Autothrottle system

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

74 8921, 74491, 244234, B64C 1700

Patent

active

046519548

ABSTRACT:
An autothrottle system for an aircraft includes a throttle lever actuator which is easily retrofitted to an existing throttle quadrant and employs a D.C. stepping motor to slew the throttle levers and eliminate the need for a feedback loop.

REFERENCES:
patent: 3599510 (1971-08-01), Scott et al.
patent: 4082007 (1978-04-01), Strickland
patent: 4093158 (1978-06-01), Clews et al.
patent: 4237833 (1980-12-01), Des Lauriers

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