美利体育登录入口官网

航天系列 钢材 X5CrNiCu15-5 (1.4545) 可消耗电极重熔 固溶处理和析出处理 板材 6 mm < a = 20 mm 1 070 MPa = Rm = 1 220 MPa

Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted - Solution treated and precipitation treated - Plates - 6 mm < a = 20 mm - 1 070 MPa = Rm = 1 220 MPa

普通美利体育官网首页网址用无缝与焊接铁素体/奥氏体不锈钢

Standard Specification for Seamless and Welded Ferritic/Austenitic Stainless Steel Pipe

淀积硬化镍合金钢棒和钢丝的标准规范

Standard Specification for Precipitation Hardening Nickel Alloys Bar and Wire

沉淀硬化铬-镍-铜-钼钢铸件规范(950 MPa) (Cr 14.0, Ni 4.5, Cu 2.5, Mo 1.5)

Specification for precipitation hardening chromium-nickel-copper-molybdenum steel castings (950 MPa) (Cr 14.0, Ni 4.5, Cu 2.5, Mo 1.5)

镍-铁-铬-钼-铝-钛热阻合金板材、薄板材和带材规范(镍/钴 43.5、铬 16.5、钼 3.3、铝 1.2、钛 1.2、其余部分为铁)

Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy plate, sheet and strip (Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder)

铝-铜-镁-硅-锰合金锻件和锻件规范 —（固溶处理和沉淀处理）（Cu 4.4、Mg 0.5、Si 0.7、Mn 0.8）

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

铝-铜-硅-镁合金锻件、棒材、挤压型材和锻件规范 —（固溶处理和沉淀处理）（Cu 1.5、Si 1、Mg 0.8）

Specification for Forging stock, bars, extruded sections and forgings of aluminium - copper - silicon - magnesium alloy — (Solution treated and precipitation treated) (Cu 1.5, Si 1, Mg 0.8)

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)

铝-锌-镁-铜-铬合金板规范 —（固溶处理、控制拉伸和沉淀处理）（Zn 5.8、Mg 2.5、Cu 1.6、Cr 0.15）

Specification for Plate ofaluminium - zinc - magnesium - copper - chromium alloy — (Solution treated, controlled stretched and precipitation treated) (Zn 5.8, Mg 2.5, Cu 1.6, Cr 0.15)

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)

耐热镍铬钴钛铝合金冷拔和固溶处理钢丝弹簧和弹簧(镍基Cr19.5-Co18.0-Ti2.5-Al1.5)规格

Specification for nickel-chromium-cobalt-titanium- aluminium heat-resisting alloy cold drawn and solution treated wire for springs and springs (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)

铝-铜-镁-硅-锰合金管规范—（固溶处理和沉淀处理）（Cu 4.4、Mg 0.5、Si 0.7、Mn 0.8）

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

铝-铜-镁-硅-锰合金的整体冷锻制铆钉用金属线规范(用于溶解处理和自然老化状态)(直径不超过10 mm)(Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8)(2014A)

Specification for wire for solid cold-forged rivets of aluminium-copper-magnesium-silicon-manganese alloy (for use in the solution treated and naturally aged condition) (not exceeding 10 mm diameter) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8) (2014A)

航空航天系列 钢X7CrNiAl17-7（1.4568） 空气熔化 溶液处理和沉淀硬化 薄板和带材 a＜LE＞6毫米 1240兆帕＜LE＞Rm＜LE＞1450兆帕

Aerospace series. Steel X7CrNiAl17-7 (1.4568). Air melted. Solution treated and precipitation hardened. Sheet and strip. a 6 mm. 1 240 MPa Rm 1 450 MPa

航空航天系列.FE-PM3801(X5CrNiCu17-4)型钢.空气熔炼、溶解处理和沉淀处理的棒材.a/D≤200mm.Rm≥930MPa

Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D 200 mm, Rm 930 MPa

航空航天系列.FE-PM1802(X5CrNiCu15-5)型钢.自耗电极再熔炼、溶解处理和沉淀处理的薄板材和带材.a≤6mm.1070MPa≤Rm≤1220MPa

Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted, solution treated and precipitation treated, sheet and strip a 6mm, 1070 MPa Rm 1220 MPa

