49.035 航空航天制造用零部件 标准查询与下载

SN EN 6057-2021 航空航天系列 带轴承 EN 4265 耐腐蚀钢、内螺纹柄的杆端 尺寸和载荷，英制系列

Aerospace series - Rod-end with bearing EN 4265 in corrosion resisting steel, internal threaded shank - Dimensions and loads, Inch series

LST EN 6057-2021 航空航天系列 带轴承 EN 4265 耐腐蚀钢、内螺纹柄的杆端 尺寸和载荷，英制系列

Aerospace series - Rod-end with bearing EN 4265 in corrosion resisting steel, internal threaded shank - Dimensions and loads, Inch series

ASTM F3498-21 制定简化疲劳载荷谱的标准实施规程

1.1?This practice provides data to develop simplified loading spectra that can be used to perform structural durability analysis for aeroplanes, specifically for wings of small aeroplanes. The material was developed through open consensus of international experts in general avia

Standard Practice for Developing Simplified Fatigue Load Spectra

UNI EN 6057-2020 航空航天系列 带轴承 EN 4265 耐腐蚀钢、内螺纹柄的杆端 尺寸和载荷，英制系列

Aerospace series - Rod-end with bearing EN 4265 in corrosion resisting steel, internal threaded shank - Dimensions and loads, Inch series

BS EN 6057:2020 航空航天系列 杆端轴承采用耐腐蚀钢 EN 4265 内螺纹柄 尺寸和载荷 英制系列

What is BS EN 6057 about?    BS EN 6057 specifies the characteristics of adjustable rod-ends consisting of:   A spherical plain bearing, metal to metal, in corrosion resisting steel, wide series (EN 4265).   A rod-end with internal threaded shank.   Note: This document is published at edition P2. Former P1 and drafts may exist of Airbus development only but without any ASD-STAN official publication. In consequence configuration management discrepancies with these unofficial documents are under Airbus responsibility.  Who is BS EN 6057 for?

Aerospace series. Rod-end with bearing EN 4265 in corrosion resisting steel, internal threaded shank. Dimensions and loads, Inch series

DS/EN 6057:2020 航空航天系列 – 带 EN 4265 耐腐蚀钢轴承的杆端，内螺纹柄 – 尺寸和载荷，英制系列

Aerospace series – Rod-end with bearing EN 4265 in corrosion resisting steel, internal threaded shank – Dimensions and loads, Inch series

20/30427533 DC BS EN 4157 航空航天系列 杆端 带有自调心双列球轴承和钢制螺纹杆 尺寸和载荷 英制系列

BS EN 4157. Aerospace series. Rod end, with self-aligning double row ball bearings and threaded shank in steel. Dimensions and loads, Inch series

19/30398513 DC BS EN 4157 航空航天系列 杆端 带有自调心双列球轴承和钢制螺纹杆 尺寸和载荷 英制系列

BS EN 4157. Aerospace series. Rod end, with self-aligning double row ball bearing and threaded shank in steel. Dimensions and loads, Inch series

20/30426552 DC BS EN 4880 航空航天系列 标准件通用技术条件

BS EN 4880. Aerospace series. General technical specification for standard parts

ASTM E3205-20 金属材料小冲孔试验的标准试验方法

1.1 This test method covers procedures for conducting the small punch deformation test for metallic materials. The results can be used to derive estimates of yield and tensile strength up to 450 °C, and estimates of the ductile-to-brittle transition temperature from the results of small punch bulge tests in the temperature range from -193 °C to 350 °C for iron based materials or 0.4 Tm for other metallic materials, where Tm is their melting temperature in K. 1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this 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 Test Method for Small Punch Testing of Metallic Materials

