美利体育登录入口官网

镁合金的热处理标准实施规程

Standard Practice for Heat Treatment of Magnesium Alloys

镁合金热处理标准实践

Standard Practice for Heat Treatment of Magnesium Alloys

锻铝合金热处理标准实践

Standard Practice for Heat Treatment of Wrought Aluminum Alloys

铝-铜-镁-硅-锰合金板材规范 —（固溶处理、控制拉伸和沉淀处理）（Cu 4.4、Mg 0.5、Si 0.7、Mn 0.8）

Specification for Plate ofaluminium - copper - magnesium - silicon - manganese alloy — (Solution treated, controlled stretched and precipitation treated) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)

铬-镍-铜-钼耐腐蚀钢（沉淀硬化）钢坯、锻件和零件规范（93 和 1080 MPa）

Specification for Chromium - nickel - copper - molybdenum corrosion - resisting steel (precipitation hardening) billets, forgings and parts (93 & 1080 MPa)

铬-钴-钼-钒-铌耐热钢坯料、棒材、锻件和零件规范（自耗电极重熔）（1000-1140 MPa）-（Cr 10.5、Co 6、Mo 0.8、V 0.2、Nb 0.3）

Specification for Chromium – cobalt – molybdenum – vanadium – niobium heat - resisting steel billets, bars, forgings and parts (consumable electrode remelted) (1000 – 1140 MPa) — (Cr 10.5, Co 6, Mo 0.8, V 0.2, Nb 0.3)

航空航天.锻造钛和钛合金的热处理

Aerospace; heat treatment of wrought titanium and titanium alloys

镍基高温合金

High-temperature resistant nickel-based alloy Ni-P96-HT cold-drawn and annealed wire of 10 mm diameter for aerospace applications

航空航天系列 钛合金 TI-P64001 固溶处理和时效 加工用棒材 D 75 mm

Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Bar for machining - D 75 mm; German and English version EN 3314:2019

航空航天系列-TI-P64001钛合金-固溶处理和时效-锻件-直径75毫米

Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Forgings - De 75 mm

铸造铝合金热处理

Heat treatment of cast aluminium alloys

铍青铜金相分析方法

Metallographic analysis method of beryllium bronze

弹性元件用精密合金热处理 工艺说明书

Specification for Heat Treatment Process of Precision Alloys for Elastic Components

轴尖合金热处理工艺

Shaft tip alloy heat treatment process

铸造铝合金的热处理

Heat Treatment of Cast Aluminum Alloy

弹性合金的热处理

Heat Treatment of Elastic Alloys

改良耐腐蚀铝合金棒,杆材和型材挤压制品7075-T76

Aluminum Alloy Bar, Rod, and Shapes, Extruded, 7075-T76 Improved Exfoliation Resistance

铝合金 6162，棒材、棒材、型材、管材和线材，挤压

Aluminum Alloy 6162, Bar, Rod, Shapes, Tube, and Wire, Extruded

铝合金 2024，棒材、棒材、型材、管材和线材，挤压

Aluminum Alloy 2024, Bar, Rod, Shapes, Tube, and Wire, Extruded

轧制、拉制或冷轧成品7075铝合金棒材、杆材、线材和特殊型材

Aluminum Alloy 7075, Bar, Rod, Wire, and Special Shapes; Rolled, Drawn, or Cold Finished

铝合金管 无缝 拉制 1.8Cu 1.0Mg 0.8Si 0.20Cr 固溶热处理 拉伸消除应力 并时效 (2013-T6511)

Aluminum Alloy Tubing, Seamless, Drawn 1.8Cu - 1.0Mg - 0.8Si - 0.20Cr Solution Heat Treated, Stress-Relieved by Stretching, and Aged (2013-T6511)

铝合金薄板和中厚板 Alclad 6.8Zn 2.8Mg 2.0Cu 0.23Cr（Alclad 7178-0）退火

Aluminum Alloy Sheet and Plate@ Alclad 6.8Zn - 2.8Mg - 2.0Cu - 0.23Cr (Alclad 7178-0) Annealed

铝合金 轧制或锻造环 成分：5.6Zn 2.5Mg 1.6Cu 0.23Cr（7075-T7351 7075-T7352） 固溶热处理 机械应力消除 以及析出热处理

Aluminum Alloy, Rolled or Forged Rings, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7351, 7075-T7352), Solution Heat Treated, Mechanically Stress Relieved, and Precipitation Heat Treated

合金 耐腐蚀 棒材 20Cr 35Ni 35Co 10Mo (MP35N?) 真空感应加自耗电极真空重熔溶液热处理以强化工件

Alloy, Corrosion-Resistant, Bars 20Cr - 35Ni - 35Co - 10Mo (MP35N?) Vacuum Induction Plus Consumable Electrode Vacuum Remelted Solution Heat Treated for Work Strengthening

航空系列 钢FE-PM1507 (X1CrNiMoAlTi12-11-2) 真空感应熔炼和可耗电极重熔 解析处理和沉淀强化处理 锻件 a或D ≤ 200 mm Rm ≥ 1650 MPa

Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥ 1 650 MPa

钢锭模

Ingot mold