Turbocharger control system and propeller control system by a motor
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United States of America Patent
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N/A
Issued Date -
Nov 17, 2005
app pub date -
Jun 29, 2005
filing date -
Mar 16, 2002
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
An aircraft control system includes a propeller governor in which a motor is used to apply a compression force on a speeder spring, and a turbocharger in which a motor is used to actuate a needle valve associated with a diaphragm cell. An electronic control unit may be used to control the motor in the propeller governor and the motor in the turbocharger. The integration of the propeller governor and the turbocharger into a single control system decreases the number of individual adjustments that must be performed manually by the pilot.
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