeoff or landing, thereby generating pitching moments in a direction for lifting the nose, Therefore, the pitching moments which are generated in a nose-lowering direction as when landing gear and flaps are lowered can be canceled out.


Inventors:
ABE SHIGEKI
Application Number:
JP4373694A
Publication Date:
October 03, 1995
Filing Date:
March 15, 1994
Export Citation:
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Assignee:
MITSUBISHI HEAVY IND LTD
International Classes:
B64C9/02; (IPC1-7): B64C9/02
Attorney, Agent or Firm:
Akasaka Saka (1 person outside)



 
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