V13 航空与航天用非金属材料 标准查询与下载

SAE AMS3690C-2009 室温固化环氧树脂复合粘合剂

This specification covers a two-component compound, an epoxy resin base and a hardener, in the form of a paste. This adhesive compound has been used typically for non-structural bonding of metallic alloys and thermosetting plastics to themselves and to each other; it is intended primarily as an adhesive for electrical components nd devices operating at not higher than 185 °F (85 °C), but usage is not limited to such applications.

Adhesive Compound, Epoxy, Room Temperature Curing

SAE AMS3202M-2009 耐干热丁腈橡胶(NBR),55-65

This specification covers a nitrile (NBR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. These products have been used typically for parts such as packings, bushings, grommets, and seals requiring resistance to dry heat, but usage is not limited to such applications. Each application should be considered individually.

Butadiene Acrylonitrile (NBR) Rubber Dry Heat Resistant, 55-65

SAE AMS-I-83387A-2009 磁性橡胶的检查过程

This specification covers both the material and the examination process of an inspection material in the form of a dispersion of magnetic particles in a controlled viscosity rubber base that cures at room temperature by addition of one or more curing agents. The test object is magnetized with the uncured rubber covering the area of interest. The magnetic particles then migrate to the leakage field caused by the discontinuity. As the rubber cures, discontinuity indications remain in place on the rubber. The product may be supplied in a variety of viscosities and colors.

Inspection Process, Magnetic Rubber

SAE AMS3197L-2009 氯丁(CR)橡胶软海绵

This specification covers a chloroprene (CR) rubber sponge in the form of sheet, strip, molded shapes, or other forms, as ordered. These products have been used typically for general applications requiring the use of open-cell, soft sponge rubber pads and seals operating from -40 to +176 °F (-40 to +80 °C) but usage is not limited to such applications.

Sponge, Chloroprene (CR) Rubber, Soft

DIN 65671:2009 航空航天.玻璃纤维和非活性热塑塑料制预浸渍纤维薄板材和带材.技术规范.德文文本和英文文本

This standard is applicable to fabric sheet and tape prepregs from glass fibres and non-reactive thermo- plastics, hereinafter called prepregs.

Aerospace - Fabric sheet and tape prepreg from glas fibres and non-reactive thermoplastics - Technical specification; Text in German and English

DIN 65672:2009 航空航天.连续丝纤维增强的非电抗热塑层压板.试验板的制备.德文文本和英文文本

This standard specifies the preparation of laminate test panels from textile fabrics, UD products and non-reactive thermoplastics. From the panels test specimen are taken in accordance with the test standard, the specimens being intended for the determination of the characteristics of continuous filament fibre reinforced thermoplastics and for verifying the laminate and sandwich properties.

Aerospace - Continuous filament fibre reinforced laminates with non-reactive thermoplastics - Preparation of test panels; Text in German and English

DIN 65628:2009 航空航天.玻璃纤维和非活性热塑塑料制预浸渍纤维薄板材和带材.技术规范.德文和英文文本

This standard is applicable to fabric sheet and tape prepregs from aramid fibres and non-reactive thermoplastics, hereinafter called prepregs.

Aerospace - Fabric sheet and tape prepreg from aramid fibres and non-reactive thermoplastics - Technical specification; Text in German and English

SAE AMS3275C-2009 非石棉纤维,耐燃料及耐油丁腈橡胶(NBR)薄板

This specification covers a compressed non-asbestos fiber and acrylonitrile butadiene (NBR) rubber in the form of sheet. This sheet has been used typically for gaskets, sealing between metal surfaces, in contact with fuels or with lubricating oil up to 302 °F (150 °C), but usage is not limited to such applications. Each application should be considered individually.

Sheet, Acrylonitrile Butadiene (NBR) Rubber and Non-Asbestos Fiber, Fuel and Oil Resistant

SAE AMS3201L-2009 耐干热丁腈橡胶(NBR),35-45

This specification covers a nitrile (NBR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. These products have been used typically for parts, such as packings, bushings, grommets, and seals requiring resistance to dry heat, but usage is not limited to such applications. Each application should be considered individually.

