This report presents a study of an instrument that can warn the pilot of the turning of his airplane. This instrument must satisfy three conditions: 1) It must give useful indication immediately from take-off; 2) The indications must be instantaneous and require no exertion by the pilot; 3) The indicator must be sensitive only to changes of orientation in the horizontal plane. Different solutions are presented such as a gyroscope driven by the suction of a Venturi tube.
Turn indicator
Congres International de la Navigation Aerienne (1st : 1921 : Paris, France)
1922-08-01
Sonstige
Keine Angabe
Englisch
Europäisches Patentamt | 2015
|SAE Technical Papers | 1976
Emerald Group Publishing | 1931