航空航天系列.FE-PM2701(X2NiCoMo18-8-5)钢.真空感应熔炼和真空电弧再熔炼.固溶处理和沉淀处理.锻件.a或D≤150 mm .1750 MPa≤Rm≤2000 MPa

Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Forgings - a or D 150 mm - 1750 MPa Rm 2000 MPa

航空航天系列.FE-PA2601(X6NiCrTiMoV26-15)型耐热合金.溶解处理和沉淀处理.棒材和型材.a/D≤100mm、Rm≥900MPa

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D ≤ 100 mm, Rm ≥ 900 MPa

航空航天系列.FE-PA2601(X6NiCrTiMoV26-15)型耐热合金.溶解处理和沉淀处理.棒材和型材.De≤100mm、Rm≥960MPa

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De ≤ 100 mm, Rm ≥ 960 MPa

航空航天系列.NI-PH3601(NiCr22Mo9Nb)型耐热合金.溶解处理的锻件.De≤200mm

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De 200 mm

航空航天系列 耐热合金X12CrNiCoMoW21-20 溶液处理 锻件 深度≤100毫米

Aerospace series. Heat resisting alloy X12CrNiCoMoW21-20. Solution treated. Forgings. De ≤ 100 mm

航空航天系列–FEPM1506型钢(X1CrNiMoAlTi12-10-2)–真空感应熔炼和消耗电极再熔炼–溶解处理和沉淀处理–钢筋–a或D≤ 200 mm —Rm ≥ 1 400 MPa

Aerospace series — Steel FEPM1506 (X1CrNiMoAlTi12-10-2) — Vacuum induction melted and consumable electrode remelted — Solution treated and precipitation treated —Bars — a or D ≤ 200 mm —Rm ≥ 1 400 MPa

不锈钢耐晶间腐蚀的测定.第2部分:铁素体、奥氏体、铁素体－奥氏体(二相)不锈钢.含有硫酸的介质中的腐蚀试验

Determination of resistance to intergranular corrosion of stainless steels - Ferritic, austenitic and ferritic-austenitic (duplex) stainless steels - Corrosion test in media containing sulfuric acid

铝-镁-硅-铜-铬合金管规范 —（固溶处理和人工时效：未进行液压测试）（厚度不超过 10 毫米）（Mg 1.0、Si 0.6、Cu 0.28、Cr 0.2）

Specification for Tube of aluminium - magnesium - silicon - copper - chromium alloy — (Solution treated and artificially aged : not tested hydraulically) (Not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)

航空航天系列 耐热合金FE PA2601 (X6NiCrTiMoV26-15) 固溶处理和沉淀处理-铆钉用线材- 2mm≤D≤10 mm Rm≥960 MPa ：（草案）

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated - Wires for rivets -2 mm <= D <= 10 mm - Rm >= 960 MPa

航空航天系列 高温合金 NI-PH2301（NiCr21Fe18Mo9） 固溶处理 棒材和型材 < 200 mm

Aerospace series high temperature alloy NI-PH2301 (NiCr21Fe18Mo9) Solution treated bars and profiles < 200 mm

航空航天系列 高温抗合金 NI-PH1303 (NiCo20Cr20Mo5Ti2Al) 固溶处理 无缝管

Aerospace series - Heat resisting alloy NI-PH1303 (NiCo20Cr20Mo5Tl2Al), solution treated - Seamless tubes, D <= 50 mm, a <= 3 mm

航空用高温抗蚀合金FE-PA2601(X6NiCrTiMoV26-15) 溶液处理及沉淀处理 合模锻造件 < 100 mm, > 960 MPa

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15), Solution treated and precipitation treated - Hand and die forgings, D, < 100 mm, > 960 MPa

航空航天系列 抗高温合金 CO-PH1402 自耗电极重熔 固溶处理 锻件和坯料

Aerospace series high temperature alloy CO-PH1402 consumable electrode remelting solution treatment forgings and billets

