49.025.01 航空航天制造用材料综合 标准查询与下载

T/YH 1020-2020 智能化激光选区熔化增材制造工艺参数数据接口规范

本标准规定了激光选区熔化增材制造的工艺过程及成形质量的参数种类、配置文件格式、数据接口格式。 本标准适用于激光选区熔化增材制造设备工艺参数数据库的构建、使用以及扩充，模型数据处理及控制软件的设计。

Standard specification for parameter data interfaces to smart additive manufacturing process of selective laser melting

ASTM E1235-12(2020) 航天器环境控制区非挥发性残留物（NVR）的重量测定标准试验方法

Standard Test Method for Gravimetric Determination of Nonvolatile Residue (NVR) in Environmentally Controlled Areas for Spacecraft

ASTM E1234-12(2020) 航天器环境控制区用不挥发残留物（NVR）样品板的搬运、运输和安装的标准实施规程

1.1 This practice covers the handling, transporting, and installing of sample plates used for the gravimetric determination of nonvolatile residue (NVR) within and between facilities. 1.2 The values stated in SI units are to be regarded as the standard. 1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.4 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Practice for Handling, Transporting, and Installing Nonvolatile Residue (NVR) Sample Plates Used in Environmentally Controlled Areas for Spacecraft

ASTM E1235-12(2020)e1 航天器环境控制区非挥发性残留物（NVR）的重量测定标准试验方法

1.1 This test method covers the determination of nonvolatile residue (NVR) fallout in environmentally controlled areas used for the assembly, testing, and processing of spacecraft. 1.2 The NVR of interest is that which is deposited on sampling plate surfaces at room temperature: it is left to the user to infer the relationship between the NVR found on the sampling plate surface and that found on any other surfaces. 1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.4 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.5 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Test Method for Gravimetric Determination of Nonvolatile Residue (NVR) in Environmentally Controlled Areas for Spacecraft

ASTM E399-20 金属材料线弹性平面应变断裂韧性K_IC的标准试验方法

1.1 This test method covers the determination of fracture toughness (KIc and optionally KIsi) of metallic materials under predominantly linear-elastic, plane-strain conditions using fatigue precracked specimens having a thickness of 1.6 mm (0.063 in.) or greater2 subjected to slowly, or in special (elective) cases rapidly, increasing crack-displacement force. Details of test apparatus, specimen configuration, and experimental procedure are given in the annexes. Two procedures are outlined for using the experimental data to calculate fracture toughness values: 1.1.1 The KIc test procedure is described in the main body of this test standard and is a mandatory part of the testing and results reporting procedure for this test method. The KIc test procedure is based on crack growth of up to 2 % percent of the specimen width. This can lead to a specimen size dependent rising fracture toughness resistance curve, with larger specimens producing higher fracture toughness results. 1.1.2 The KIsi test procedure is described in Appendix X1 and is an optional part of this test method. The KIsi test procedure is based on a fixed amount of crack extension of 0.5 mm, and as a result, KIsi is less sensitive to specimen size than KIc. This less size-sensitive fracture toughness, KIsi, is called size-insensitive throughout this test method. Appendix X1 contains an optional procedure for reinterpreting the forcedisplacement test record recorded as part of this test method to calculate the additional fracture toughness value, KIsi. NOTE 1—Plane-strain fracture toughness tests of materials thinner than 1.6 mm (0.063 in.) that are sufficiently brittle (see 7.1) can be made using other types of specimens (1).3 There is no standard test method for such thin materials. 1.2 This test method is divided into two parts. The first part gives general recommendations and requirements for testing and includes specific requirements for the KIc test procedure. The second part consists of Annexes that give specific information on displacement gage and loading fixture design, special requirements for individual specimen configurations, and detailed procedures for fatigue precracking. Additional annexes are provided that give specific procedures for beryllium and rapid-force testing, and the KIsi test procedure, which provides an optional additional analysis procedure for the test data collected as part of the KIc test procedure. 1.3 General information and requirements common to all specimen configurations: Section Referenced Documents 2 Terminology 3 Stress-Intensity Factor 3.1.1 Plane-Strain Fracture Toughness 3.1.2 Crack Plane Orientation 3.1.4 Summary of Test Method 4 Significance and Use 5 Significance 5.1 Precautions 5.1.1 – 5.1.5 Practical Applications 5.2 Apparatus (see also 1.4) 6 Tension Machine 6.1 Fatigue Machine 6.2 Loading Fixtures 6.3 Displacement Gage, Measurement 6.4 Specimen Size, Configurations, and Preparation (see also 1.5) 7 Specimen Size Estimates 7.1 Standard and Alternative Specimen Configurations 7.2 Fatigue Crack Starter Notches 7.3.1 Fatigue Precracking (see also 1.6) 7.3.2 Crack Extension Beyond Starter Notch 7.3.2.2 General Procedure 8 Specimen Measurements Thickness 8.2.1 Width 8.2.2 Crack Size 8.2.3 Crack Plane Angle 8.2.4 Specimen Testing Loading Rate 8.3 Test Record 8.4 Calculation and Interpretation of Results 9 Test Record Analysis 9.1 Pmax/PQ Validity Requirement 9.1.3 Specimen Size Validity Requirements 9.1.4 Reporting 10 1 This test method is under the jurisdiction of ASTM Committee E08 on Fatigue and Fracture and is the direct responsibility of Subcommittee E08.07 on Fracture Mechanics. Current edition approved Jan. 1, 2020. Published April 2020. Originally approved in 1970. Last previous edition approved in 2019 as E399 – 19. DOI: 10.1520/E0399-20. 2 For additional information relating to the fracture toughness testing of aluminum alloys, see Practice B645. 3 The boldface numbers in parentheses refer to the list of references at the end of this standard. Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee. 1 Section Precision and Bias 11 1.4 Specific requirements related to test apparatus: Double-Cantilever Displacement Gage Annex A1 Testing Fixtures Annex A2 Bend Specimen Loading Fixture Annex A2.1 Compact Specimen Loading Clevis Annex A2.2 1.5 Specific requirements related to individual specimen configurations: Bend Specimen SE(B) Annex A3 Compact Specimen C(T) Annex A4 Disk-Shaped Compact Specimen DC(T) Annex A5 Arc-Shaped Tension Specimen A(T) Annex A6 Arc-Shaped Bend Specimen A(B) Annex A7 1.6 Specific requirements related to special test procedures: Fatigue Precracking KIc and KIsi Specimens Annex A8 Hot-Pressed Beryllium Testing Annex A9 Rapid-Force Testing Annex A10 Determination of KIsi Appendix X1 1.7 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only. 1.8 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.9 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness K_IC of Metallic Materials