ASTM F311-08(2020) 用薄膜过滤器进行颗粒污染分析的航空航天液体样品处理的标准实施规程

1.1 This practice covers the processing of liquids in preparation for particulate contamination analysis using membrane filters and is limited only by the liquid-to-membrane filter compatibility. 1.2 The practice covers the procedure for filtering a measured volume of liquid through a membrane filter. When this practice is used, the particulate matter will be randomly distributed on the filter surface for subsequent contamination analysis methods. 1.3 The practice describes procedures to allow handling particles in the size range between 2 and 1000 µm with minimum losses during handling. 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 Practice for Processing Aerospace Liquid Samples for Particulate Contamination Analysis Using Membrane Filters

ASTM F331-13(2020) 航空航天部件溶剂提取物的不挥发残留物的标准试验方法（使用闪蒸器）

1.1 This test method covers the determination of nonvolatile matter, that is, residue on evaporation, in solvent extract from aerospace components, using a rotary flash evaporator. 1.2 The procedure for extraction from components is described in practices such as Practice F303. Before subjecting the extract to the following method, it should be processed to remove the insoluble particulate in accordance with Practice F311 (Note 1). Particle count analysis of the removed particulate may then be performed in accordance with Test Method F312. If particulate is not removed from the extract prior to performing this method, this should be noted on the test report. NOTE 1—Membrane filters with a maximum extractable content of 0.5 weight % should be used on samples to be processed by this test method. Conventional membranes contain 5 to 10 % extractables. For obtaining very low background levels, consideration should be given to using membranes without grid marks. 1.3 The values stated in SI units are to be regarded as standard. 1.4 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. 1.5 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 Nonvolatile Residue of Solvent Extract from Aerospace Components (Using Flash Evaporator)

BS EN 6046:2020 航空航天系列 轴承 球形 滑动 耐腐蚀钢 窄系列 尺寸和负载 英制系列

What is BS EN 6046 about?    BS EN 6046 specifies the characteristics of inch based spherical plain bearing, metal to metal, in corrosion resisting steel, narrow series.   They shall be used in the temperature range as determined by the grease capability as below:   Code A: grease as per MIL-PRF-23827 Type I, operating temperature range −73 °C to 121 °C.   Code B: grease as per MIL-PRF-81322 , operating temperature range −54 °C to 177 °C.   Note : BS EN 6046 is published at edition P7. Form...

Aerospace series. Bearing, spherical, plain, in corrosion resisting steel. Narrow series. Dimensions and loads. Inch series

