SAE ARP 1665A-1997
飞机接收机和压力骤增测试和测试方法定义

Definition of Pressure Surge Test and Measurement Methods for Receiver Aircraft

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标准号

SAE ARP 1665A-1997

发布日期

1997年

实施日期

废止日期

无

中国标准分类号

V45

国际标准分类号

49.050

发布单位

US-SAE

引用标准

SAE AS 1284 ENFEF-TM-81-03 HYTRAN Report MDCA3060 MIL-F-17874B MIL-F-87154 MIL-T-83219 NAVAIR 06-5-504 RPL-TDR-64-25

被代替标准

SAE ARP 1665-1983

适用范围

The test procedure applies to the refueling manifold system connecting the receiver aircraft fuel tanks to the refueling source fuel pump(s) for both ground and aerial refueling. The test procedure is intended to verify that the limit value surge pressure specified for the receiver fuel system is not exceeded when refueling from a refueling source which meets the requirements of AS1284 (reference 2). This recommended practice is not directly applicable to surge pressure developed during operation of an aircraft fuel system, such as initiating or stopping engine fuel feed or fuel transfer within an aircraft, or the pressure surge produced when the fuel pumps are first started to fill an empty fuel manifold.