航空航天系列 耐热合金 NI-PH3601 (NiCr22Mo9Nb) 溶解处理 板材、带材和板材 厚度范围 0.2 mm < a < 10 mm

Aerospace series heat-resistant alloy NI-PH3601 (NiCr22Mo9Nb) Solution-treated plates, strips and sheets Thickness range 0.2 mm < a < 10 mm

航空航天系列 耐热合金 NI-PH1302 (NiCr20Co13Mo4Ti3Al) 固溶处理和冷加工 锻造紧固件棒材 3 mm D 30 mm（草案）

Aerospace series - Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) - Solution treated and cold worked - Bar for forged fasteners - 3 mm D 30 mm

航空航天系列 耐热合金 NI-PH1302 (NiCr20Co13Mo4Ti3Al) 固溶处理和冷加工 锻造紧固件棒材 3 mm D 30 mm（草案）

Aerospace series - Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) - Solution treated and cold worked - Bar for forged fasteners - 3 mm D 30 mm

航空航天系列.FE-PM3801(X5CrNiCu17-4)型钢.空气冶炼的溶解处理和沉淀处理的棒材.a或D≤200mm、R<指数m>≤1310MPa

Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D 200 mm, R<(Index)m> 1310 MPa; German and English version EN 3160:2007

航空航天系列.FE-PM3801(X5CrNiCu17-4)型钢.空气熔炼、溶解处理和沉淀处理.棒材.a或D≤200mm.R<(指数)m>≥930MPa

Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D 200 mm, R<(Index)m> 930 MPa; German and English version EN 3161:2007

航空航天系列 FE-PM3801(X5CrNiCu17-4)钢 空气熔炼、固溶处理和沉淀硬化棒材 直径≤200mm 抗拉强度≥930MPa

Aerospace series – Steel FE-PM3801 (X5CrNiCu17-4) – Air melted, solution treated and precipitation treated, bar a or D ≤ 200 mm, Rm ≥ 930 MPa

航空航天系列.FE-PM3801(X5CrNiCu17-4)型钢.空气熔炼、溶解处理和沉淀处理.薄板材和带材.a≤6mm.R<(指数)m>≥930MPa

Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, sheet and strip a 6 mm, R<(Index)m> 930 MPa; German and English version EN 3162:2007

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（草案）

Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Bar for machining - D 75 mm

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 钛合金 TI-P64001 固溶处理和时效 锻件 D 75 mm

Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Forgings - D 75 mm; German and English version EN 3315:2018

航空航天系列 - X5CrNiCu15-5(1.4545)钢 - 自耗电极重熔 - 固溶处理和沉淀硬化 - 板材 - 6mm < 厚度 ≤ 20mm - 抗拉强度1070-1220MPa

Aerospace series – Steel X5CrNiCu15-5 (1.4545) – Consumable electrode remelted – Solution treated and precipitation treated – Plates – 6 mm < a ≤ 20 mm – 1 070 MPa ≤ Rm ≤ 1 220 MPa

航空和航天用无缝钢管

Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) - Air melted - Solution treated - Seamless tube for pressure applications, D <50 mm; 0,5 mm < a < 5 mm

航空航天系列 耐热合金 NI-PH1301（NiCr19Co18Mo4Ti3Al3） 固溶处理和沉淀处理 棒材和型材 D 200 mm

Aerospace series - Heat-resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3) - Solution treated and precipitation treated - Bars and sections - D 200 mm; German and English version EN 4374:2022

航空航天系列.NI-PH3601(NiCr22Mo9Nb)型耐热合金.De≤200mm溶解处理的锻件

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging D<(Index)e> 200 mm; German and English version EN 4379:2007

航空航天系列.NI-PH3601(NiCr22Mo9Nb)型耐热镍合金.热溶处理.液压用无缝合金管.D≤50mm和a≤3mm

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated - Seamless tubes - For hydraulic application - D ≤ 50 mm, a ≤ 3 mm; German and English version EN 4382:2006

航空航天系列.FE-PM1505(X1CrNiMoAITi12-9-2)型钢.真空感应熔炼和自耗电极再熔炼.溶解处理和沉淀处理.锻件.a或D≤150mm.R<(指数)m>≥1200MPa

Aerospace series - Steel FE-PM1505 (X1CrNiMoAITi12-9-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation hardened - Forgings - a or D 150 mm - R<(Index)m> 1200 MPa; German and English

