BS S 152-1975 铬-钴-钼-钒-铌耐热钢坯、棒材、锻件及零件规范(自耗电极重熔)(1000-1140MPa)(铬10.5、钴6、钼0.8、钒0.2、铌0.3)
时间:2024-05-14 11:35:20 来源: 标准资料网 作者：标准资料网 阅读：8620
【英文标准名称】:Specificationforchromium-cobalt-molybdenum-vanadium-niobiumheat-resistingsteelbillets,bars,forgingsandparts(consumableelectroderemelted)(1000-1140MPa)(Cr10.5,Co6,Mo0.8,V0.2,Nb0.3)
【原文标准名称】:铬-钴-钼-钒-铌耐热钢坯、棒材、锻件及零件规范(自耗电极重熔)(1000-1140MPa)(铬10.5、钴6、钼0.8、钒0.2、铌0.3)
【标准号】:BSS152-1975
【标准状态】:现行
【国别】:英国
【发布日期】:1975-09-30
【实施或试行日期】:1975-09-30
【发布单位】:英国标准学会(GB-BSI)
【起草单位】:BSI
【标准类型】:()
【标准水平】:()
【中文主题词】:硬度;钴钢件;飞行器部件;钢;铌钢件;耐热材料;合金钢;抗拉强度;坯锭;锻件;热处理;化学成分;航空运输工程;高合金钢;材料的机械性能;钼钢;铬钢;名称与符号;钒钢;真空冶炼;棒材
【英文主题词】:Airtransportengineering;Aircraftcomponents;Alloysteels;Bars(materials);Billets;Chemicalcomposition;Chromiumsteels;Cobaltsteels;Designations;Forgings;Hardness;Heattreatment;Heat-resistantmaterials;High-alloysteels;Mechanicalpropertiesofmaterials;Molybdenumsteels;Niobiumsteels;Steels;Tensilestrength;Vacuummelting;Vanadiumsteels
【摘要】:SpecificationforChromium-cobalt-molybdenum-vanadium-niobiumheat-resistingsteelbillets,bars,forgingsandparts(consumableelectroderemelted)(1000-1140MPa)—(Cr10.5,Co6,Mo0.8,V0.2,Nb0.3)1Inspectionandtestingprocedure2Manufacture3Chemicalcomposition4Surfacedressing5Condition6Heattreatment7Mechanicalproperties
【中国标准分类号】:H40
【国际标准分类号】:49_025_10
【页数】:8P;A4
【正文语种】:英语
【英文标准名称】:Aluminiumandaluminiumalloys-Scrap-Part12:turningsconsistingofonesinglealloy.
【原文标准名称】:铝和铝合金.废料.第12部分:一种合金组成的车床切屑
【标准号】:NFA50-110-12-2003
【标准状态】:现行
【国别】:法国
【发布日期】:2003-09-01
【实施或试行日期】:2003-09-05
【发布单位】:法国标准化协会(AFNOR)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:可锻合金;试验;再循环;铝;芯片;金属废料;铸造合金;铸铝合金;输出;铝合金;铝锻造合金;顺序示度;特性;化学成分;组分;规范(验收);熔化
【英文主题词】:
【摘要】:
【中国标准分类号】:H61
【国际标准分类号】:13_030_50;77_120_10
【页数】:8P;A4
【正文语种】:其他
Product Code:SAE ARP4925
Title:Aerospace Design and Installation of Commercial Transport Helicopter Hydraulic Systems
Issuing Committee:A-6a1 Commercial Aircraft Committee
Scope: This SAE Aerospace Recommended Practice (ARP) establishes the factors which should be considered in the design and installation of a hydraulic system fitted to a commercial transport rotorcraft. The purpose of this document is to provide in one document information and guidelines to the designers of commercial transport rotorcraft hydraulic systems and components including: a. reliability and maintainability requirements; b. federal aviation regulations (FAR) Joint Airworthiness requirements (JAR) that are applicable to hydraulic systems; and c. design and installation practices. This document applies to the hydraulic systems installed into commercial transport rotorcraft which are designed to comply with FAR and/or JAR 29 regulations.