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Title:
FLIGHT DIRECTOR DISPLAY DEVICE
Document Type and Number:
Japanese Patent JP3558278
Kind Code:
B2
Abstract:

PROBLEM TO BE SOLVED: To provide a flight director display device capable of concentratively displaying plural maneuvering commands and reducing the work load of a pilot.
SOLUTION: The flight director FD is composed of a line LA oscillated in the horizontal direction, a line LB oscillated in the direction vertical to the line LA, a line LC shorter than the line LA and passing through an upper edge of the line LB in parallel with the line LA, a line LD connecting a left end of the line LA and a left end of the line LC, and a line LE connecting a right end of the line LA and a right end of the line LC, the line LB is displayed by a broken line connecting a middle point of the line LA and a middle point of the line LC to simulate a center line of a runway, the line LD and the line LE are displayed by a wide and thick solid line to simulate a side line of the runway, and the line LA and the line LC are displayed by a solid line to simulate a front line and an end line of the runway.


Inventors:
Fujimoto Hajime
Yuichi Kumamoto
Keiji Kobayashi
Takaki Amano
Takaaki Hira
Application Number:
JP2000086909A
Publication Date:
August 25, 2004
Filing Date:
March 27, 2000
Export Citation:
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Assignee:
Kawasaki Heavy Industries, Ltd.
International Classes:
G01C23/00; B64D45/00; G08G5/00; (IPC1-7): B64D45/00; G01C23/00; G08G5/00
Domestic Patent References:
JP57045410A
Attorney, Agent or Firm:
Keiichiro Saikyo
Minetarou Hirose
Takeshi Sugiyama



 
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