ASTM E423-71(2019) 非导电试样高温下正常光谱发射率的标准试验方法

1.1 This test method describes an accurate technique for measuring the normal spectral emittance of electrically nonconducting materials in the temperature range from 1000 to 1800 K, and at wavelengths from 1 to 35 µm. It is particularly suitable for measuring the normal spectral emittance of materials such as ceramic oxides, which have relatively low thermal conductivity and are translucent to appreciable depths (several millimetres) below the surface, but which become essentially opaque at thicknesses of 10 mm or less. 1.2 This test method requires expensive equipment and rather elaborate precautions, but produces data that are accurate to within a few percent. It is particularly suitable for 1 This test method is under the jurisdiction of ASTM Committee E21 on Space Simulation and Applications of Space Technology and is the direct responsibility of Subcommittee E21.04 on Space Simulation Test Methods. Current edition approved Oct. 1, 2019. Published October 2019. Originally approved in 1971. Last previous edition approved in 2014 as E423 – 71(2014). DOI: 10.1520/E0423-71R19. Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee. 1 research laboratories, where the highest precision and accuracy are desired, and is not recommended for routine production or acceptance testing. Because of its high accuracy, this test method may be used as a reference method to be applied to production and acceptance testing in case of dispute. 1.3 This test method requires the use of a specific specimen size and configuration, and a specific heating and viewing technique. The design details of the critical specimen furnace are presented in Ref (1),2 and the use of a furnace of this design is necessary to comply with this test method. The transfer optics and spectrophotometer are discussed in general terms. 1.4 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.5 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.6 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Test Method for Normal Spectral Emittance at Elevated Temperatures of Nonconducting Specimens

BS EN 2366:2019 航空航天系列 板材和带材 耐热合金 冷轧 厚度a≤3毫米 方面

What is BS EN 2366- Dimensions for cold rolled sheets and strips in aerospace applications  about?   BS EN 2366  is a standard that covers dimensional specifications for heat resisting alloys in aerospace applications which ensures operational safety and thermal resistance of components at high temperatures.   BS EN 2366  specifies the dimensions and tolerances of cold rolled sheets and strips in heat resisting alloys used in aerospace construction.   Who is BS EN 2366- Dimensions for cold rolled sheets and strips in aerospace applications  for?  

Aerospace series. Sheets and strips. Heat resisting alloys. Cold rolled. Thickness a ≤ 3 mm. Dimensions

BS EN 4867:2019 航空航天系列 通过变色进行激光表面打标

What is BS EN 4867- Aerospace series: Laser surface marking about?   BS EN 4867 is a European standard covering technical specifications for Aerospace series: laser surface marking by discoloration, which enables identification of products and their authenticity.   BS EN 4867 specifies the marking rules for aerospace products, semi-finished products, and ready to use parts, which need surface marking by discoloration using a laser source to identify the part and/or enhance its traceability.   BS EN 4867 provides guidance on marking, which is used on a wide range of materials (both metallic and non-metallic) and coatings (paints and varnishes).  

