SAE ARP 1281C-2002 (R)液压动力操作式飞机飞行控制装置执行机构的一般规范

标准号：SAE ARP 1281C-2002
中文标准名称：(R)液压动力操作式飞机飞行控制装置执行机构的一般规范
英文标准名称：(R) Actuators: Aircraft Flight Controls, Power Operated, Hydraulic, General Specification For
标准类型：V37
发布日期：2002/9/1 12:00:00
实施日期：1999/12/31 12:00:00
中国标准分类号：V37
国际标准分类号：49.080
引用标准：ASME Y14.24-1999;ASME Y14.34M-1996;ASME Y14.35M-1992;ASME Y14.35M-1997;ASME Y14.38-1999;ASME Y14.100-2000;ASTM B 381-2000;ASTM B 381-2002;ASTM D 1974-1998;ASTM E 1417-1999;ASTM E 1444-2001;MIL-A-8625-1993;MIL-PRF-83282-1997;MIL-STD-454-1992;SAE AIR 1916;S
适用范围：This aerospace recommended practice provides a framework and suggested procedures or values for requirements for the design, performance, and test of hydraulically powered servoactuators for use in aircraft flight control systems. The original version of this document was intended for military usage: consequently, the requirements still often reflect such use. However, the basic requirements of this ARP may and should be applicable to commercial usage as well, provided that appropriate considerations are given for the applicable FAR/JAR 25 regulations, hydraulic fluids, and environmental controls. This recommended practice is a guide and surrogate specification for preparing a detail specification for a particular servoactuator application.