| 摘要 |
An aircraft display apparatus combines a flight path vector group with a potential thrust indicator. The display apparatus comprises a display screen and a pitch ladder symbol, a horizontal line and a flight path vector group displayed on the display screen. The flight path vector group comprises a flight path vector symbol, a potential flight path vector symbol, and a potential thrust symbol. The potential thrust symbol further comprises a thrust and drag limit symbol and at least one throttle symbol. The flight path vector group is oriented on the display screen in relation to the pitch ladder and the horizontal line. The position of the potential thrust symbol relative to the pitch ladder, flight path vector symbol and the potential flight path vector symbol represents current engine power and power limits of the aircraft.
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