49.025.01 航空航天制造用材料综合 标准查询与下载

BS EN 4632-002:2009 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002部分：均质铝及铝合金组件

Aerospace series. Welded and brazed assemblies for aerospace constructions. Weldability and brazeability of materials. Homogeneous assemblies aluminium and aluminium alloys

BS EN 4632-002:2008 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002部分:均质铝及铝合金组件

This 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 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 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. It is applicable without restriction for the manufacturing of new parts or for repair.

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 002: Homogeneous assemblies aluminium and aluminium alloys

BS EN 4632-001:2009 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 一般要求

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - General requirements

BS EN 2950:2008 航空航天系列.试验方法.可锻耐热合金半成品和零件.结构和故障图,宏观和显微检查用条件.结构和不合格品图集

The present document defines the conditions for the macrographic and micrographic examination of heat resisting alloy semi-finished and parts. It includes an atlas of commonly encountered and structural defects. The present document shall be applied in conjunction with the material standards specifying the criteria of acceptance. The present document is not intended to apply to cast or powder metallurgy products.

Aerospace series - Test method - Wrought heat resisting alloys Semifinished products and parts - Conditions for macrographic and micrographic examination - Atlas of structures and defects

BS EN 4632-001:2008 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.一般要求

This standard defines weldability and brazeability degrees for metallic materials used in aerospace construction, for processes and techniques involving welding and brazing but excluding soldering. It also defines rules to be observed to determine the degree of weldability and brazeability. It is applicable without any restriction for the manufacturing of new parts and repair parts.

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - General requirements

DIN EN 4632-001:2009 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001部分:一般要求.德文版本和英文版本EN 4632-001-2008

This standard defines weldability and brazeability degrees for metallic materials used in aerospace construction, for processes and techniques involving welding and brazing but excluding soldering. It also defines rules to be observed to determine the degree of weldability and brazeability. It is applicable without any restriction for the manufacturing of new parts and repair parts.

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 001: General requirements; German and English version EN 4632-001:2008

DIN EN 2950:2009 航空航天系列.试验方法.锻造耐热合金半成品制品和部件.宏观检查和微观检查用条件.结构和缺陷图

The present document defines the conditions for the macrographic and micrographic examination of heat resisting alloy semi-finished and parts. It includes an atlas of commonly encountered and structural defects. The present document shall be applied in conjunction with the material standards specifying the criteria of acceptance. The present document is not intended to apply to cast or powder metallurgy products.

Aerospace series - Test method - Wrought heat resisting alloys Semi-finished products and parts - Conditions for macrographic and micrographic examination - Atlas of structures and defects; German and English version EN 2950:2008

DIN EN 4632-002:2009 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002部分:均质铝及铝合金组件

This 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 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 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. It is applicable without restriction for the manufacturing of new parts or for repair.

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 002: Homogeneous assemblies aluminium and aluminium alloys; German and English version EN 4632-002:2008

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.第005部分: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 - Part 005: Homogeneous assemblies of heat resisting Ni or Co base alloys

LST EN 2950-2008 航空航天系列 试验方法 锻造耐热合金半成品和零件 宏观和显微检验条件 结构和缺陷图集

Aerospace series - Test method - Wrought heat resisting alloys Semi-finished products and parts - Conditions for macrographic and micrographic examination - Atlas of structures and defects

DS/EN 2950:2008 航空航天系列 试验方法 锻造耐热合金半成品和零件 宏观和显微检验条件 结构和缺陷图集

The present document defines the conditions for the macrographic and micrographic examination of heat resisting alloy semi-finished and parts.It includes an atlas of commonly encountered and structural defects.The present document shall be applied in conjunction with the material standards specifying the criteria of acceptance.The present document is not intended to apply to cast or powder metallurgy products.

Aerospace series - Test method - Wrought heat resisting alloys Semi-finished products and parts - Conditions for macrographic and micrographic examination - Atlas of structures and defects

NF L10-008*NF EN 2950:2008 航空航天系列.试验方法.锻造耐热合金半成品和部件.宏观和微观检验条件.结构图和缺陷图

Aerospace series - Test method - Wrought heat resisting alloys Semi-finished products and parts - Conditions for macrographic and micrographic examination - Atlas of structures and defects.

