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Title:
AIRCRAFT TRACTOR
Document Type and Number:
Japanese Patent JP3023947
Kind Code:
B2
Abstract:

PURPOSE: To improve reliability in warning and monitoring and further to prevent that warning or monitoring from depending on the system of an aircraft so as not to exceed a maximum allowable turnout angle in the case of guiding the aircraft with a tractor.
CONSTITUTION: A beam is flooded from transmission/reception equipment, which is arranged on a tractor 1 at a specified angle αD to the lateral axis thereof, to the body of the aircraft. The reception equipment captures and detects the maximum reflection at a prescribed angle αL. flooding the beam of the transmission equipment perpendicularly to the body of the aircraft, a measuring signal is generated and this signal is converted to a control signal by an evaluating device. Corresponding to this control signal, a switching mechanism for operating and controlling a signal generator, a detection recorder and a driving/braking device for the tractor is controlled. The turnout angle αL at the time of maximum reflection expresses a signaling angle αS corresponding to the specified angle αD.


Inventors:
Erwin Franke
Peter Meltzer
Application Number:
JP2995294A
Publication Date:
March 21, 2000
Filing Date:
February 28, 1994
Export Citation:
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Assignee:
FC International Actien Gezel Shaft
International Classes:
B64F1/10; B60P3/11; B64F1/22; G01B21/22; G01D1/18; G01S13/931; G08B21/00; G01S13/08; G01S17/933; (IPC1-7): B64F1/10
Domestic Patent References:
JP6274797A
JP51147899A
Other References:
【文献】西独国特許出願公開4106079(DE,A1)
【文献】西独国特許出願公開3808260(DE,A1)
【文献】西独国特許出願公開3534044(DE,A1)
【文献】西独国実用新案9111127(DE,B)
【文献】欧州特許出願公開370965(EP,A2)
Attorney, Agent or Firm:
Toshio Yano (2 outside)