標(biāo)準(zhǔn)號(hào)：SAE ARP 1796A-2007
中文標(biāo)準(zhǔn)名稱(chēng)：航天器發(fā)動(dòng)機(jī)空氣釋放系統(tǒng)
英文標(biāo)準(zhǔn)名稱(chēng)：(R) Engine Bleed Air Systems for Aircraft
標(biāo)準(zhǔn)類(lèi)型：V30
發(fā)布日期：2007/3/1 12:00:00
實(shí)施日期：1999/12/31 12:00:00
中國(guó)標(biāo)準(zhǔn)分類(lèi)號(hào)：V30
國(guó)際標(biāo)準(zhǔn)分類(lèi)號(hào)：49.050
引用標(biāo)準(zhǔn)：ISO 2026-1974;RTCA DO-160;SAE AIR 1266;SAE AIR 1539-1981;SAE AIR 1826-1989;SAE ARP 699E-1997;SAE ARP 986;SAE ARP 4418-1995;ARINC 604-1;CS-25;FAR 14CFR25;FAR 14CFR121;JSSG-2009;MIL-STD-810;MS 33740
適用范圍：The purpose of this document is to provide the guidelines and recommended practices for analysis, design, and installation of aircraft engine bleed air systems. This SAE Aerospace Recommended Practice (ARP) discusses design philosophy, system and equipment requirements, installation environment and design considerations for military and commercial aircraft systems within the Air Transport Association (ATA) ATA 100 specification, Chapter 36, Pneumatic. This ATA system/chapter covers equipment used to deliver compressed air from a power source to connecting points for other systems such as air conditioning, pressurization, ice protection, cross-engine starting, air turbine motors, air driven hydraulic pumps, on board oxygen generating systems (OBOGS), on board inert gas generating systems (OBIGGS), and other pneumatic demands.