航空航天系列 耐高温合金CO-PH4101（CoCr20W15Ni） 真空熔炼 固溶处理 锻造件 直径100毫米

Aerospace series high temperature resistant alloy CO-PH4101 (CoCr20W15Ni) Vacuum melting and solution treatment forgings 100 mm in diameter

航空航天系列 - 耐热合金X12CrNiCoMoW21-20 - 固溶处理 - 锻件 - 直径100毫米

Aerospace series – Heat resisting alloy X12CrNiCoMoW21-20 – Solution treated – Forgings – De 100 mm

航空系列 耐热合金 FE-PA4901 (X12CrNiCoMoW21-20) 溶解处理 杆材和型材 100 mm

Aircraft series heat-resistant alloy FE-PA4901 (X12CrNiCoMoW21-20) solution-treated rods and profiles 100 mm

航空航天系列 - X5CrNiCu 17-4（1.4542）钢 - 空气熔炼 - 固溶处理和沉淀硬化处理 - 板材 - 6mm至100mm - Rm 1070 MPa

Aerospace series – Steel X5CrNiCu 17-4 (1.4542) – Air melted – Solution treated and precipitation treated – Plates – 6 mm a 100 mm – Rm 1 070 MPa

金属和合金的腐蚀.可溶解热处理的铝合金抗颗粒间腐蚀的测定

Corrosion of metals and alloys - Determination of resistance to intergranular corrosion of solution heat-treatable aluminium alloys (ISO 11846:1995); German version EN ISO 11846:2008

航空航天系列.FE-PA2601(X6NiCrTiMoV26-15)型耐热合金.溶解处理和沉淀处理.棒材和型材.De小于等于100mm,Rm大于等于960MPa

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De <= 100 mm, Rm >= 960 MPa

铸造铝合金热处理

Heat treatment of cast aluminium alloys

变形铝合金热处理要求

Heat treatment requirements for deformed aluminum alloys

铸造铝合金热处理

Cast aluminum alloy heat treatment

航空用高温合金冷轧板规范

Specification for cold-rolled superalloy sheets for aviation

航天航空用TB5钛合金板材规范

Specification of TB5 titanium alloy sheet for aerospace

铸造铝合金热处理

Heat treatment of cast aluminum alloy

镁合金铸件热处理

Heat Treatment of Magnesium Alloy Castings

航空用高温合金热处理工艺

Heat treatment of superalloy for aviation

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

航空用不锈钢耐热钢铸件热处理

Heat treatment of castings of stainless steel and heat-resistant steel for aviation

航空用不锈钢热处理

Heat treatment of stainless steel for aviation

高温合金热处理

Heat treatment of superalloy

航空航天系列 耐热合金 FE-PA2601 (X6NiCrTiMoV26-15) 固溶处理及沉淀硬化处理 铆钉用线材 直径 2 毫米 ≤ D ≤ 10 毫米 抗拉强度 Rm ≥ 960 兆帕

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated - Wires for rivets - 2 mm ≤ D ≤ 10 mm - Rm ≥ 960 MPa

航空航天系列 耐热合金 FE-PA2602 (X4NiCrTiMoV26-15) 固溶处理与沉淀处理 锻件 直径 De ≤ 100 mm 抗拉强度 Rm ≥ 850 MPa

Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Solution treated and precipitation treated - Forgings - De ≤ 100 mm - Rm ≥ 850 MPa

航空航天系列 耐热合金 NI-PH2601 固溶处理及冷加工 锻制紧固件用棒材 D ≤ 50 mm 1 270 MPa ≤ Rm ≤ 1 550 MPa

Aerospace series - Heat resisting alloy NI-PH2601 - Solution treated and cold worked - Bar for forged fasteners - D ≤ 50 mm - 1 270 MPa ≤ Rm ≤ 1 550 MPa

航空航天系列 耐热合金NI-PH1302 (NiCr20Co13Mo4Ti3Al) 固溶处理及冷加工 锻造紧固件用棒材 3 mm ≤ D ≤ 30 mm

Aerospace series - Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) - Solution treated and cold worked - Bar for forged fasteners - 3 mm ≤ D ≤ 30 mm

