49.025.50 粘合劑 標準查詢與下載

ASTM D6465-99(2024) 航空航天和通用粘合劑和密封劑選擇的標準指南

Standard Guide for Selecting Aerospace and General Purpose Adhesives and Sealants

ASTM F942-18(2023)e1 航空航天透明外殼夾層材料試驗方法選擇的標準指南

1.1 This guide summarizes the standard test methods available for determining physical and mechanical characteristics of interlayer materials used in multi-ply aerospace transparent enclosures. 1.2 Interlayer materials are used to laminate glass-to-glass, glass-to-plastic, and plastic-to-plastic. Interlayer materials are basically transparent adhesives with high-quality optical properties. They can also serve as an energy absorbing medium, a fail-safe membrane to contain cockpit pressure and to prevent entry of impact debris; a strain insulator to accommodate different thermal expansion rates of members being laminated and as an adherent to prevent spalling of inner surface ply material fragments. The relative importance of an interlayer characteristic will be a function of the prime use it serves in its particular application. 1.3 This guide, as a summary of various methods in Section 2, is intended to facilitate the selection of tests that can be applied to interlayer materials. 1.4 The test methods listed are for use in determining basic design characteristics and in assuring lot-to-lot uniformity of the materials being tested except as noted in 3.3. 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 Guide for Selection of Test Methods for Interlayer Materials for Aerospace Transparent Enclosures

T/NXCL 010-2021 低溫固化型銀導體漿料

本文件規定了低溫固化型銀導體漿料的分類、技術要求、試驗方法、檢驗規則和包裝、標志、運輸、貯存。本文件適用于薄膜開關及柔性印刷電路用銀漿料、浸漬型鉭電容器用銀漿料、以及銀導電膠等低溫固化型銀導體漿料。

Low temperature curing silver conductor paste

ASTM D6412/D6412M-99(2020) 用于粘結金屬和非金屬材料的環氧（柔性）粘合劑的標準規范

1.1 The specification covers a two-part modified epoxy paste adhesive for bonding metallic and nonmetallic materials. The adhesive should be suitable for forming bonds that can withstand environmental exposure to temperatures from –184 to 82 °C [–300 to 180 °F] when exposed to an expected combination of stress, temperature, and relative humidity to be encountered in service. NOTE 1—When coordinated through the Department of Defense (DoD) and the National Aeronautics and Space Administration (NASA), this practice will be a direct replacement of MIL-A-82720 (OS), MIS-26872, and MSFC-SPEC-2037. 1.2 The values stated in SI units or inch-pound units are to be regarded separately as standard. Within the text, the inch-pound units are shown in brackets. The values stated in each system are not exact equivalents; therefore, each system must be used independently of the other. Combining values from the two systems may result in nonconformance with this specification. 1.3 The following precautionary statement pertains to the test method portion only, Section 8, of this specification: 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 Specification for Epoxy (Flexible) Adhesive For Bonding Metallic And Nonmetallic Materials

BS EN 2667-3:2019 航空航天系列 非金屬材料 發泡結構粘合膜 測試方法-膨脹率和揮發物含量

What is BS EN 2667-3- Aerospace series: Foaming structural adhesive films about? ? BS EN 2667-3 is a standard that covers technical specifications for the Aerospace series: structural foaming adhesive films that ensure advanced bonding and fire resistance in aerospace applications. ? BS EN 2667-3 specifies the test method for determining the expansion ratio and the volatile content in structural foaming adhesive films. ? Who is BS EN 2667-3- Aerospace series: Foaming structural adhesive films for? ? BS EN 2667-3 on aerospace series: Foaming structural adhesive films applies to: ? Manufacturers of adhesive films ?

Aerospace series. Non-metallic materials. Foaming structural adhesive films. Test methods - Expansion ratio and volatile content

ASTM F942-18 航空航天透明罩內層材料試驗方法選擇標準指南

1.1 This guide summarizes the standard test methods available for determining physical and mechanical characteristics of interlayer materials used in multi-ply aerospace transparent enclosures. 1.2 Interlayer materials are used to laminate glass-to-glass, glass-to-plastic, and plastic-to-plastic. Interlayer materials are basically transparent adhesives with high-quality optical properties. They can also serve as an energy absorbing medium, a fail-safe membrane to contain cockpit pressure and to prevent entry of impact debris; a strain insulator to accommodate different thermal expansion rates of members being laminated and as an adherent to prevent spalling of inner surface ply material fragments. The relative importance of an interlayer characteristic will be a function of the prime use it serves in its particular application. 1.3 This guide, as a summary of various methods in Section 2, is intended to facilitate the selection of tests that can be applied to interlayer materials. 1.4 The test methods listed are for use in determining basic design characteristics and in assuring lot-to-lot uniformity of the materials being tested except as noted in 3.3. 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 Guide for Selection of Test Methods for Interlayer Materials for Aerospace Transparent Enclosures

