標(biāo)準(zhǔn)號：SAE ARP 994A-2012
中文標(biāo)準(zhǔn)名稱：航空液壓傳動系統(tǒng)用管道系統(tǒng)安裝設(shè)計(jì)推薦性操作規(guī)程
英文標(biāo)準(zhǔn)名稱：Recommended Practice for the Design of Tubing Installations for Aerospace Fluid Power Systems
標(biāo)準(zhǔn)類型：V38
發(fā)布日期：2012/8/22 12:00:00
實(shí)施日期：1999/12/31 12:00:00
中國標(biāo)準(zhǔn)分類號：V38
國際標(biāo)準(zhǔn)分類號：49.080
引用標(biāo)準(zhǔn)：ASTM B 338-2010;ISO 12-1987;MIL-DTL-5541-2011;MIL-PRF-5606-2006;MIL-PRF-7808-1997;SAE AIR 737;SAE AIR 797;SAE AIR 1047;SAE AIR 1569;SAE AIR 4918-1994;SAE AIR 5386-2002;SAE AMS-S-8802-1999;SAE AMS-T-6845;SAE AMS-T-7081-1999;SAE AMS-T-8506-1999;SAE AMS 2430
適用范圍：This document is a compendium of recommended practices for the design of tubing systems that are used for the transmission of liquid and gasses in fluid power systems for aerospace vehicles such as aircraft, missiles and booster. The primary emphasis is given to recommended practices for line sizing, tube routing, supports and clamping, stress considerations and permissible defects, and provisions for flexure through the use of flexible hoses, coiled tubes, swivel joints, and expansion glands. The sections regarding rubing materials and fitting types are included for reference, but particular recommendations are purposely avoided since their selection is dependent upon the specific requirements of each particular vehicle system and many other factors. Fluid power systems are differentiated from the normal aircraft fuel and oil systems and the various fluid systems used for environmental control and air conditioning systems; however, the practices cited herein will in many cases be applicable to these other systems.