SAE ARP 584C-2012 飞机液压装置用耐腐蚀钢尾管

标准号：SAE ARP 584C-2012
中文标准名称：飞机液压装置用耐腐蚀钢尾管
英文标准名称：Coiled Tubing, Corrosion Resistant Steel, Hydraulic Applications, Aerospace
标准类型：V21
发布日期：2012/1/17 12:00:00
实施日期：1999/12/31 12:00:00
中国标准分类号：V21
国际标准分类号：49.080
引用标准：SAE AIR 1379;SAE AMS-T-6845;SAE ARP 4146-1990;SAE ARP 4752-1994;SAE ARP 4925-1996;SAE AS 5440-1998;SAE AS 33611-1997
适用范围：This SAE Aerospace Recommended Practice (ARP) addresses the design, installation and testing of coiled tube assemblies ranging from 1/4 inch (6.3 mm) to 1.0 inch (25 mm) diameter using CRES tubing per AMS-T-6845, unless otherwise approved by Procuring Activity. This ARP specifically details three different configurations of coiled tubing. These configurations should be compatible with pressure levels up to 3000 psi (20.7 MPa) upon the completion of the analysis for the actual stress and life requirement of the intended application. However, formal qualification tests are recommended to verify the satisfactory installation, clamping, and the life of each unique design.