V11 航空与航天用金属铸锻材料 标准查询与下载

SAE AS1580D-2012 3000 psi钛焊接环

Ring, Weld, 3000 psi Titanium

SAE AMS5553G-2012 退火的低(最大0.02)碳镍制薄板材和带材

This specification covers nickel in the form of sheet and strip. These products have been used typically for parts requiring excellent corrosion resistance, and/or strong magnetic properties, but usage is not limited to such applications.

Nickel, Sheet and Strip, Low (0.02 max) Carbon, Annealed

SAE AMS5046D-2012 硬质碳钢、薄板钢、带钢和板钢(SAE 1020和1025)

This specification covers two types of carbon steel in the form of sheet, strip, and plate. These products have been used typically for use in fabrication of fittings, but usage is not limited to such applications. These products are not typically used for deep forming or cupping operations.

Carbon Steel, Sheet, Strip, and Plate (SAE 1020 and 1025) Annealed

SAE AMS5412A-2012 真空熔化和真空铸造的耐腐蚀的拉伸强度195psi(1344MPa)均质的溶液和沉淀热处理的合金熔模铸件13Cr 8.0Ni 2.2Mo 1.1Al

This specification covers a corrosion-resistant steel in the form of investment castings. Primarily for parts requiring corrosion resistance and strength up to 600 °F (316 °C).

Steel Castings, Vacuum Melted, Vacuum Cast, Investment, Corrosion Resistant 13Cr 8.0Ni 2.2Mo 1.1Al (195 psi) (1344 MPa) Tensile Strength (Condition H1000) Homogenized, Solution, Precipitation Heat Treated

SAE AMS4405A-2012 溶液热处理和自然老化的铝合金包铝的薄板(6156-T4) 1.0Si 0.90Cu 0.60Mn 0.90Mg

This specification covers an aluminum alloy procured in the form of sheet Alclad on both sides. These products have been used typically for formed structural parts requiring good formability in T4 temper and ability to develop improved resistance to fatigue crack growth and high toughness with moderate strength when aged to T62 temper, but usage is not limited to such applications.

Aluminum Alloy, Alclad Sheet (6156-T4) 1.0Si 0.90Cu 0.60Mn 0.90Mg Solution Heat Treated and Naturally Aged

SAE AMS-QQ-A-367D-2012 铝合金锻件

This specification covers aluminum alloy die forgings and hand forgings.

Aluminum Alloy Forgings

NF L10-302:2012 航空航天系列 - 抗拉强度≤1450 MPa的镀镉钢, 铜, 铜合金以及镍合金.

Aerospace series - Cadmium plating of steels with specified tensile strength inferior or equal 1 450 MPa, copper, copper alloys and nickel alloys.

NF L06-402*NF EN 4678:2012 航空航天系列 - 航空航天结构用焊接和钎焊件 - 激光束焊金属材料接缝 - 焊件质量.

Aerospace series - Weldments and brazements for aerospace structures - Joints of metallic materials by laser beam welding - Quality of weldments.

DIN EN 3120:2012 航空航天系列.钛合金TI-P64003-冷处理和应力.压力系统的无缝钢管要求- 4 mm D 51 mm, 690 MPa R_m 1030 MPa.德文和英文版本 EN 3120-2012

Aerospace series - Titanium alloy TI-P64003 - Cold worked and stress relieved - Seamless tube for pressure systems - 4 mm D 51 mm, 690 MPa R_m 1030 MPa; German and English version EN 3120:2012

DIN EN 2252:2012 航空航天系列.钢 FE-PL1505 (15CrMoV6) - 1 080 MPa R_m 1 250 MPa - 锻件 - D_e - D 100 mm. 德文和英文版本 EN 2252-2012

Aerospace series - Steel FE-PL1505 (15CrMoV6) - 1 080 MPa R_m 1 250 MPa - Forgings - D_e 100 mm; German and English version EN 2252:2012

BS EN 3355:2012 航空航天系列. TI-P64001 (Ti-6Al-4V)钛合金.退火.挤压型材.De≤150 mm. 900 MPa≤Rm≤1160 MPa

Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Extruded section. De 150 mm. 900 MPa Rm 1160 MPa

BS EN 2213:2012 航空航天系列.FE-PL1505 (15CrMoV6)钢制.气融.淬火与回火.钢筋.De 16 mm. 980 MPa Rm 1180 MPa

Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Bars. De 16 mm. 980 MPa Rm 1180 MPa

SAE AMS7498N-2012 闪焊钛和钛合金环材

This specification covers flash welded rings made of titanium and selected titanium alloys. These rings have been used typically for parts such as flanges and rings, but usage is not limited to such applications.

Rings, Flash Welded Titanium and Titanium Alloys

SAE AMS7725E-2012 高密度烧结的钨合金型材

This specification covers four classes of tungsten heavy metal in the form of sintered and annealed shapes. This material has been used typically for parts, such as counterbalance weights or projectiles, for which mechanical properties are tested from the sintered and annealed shapes and that require high weight per unit volume, but usage is not limited to such applications.

Tungsten Alloy Shapes, Sintered, High Density

NF L10-591*NF EN 4683:2012 航空航天系列.FE-WM 3504(X4CrNiMo16-5-1)型钢.空气熔炼.焊接填充金属.线材和棒材

Aerospace series - Steel FE-WM 3504 (X4CrNiMo16-5-1) - Air melted - Filller metal for welding - Wire and rod.

NF L11-300-007*NF EN 4700-007:2012 航空航天系列.耐热合金钢.锻件制品.技术规范.第007部分:再熔化坯料

Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 007 : remelting stock.

NF L11-300-002:2012 航空航天系列.耐热合金钢.锻件制品.技术规范.第002部分:棒材和切片

Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002 : bar and section.

DIN EN 4656:2012 航空航天系列.钢 FE-PM1507 (X1CrNiMoAlTi12-11-2)真空感应熔化和熔化电极再熔化溶液处理和沉淀处理 -条-a或 200 mm - Rm 1520 MPa.德文和英文版本 EN 46

Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars - a or D 200 mm - Rm 1520 MPa; German and English version EN 46

BS EN 3312:2012 航空航天系列.钛合金Ti-6Al-4V.退火.锻件De = 150 mm

Aerospace series. Titanium alloy Ti-6Al-4V. Annealed. Forgings De = 150 mm

BS EN 3120:2012 航空航天系列.钛合金TI-P64003.冷拔和去除应力.压力系统用无缝管.4 mm D 51 mm. 690 MPa Rm 1030 Mpa

Aerospace series. Titanium alloy TI-P64003. Cold worked and stress relieved. Seamless tube for pressure systems. 4 mm D 51 mm. 690 MPa Rm 1030 MPa