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WAY AND ADJUSTMENT ELEMENT OF THE TARGET VALUE OF THE PARAMETER THAT AFFECT ON GAS-TURBINE ENGINE DRAFT

机译:影响燃气轮机工程参数的目标值的方法和调整要素

摘要

FIELD: engines and pumps.;SUBSTANCE: there is a way of target value adjustment of at least one parameter that affect on a draft of a gas-turbine engine that sets in motion an air vehicle during the air vehicle flight stage. It comprises: a stage at which one obtains a current value of at least one engine target variable, a stage at which one derives a decrement value for the at least one noted parameter from the predetermined table; the noted parameter is connected with the current value of at a minimum one mentioned engine target variable. The method also comprises a stage at which one regulates target value of at least one noted parameter by virtue of applying the decrement value to this parameter. The decrement value is derived from the table. Besides, the appliance for the gas-turbine engine draft control is presented. It sets in motion an air vehicle during the flight stage. The appliance also regulates the target value for at least one parameter that affect on the noted draft which is regulated with the aid of the claimed adjustment method.;EFFECT: invention allows to reduce the air vehicle draft by simultaneous numerous target values adjustment without being limited to one particular engine type.;9 cl, 4 dwg
机译:领域:有一种方法,其目标是至少调节一个参数的目标值,该目标参数会影响在飞机飞行阶段使飞机运动的燃气涡轮发动机的吃水深度。它包括:一个阶段,在该阶段中,获得至少一个发动机目标变量的当前值;在该阶段,其从预定表中导出至少一个所述参数的减量值;所述参数与至少一个提到的发动机目标变量的当前值相关。该方法还包括一个阶段,在该阶段,通过将减量值应用于该参数来调节至少一个所述参数的目标值。减量值是从表中得出的。此外,介绍了用于燃气涡轮发动机吃水控制的设备。它在飞行阶段使飞机飞行。该设备还调节至少一个影响所述吃水深度的参数的目标值,该参数借助于要求保护的调节方法进行调节。效果:本发明允许通过同时进行多个目标值调节而减少飞行器吃水深度,而不受限制到一种特定的发动机类型。; 9 cl,4 dwg

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