| 摘要 |
A method, computer program, or apparatus for determining with various degrees of precision the power delivered by an engine and also the best possible power of the engine for the given operating conditions. Typically, this invention is for an aircraft engine. The disclosed invention uses a variety of parameters, such as the rotation rate, manifold pressure, outside air temperature, and fuel flow to calculate or approximate the power delivered by the engine and the best power available from the engine. The engine's altitude does not have to be involved in the calculations. Display of the calculated engine power is provided relative to best power and/or maximum engine power.
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