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autothrottle
An autothrottle (automatic throttle) allows a pilot to control the power setting of an aircraft's engines by specifying a desired flight characteristic, rather than manually controlling the fuel flow. These systems can conserve fuel and extend engine life by metering the precise amount of fuel required to attain a specific target indicated air speed, or the assigned power for different phases of flight. A/T and AFDS (Auto Flight Director Systems) work together to fulfill the whole flight plan and greatly reduce the pilots' work load.
==Working modes==
There are two parameters that an A/T (autothrottle) can maintain, or try to attain: speed and thrust.
In speed mode the throttle is positioned to attain a set target speed. This mode controls aircraft speed within safe operating margins. For example, if the pilot selects a target speed which is slower than stall speed, or a speed faster than maximum speed, the autothrottle system will maintain a speed closest to the target speed that is within the range of safe speeds.
In the thrust mode the engine is maintained at a fixed power setting according to the different flight phases. For example, during takeoff, A/T maintains constant takeoff power until takeoff mode is finished. During climb, A/T maintains constant climb power; in descent, A/T retards the throttle to IDLE position, and so on. When A/T is working in thrust mode, speed is controlled by pitch (or the control column), and NOT protected by A/T. A radar altimeter feeds data to the autothrottle mostly in this mode. (In Boeing it feeds data to the autothrottle every time. See below.)
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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