標(biāo)準(zhǔn)號(hào)：SAE ARP 584C-2012
中文標(biāo)準(zhǔn)名稱：飛機(jī)液壓裝置用耐腐蝕鋼尾管
英文標(biāo)準(zhǔn)名稱：Coiled Tubing, Corrosion Resistant Steel, Hydraulic Applications, Aerospace
標(biāo)準(zhǔn)類型：V21
發(fā)布日期：2012/1/17 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)：V21
國(guó)際標(biāo)準(zhǔn)分類號(hào)：49.080
引用標(biāo)準(zhǔn)：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
適用范圍：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.