標(biāo)準(zhǔn)號(hào)：SAE AIR 1277B-2005
中文標(biāo)準(zhǔn)名稱：軍用航空電子設(shè)備的冷卻
英文標(biāo)準(zhǔn)名稱：(R) Cooling of Military Avionic Equipment
標(biāo)準(zhǔn)類型：V40
發(fā)布日期：2005/2/1 12:00:00
實(shí)施日期：1999/12/31 12:00:00
中國(guó)標(biāo)準(zhǔn)分類號(hào)：V40
國(guó)際標(biāo)準(zhǔn)分類號(hào)：49.060
引用標(biāo)準(zhǔn)：STANAG 2895-1990;MIL-HDBK-217-1991;SAE AIR 1168/10-1992;SAE AIR 1706;SAE AIR 1811-1985;SAE AIR 1812-1985;SAE AIR 1823;SAE AIR 1957-2002;SAE ARP 217;AFGS-87145;AR 70-38;JSSG-2009;MIL-E-18927;MIL-HDBK-175;MIL-HDBK-251;MIL-HDBK-310;MIL-HDBK-454;MIL-HDBK-781
適用范圍：This SAE Aerospace Information Report (AIR) contains information on the thermal design requirements of airborne avionic systems used in military airborne applications. Methods are explored which are commonly used to provide thermal control of avionic systems. Both air and liquid cooled systems are discussed. This document describes guidelines for the configuration and design of military aircraft subsystems that provide cooling to airborne avionic systems and recommendations for the basic cooling concepts, analytical methods and design practices used for the thermal design of those airborne avionic systems. The efficient design of the interface between the airframe system and the avionic system is considered.