V13 航空与航天用非金属材料 标准查询与下载

SAE AMS1528D-2008 飞行器外表面用压力喷洒式乳状清洁剂

This specification covers an emulsion-type, low-foaming cleaner in the form of a liquid. This cleaner has been used typically for removing soils from painted and unpainted exterior surfaces of aircraft by pressure spray or manual applications, but usage is not limited to such applications.

Cleaner for Aircraft Exterior Surfaces, Emulsion, Pressure-Spray Type

SAE AMS1551A-2008 涡轮发动机气路用含水型清洁剂

This specification covers a solvent-free cleaner in the form of an aqueous-base liquid concentrate or a ready-to-use liquid. This cleaner has been used typically for cleaning installed turbine engines by spraying diluted cleaner or ready-to-use cleaner into the intake during a starter crank operation or on-line engine cleaning in accordance with the engine manufacturer's procedure, but usage is not limited to such applications.

Cleaner, Turbine Engine Gas Path Aqueous Type

SAE AMS-C-27725C-2008 用于250℉(121℃)的航空器整体燃料箱用聚亚安酯防腐蚀涂层

This specification covers two types of polyurethane coatings. The coating materials covered by this specification have been used typically for the protection of aircraft integral fuel tanks against corrosion from fuel contaminants but usage is not limited to such applications. They are suitable for use in a service temperature range from -65 to +250 ?F (-54 to +121 ?C).

Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks for Use to 250 °F (121 °C)

SAE AS27198A-2008 槽内铸模的平密封橡胶(-65～+350℉耐燃)

Seal, Plain, Rubber, (-65 to + 350 Degrees F Fuel Resistant), Mold in GrooveTABLE 1 is about NOMINAL TUBE OD REF. etc..

Seal, Plain, Rubber, (-65 to + 350 Degrees F Fuel Resistant), Mold in Groove

SAE AMS3251H-2008 通用中型合成橡胶和软木合成物

This specification covers a synthetic rubber and cork composition in the form of sheet, strip, and molded shapes. This product has been used typically for parts, such as packings, seals, grommets, line support blocks, and tank strap pads, where cushioning and vibration damping are of prime importance, but usage is not limited to such applications.

Synthetic Rubber and Cork Composition General Purpose Medium

SAE AMS3278A-2008 密封和涂料混合物:通用整体燃料罐/燃料腔用耐高拉伸强度/延伸的聚氨酯(PUR)燃料

This specification covers polyurethane (PUR) in the form of two-component sealing compounds. This product has been used typically for contact with fuels, but usage is not limited to such applications. Each application should be considered separately. This polyurethane (PUR) has a service temperature range of -65 to +250 °F (-54 to 121 °C) with a continuous fuel service temperature range of -65 to +160 °F (-54 to +71 °C). It may be used for faying surface sealing, wet-installation of fasteners, overcoat of fasteners, sealing joints and seams and, in some cases, as a non-structural adhesive. NOTE: The use of an adhesion promoter shall be required to obtain proper adhesion.

Sealing and Coating Compound: Polyurethane (PUR) Fuel Resistant High Tensile Strength / Elongation For Integral Fuel Tanks / Fuel Cavities / General Purpose

SAE AMS3250J-2008 通用软质合成橡胶和软木合成物

This specification covers a synthetic rubber and cork composition in the form of sheet, strip, and molded shapes. Application This product has been used typically for parts, such as packings, seals, grommets, line support blocks, and tank strap pads, where cushioning and vibration damping are of prime importance, but usage is not limited to such applications.

Synthetic Rubber and Cork Composition General Purpose Soft

ASTM F1111-08b(2013) 飞机保养化学品对低脆性镉板腐蚀性的标准试验方法

3.1 The data generated by this test method shall be used to determine whether low embrittling cadmium plated parts are liable to be corroded or damaged by application of the test material during routine maintenance operations. 1.1 This test method is intended as a means of determining the corrosive effects of aircraft maintenance chemicals on low-embrittling cadmium plating used on aircraft high-strength steel, under conditions of total immersion by quantitative measurements of weight change. 1.2 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. For specific hazard statements see Section 6, 4.1.

Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals

ASTM F790-08(2013) 航空航天塑料透明外壳用试验材料的标准规范

3.1 This guide is intended for use by material suppliers, aircraft transparent enclosure fabricators, air-frame manufacturers, government agencies, and others that may become involved in the testing of transparency components. These test methods provide data on both individual materials and material combinations commonly utilized in the fabrications of aerospace transparent enclosures comprised of monolithic plastic, coated monolithic plastic or laminated constructions containing plastics. 3.2 Primary properties and their long term stability are critical to the performance of aerospace transparent enclosures. Property measurement tests define as-manufactured material properties of these materials. Aging procedures provide for exposure of parts or representative sections to environments that may induce changes in material properties as determined in property measurement tests. Property measurement tests performed before and after aging exposure provide a means of estimating the potential usable life span of a transparency or to compare the durability of one material with another. 3.3 When employing these test methods for comparison of materials for weathering effects the user should be aware that the many factors influencing degradation due to weathering vary from one location to another. For direct weathering comparisons, all material(s) should undergo exposure conditions and property measurements testing at the same time. 3.4 The test methods listed include those considered critical to the performance of aircraft transparent enclosures. Other test methods to evaluate materials may also be performed. Additional test methods are in preparation and will be incorporated. The user is advised to employ the latest revision of any test method. 3.5 The dominant component of all transparent enclosures is one, or more, rigid transparent sheet(s). The sheet(s) must permit the necessary visibility while providing structural integrity and protecting the aircraft interior from external environments as required by the specific aircraft design. 3.6 In its most simple form, the rigid transparent sheet may be the only component of a transparent enclosure. 3.7 When more than one rigid transparent sheet is employed, the sheets are laminated with a controlled thickness with either an air gap or with a transparent adhesive known as an interlayer. 3.8 Transparent enclosure designs may use multiple rigid transparent sheets to take advantage of specific properties of different materials. In this instance, there will be functions required of one of the sheets but not the other. 3.9 The test methods, practices and guides listed are a summary of the available test methods applicable to plastic transparent enclosures. They are presented in this format to simplify the search and to enable the user to determine if a method applicable to his requirements is available. 1.1 This guide is intended to summarize the standard test methods available on individual and composite materials utilized in fabrication of aerospace plastic transparent enclosures. As such, it is intended to specifically include transparent thermoplastics, transparent elastomers, and reinforced plastics, whether thermoplastic or thermosetting. 1.2 This guide is intended as an aid in the search for test methods pertinent to A......

Standard Guide for Testing Materials for Aerospace Plastic Transparent Enclosures

ASTM E377-08 烧蚀材料内部温度测量的标准实施规程

Internal temperature measurements are made on both in-flight vehicles and on-ground test specimens; and, because of the importance of the temperature measurements to the design of various missile and spacecraft heat shields, it is essential that care be taken to minimize the sources of error in obtaining these measurements. Over the past several years, the problems of using thermocouples to obtain accurate temperature measurements in low-conductivity specimens have been studied by various people to isolate the sources of error and to establish improved temperature measurement techniques. The major sources of error are listed in this document and recommended solutions to the problems are given.1.1 This practice covers methods for instrumenting low-conductivity specimens for testing in an environment subject to rapid thermal changes such as produced by rocket motors, atmospheric re-entry, electric-arc plasma heaters, and so forth. Specifically, practices for bare-wire thermocouple instrumentation applicable to sheath-type thermocouples are discussed. 1.2 The values stated in inch-pound units are to be regarded as the standard. The metric equivalents of inch-pound units may be approximate. 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 Practice for Internal Temperature Measurements in Low-Conductivity Materials

ASTM F790-08 航空航天塑料透明外壳用试验材料的标准规范

This guide is intended for use by material suppliers, aircraft transparent enclosure fabricators, air-frame manufacturers, government agencies, and others that may become involved in the testing of transparency components. These test methods provide data on both individual materials and material combinations commonly utilized in the fabrications of aerospace transparent enclosures comprised of monolithic plastic, coated monolithic plastic or laminated constructions containing plastics. Primary properties and their long term stability are critical to the performance of aerospace transparent enclosures. Property measurement tests define as-manufactured material properties of these materials. Aging procedures provide for exposure of parts or representative sections to environments that may induce changes in material properties as determined in property measurement tests. Property measurement tests performed before and after aging exposure provide a means of estimating the potential usable life span of a transparency or to compare the durability of one material with another. When employing these test methods for comparison of materials for weathering effects the user should be aware that the many factors influencing degradation due to weathering vary from one location to another. For direct weathering comparisons, all material(s) should undergo exposure conditions and property measurements testing at the same time. The test methods listed include those considered critical to the performance of aircraft transparent enclosures. Other test methods to evaluate materials may also be performed. Additional test methods are in preparation and will be incorporated. The user is advised to employ the latest revision of any test method. The dominant component of all transparent enclosures is one, or more, rigid transparent sheet(s). The sheet(s) must permit the necessary visibility while providing structural integrity and protecting the aircraft interior from external environments as required by the specific aircraft design. In its most simple form, the rigid transparent sheet may be the only component of a transparent enclosure. When more than one rigid transparent sheet is employed, the sheets are laminated with a controlled thickness with either an air gap or with a transparent adhesive known as an interlayer. Transparent enclosure designs may use multiple rigid transparent sheets to take advantage of specific properties of different materials. In this instance, there will be functions required of one of the sheets but not the other. The test methods, practices and guides listed are a summary of the available test methods applicable to plastic transparent enclosures. They are presented in this format to simplify the search and to enable the user to determine if a method applicable to his requirements is available.1.1 This guide is intended to summarize the standard test methods available on individual and composite materials utilized in fabrication of aerospace plastic transparent enclosures. As such, it is intended to specifically include transparent thermoplastics, transparent elastomers, and reinforced plastics, whether thermoplastic or thermosetting. 1.2 This guide is intended as an aid in the search for test methods pertinent to Aerospace Plastic Transparent Enclosures. It should be understood that all methods listed may not apply to all enclosures. 1.3 The standards included refer to the properties or aspects listed in Table 1. The properties or aspects are listed in alphabetical order and the descriptions used are intended to facilitate the search. 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 and health practices and determi......

