49.025.10 钢 标准查询与下载

21/30431252 DC BS EN 3525 航空航天系列 钢 15CrMoV6 (1.7334) 空气融化了 经过硬化和回火 盘子 6毫米≤a≤20毫米 1 080 MPa ≤ Rm ≤ 1 280 MPa

BS EN 3525. Aerospace series. Steel 15CrMoV6 (1.7334). Air melted. Hardened and tempered. Plates. 6 mm ≤ a ≤ 20 mm. 1 080 MPa ≤ Rm ≤ 1 280 MPa

OENORM EN 2213-2021 航空航天系列 钢 15CrMoV6（1.7334） 空气熔炼 淬火和回火 棒材 De <= 16 mm 980 MPa <= Rm <= 1180 MPa

Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Bars - De <= 16 mm - 980 MPa <= Rm <= 1180 MPa

OENORM EN 3523-2021 航空航天系列 钢 15CrMoV6（1.7334） 空气熔炼 淬火和回火 机加工棒材 De <= 100 mm 1080 MPa <= Rm <= 1280 MPa

Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Bar for machining - De <= 100 mm - 1080 MPa <= Rm <= 1280 MPa

prEN 3524-2021 航空航天系列 - 钢 15CrMoV6 (334) - 空气熔炼 - 淬火和回火 - 板材和带材 - 2 mm ≤ a ≤ 6 mm - 1080 MPa ≤ Rm ≤ 1280 MPa

Aerospace series - Steel 15CrMoV6 (334) - Air melted - Hardened and tempered - Sheets and strips - 2 mm ≤ a ≤ 6 mm - 1080 MPa ≤ Rm ≤ 1280 MPa

prEN 3525-2021 航空航天系列 - 钢 15CrMoV6 (334) - 空气熔炼 - 淬火和回火 - 板材 - 6 mm ≤ a ≤ 20 mm - 1080 MPa ≤ Rm ≤ 1280 MPa

Aerospace series - Steel 15CrMoV6 (334) - Air melted - Hardened and tempered - Plates - 6 mm ≤ a ≤ 20 mm - 1080 MPa ≤ Rm ≤ 1280 MPa

21/30431240 DC BS EN 2213 航空航天系列 钢 15CrMoV6 (1.7334) 空气融化了 经过硬化和回火 酒吧 德≤16毫米 980兆帕≤Rm≤1180兆帕

BS EN 2213. Aerospace series. Steel 15CrMoV6 (1.7334). Air melted. Hardened and tempered. Bars. De ≤ 16 mm. 980 MPa ≤ Rm ≤ 1 180 MPa

21/30431243 DC BS EN 2252 航空航天系列 钢 15CrMoV6 (1.7334) 锻件 酒吧 De≤100毫米 1 080 MPa ≤ Rm ≤ 1 250 MPa

BS EN 2252. Aerospace series. Steel 15CrMoV6 (1.7334). Forgings. Bars. De ≤ 100 mm. 1 080 MPa ≤ Rm ≤ 1 250 MPa

21/30431246 DC BS EN 3523 航空航天系列 钢 15CrMoV6 (1.7334) 空气融化了 经过硬化和回火 机加工用棒材 De≤100毫米 1 080 MPa ≤ Rm ≤ 1 280 MPa

BS EN 3523. Aerospace series. Steel 15CrMoV6 (1.7334). Air melted. Hardened and tempered. Bar for machining. De ≤ 100 mm. 1 080 MPa ≤ Rm ≤ 1 280 MPa

prEN 2252-2021 航空航天系列 - 钢 15CrMoV6 (1.7334) - 锻件 - 棒材 - De ≤ 100 mm - 1080 MPa ≤ Rm ≤ 1250 MPa

Aerospace series - Steel 15CrMoV6 (1.7334) - Forgings - Bars - De ≤ 100 mm - 1080 MPa ≤ Rm ≤ 1250 MPa

prEN 3523-2021 航空航天系列 - 钢 15CrMoV6 (1.7334) - 空气熔炼 - 淬火和回火 - 机加工棒材 - De ≤ 100 mm - 1080 MPa ≤ Rm ≤ 1280 MPa

Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Bar for machining - De ≤ 100 mm - 1080 MPa ≤ Rm ≤ 1280 MPa

prEN 2213-2021 航空航天系列 - 钢 15CrMoV6 (1.7334) - 空气熔炼 - 淬火和回火 - 棒材 - De ≤ 16 mm - 980 MPa ≤ Rm ≤ 1180 MPa

Aerospace series - Steel 15CrMoV6 (1.7334) - Air melted - Hardened and tempered - Bars - De ≤ 16 mm - 980 MPa ≤ Rm ≤ 1180 MPa

ASTM E192-20 投资钢铁铸件用于航空航天应用的标准参考射线照片

1.1 The reference radiographs provided in the adjunct to this standard illustrate various types and degrees of discontinuities occurring in thin-wall steel investment castings.2 Use of this standard for the specification or grading of castings requires procurement of the adjunct reference radiographs which illustrate the discontinuity types and severity levels. They are intended to provide the following: 1.1.1 A guide enabling recognition of thin-wall steel casting discontinuities and their differentiation both as to type and degree through radiographic examination. 1.1.2 Example radiographic illustrations of discontinuities and a nomenclature for reference in acceptance standards, specifications, and drawings. 1.2 Two illustration categories are covered as follows: 1.2.1 Graded—Six common discontinuity types each illustrated in eight degrees of progressively increasing severity. 1.2.2 Ungraded—Twelve single illustrations of additional discontinuity types and of patterns and imperfections not generally regarded as discontinuities. 1.3 The reference radiographs were developed for casting sections up to 1 in. (25.4 mm) in thickness. 1.4 This document may be used where there is no other applicable document existing or for other material thicknesses for which it is found to be applicable and for which agreement has been reached between the purchaser and manufacturer. NOTE 1—The set of reference radiographs, produced with X-rays in the range from 130 to 250 kVp, consist of 16 plates (81⁄2 by 11 in. (216 by 279 mm)) in a 93⁄4 by 111⁄2 in. (248 by 292 mm) ring binder. 1.5 From time to time, there may be minor changes to the process for manufacturing of the reference radiograph adjunct materials. These changes could include changes in the films or processing chemicals used, changes in the dies or printing for the cardboard mats, etc.; however, in all cases, these changes are reviewed by the Illustration Monitoring Subcommittee and all reference radiographs are reviewed against a fixed prototype image to ensure that there are no changes to the acceptance level represented by the reference radiographs. Therefore, the adjunct reference radiographs remain valid for use with this standard regardless of the date of production or the revision level of the text standard. 1.6 These film reference radiographs are not intended to illustrate the types and degrees of discontinuities found in aerospace investment castings when performing digital X-ray imaging. When performing digital X-ray imaging of these castings, refer to Digital Reference Images E2660. 1.7 Units—The values stated in inch-pound units are to be regarded as the standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard. 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.

Standard Reference Radiographs of Investment Steel Castings for Aerospace Applications

20/30425165 DC BS EN 3487 航空航天系列 钢 X6CrNiTi18-10 (1.4541) 空气融化了 软化了 机加工用棒材 a或D≤250毫米 500兆帕≤Rm≤700兆帕

BS EN 3487. Aerospace series. Steel X6CrNiTi18-10 (1.4541). Air melted. Softened. Bars for machining. a or D ≤ 250 mm. 500 MPa ≤ Rm ≤ 700 MPa

20/30425168 DC BS EN 3488 航空航天系列 钢 X6CrNiTi18-10 (1.4541) 空气融化了 软化了 板材和带材 a≤6毫米 500兆帕≤Rm≤700兆帕

BS EN 3488. Aerospace series. Steel X6CrNiTi18-10 (1.4541). Air melted. Softened. Sheets and strips. a ≤ 6 mm. 500 MPa ≤ Rm ≤ 700 MPa

20/30425171 DC BS EN 3480 航空航天系列 钢 X6CrNiTi18-10 (1.4541) 空气融化了 软化了 盘子 6 毫米 < a ≤ 50 毫米 500兆帕≤Rm≤700兆帕

