標準號：SAE ARP 4379A-2007
中文標準名稱：航空航天.活塞隔離開的圓柱狀液壓蓄能器
英文標準名稱：(R) Aerospace - Accumulator, Hydraulic, Cylindrical, Piston Separated
標準類型：V29
發布日期：1999/12/31 12:00:00
實施日期：1999/12/31 12:00:00
中國標準分類號：V29
國際標準分類號：49.080
引用標準：MIL-PRF-5606-2006;MIL-PRF-83282-1997;RTCA DO-160;SAE AIR 4150-1993;SAE AIR 4543-1992;SAE AMS-P-83461-1998;SAE ARP 1288;SAE ARP 1288A-1992;SAE ARP 1383B-2003;SAE ARP 4386B-2002;SAE ARP 4752-1994;SAE ARP 4925-1996;SAE AS 1241C-1997;SAE AS 4059E-2005;SAE AS
適用范圍：This SAE Aerospace Recommended Practice (ARP) is intended as a guide in defining the requirements for aerospace piston separated hydraulic accumulators, including details pertinent to the design, fabrication, and performance of the accumulator. This type of accumulator has a piston separator and contains both high-pressure gas and fluid. The accumulator is used in aerospace hydraulic systems of the following types as defined in SAE AS 5440 with design operating pressures of up to 8000 psi (55,160 kPa). Type I: -65 to +160 °F (-54 to +71 °C) fluid temperature Type II: -65 to +275 °F (-54 to +135 °C) fluid temperature For commercial aerospace or helicopter applications, the information and guidelines of SAE ARP 4752 or SAE ARP 4925 respectively, are considered.