LST EN 4632-001-2008 航空航天系列 航空航天结构的焊接和钎焊组件 材料的可焊性和可钎焊性 第001部分：一般要求

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 001: General requirements

LST EN 4632-002-2008 航空航天系列 航空航天结构用焊接和钎焊组件 材料的可焊性和钎焊性 第002部分：铝和铝合金的均质组件

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 002: Homogeneous assemblies aluminium and aluminium alloys

EN 2950:2008 航空航天系列的试验方法.锻造耐热合金半成品制品和部件.宏观检查和微观检查用条件.结构和缺陷图

The present document defines the conditions for the macrographic and micrographic examination of heat resisting alloy semi-finished and parts. It includes an atlas of commonly encountered and structural defects. The present document shall be applied in conjunction with the material standards specifying the criteria of acceptance. The present document is not intended to apply to cast or powder metallurgy products.

Aerospace series - Test method - Wrought heat resisting alloys Semi-finished products and parts - Conditions for macrographic and micrographic examination - Atlas of structures and defects

SAE AMS3175-2008 涂覆前非铬酸盐表面的预处理

1.1 FormThis specification establishes the performance requirements for non-chromated materials used for surface preparation of metallic aircraft surfaces prior to applying organic coatings.1.2 ApplicationPretreatment 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.1.3 ClassificationPretreatment materials shall be qualified by Type and Class as defined below. The pretreatment material is to be tested and evaluated in conjunction with either MIL-PRF-23377 or MIL-PRF-85582 industry qualified primers.Type 1: Suitable for spray applicationType 2: Suitable for immersion applicationType 3:* Suitable for manual or hand application (i.e., brush, wipe, or other touch up methods)*NOTE: If Product is already qualified to a Type 1 or Type 2 and there is no formula change for the Type 3, limited testing per Table 4 is permitted.Class C: Qualified for use with primers that contain hexavalent chromiumClass N: Qualified for use with primers that are free from: barium, hexavalent chromium, cadmium, arsenic, copper, nickel, mercury, or lead)Grade I: 0 to 250 g/l (0 to 2.1 lb/gal) Volatile Organic Content (VOC) Grade II: 251 to 780 g/l (2.11 to 6.55 lb/gal) Volatile Organic Content (VOC)1.4 Safety-Hazardous MaterialsWhile the materials, methods, applications, and processes described or referenced in this specification may involve the use of hazardous materials, this specification does not address the hazards which may be involved in such use. It is thesole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved.

Non-Chromated Surface Pretreatment Prior to Painting

DS/EN 4632-001:2008 航空航天系列 航空航天结构的焊接和钎焊组件 材料的可焊性和可钎焊性 第001部分：一般要求

This standard defines weldability and brazeability degrees for metallic materials used in aerospace construction, for processes and techniques involving welding and brazing but excluding soldering.It also defines rules to be observed to determine the degree of weldability and brazeability.It is applicable without any restriction for the manufacturing of new parts and repair parts.

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 001: General requirements

DS/EN 4632-002:2008 航空航天系列 航空航天结构用焊接和钎焊组件 材料的可焊性和钎焊性 第002部分：铝和铝合金的均质组件

This 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 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 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

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 002: Homogeneous assemblies aluminium and aluminium alloys

EN 4632-001:2008 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001部分:一般要求

This standard defines weldability and brazeability degrees for metallic materials used in aerospace construction; for processes and techniques involving welding and brazing but excluding soldering. It also defines rules to be observed to determine the degree of weldability and brazeability. It is applicable without any restriction for the manufacturing of new parts and repair parts.

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 001: General requirements

EN 4632-002:2008 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002部分:均质铝及铝合金组件

This 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 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 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. It is applicable without restriction for the manufacturing of new parts or for repair.

Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 002: Homogeneous assemblies aluminium and aluminium alloys