Aerospace series. Laser surface marking by discoloration

ASTM E399-19 金属材料线弹性平面应变断裂韧性K_IC的标准试验方法

1.1 This test method covers the determination of fracture toughness (KIc) of metallic materials under predominantly linear-elastic, plane-strain conditions using fatigue precracked specimens having a thickness of 1.6 mm (0.063 in.) or greater2 subjected to slowly, or in special (elective) cases rapidly, increasing crack-displacement force. Details of test apparatus, specimen configuration, and experimental procedure are given in the Annexes. NOTE 1—Plane-strain fracture toughness tests of thinner materials that are sufficiently brittle (see 7.1) can be made using other types of specimens (1).3 There is no standard test method for such thin materials. 1.2 This test method is divided into two parts. The first part gives general recommendations and requirements for KIc testing. The second part consists of Annexes that give specific information on displacement gage and loading fixture design, special requirements for individual specimen configurations, and detailed procedures for fatigue precracking. Additional annexes are provided that give specific procedures for beryllium and rapid-force testing. 1.3 General information and requirements common to all specimen configurations: Section Referenced Documents 2 Terminology 3 Stress-Intensity Factor 3.1.1 Plane-Strain Fracture Toughness 3.1.2 Crack Plane Orientation 3.1.4 Section Summary of Test Method 4 Significance and Use 5 Significance 5.1 Precautions 5.1.1 – 5.1.5 Practical Applications 5.2 Apparatus (see also 1.4) 6 Tension Machine 6.1 Fatigue Machine 6.2 Loading Fixtures 6.3 Displacement Gage, Measurement 6.4 Specimen Size, Configurations, and Preparation (see also 1.5) 7 Specimen Size Estimates 7.1 Standard and Alternative Specimen Configurations 7.2 Fatigue Crack Starter Notches 7.3.1 Fatigue Precracking (see also 1.6) 7.3.2 Crack Extension Beyond Starter Notch 7.3.2.2 General Procedure 8 Specimen Measurements Thickness 8.2.1 Width 8.2.2 Crack Size 8.2.3 Crack Plane Angle 8.2.4 Specimen Testing Loading Rate 8.3 Test Record 8.4 Calculation and Interpretation of Results 9 Test Record Analysis 9.1 Pmax/PQ Validity Requirement 9.1.3 Specimen Size Validity Requirements 9.1.4 Reporting 10 Precision and Bias 11 1.4 Specific requirements related to test apparatus: Double-Cantilever Displacement Gage Annex A1 Testing Fixtures Annex A2 Bend Specimen Loading Fixture Annex A2.1 Compact Specimen Loading Clevis Annex A2.2 1.5 Specific requirements related to individual specimen configurations: Bend Specimen SE(B) Annex A3 Compact Specimen C(T) Annex A4 Disk-Shaped Compact Specimen DC(T) Annex A5 Arc-Shaped Tension Specimen A(T) Annex A6 Arc-Shaped Bend Specimen A(B) Annex A7 1 This test method is under the jurisdiction of ASTM Committee E08 on Fatigue and Fracture and is the direct responsibility of Subcommittee E08.07 on Fracture Mechanics. Current edition approved June 15, 2019. Published August 2019. Originally approved in 1970. Last previous edition approved in 2017 as E399 – 17. DOI: 10.1520/E0399-19. 2 For additional information relating to the fracture toughness testing of alumi– inum alloys, see Practice B645. 3 The boldface numbers in parentheses refer to the list of references at the end of this standard. Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee. 1 1.6 Specific requirements related to special test procedures: Fatigue Precracking KIc Specimens Annex A8 Hot-Pressed Beryllium Testing Annex A9 Rapid-Force Testing Annex A10 1.7 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only. 1.8 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.9 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness K_IC of Metallic Materials

BS EN 2369:2018 航空航天系列 电线、耐热合金 直径 0.2 毫米 ≤ D ≤ 8 毫米 方面

What is BS EN 2369 - Heat-resisting alloy wires about?    BS EN 2369 is a European Standard that specifies the dimensions and tolerances of heat-resisting alloys wire used in aerospace construction.   BS EN 2369 covers alloy wires of diameter 0,2 mm ≤ D≤ 8mm.   Who is BS EN 2369 - Heat-resisting alloy wires for?   BS EN 2369

Aerospace series. Wires, heat resisting alloys. Diameter 0,2 mm ≤ D ≤ 8 mm. Dimensions