BS EN 3480. Aerospace series. Steel X6CrNiTi18-10 (1.4541). Air melted. Softened. Plate. 6 mm < a ≤ 50 mm. 500 MPa ≤ Rm ≤ 700 Mpa

20/30425162 DC BS EN 2467 航空航天系列 钢 X2CrNi18-9 (1.4307) 空气融化了 软化了 板材、片材和带材 0.4 毫米 ≤ a ≤ 20 毫米 520兆帕≤Rm≤670兆帕

BS EN 2467. Aerospace series. Steel X2CrNi18-9 (1.4307). Air melted. Softened. Plates, sheets and strips. 0,4 mm ≤ a ≤ 20 mm. 520 MPa ≤ Rm ≤ 670 MPa

ASTM A985/A985M-20 钢制熔模铸件的标准规范对含压部件的一般要求

Standard Specification for Steel Investment Castings General Requirements, for Pressure-Containing Parts

BS EN 3358:2020 航空航天系列 钢 FE-PM1503 (X3CrNiMoAl 13-8-2) 真空感应熔化和自耗电极重熔 固溶处理和沉淀处理 机加工用棒材 a或D≤150毫米 Rm≥1 400 MPa

1   Scope This document specifies the requirements relating to: Steel FE-PM1503 (X3CrNiMoAl 13-8-2) Vacuum induction melted and consumable electrode remelted Solution treated and precipitation treated Bar for machining a or D  ≤ 150 mm R m  ≥ 1 400 MPa for aerospace applications.

Aerospace series. Steel FE-PM1503 (X3CrNiMoAl 13-8-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bar for machining. a or D ≤ 150 mm. Rm ≥ 1 400 MPa

BS EN 3468:2019 航空航天系列 钢 X8CrNiTi18-10 (1.4878/1.4544) 软化了 500兆帕≤Rm≤700兆帕 锻件 深度≤100毫米

What is BS EN 3468- Aerospace series: Steel X8CrNiTi18-10 (1.4878/1.4544) forgings about?   BS EN 3468 is a metallic material standard that covers technical specifications for the Aerospace series: Steel X8CrNiTi18-10 (1.4878/1.4544) forgings that ensures structural reliability, operability and corrosion resistance of parts and components.   BS EN 3468 specifies the requirements relating to Steel X8CrNiTi18-10 (1.4878/1.4544) forgings with the softened delivery condition. BS EN 3468 sets tensile strength range of 500 MPa ≤ Rm ≤ 700 MPa and limit dimension (De) ≤ 100 mm for aerospace applications.   Who is BS EN 3468- Aerospace series: Steel X8CrNiTi18-10 (1.4878/1.4544) forgings

Aerospace series. Steel X8CrNiTi18-10 (1.4878/1.4544). Softened. 500 MPa ≤ Rm ≤ 700 MPa. Forgings. De ≤ 100 mm

BS EN 3489:2019 航空航天系列 钢 X8CrNiTi18-10 (1.4878/1.4544) 软化了 500≤Rm≤750兆帕 结构用管 0.5 ≤ a ≤ 5 毫米

What is BS EN 3489- Aerospace series: Steel X8CrNiTi18-10 (1.4878/1.4544) tubes for structures about?   BS EN 3489 is a metallic material standard covering technical specifications for the Aerospace series: Steel X8CrNiTi18-10 (1.4878/1.4544) tubes for structures that enhance structural stability and corrosion resistance.   BS EN 3489 specifies the requirements relating to Steel X8CrNiTi18-10 (1.4878/1.4544) tubes for structures in softened delivery conditions.    BS EN 3489 specifies a tensile strength range of 500 ≤ Rm ≤ 750 MPa and a limit dimension range of 0.5 ≤ a ≤ 5 mm for aerospace applications.  

Aerospace series. Steel X8CrNiTi18-10 (1.4878/1.4544). Softened. 500 ≤ Rm ≤ 750 MPa. Tubes for structures. 0,5 ≤ a ≤ 5 mm