49.025.01 航空航天制造用材料综合 标准查询与下载

LST EN 4632-004-2012 航空航天系列 航空航天结构材料的焊接性和钎焊性 第004部分：高合金钢均质组件的焊接和钎焊

Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 004: Welding and brazing of homogeneous assemblies of high alloyed steels

DS/EN 4050-3:2012 航空航天系列金属材料试验方法棒材、板材、锻坯和锻件的超声波检验第3部分：标准试块

This European Standard specifies the requirements for the manufacture, checking and marking of the series of ultrasonic testing reference blocks containing flat bottom holes (FBH) which define the indicated defect size to which reference is made in EN sta

Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 3: Reference blocks

DS/EN 4050-2:2012 航空航天系列金属材料试验方法棒材、板材、锻坯和锻件的超声波检验第2部分：试验性能

This European Standard specifies the method of performing ultrasonic testing. The general requirements are given in EN 4050 1.

Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 2: Performance of test

DS/EN 4268:2012 航空航天系列金属材料热处理设备一般要求

This European Standard covers the general requirements for heat treatment facilities processing semi-finished products and parts in metallic aerospace materials.It defines the terms used herein and describes the test procedures and requirements for mandat

Aerospace series - Metallic materials - Heat treatment facilities - General requirements

DS/EN 4050-4:2012 航空航天系列金属材料试验方法棒材、板材、锻坯和锻件的超声波检验第4部分：验收准则

This European Standard specifies the acceptance criteria for products ultrasonically inspected in accordance with EN 4050 1.

Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria

DS/EN 4050-1:2012 航空航天系列金属材料试验方法棒材、板材、锻坯和锻件的超声波检验第1部分：一般要求

This European Standard defines the ultrasonic inspection procedure for rolled, drawn, extruded and forged billets, bars and plates, rolled rings and forgings with a uniform square, rectangular or round cross section. It does not cover critical rotating pa

Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 1: General requirements

EN 4632-004:2012 航空航天系列.可焊性材料.航空航天结构- 004部分:焊接和钎焊高合金钢均匀总成

This European Standard specifies the weldability and brazeability of materials or material families used in the aerospace industry. It comprises a series of sheets, by materials or material family, which: indicate the main titles, the typical chemical composition and the main characteristics, contain recommendations for welding and brazing, indicate a degree of weldability or brazeability for a given process under defined conditions, indicate a value for the welded joint mechanical resistance coefficient for each welding process when extracted from relevant bibliographical references. Joint coefficient is the ratio of stress resistance transversally to welded joint over tensile strength of parent alloy. It recommends ISO/TR 17671-3 and EN 1011-3 for pre-heating conditions specially for the welding of martensitic steels. These conditions depend on the line energy of welding, thickness, arc welding process and of hydrogen rate in filler metal. It applies unreservedly to the manufacturing of new parts or for repair.

Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 004: Welding and brazing of homogeneous assemblies of high alloyed steels

DS/EN 4678:2011 航空航天系列 航空航天结构用焊件和钎焊件 激光束焊接金属材料接头 焊件质量

This standard defines the rules to be observed to ensure the quality of aerospace structures in metallic materials by (solid code 521 and gas code 522 and diode laser Semi-conductor 523 according to EN ISO 4063:2009) laser beam welding, implemented automatically, semi-automatically or manually.It is applicable without any restriction for the manufacturing of new parts or repair parts, these operations being under the responsibility of an approved Design Authority or repairer.

Aerospace series - Weldments and brazements for aerospace structures - Joints of metallic materials by laser beam welding - Quality of weldments

SAE AMS3175A-2011 非铬酸盐表面预处理涂装前

This specification establishes the performance requirements for non-chromated materials used for surface preparation of metallic aircraft surfaces prior to applying organic coatings. Pretreatment materials qualified to this specification may be used on metallic surfaces that are subsequently painted. These include, but are not limited to, external and internal aircraft surfaces,off-aircraft part surfaces, and aircraft surfaces undergoing touch-up/repairs.

Non-Chromated Surface Pretreatment Prior to Painting

DS/EN 3873:2010 航空航天系列金属材料试验方法用角裂（CC）试件测定疲劳裂纹扩展率

This standard specifies the requirements for determining fatigue crack growth rates using the corner-crack (CC) test piece. Crack development is measured using a potential-drop system, and the calculated crack depths can be corrected via marker bands created on the fracture surface during the test. Results are expressed in terms of the crack-tip stress-intensity range (deltaK), with crack depths and test stress level noted.