BS EN 2667-2:2018 航空航天系列. 非金屬材料. 發泡結構膠. 試驗方法. 壓管剪

Aerospace series. Non-metallic materials. Foaming structural adhesives. Test methods. Compressive tube shear

EN 2667-2:2018 航空航天系列非金屬材料發泡結構膠試驗方法第2部分：壓縮管剪切

Aerospace series - Non-metallic materials - Foaming structural adhesives - Test methods - Part 2: Compressive tube shear

SAE AMS3809A-2015 膠帶，粘性，壓敏，雙面，地毯捆綁

This specification covers a fabric in the form of a double-faced, pressure-sensitive, adhesive tape.

Tape, Adhesive, Pressure-Sensitive, Double-Faced, Carpet Tie Down

SAE AMS2980/5A-2014 碳纖維織物和環氧樹脂濕浸漬增強修復材料.第5部分:材料規范:平織、193 g/m²環氧和碳纖維織物

This Material Specification defines the requirements of carbon fiber fabric and epoxy resin systems used for wet lay-up repair of carbon fiber reinforced epoxy structures, qualified according to AMS 2980/1 and 2980/2.

Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 5 - Material Specification: Carbon Fiber Fabrics, Plain Weave, 193 g/m2, and Epoxy Resin

SAE AMS2980/2B-2014 技術規范:碳纖維織物和環氧樹脂濕浸漬增強修復材料.第2部分:合格鑒定計劃

AMS 2980/2 gives specific information about the qualification program for carbon fiber fabric, epoxy systems and the material combination used for wet lay-up repair of carbon fiber reinforced epoxy structures.

Technical Specification: Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 2 - Qualification Program

SAE AMS2980/1B-2014 技術規范:碳纖維織物和環氧樹脂濕浸漬增強修復材料.第1部分:一般要求

AMS 2980/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric and epoxy resin systems used for wet lay-up repair of carbon fiber reinforced epoxy structures.

Technical Specification: Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 1 - General Requirements

SAE AMS2980/3B-2014 技術規范:碳纖維織物和環氧樹脂濕浸漬增強修復材料采購規范.織物

The PS specifies the batch release and delivery requirements for carbon fiber and carbon fabric used for wet lay-up repair purposes.

Technical Specification: Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Purchasing Specification - Fabric

SAE AMS2980/4B-2014 技術規范:碳纖維織物和環氧樹脂濕浸漬增強修復材料采購規范.樹脂

This PS specifies the batch release and delivery requirements for epoxy resin systems (base resin and curing agent) used for wet lay-up repair purposes.

Technical Specification: Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Purchasing Specification - Resin

SAE AMS2980B-2014 技術規范:碳纖維織物和環氧樹脂潮濕堆積修復材料.第0部分:介紹

This document (Technical Specification) gives information about qualification rules and the relation between the different specification parts involved, such as Technical Specification (TS), Material Specification (MS), and Purchasing Specification (PS). The link to material qualification and qualified products is presented.

Technical Specification: Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material, Part 0 - Introduction

NF L17-021*NF EN 4492:2013 航空航天系列.非金屬材料.厭氧乳化劑化合物.螺紋鎖.扭矩強度19 Nm

Aerospace series - Non-metallic materials - Anaerobic polymerisable compounds - Threadlocking - Torque strength 19 Nm

NF L17-313*NF EN 4106:2013 航空航天系列.非金屬材料.結構型膠黏劑系統.糊狀膠粘劑.技術規范

Aerospace series - Non-metallic materials - Structural adhesive systems - Paste adhesive - Technical specification

DIN EN 4491:2013 航空航天系列. 非金屬材料. 厭氧可聚合化合物. 螺紋鎖固. 抗扭強度16 Nm; 德文和英文版本EN 4491-2013

Aerospace series - Non-metallic materials - Anaerobic polymerisable compounds - Threadlocking - Torque strength 16 Nm; German and English version EN 4491:2013

DIN EN 4106:2013 航空航天系列. 非金屬材料. 結構型粘合系統. 糊狀粘合劑. 技術規范; 德文和英文版本EN 4106-2013

Aerospace series - Non-metallic materials - Structural adhesive systems - Paste adhesive - Technical specification; German and English version EN 4106:2013

DIN EN 4492:2013 航空航天系列.非金屬材料.厭氧聚合物.螺紋鎖.扭矩強度19 Nm.德文和英文版本EN 4492-2013

Aerospace series - Non-metallic materials - Anaerobic polymerisable compounds - Threadlocking - Torque strength 19 Nm; German and English version of EN 4492:2013