标准摘要
[中文适用范围]： 本文件规定了可变排量单向和双向液压马达的一般要求，适用于压力高达 35000 kPa (5000 psi) 的飞机液压系统。 这些要求包括： ——设计要求； ——测试要求。 本文件涵盖了主要和辅助功能电机（参见第 4 条）；然而，具有内部旋转角度限制的执行器和低速电机不包括在内。 本文档旨在与每个应用程序特有的详细规范结合使用。 [外文原描述]： This document establishes the general requirements for variable displacement uni-directional and bi-directional hydraulic motors, suitable for use in aircraft hydraulic systems at pressures up to 35 000 kPa (5 000 psi). These requirements include: — design requirements; — test requirements. Primary and secondary function motors (see Clause 4) are covered in this document; however, actuators with internal rotation angle limits and low-speed motors are not covered. This document is intended to be used in conjunction with the detail specification that is particular to each application.
英文名称Aerospace fluid systems and components — Variable displacement hydraulic motors — General specifications