航空航天系列 钢 FE-PM3801 (X5CrNiCu17-4) 真空熔炼、固溶处理及沉淀处理 棒材直径或边长≤200 mm 抗拉强度≥1310 MPa

Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D ≤ 200 mm, Rm ≥ 1 310 MPa

航空航天系列 钢 X5CrNiCu15-5 (1.4545) 消耗电极重熔 固溶处理及时效处理 板材 6 mm < a ≤ 20 mm 1 070 MPa ≤ Rm ≤ 1 220 MPa

Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted - Solution treated and precipitation treated - Plates - 6 mm < a ≤ 20 mm - 1 070 MPa ≤ Rm ≤ 1 220 MPa

航空航天系列-NiCr19Fe19Nb5Mo3（2.4668）耐热合金 固溶处理和沉淀处理 棒材和型材 De≤200 mm

Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated - Bar and section, De ≤ 200 mm

航空系列 耐热合金 NI-PH3601 (NiCr22Mo9Nb) 固溶处理 锻件 De ≤ 200 mm

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De ≤ 200 mm

航空航天系列 耐热合金 X12CrNiCoMoW21-20 固溶处理 锻件 De ≤ 100 mm

Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated - Forgings - De ≤ 100 mm

航空航天系列 耐热合金 X12CrNiCoMoW21-20 固溶处理 棒材和型材 De ≤ 100 mm

Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated - Bars and sections - De ≤ 100 mm

增材制造CoCrFeNiTi基多主元合金的组织改性

Microstructure Modification of Additively Manufactured CoCrFeNiTi-based Multi-principal Element Alloy

压水堆核电厂用不锈钢第33部分:反应堆冷却剂管道用 015Cr17Ni12Mo2N不锈钢锻管

Stainless steel for pressurized water reactor unclear power plants.Part 33: 015Cr17Ni12Mo2N stainless steel forged pipes for reactor coolant piping

压水堆核电厂用其他材料 第23部分:控制棒驱动机构用镍基合金丝

Other Material for pressurized water reactor nuclear power plants.Part 23: Ni-base-alloy Wires used for CRDM

航空航天系列 FE-PM3801（X5CrNiCu17-4）型钢 空气熔炼、溶解处理和沉淀处理的棒材 a/D≤200mm Rm≥1310MPa

Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D < or = 200 mm, Rm > or = 1 310 MPa

铝合金铸件 砂 中等耐热性 4.0Cu 2.0Ni 1.5Mg 0.12Ti（242.0P）固溶热处理和稳定（UNS A02420）

Aluminum Alloy Castings@ Sand@ Moderate Heat Resistance 4.0Cu - 2.0Ni - 1.5Mg - 0.12Ti (242.0P) Solution Heat Treated and Stabilized (UNS A02420)

铸件 砂 10Mg 固溶热处理和自然时效

Castings@ Sand 10Mg Solution Heat Treated and Naturally Aged

耐腐蚀钢、棒材、线材、锻件、机械管材和环 16Cr 4.0Ni 0.30Cb（Nb） 4.0Cu 固溶和沉淀热处理（H1075）

Steel, Corrosion Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb (Nb) - 4.0Cu Solution and Precipitation Heat Treated (H1075)

钢，耐腐蚀和耐热，棒材和线材 15Cr 25.5Ni 1.2Mo 2.1Ti 0.006B 0.30V 自耗电极熔化 1800°F（982°C）固溶处理和加工强化 160 ksi（1103 MPa）抗拉强度

Steel, Corrosion and Heat-Resistant, Bars and Wire 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Consumable Electrode Melted 1800 °F (982 °C) Solution Treated and Work-Strengthened 160 ksi (1103 MPa) Tensile Strength

航空系列 钢FE-PM3801（X5CrNiCu17-4） 空气熔炼 溶液处理和沉淀强化 直径a或D≤200 mm 抗拉强度≥930 MPa

Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D ≤ 200 mm, Rm ≥ 930 MPa

航空系列 钛合金TI-P64001 固溶处理和时效处理 锻件 De = 75 mm

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

航空航天系列 钢X3CrNiMoAl13-8-2 (1.4534) 解析退火并时效硬化 1 400 = Rm = 1 550 MPa 锻件 De = 100 mm

