Title:
HELICOPTER LANDING INDUCTIVE DEVICE
Document Type and Number:
Japanese Patent JPH1067399
Kind Code:
A
Abstract:
To provide a landing inductive device which permits a pilot to identify an approach line to a landing zone easily and can attain prompt and safe landing of a helicopter.
This landing inductive device, which guides a helicopter to a landing zone indicated by a boundary light C, is provided with the first landing guide light A which illuminates the light of different color from that of the light which the boundary light C disposed so as to put the landing zone between them illuminates, and the second landing guide light B which illuminates the light of different color from that of the light which the boundary light C illuminates. Illumination from the first and second landing guide lights indicates an approach line to the landing zone.
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Inventors:
NAGATA KOJIRO
KOBAYASHI MASASHI
KOBAYASHI MASASHI
Application Number:
JP22792296A
Publication Date:
March 10, 1998
Filing Date:
August 29, 1996
Export Citation:
Assignee:
JAPAN AIRCRAFT MFG CO
International Classes:
B64F1/20; (IPC1-7): B64F1/20
Attorney, Agent or Firm:
Utaka Katsumi
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