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首页> 外文期刊>Journal of Computer and Systems Sciences International >Determination of Energetic Characteristics of Servo Actuators of Electric Hydrostatic Servo Drives of Aircraft
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Determination of Energetic Characteristics of Servo Actuators of Electric Hydrostatic Servo Drives of Aircraft

机译：飞机电动静液压伺服驱动器伺服驱动器能量特性的确定

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摘要

In this paper, relations for calculating the energetic characteristics of servo actuators of electrohy-drostalic servo drives of aircraft are obtained. The relations are considered for determining the power consumed by an servo actuator for realization of static regimes of drive operation, as well as the harmonic law of drive motion. These regimes are typical for technical specifications for designing control surface actuators. A particular example of the parametric synthesis of an actuator of the drive is presented. The result of calculation by the obtained expressions is compared with the results of simulating the energetic consumption of the drive. The obtained results can be considered as source data for forming the requirements for an onboard energetic system when the electrohydrostatic control surfaces are employed.
机译：本文获得了计算飞机电液伺服驱动器伺服驱动器能量特性的关系式。考虑这些关系以确定伺服致动器消耗的功率，以实现驱动操作的静态状态以及驱动运动的谐波定律。这些规范对于设计控制表面执行器的技术规范来说是典型的。给出了驱动器的致动器的参数综合的特定示例。将获得的表达式的计算结果与模拟驱动器能量消耗的结果进行比较。当使用静电静力控制表面时，获得的结果可以视为形成车载高能系统要求的源数据。

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