49.025.40 橡胶和塑料 标准查询与下载

ASTM D3518/D3518M-18 通过a±拉伸试验测定聚合物基复合材料平面内剪切响应的标准试验方法；45°；层压材料

1.1 This test method determines the in-plane shear response of polymer matrix composite materials reinforced by highmodulus fibers. The composite material form is limited to a continuous-fiber-reinforced composite 645° laminate capable of being tension tested in the laminate x direction. 1.2 The values stated in either SI units or inch-pound units are to be regarded separately as standard. 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 the standard. 1.2.1 Within the text, the inch-pound units are shown in brackets. 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 In-Plane Shear Response of Polymer Matrix Composite Materials by Tensile Test of a ±45° Laminate

DIN EN 2796:2018 航空航天系列 氟碳橡胶（FKM） 低压缩形变 硬度 60 IRHD

This European Standard specifies the properties of fluorocarbon rubber (FKM)1), low compression set, hardness 60 IRHD, for aerospace applications.

Aerospace series - Fluorocarbon rubber (FKM) - Low compressions set - Hardness 60 IRHD; German and English version EN 2796:2018

ASTM D8101/D8101M-18 用于测量复合材料穿透钝弹的影响的标准测试方法

1.1 This test method measures the resistance of flat composite panels in one specific clamping configuration to penetration by a blunt projectile in free flight. In this test method, the term “penetration” is defined as the case in which the projectile travels completely through the composite panel and fully exits the back side. The composite materials may be continuous fiber angle-ply, woven or braided fiber-reinforced polymer matrix composites, or chopped fiber-reinforced composites. The resistance to penetration is quantified by a statistical function that defines the probability of penetration for a given kinetic energy. 1.2 This test method is intended for composite test panels in which the thickness dimension is small compared with the test panel width and length (span to thickness on the order of 40 or greater). 1.3 This test method is intended for applications such as jet engine fan containment, open rotor engine blade containment, or other applications in which protection is needed for projectiles at velocities typically lower than seen in ballistic armor applications. The typical impact velocity that this test is intended for is in the range of 100 to 500 m/s [300 to 1500 ft/s], as opposed to higher velocities associated with armor penetration. 1.4 A flat composite panel is fixed between a circularshaped clamping fixture and a large base fixture each with a large coaxial hole defining a region of the panel that is subjected to impact in the direction normal to the plane of the flat panel by a blunt projectile. Clamping pressure is provided by 28 through bolts that pass through the front clamp, the test specimen, and the back plate. The mass, geometry, desired impact kinetic energy, and impact orientation of the projectile with respect to the panel are specified before the test. Equipment and procedures are required for measuring the actual impact velocity and orientation during the test. The impact penetration resistance can be quantified by either the velocity or kinetic energy required for the projectile to penetrate the test panel fully. A number of tests are required to obtain a statistical probability of penetration for given impact conditions. 1.5 This test method measures the penetration resistance for a specific projectile and test configuration and can be used to screen materials for impact penetration resistance, compare the impact penetration resistance of different composite materials under the same test geometry conditions, or assess the effects of in-service or environmental exposure on the impact penetration resistance of materials. 1.6 The impact penetration resistance is highly dependent on the test panel materials and architecture, projectile geometry and mass, and panel boundary conditions. Results are not generally scalable to other configurations but, for the same test configurations, may be used to assess the relative impact penetration resistance of different materials and fiber architectures. 1.7 The values stated in either SI units or inch-pound units are to be regarded separately as standard. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in nonconformance with the standard. Within the text, the inch-pound units are shown in brackets. 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. 1 This test method is under the jurisdiction of ASTM Committee D30 on Composite Materials and is the direct responsibility of Subcommittee D30.05 on Structural Test Methods. Current edition approved Oct. 15, 2018. Published February 2019. Originally approved in 2017. Last previous edition approved in 2017 as D8101/D8101M – 17. DOI: 10.1520/D8101_D8101M-18. 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 

Standard Test Method for Measuring the Penetration Resistance of Composite Materials to Impact by a Blunt Projectile

DIN EN 2799:2018 航空航天系列 氟碳橡胶（FKM） 低压缩形变 硬度 90 IRHD

This European Standard specifies the properties of fluorocarbon rubber (FKM)1), low compression set, hardness 90 IRHD, for aerospace applications.

