49.025.01 航空航天制造用材料综合 标准查询与下载
共找到 372 条与 航空航天制造用材料综合 相关的标准，共 25 页
Aerospace series. Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668). Non heat treated. Forging stock. a or D
- ICS
- 49.025.01
- CCS
- V11
- 发布
- 2015-09-30
- 实施
- 2015-09-30
This European Standard specifies the requirements relating to: Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) Non heat treated Forging stock a or D 300 mm for aerospace applications.
Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) - Non heat treated - Forging stock - a or D ��300 mm
- ICS
- 49.025.01
- CCS
- V11
- 发布
- 2015-09-01
- 实施
3.1 This practice is a guideline for proper materials and process selection and application. The specific application of these guidelines must take into account contractual agreements, functional performance requirements for particular programs and missions, and the actual environments and exposures anticipated for each material and the equipment in which the materials are used. Guidelines are not replacements for careful and informed engineering judgment and evaluations and all possible performance and design constraints and requirements cannot be foreseen. This practice is limited to unmanned systems and unmanned or external portions of manned systems, such as the Space Station. Generally, it is applicable to systems in low earth orbit, synchronous orbit, and interplanetary missions. Although many of the suggestions and cautions are applicable to both unmanned and manned spacecraft, manned systems have additional constraints and requirements for crew safety which may not be addressed adequately in unmanned designs. Because of the added constraints and concerns for human-rated systems, these systems are not addressed in this practice. 1.1 The purpose of this practice is to aid engineers, designers, quality and reliability control engineers, materials specialists, and systems designers in the selection and control of materials and processes for spacecraft, external portion of manned systems, or man-tended systems. Spacecraft systems are very different from most other applications. Space environments are very different from terrestrial environments and can dramatically alter the performance and survivability of many materials. Reliability, long life, and inability to repair defective systems (or high cost and difficultly of repairs for manned applications) are characteristic of space applications. This practice also is intended to identify materials processes or applications that may result in degraded or unsatisfactory performance of systems, subsystems, or components. Examples of successful and unsuccessful materials selections and uses are given in the appendices.
Standard Practice for the Selection of Spacecraft Materials
- ICS
- 49.025.01
- CCS
- 发布
- 2015
- 实施
Aerospace - Alternative materials for fasteners; Inactive for new design
- ICS
- 49.025.01
- CCS
- V20
- 发布
- 2014-12
- 实施
本标准规定了民用飞机机舱内部非金属材料燃烧试验的试验类型、试验设备和器材、试样、试验要求、试验程序及试验报告。 本标准适用于民用飞机机舱内部非金属材料燃烧性能试验。
Burning test method for cabin interior nonmetallic material of civil aircraft
- ICS
- 49.025.01
- CCS
- V13
- 发布
- 2014-05-19
- 实施
- 2014-10-01
本标准规定了民用飞机机舱内部非金属材料燃烧试验类型、试验类型所对应的机舱内部非金属材料应用部位及燃烧性能要求等。 本标准适用于民用飞机机舱内部非金属材料性能检验。
Requirements of burning performance for cabin interior nonmetallic material of civil aircraft
- ICS
- 49.025.01
- CCS
- V13
- 发布
- 2014-05-19
- 实施
- 2014-10-01
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 004: Welding and brazing of homogeneous assemblies of high alloyed steels; German version EN 4632-004:2012, Corrigendum to DIN EN 4632-004:2013-11
- ICS
- 49.025.01
- CCS
- V22
- 发布
- 2014-03
- 实施
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys; German version EN 4632-006:2013
- ICS
- 49.025.01
- CCS
- V22
- 发布
- 2013-11-01
- 实施
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 004: Welding and brazing of homogeneous assemblies of high alloyed steels; German version EN 4632-004:2012
- ICS
- 49.025.01
- CCS
- V22
- 发布
- 2013-11-01
- 实施
his specification establishes the classification, technical requirements, tests, and test procedures for the qualification, approval, and quality verification of all materials used in the liquid penetrant methods of inspection with the exception of those excluded in the application section.
Inspection Material, Penetrant
- ICS
- 49.025.01
- CCS
- 发布
- 2013-10-17
- 实施
Aerospace series. Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20). As forged. Forging stock. a or D
- ICS
- 49.025.01
- CCS
- V11
- 发布
- 2013-08-31
- 实施
- 2013-08-31
Aerospace series. Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20). As forged. Forging stock. a or D
- ICS
- 49.025.01
- CCS
- V11
- 发布
- 2013-08-31
- 实施
- 2013-08-31
This standard specifies the requirements relating to: Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) As forged Forging stock a or D 200 mm 690 MPa < Rm < 880 MPa for aerospace applications.
Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D <= 200 mm - 690 MPa <= Rm <= 880MPa
- ICS
- 49.025.01
- CCS
- 发布
- 2013-08-02
- 实施
- 2013-08-02
This standard specifies the requirements relating to: Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) As forged Forging stock a or D
Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D <= 200 mm - 690 MPa <= Rm <= 960MPa
- ICS
- 49.025.01
- CCS
- 发布
- 2013-08-02
- 实施
- 2013-08-02
Aerospace series. Weldability and brazeability of materials in aerospace constructions. Homogeneous assemblies of titanium alloys
- ICS
- 49.025.01
- CCS
- V11
- 发布
- 2013-04-30
- 实施
- 2013-04-30
This European Standard defines degrees of weldability and brazeability for materials or families of materials used in the aerospace applications. It comprises a series of sheets, by materials or by material family, which: indicate the main titles, the typical chemical composition and the main characteristics, contain recommendations for welding and brazing, indicate a degree of weldability or brazeability for a given process under defined conditions. It is applicable without restriction for the manufacturing of new parts or for repair.
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys
- ICS
- 49.025.01
- CCS
- V10
- 发布
- 2013-03-01
- 实施
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 004: welding and brazing of homogeneous assemblies of high alloyed steels
- ICS
- 49.025.01
- CCS
- V22
- 发布
- 2013-02-28
- 实施
- 2013-02-28
This European Standard specifies the specific rules for the drafting and presentation of heat resisting alloy material standards for aerospace applications.It should be used in conjunction with EN 4500-001.
Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 003: Specific rules for heat resisting alloys
- ICS
- 49.025.01
- CCS
- 发布
- 2012-11-16
- 实施
- 2012-11-16
This European Standard specifies the general rules for the drafting and presentation of metallic material standards for aerospace applications.It is supported by additional rules specific to:- Aluminium, aluminium alloys and magnesium alloys EN 4500-2;- H
Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 001: General rules
- ICS
- 49.025.01
- CCS
- 发布
- 2012-11-16
- 实施
- 2012-11-16
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 004: Welding and brazing of homogeneous assemblies of high alloyed steels
- ICS
- 49.025.01
- CCS
- 发布
- 2012-10-31
- 实施
- 2012-10-31