Butadiene Acrylonitrile (NBR) Rubber, Dry Heat Resistant, 35-45

SAE AMS3332E-2009 耐极低温度硅橡胶,15-30

This specification covers an extreme low-temperature-resistant silicone rubber in the form of sheet, strip, and molded shapes Primarily for rubber-like parts required to operate or seal from -112 to +446 °F (-80 to +230 °C), compounded especially for operation at extreme low temperatures. Silicone rubber is resistant to deterioration by weathering and by high-aniline-point petroleum-base oils and remains flexible over the temperature range noted. This material is not normally suitable for use in contact with low-aniline-point petroleum-base fluids, including fuels, due to excessive swelling.

Silicone Rubber, Extreme Low Temperature Resistant, 15-30

SAE AMS3327D-2009 耐高温燃料耐油氟硅(FVMQ)橡胶,70-80

This specification covers a fluorosilicone (FVMQ) rubber in the form of sheet, strip, and molded shapes. These products have been used typically for parts requiring resistance to jet fuel and lubricating oils, but usage is not limited to such applications. Generally, products are usable over a temperature range of -76 to +302 °F (-60 to +150 °C) ; each application, however, has to be considered individually.

Fluorosilicone (FVMQ) Rubber, High Temperature Fuel and Oil Resistant 70-80

SAE AMS3334E-2009 耐极低温度硅橡胶,35-45

This specification covers a silicone rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. Primarily for rubber-like parts required to operate or seal from -112 to +248 °F (-80 to +120 °C), compounded especially for operation at extreme low temperatures. Silicone rubber is resistant to deterioration by weathering and by high-aniline-point petroleum-base oils and remains flexible over the temperature range noted. These products are not normally suitable for use in contact with low-aniline-point petroleum-base fluids, including fuels, due to excessive swelling.

Silicone Rubber, Extreme Low Temperature Resistant, 35-45

SAE AMS3204M-2009 耐低温合成橡胶,25-35

This specification covers a synthetic rubber in the form of sheet, strip, tubing, extrusion, and molded shapes. These products have been typically used for parts, such as sleeves, fairings, grommets, and window channels, where resistance to low temperature is of prime importance, but usage is not limited to such applications. Each application should be considered individually.

Rubber Synthetic Low-Temperature Resistant, 25-35

SAE AMS3307D-2009 不耐油低压缩永久变形硅橡胶(VMQ),65-75

This specification covers a silicone (VMQ) rubber in the form of sheet, strip, and molded shapes. Primarily for parts required to operate or seal from -55 to +200 °C (-67 to +392 °F), compounded especially for low compression set. Silicone rubber is resistant to deterioration by ozone, smog, and weathering and remains flexible over the temperature range noted. These products are not intended for use with petroleum-base fluids or lubricants. Certain design applications may cause these products to be susceptible to cutting, tearing, and abrasion.

Rubber, Silicone (VMQ) Low Compression Set, Non-Oil-Resistant, 65-75

SAE AMS3325E-2009 耐燃料及耐油氟硅(FVMQ)橡胶,55-65

This specification covers a fluorosilicone (FVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. These products have been used typically for parts requiring resistance to jet fuel and lubricating oils, but usage is not limited to such applications. Generally, products are usable over a temperature range of -76 to +302 °F (-60 to + 150 °C ); each application, however, has to be considered individually.

Fluorosilicone (FVMQ) Rubber, Fuel and Oil Resistant, 55-65

SAE AMS3100C-2009 聚硫密封剂用附着力助剂

This specification covers adhesion promoters in the formof a liquid, either in bulk or aerosol form. This product has been used typically to enhance the adhesion of polysulfide sealing compounds or adhesives to AMS-C-27725 integral fuel tank coating, MIL-PRF-23377 epoxy primer, MIL-PRF-85582 water borne primer, and bare titanium alloy substrates, but usage is not limited to such applications. Care should be exercised around plastic substrates (e.g. polycarbonates, acrylics) as the formulary solvents may tend to craze these surfaces.

Adhesion Promoter For Polysulfide Sealing Compounds

ASTM F1362-09 航天工业用上釉叠层材料的剪切强度和剪切模数测试方法

The basic material properties obtained from this test method can be used in the control of the quality of interlayers, in the theoretical equations for designing laminated transparencies, and in the evaluation of new interlayers.1.1 This test method covers the determination of the shear strength and shear modulus of interlayer materials that are restrained by relatively high modulus plies in laminated transparencies. This test method can be used with single or multiple plies of the same interlayer materials. 1.2 The values stated in SI units are to be regarded as the standard. The values in parentheses are for information only. 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 and health practices and determine the applicability of regulatory limitations prior to use.