BS EN 6064:2017 航空航天系列 通过差示扫描量热法 (DSC) 分析非金属材料（固化）以确定固化程度

What is BS EN 6064- Determination of the extent of cure in non-metallic materials about? BS EN 6064 is a standard that serves technical specifications for the determination of the extent of cure in non-metallic materials that ensures the quality and longevity in aerospace applications. BS EN 6064 defines the procedure for estimating the extent of cure of certain non-metallic materials (e.g., pre-impregnated and neat resin systems, adhesives) for aerospace use. The extent of cure is estimated by Differential Scanning Calorimetry (DSC) measurements of uncured and cured materials. When BS EN 6064 is combined with other techniques, they can deliver additional evidence on the extent of the cure. Note: BS EN 6064 does not give any directions to meet the health and safety requirements. Who is BS EN 6064- Determination of the extent of cure in non-metallic materials for? BS EN 6064 on the determination of the extent of cure in non-metallic materials applies to: Manufacturers of non-metallic materials for aerospace applications Dealers and importers of non-metallic materials for aerospace applications Testing houses and labs in the aerospace industry Aeronautical and aerospace engineers Inspection services in the aerospace industry

Aerospace series. Analysis of non-metallic materials (cured) for the determination of the extent of cure by Differential Scanning Calorimetry (DSC)

EN 6041:2018 航空航天系列 非金属材料 试验方法 差示扫描量热法（DSC）分析非金属材料（未固化）

Aerospace series - Non-metallic materials - Test method - Analysis of non-metallic materials (uncured) by Differential Scanning Calorimetry (DSC)

EN 6018:2017 航空航天系列金属材料试验方法位移法密度测定

Aerospace series - Test methods for metallic materials - Determination of density according to displacement method

NF L10-718*NF EN 4376:2017 航空航天系列 耐热合金 NiCr19Fe19Nb5Mo3（2.4668）固溶处理和沉淀处理 棒材和型材，De < or = 200 mm

La présente norme spécifie les exigences relatives à :Alliage résistant à chaud NiCr19Fe19Nb5Mo3 (2.4668) Mis en solution et précipitéBarres et profilésDe? 200 mmpour les applications aérospatiales.

Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated - Bar and section, De < or = 200 mm

BS EN 6041:2018 航空航天系列 非金属材料 测试方法 通过差示扫描量热法 (DSC) 分析非金属材料（未固化）

What is BS EN 6041- Analysis of non-metallic materials by Differential Scanning Calorimetry about? BS EN 6041 is a standard that serves technical specifications for analysis of non-metallic materials by Differential Scanning Calorimetry method that enables derivation of cure cycle and ageing behavior. BS EN 6041 test method defines the procedure for determining the curing-characteristic and glass transition temperature of non-metallic materials (e.g. preimpregnated and neat resin systems, adhesives) for aerospace use by Differential Scanning Calorimetry (DSC). The results obtained in BS EN 6041 can be useful for: Derivation of the optimum cure cycle Assessment of the condition of the resin Assessment of the ageing behavior of the resin Note: BS EN 6041 does not give any directions to meet the health and safety requirements. Who is BS EN 6041- Analysis of non-metallic materials by Differential Scanning Calorimetry for? BS EN 6041 on analysis of non-metallic materials by Differential Scanning Calorimetry applies to: Manufacturers of adhesives and resins for aerospace applications Dealers and importers of adhesives and resins for aerospace applications Testing houses and l...

Aerospace series. Non-metallic materials. Test method. Analysis of non-metallic materials (uncured) by Differential Scanning Calorimetry (DSC)

DIN EN 4376:2016 航空航天系列 耐热合金NiCr19Fe19Nb5Mo3（2.4668）固溶处理和沉淀处理 棒材和型材，De<=200mm

Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated - Bar and section, De <= 200 mm; German and English version EN 4376:2016

DIN EN 4377:2016 航空航天系列.耐热合金NiCr19Fe19Nb5Mo3(2.4668).非热处理.锻坯.a/D≤300 mm.德文和英文版本EN 4377-2015

Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) - Non heat treated - Forging stock - a or D <= 300 mm; German and English version EN 4377:2015

BS EN 4376:2016 航空航天系列. 耐热合金NiCr19Fe19Nb5Mo3 (2.4668). 溶解处理和沉淀处理. 棒材和型材. De≤200 mm

Aerospace series. Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated. Bar and section, De 200 mm

EN 4376:2016 航空航天系列-耐热合金NiCr19Fe19Nb5Mo3(2.4668)的溶液处理和沉淀处理-棒材和型材,De$3L200mm

This European Standard specifies the requirements relating to: Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668); Solution treated and precipitation treated; Bar and section; De 200 mm; for aerospace applications.

Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated - Bar and section@ De ��200 mm

GSO ISO 16691:2015 航空航天系统 航天器热控制涂层 一般要求

  Scope is not provided for this standard

Space systems -- Thermal control coatings for spacecraft -- General requirements