標準號：SAE ARP 1281C-2002
中文標準名稱：(R)液壓動力操作式飛機飛行控制裝置執(zhí)行機構(gòu)的一般規(guī)范
英文標準名稱：(R) Actuators: Aircraft Flight Controls, Power Operated, Hydraulic, General Specification For
標準類型：V37
發(fā)布日期：2002/9/1 12:00:00
實施日期：1999/12/31 12:00:00
中國標準分類號：V37
國際標準分類號：49.080
引用標準：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
適用范圍：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.