Standard Test Method for Shear Strength and Shear Modulus of Aerospace Glazing Interlayer Materials

ASTM F428-09 航空航天用玻璃外壳抗划痕硬度的标准试验方法

Scratches exist on all glass surfaces. Often there are very fine scratches from cleaning operations that are not visible when looking through the glass. Visible scratches may be distracting to the observer looking through the transparency. Therefore, a procedure to define the severity scratches is useful. A visual standard is used because it is not practical to measure the dimensions of the fine scratches in the scope of this test method.1.1 This test method covers the visual inspection of scratches on the glass surface of aerospace transparent enclosures. 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 may involve hazardous materials, operations, and equipment. 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.

Standard Test Method for Intensity of Scratches on Aerospace Glass Enclosures

ASTM F548-09 航空航天透明塑料抗划痕强度试验方法

Scratches exist on all transparent plastic surfaces. Usually they are very fine scratches from cleaning operations that are not visible when looking through the plastic. Deeper scratches may result from careless cleaning or handling. While these may not be deep enough to affect the structural integrity of the part, their appearance in certain locations may be distracting to the observer looking through the plastic. Therefore, a procedure to define these scratches is useful.1.1 This test method covers the visual inspection of shallow or superficial scratches on the surface of aerospace transparent plastic materials. 1.2 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.

Standard Test Method for Intensity of Scratches on Aerospace Transparent Plastics

ASTM E2662-09 用于航空航天器的平板复合材料和夹层芯材X线检查的标准实施规程

Radiologic examination may be used during product and process design optimization, on line process control, after manufacture inspection, and in service inspection. In addition to verifying structural placement, radiologic examination can be used in the case of honeycomb core materials to detect node bonds, core-to-core splices, and core-to-structure splices. Radiologic examination is especially well suited for detecting sub-surface flaws. The general types of defects detected by radiologic examination include blown core, core corrosion, damaged filaments, density variation, entrapped fluid, fiber debonding, fiber misalignment, foreign material, fractures, inclusions, microcracks, node bond failure, porosity/voids, and thickness variation. Factors that influence image formation and X-ray attenuation in radiologic examination , and which are relevant to interpreting the images for the conditions of interest, should be included in the examination request. Examples are, but not limited to, the following: laminate (matrix and fiber) material, lay-up geometry, fiber volume fraction (flat panels); facing material, core material, facing stack sequence, core geometry (cell size); core density, facing void content, adhesive void content, and facing volume percent reinforcement (sandwich core materials); overall thickness, specimen alignment, specimen geometry relative to the beam (flat panels and sandwich core materials).1.1 This practice is intended to be used as a supplement to Practices E 1742, E 1255, and E 2033. 1.2 This practice describes procedures for radiologic examination of flat panel composites and sandwich core materials made entirely or in part from fiber-reinforced polymer matrix composites. Radiologic examination is: a) radiographic (RT) with film, b) Computed Radiography (CR) with Imaging Plate, c) Digital Radiology (DR) with Digital Detector Array’s (DDA), and d) Radioscopic (RTR) Real Time Radiology with a detection system such as an Image Intensifier. The composite materials under consideration typically contain continuous high modulus fibers (> 20 GPa), such as those listed in 1.4. 1.3 This practice describes established radiological examination methods that are currently used by industry that have demonstrated utility in quality assurance of flat panel composites and sandwich core materials during product process design and optimization, process control, after manufacture inspection, in service examination, and health monitoring. 1.4 This practice has utility for examination of flat panel composites and sandwich constructions 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. Typical as-fabricated geometries include uniaxial, cross ply and angle ply laminates; as well as honeycomb core sandwich constructions. 1.5 This practice does not specify accept-reject criteria and is not intended to be used as a means for approving flat panel composites or sandwich core materials for service. 1.6 To ensure proper use of the referenced standards, there are recognized nondestructive testing (NDT) specialists that are certified according to 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. 1.7 Thi......

Standard Practice for Radiologic Examination of Flat Panel Composites and Sandwich Core Materials Used in Aerospace Applications