Aerospace series - Fluorocarbon rubber (FKM) - Low compressions set - Hardness 90 IRHD; German and English version EN 2799:2018

BS EN 2796:2018 航空航天系列 氟碳橡胶（FKM） 低压缩设置 硬度60IRHD

Aerospace series. Fluorocarbon rubber (FKM). Low compressions set. Hardness 60 IRHD

EN 2796:2018 航空航天系列 氟碳橡胶（FKM） 低压缩形变 硬度 60 IRHD

Aerospace series - Fluorocarbon rubber (FKM) - Low compressions set - Hardness 60 IRHD

BS EN 2799:2018 航空航天系列 氟碳橡胶（FKM） 低压缩设置 硬度90IRHD

Aerospace series. Fluorocarbon rubber (FKM). Low compressions set. Hardness 90 IRHD

DIN EN 2899:2018 航空航天系列.硫化橡胶.与硫化橡胶接触的金属潮湿环境中的腐蚀敏感性试验; 德文和英文版本EN 2899-2018

This document defines tests on the susceptibility to corrosion in a damp atmosphere of metals in contact with vulcanized rubbers.

Aerospace series - Vulcanized rubbers - Test on the susceptibility to corrosion in a damp atmosphere of metals in contact with vulcanized rubbers; German and English version EN 2899:2018

EN 2799:2018 航空航天系列 氟碳橡胶（FKM） 低压缩形变 硬度 90 IRHD

Aerospace series - Fluorocarbon rubber (FKM) - Low compressions set - Hardness 90 IRHD

BS EN 2899:2018 航空航天系列 硫化橡胶 与硫化橡胶接触的金属在潮湿气氛中的腐蚀敏感性试验

What is BS EN 2899- Susceptibility of metals to corrosion in contact with vulcanized rubbers about? BS EN 2899 is a standard that serves technical specifications on the susceptibility of metals to corrosion in contact with vulcanized rubbers that enables detection and prevention of corrosion in metal parts in aerospace applications. BS EN 2899 defines tests on the susceptibility to corrosion in a damp atmosphere of metals in contact with vulcanized rubbers. Who is BS EN 2899- Susceptibility of metals to corrosion in contact with vulcanized rubbers for? BS EN 2899 on the susceptibility of metals to corrosion in contact with vulcanized rubbers applies to: Manufacturers of vulcanized rubbers for aerospace applications Dealers and importers of vulcanized rubbers for aerospace applications Testing houses and labs in the aerospace industry Safety and quality assurance services Why should you use BS EN 2899- Susceptibility of metals to corrosion in contact with vulcanized rubbers ? Vulcanized rubber is a rubber that is hardened through heat and sulfur. It is made by a curing process in which the rubber's elastomers harden in response to heat and sulfur. The resulting rubber has good tensile strength, viscosity, hardness and extensibility. In aerospace applications, vulcanized rubber often comes in con...

Aerospace series. Vulcanized rubbers. Test on the susceptibility to corrosion in a damp atmosphere of metals in contact with vulcanized rubbers

EN 2899:2018 航空航天系列 硫化橡胶 与硫化橡胶接触的金属在潮湿环境中的腐蚀敏感性试验

Aerospace series - Vulcanized rubbers - Test on the susceptibility to corrosion in a damp atmosphere of metals in contact with vulcanized rubbers

DIN EN 2795:2018 航空航天系列 氟碳橡胶（FKM） 低压缩形变 硬度 50 IRHD

This document specifies the properties of fluorocarbon rubber (FKM), low compression set, hardness 50 IRHD, for aerospace applications.

Aerospace series - Fluorocarbon rubber (FKM) - Low compressions set - Hardness 50 IRHD; German and English version EN 2795:2018

BS EN 2795:2018 航空航天系列 氟橡胶（FKM） 低压缩形变 硬度 50IRHD

1   Scope This document specifies the properties of fluorocarbon rubber (FKM) 1) , low compression set, hardness 50 IRHD, for aerospace applications.

Aerospace series. Fluorocarbon rubber (FKM). Low compressions set. Hardness 50 IRHD

NF L17-261:2018 航空航天系列.硅氟橡胶.61类.特性

Aerospace series - Fluorosilicone rubbers - Class 61 - Characteristics

BS EN 2850:2017 航空航天系列. 碳纤维热固性树脂.单向层压板. 平行于纤维方向的压缩试验

Aerospace series. Carbon fibre thermosetting resin - Unidirectional laminates. Compression test parallel to fibre direction

ASTM D3039/D3039M-17 聚合物基复合材料拉伸性能的标准试验方法

1.1 This test method determines the in-plane tensile properties of polymer matrix composite materials reinforced by high-modulus fibers. The composite material forms are limited to continuous fiber or discontinuous fiber-reinforced composites in which the laminate is balanced and symmetric with respect to the test direction. 1.2 The values stated in either 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 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 Test Method for Tensile Properties of Polymer Matrix Composite Materials

