標準號：SAE ARP 1796A-2007
中文標準名稱：航天器發動機空氣釋放系統
英文標準名稱：(R) Engine Bleed Air Systems for Aircraft
標準類型：V30
發布日期：2007/3/1 12:00:00
實施日期：1999/12/31 12:00:00
中國標準分類號：V30
國際標準分類號：49.050
引用標準：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.