ASTM E3166-20e1 制造后金属附加制造的航空航天零件的无损检验的标准指南

1.1 This guide discusses the use of established and emerging nondestructive testing (NDT) procedures used to inspect metal parts made by additive manufacturing (AM). 1.2 The NDT procedures covered produce data related to and affected by microstructure, part geometry, part complexity, surface finish, and the different AM processes used. 1.3 The parts tested by the procedures covered in this guide are used in aerospace applications; therefore, the inspection requirements for discontinuities and inspection points in general are different and more stringent than for materials and components used in non-aerospace applications. 1.4 The metal materials under consideration include, but are not limited to, aluminum alloys, titanium alloys, nickel-based alloys, cobalt-chromium alloys, and stainless steels. 1.5 The manufacturing processes considered use powder and wire feedstock, and laser or electron energy sources. Specific powder bed fusion (PBF) and directed energy deposition (DED) processes are discussed. 1.6 This guide discusses NDT of parts after they have been fabricated. Parts will exist in one of three possible states: (1) raw, as-built parts before post-processing (heat treating, hot isostatic pressing, machining, etc.), (2) intermediately machined parts, or (3) finished parts after all post-processing is completed. 1.7 The NDT procedures discussed in this guide are used by cognizant engineering organizations to detect both surface and volumetric flaws in as-built (raw) and post-processed (finished) parts. 1.8 The NDT procedures discussed in this guide are computed tomography (CT, Section 7, including microfocus CT), eddy current testing (ET, Section 8), optical metrology (MET, Section 9), penetrant testing (PT, Section 10), process compensated resonance testing (PCRT, Section 11), radiographic testing (RT, Section 12), infrared thermography (IRT, Section 13), and ultrasonic testing (UT, Section 14). Other NDT procedures such as leak testing (LT) and magnetic particle testing (MT), which have known utility for inspection of AM parts, are not covered in this guide. 1.9 Practices and guidance for in-process monitoring during the build, including guidance on sensor selection and inprocess quality assurance, are not covered in this guide. 1.10 This guide is based largely on established procedures under the jurisdiction of ASTM Committee E07 on Nondestructive Testing and is the direct responsibility of the appropriate subcommittee therein. 1.11 This guide does not recommend a specific course of action for application of NDT to AM parts. It is intended to increase the awareness of established NDT procedures from the NDT perspective. 1.12 Recommendations about the control of input materials, process equipment calibration, manufacturing processes, and post-processing are beyond the scope of this guide and are under the jurisdiction of ASTM Committee F42 on Additive Manufacturing Technologies. Standards under the jurisdiction of ASTM F42 or equivalent are followed whenever possible to ensure reproducible parts suitable for NDT are made. 1.13 Recommendations about the inspection requirements and management of fracture critical AM parts are beyond the scope of this guide. Recommendations on fatigue, fracture mechanics, and fracture control are found in appropriate end user requirements documents, and in standards under the jurisdiction of ASTM Committee E08 on Fatigue and Fracture. NOTE 1—To determine the deformation and fatigue properties of metal parts made by additive manufacturing using destructive tests, consult Guide F3122. NOTE 2—To quantify the risks associated with fracture critical AM parts, it is incumbent upon the structural assessment community, such as ASTM Committee E08 on Fatigue and Fracture, to define critical initial flaw sizes (CIFS) for the part to define the objectives of the NDT. 1.14 This guide does not specify accept-reject criteria used in procurement or as a means for approval of AM parts for 1 This guide is under the jurisdiction of ASTM Committee E07 on Nondestructive Testing and is the direct responsibility of Subcommittee E07.10 on Specialized NDT Methods. Current edition approved Feb. 1, 2020. Published July 2020. DOI: 10.1520/ E3166-20E01. 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 service. Any accept-reject criteria are given solely for purposes of illustration and comparison. 1.15 Units—The values stated in SI units are to be regarded as standard. The values given in parentheses after SI units are provided for information only and are not considered standard. 1.16 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. 1.17 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 Guide for Nondestructive Examination of Metal Additively Manufactured Aerospace Parts After Build

KS W ISO 14210-2019 航空航天 机身球轴承 单列 刚性 密封 扭矩管设计 轻型 英制系列

Aerospace－Airframe ball bearings, single-row, rigid, sealed,torque tube design, light duty－Inch series

KS W ISO 14194-2019 航空航天 机身调心滚子轴承 双列 调心 密封 加长内圈 重载 英制系列

Aerospace－Airframe spherical roller bearings, double-row,self-aligning, sealed, extended inner ring, heavy duty－Inch series

KS W ISO 14197-2019 航空航天 机身调心滚子轴承 单列 调心 密封 中型 英制系列

Aerospace－Airframe spherical roller bearings, single-row,self-aligning, sealed, intermediate duty－Inch series

KS W ISO 14206-2019 航空航天 机身球轴承 单列 刚性 密封 轻型 英制系列

Aerospace－Airframe ball bearings,single-row, rigid, sealed, light duty－Inch series

KS W ISO 9762-2019 航空航天 飞机控制钢丝绳组件 尺寸和端部配件组合

Aerospace－Aircraft control wire rope assemblies－Dimensions and end-fitting combinations

KS W ISO 14193-2019 航空航天 机身调心滚子轴承 单列 调心 密封 加长内圈 中间负荷 英制系列

Aerospace－Airframe spherical roller bearings, single-row,self-aligning, sealed, extended inner ring,intermediate duty－Inch series