EN 2850:2017 航空航天系列碳纤维热固性树脂单向层压板平行于纤维方向的压缩试验

Aerospace series - Carbon fibre thermosetting resin - Unidirectional laminates - Compression test parallel to fibre direction

DIN 65262-1:2017 航空航天系列 密封化合物 第1部分：聚硫化物聚合物基，技术规范

Aerospace series - Sealing compounds - Part 1: Polysulphide polymer base, Technical specification; Text in German and English

DIN EN 2823:2017 航空航天系列-纤维增强塑料-暴露于潮湿大气对物理和机械特性影响的测定

Aerospace series - Fibre reinforced plastics - Determination of the effect of exposure to humid atmosphere on physical and mechanical characteristics; German and English version EN 2823:2017

ASTM E2533-17 航空航天应用中使用的聚合物基体复合材料无损检测标准指南

1.1 This guide provides information to help engineers select appropriate nondestructive testing (NDT) methods to characterize aerospace polymer matrix composites (PMCs). This guide does not intend to describe every inspection technology. Rather, emphasis is placed on established NDT methods that have been developed into consensus standards and that are currently used by industry. Specific practices and test methods are not described in detail, but are referenced. The referenced NDT practices and test methods have demonstrated utility in quality assurance of PMCs during process design and optimization, process control, after manufacture inspection, in-service inspection, and health monitoring. 1.2 This guide does not specify accept-reject criteria and is not intended to be used as a means for approving composite materials or components for service. 1.3 This guide covers the following established NDT methods as applied to PMCs: Acoustic Emission (AE, 7), Computed Tomography (CT, 8), Leak Testing (LT, 9), Radiographic Testing, Computed Radiography, Digital Radiography, and Radioscopy (RT, CR, DR, RTR, 10), Shearography (11), Strain Measurement (contact methods, 12), Thermography (13), Ultrasonic Testing (UT, 14), and Visual Testing (VT, 15). 1.4 The value of this guide consists of the narrative descriptions of general procedures and significance and use sections for established NDT practices and test methods as applied to PMCs. Additional information is provided about the use of currently active standard documents (an emphasis is placed on applicable standard guides, practices, and test methods of ASTM Committee E07 on Nondestructive Testing), geometry and size considerations, safety and hazards considerations, and information about physical reference standards. 1.5 To ensure proper use of the referenced standard documents, there are recognized NDT specialists that are certified in accordance with industry and company NDT specifications. It is recommended that a NDT specialist be a part of any composite component design, quality assurance, in-service maintenance or damage examination. 1.6 This guide summarizes the application of NDT procedures to fiberand fabric-reinforced polymeric matrix composites. The composites of interest are primarily, but not exclusively limited to those containing high modulus (greater than 20 GPa (3×106 psi)) fibers. Furthermore, an emphasis is placed on composites with continuous (versus discontinuous) fiber reinforcement. 1.7 This guide is applicable to PMCs containing but not limited to bismaleimide, epoxy, phenolic, poly(amide imide), polybenzimidazole, polyester (thermosetting and thermoplastic), poly(ether ether ketone), poly(ether imide), polyimide (thermosetting and thermoplastic), poly(phenylene sulfide), or polysulfone matrices; and alumina, aramid, boron, carbon, glass, quartz, or silicon carbide fibers. 1.8 The composite materials considered herein include uniaxial laminae, cross-ply laminates, angle-ply laminates, and sandwich constructions. The composite components made therefrom include filament-wound pressure vessels, flight control surfaces, and various structural composites. 1.9 For current and potential NDT procedures for finding indications of discontinuities in the composite overwrap in filament-wound pressure vessels, also known as composite overwrapped pressure vessels (COPVs), refer to Guide E2981. 1.10 For a summary of the application of destructive ASTM standard practices and test methods (and other supporting standards) to continuous-fiber reinforced PMCs, refer to Guide D4762. 1.11 The values stated in SI units are to be regarded as the standard. The values given in parentheses are provided for information only. 1.12 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 and health practices and determine the applicability of regulatory limitations prior to use. 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 June 1, 2017. Published June 2017. Originally approved in 2009. Last previous edition approved in 2016 as E2533–16a. DOI: 10.1520/E2533-17. 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 1.13 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 Testing of Polymer Matrix Composites Used in Aerospace Applications