Standard Guide for Testing Materials for Aerospace Plastic Transparent Enclosures

BS 2F 151:2007 航空航天用无梭编织棉网规范

This British Standard specifies the requirements for shuttleless woven cotton webbing in a range of widths for aerospace purposes. NOTE The latest revision of an Aerospace Series standard is indicated by a prefix number.

Specification for Shuttleless woven cotton webbing for aerospace purposes

BS 6F 49:2007 航空航天用梭编织棉网规范

This British Standard specifies the requirements for shuttle woven cotton webbing in a range of widths for aerospace purposes. NOTE The latest revision of an Aerospace Series standard is indicated by a prefix number.

Specification for shuttle woven cotton webbing for aerospace purposes

DIN EN 2434-005:2007 航空航天系列.涂料和清漆.双组分冷固化聚氨酯光洁度.第005部分:军用高柔性和耐化学试剂性

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 005: High flexibility and chemical agent resistance for military application; German and English version EN 2434-005:2006

DIN EN 4588:2007 航空航天系列.涂料和清漆.防滑双组分冷加工聚氨酯涂料

Aerospace series - Paints and varnishes - Two component, cold curing polyurethane paint, anti slip; German and English version EN 4588:2007

DIN EN 3840:2007 航空航天系列.涂料和清漆.技术规范

This standard defines the technical requirements for the qualification, manufacture, inspection and the delivery of paints and varnishes for use in aerospace applications. It shall be applied in conjunction with the EN material specification.

Aerospace series - Paints and varnishes - Technical specification; German and English version EN 3840:2007

BS EN 3840:2007 航空航天系列.涂料和清漆.技术规范

This standard defines the technical requirements for the qualification, manufacture, inspection and the delivery of paints and varnishes for use in aerospace applications. It shall be applied in conjunction with the EN material specification.

Aerospace series - Paints and varnishes - Technical specification

BS EN 4170:2007 航空航天系列.涂料和清漆.防冷裂缝温度循环测量的试验方法

This standard describes a procedure of ageing to assess the resistance of a coated panel (metallic or organic substrate) to a temperature cycle (cold, hot, hot and wet) for aerospace purposes. This test deals with the assessment of the capability of the paint to support modification of internal stresses without any crack formation, peeling or other defects due to modification of the mechanical properties of the paint system.

Aerospace series - Paints and varnishes - Test method for measurement of resistance to cold crack temperature cycle

SAE AMS3819C-2007 航空器主要和次要结构表面用织物清洁处理

This specification covers both woven and nonwoven absorbent materials supplied as either dry cloths or as presaturated cloths for solvent cleaning process applications. These products have been used typically in cleaning smooth or textured, metallic and nonmetallic surfaces preparatory to processing operations which are sensitive to residual surface contamination, but usage is not limited to such applications. Cloths qualified to this specification are not intended for use on transparencies.

Cloths, Cleaning For Aircraft Primary and Secondary Structural Surfaces

DIN EN 2436-006:2007 航空航天系列.涂料和清漆.不含铬酸盐的双组分冷加工环氧底漆的耐腐蚀性.第006部分:军用强耐腐蚀性

This standard defines the requirements for a two component,chromated and lead free epoxy,high corrosion resistant primer. The coating shall be suitable for use on chromic acid anodised or conversion coated aluminium alloys,fibre reinforced composite materials and other suitably prepared substrates.

Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing epoxy primer - Part 006: High corrosion resistance for military application; German and English version EN 2436-006:2006