Control lever assembly for setting engine thrust in an aircraft

Details Control lever assembly for setting engine thrust in an aircraft Control lever assembly for setting engine thrust in an aircraft

G - Physics

05

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G05G 1/04 (2006.01) B64D 31/04 (2006.01) G01D 5/34 (2006.01) G05G 7/10 (2006.01)

Patent

CA 2131578

In a control lever assembly for setting the engine thrust in an aircraft with a control lever and a thrust control signal transmitter for generating discrete thrust settings, the thrust control signal transmitter is a high-resolution digital, optical absolute angle sensor, which is rigidly coupled with the control lever. The control lever assembly provides the various discrete thrust settings, when predetermined associated output data of the digital absolute angle sensor are reached. A particularly advantageous design of the optical absolute angle sensor is described.

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