Aerospace series - Steel X3CrNiMoAl13-8-2 (1.4534) - Solution annealed and precipitation hardened - 1 400 = Rm = 1 550 MPa - Forgings - De = 100 mm

航空系列 耐热合金FE-PA2602（X4NiCrTiMoV26-15） 解析处理和时效处理 杆材和锻件 直径 = 100 mm

Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Solution treated and precipitation treated - Bars and sections - De = 100 mm

航天系列 耐热合金FE-PA2601（X6NiCrTiMoV26-15） 解析时效处理 棒材或型材直径D≤100mm 抗拉强度Rm≥900 MPa

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D ≤ 100 mm, Rm ≥ 900 MPa

Aerospace系列 耐热合金FE-PA2601（X6NiCrTiMoV26-15） 固溶处理和时效处理 棒材和型材De ≤ 100 mm Rm ≥ 960 MPa

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De ≤ 100 mm, Rm ≥ 960 MPa

航空系列 抗高温合金NiCr19Fe19Nb5Mo3（2.4668）固溶处理和时效处理 杆和型材 De ≤ 200 mm

Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated - Bar and section, De ≤ 200 mm

航空系列 抗高温合金NI-PH3601（镍铬22钼9铌） 预热处理 锻造直径≤200毫米

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De ≤ 200 mm

航空系列 抗热合金NI-PH3601（NiCr22Mo9Nb） 解析处理 无缝管 用于液压应用 直径D≤50 mm 壁厚a≤3 mm

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated - Seamless tubes - For hydraulic application - D ≤ 50 mm, a ≤ 3 mm

航空航天系列 钢FE-PM1505 (X1CrNiMoAlTi12-9-2) 真空感应熔炼并用可耗电极重熔 解析时效处理 杆材 直径或边长a或D ≤ 150 mm 抗拉强度 ≥ 1300 MPa

Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bar - a or D ≤ 150 mm - Rm ≥ 1 300 MPa

航空系列 耐热合金X12CrNiCoMoW21-20 解析处理 锻件 直径≤100毫米

Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated - Forgings - De ≤ 100 mm

航空航天系列 耐热合金X12CrNiCoMoW21-20.固溶处理 棒材和型材.De=100毫米

Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated - Bars and sections - De = 100 mm

航空系列 抗热合金X12CrNiCoMoW21-20 解析处理 板和带材 a = 3 mm

Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated - Sheets and strips - a = 3 mm

Aerospace系列 耐热合金X12CrNiCoMoW21-20 解析处理并退火 板和带 厚度3毫米 < a = 50毫米

Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated and descaled - Sheets and plates - 3 mm < a = 50 mm

航空航天系列 钢 FE-PM3801(X5CrNiCu17-4)空气熔炼、固溶处理和沉淀处理 bar a 或 D <= 200mm Rm >= 930 MPa

Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, bar a or D <= 200 mm, Rm >= 930 MPa (Endorsed by AENOR in November of 2007.)

航空航天系列 耐热合金 FE-PA2601(X6NiCrTiMoV26-15)固溶处理和沉淀处理 棒材和截面 a 或 D <= 100mm Rm >= 900 MPa

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D <= 100 mm, Rm >= 900 MPa (Endorsed by AENOR in November of 2007.)

航空航天系列 耐热合金 NI-PH3601(NiCr22Mo9Nb)固溶处理 锻造 De <= 200mm

Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De <= 200 mm (Endorsed by AENOR in January of 2008.)

航空航天系列 钢 X5CrNiCu15-5 (1.4545) 消耗电极重熔 溶液处理和沉淀处理 板材 6 毫米 < a

Aerospace series - Steel X5CrNiCu15-5 (1.4545) - Consumable electrode remelted - Solution treated and precipitation treated - Plates - 6 mm < a <= 20 mm - 1 070 MPa <= Rm <= 1 220 MPa

手表用不锈钢扁钢

Stainess steel flats for wrist watch

耐蚀合金热轧板

Hot-rolled plates of corrosion-resisting alloys