首页> 外文会议>International Conference on Aerospace Technology, Communications and Energy Systems >Derated Thrust:Method Analysis for Optimizing Turbofan Engine Takeoff Performances(SFC,EGT)Due to Lower Maximum Takeoff Weight(MTOW)Requirement
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Derated Thrust:Method Analysis for Optimizing Turbofan Engine Takeoff Performances(SFC,EGT)Due to Lower Maximum Takeoff Weight(MTOW)Requirement

机译:降级推力:用于优化涡轮机发动机起飞表演(SFC,EGT)的方法分析,由于较低的起飞重量(MTOW)要求

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Reduced thrust or derate has been practiced commonly nowadays as a standard procedure of takeoff.Since power is being used at maximum during takeoff phase,the practice has many benefits for the operation of aircraft.Not only it reduced fuel consumption during the takeoff phase,but also reduced engine's wear and tear that caused by stress and a very high temperature.Exhaust Gas Temperature(EGT)is one of the most important parameters that used to monitor the engine deterioration.There is a definite correlation between reducing takeoff thrust and EGT reduction,where both values are contradicting one another.However,there must be some calculation by the flight crew on how much percentage of derate is eligible prior to takeoff.The goal of this paper is to find the effectiveness of derate to reduce EGT in order to improve performance,prolong engine life and reduce operating costs of the operators.
机译:现在,推力或乏味通常作为起飞的标准程序。在起飞阶段最多使用时,该实践具有许多对飞机运行的好处。只有它在起飞阶段时才能降低燃料消耗,但是 还减少了由应力和非常高的温度引起的发动机的磨损和撕裂。Apthause气体温度(EGT)是用于监测发动机恶化的最重要参数之一。还原起飞推力和EGT之间的明确相关性, 如果两个值都相互矛盾。无论何种价值,飞行机组人员都必须有一些乏味百分比在起飞之前有资格计算的。本文的目标是找到逃号的有效性,以减少EGT以改善 性能,延长发动机寿命,降低运营商的运营成本。

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