Aerospace series - Test methods for metallic materials - Determination of fatigue crack growth rates using Corner-Cracked (CC) test pieces

DIN EN 4632-005:2010 航空航天系列.航空航天结构用焊接及铜焊组件.材料的可焊接性和可铜焊接性.第005部分:耐热镍基或钴基合金均匀组件.德文和英文版本EN 4632-005-2009

Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 005: Homogeneous assemblies of heat resisting Ni or Co base alloys; German and English version EN 4632-005:2009

NF L06-380-005*NF EN 4632-005:2010 航空航天系列.航空航天结构用材料的可焊接性和可铜焊性.第005部分:耐热Ni或Co基合金的类似组件.

Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 005 : homogeneous assemblies of heat resisting Ni or Co base alloys.

DIN EN 4632-003:2010 航空航天系列.航空航天结构用焊接及铜焊组件.材料的可焊接性和可铜焊接性.第003部分:非合金和低合金钢均质装配的焊接和钎焊.德文和英文版本EN 4632-003-2010

Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 003: Welding and brazing of homogeneous assemblies of unalloyed and low alloy steels; German and English version EN 4632-003:2010

BS EN 4632-005:2009 航空航天系列.航空航天结构用材料的可焊接性和可铜焊性.耐热Ni 或Co基合金的类似组件

This European Standard defines degrees of weldability and brazeability for materials or families of materials used in the aerospace industry. It comprises a series of sheets, by materials or by material family, which:  indicate the main titles, the chemical composition and the main characteristics;  contain recommendations for welding and brazing;  indicate a degree of weldability or brazeability for a given process under defined conditions;  indicate a value of the mechanical strength coefficient of the welded joint for each welding process, when it could be extracted from bibliographic references referring to it. The joint coefficient is expressed as a ratio of the tensile strength of the welded joint to the tensile strength of the base alloy (to be in accordance with EN 4632-002). It is applicable without restriction for the manufacturing of new parts or for repair.

Aerospace series - Weldability and brazeability of materials in aerospace constructions - Homogeneous assemblies of heat resisting Ni or Co base alloys

BS EN 4632-005:2010 航空航天系列 航空航天结构用材料的可焊接性和可铜焊性 耐热Ni 或Co基合金的类似组件

Aerospace series. Weldability and brazeability of materials in aerospace constructions. Homogeneous assemblies of heat resisting Ni or Co base alloys

LST EN 4632-005-2010 航空航天系列 航空航天结构中材料的可焊性和可钎焊性 第005部分：耐热镍基或钴基合金的均质组件

Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 005: Homogeneous assemblies of heat resisting Ni or Co base alloys

BS 4HR 100:2010+A1:2012 航空航天系列.可锻耐热合金的检验、试验和验收用规程

Aerospace series. Procedure for inspection, testing and acceptance of wrought heat-resisting alloys

BS 2HC 100:2010 铁、镍、铜、钴和难熔金属基合金铸件的检验、试验和验收用程序

This British Standard specifies procedures for inspection, testing and acceptance of iron, nickel, copper, cobalt and refractory metal base alloy castings for aerospace purposes. The standard is applicable to material specifications in the British Standard Aerospace HC series and also to other British Standard material specifications for iron, nickel, copper, cobalt and refractory metal base alloy castings which are suitable for aerospace use.

Procedure for inspection, testing and acceptance of iron, nickel, copper, cobalt and refractory metal base alloy castings

DS/EN 4632-005:2009 航空航天系列 航空航天结构中材料的可焊性和可钎焊性 第005部分：耐热镍基或钴基合金的均质组件

This European Standard defines degrees of weldability and brazeability for materials or families of materials used in the aerospace industry.It comprises a series of sheets, by materials or by material family, which:- indicate the main titles, the chemical composition and the main characteristics;- contain recommendations for welding and brazing;- indicate a degree of weldability or brazeability for a given process under defined conditions;- indicate a value of the mechanical strength coefficient of the welded joint for each welding process, when it could be extracted from bibliographic references referring to it. The joint coefficient is expressed as a rat

Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 005: Homogeneous assemblies of heat resisting Ni or Co base alloys

DS/EN 3987:2009 航天系列 金属材料试验方法 恒幅力控制高周疲劳试验

This document applies to constant amplitude force-controlled high cycle fatigue (HCF) testing of metallic materials governed by EN Aerospace standards. It defines the mechanical properties that may need to be determined, the equipment, test pieces, methodology of test and presentation of results.It applies to uniaxially loaded tests carried out on plain or notched test pieces at ambient and elevated temperatures. It is not intended to cover the testing of more complex test pieces, full scale components or structures, although the methodology could well be adopted to provide for such tests.The purpose of this document is to ensure the compatibility and repro

Aerospace series - Test methods for metallic materials - Constant amplitude force-controlled high cycle fatigue testing