美利体育登录入口官网

美利体育登录入口官网:沉淀处理

沉淀处理是一种热处理工艺,通过控制温度和时间使材料内部析出细小沉淀相(强化相),从而提高材料的强度和硬度。典型工艺如铝合金在315°C至330°C保温2小时,或部分合金在600°C±10°C保温16小时后空冷。


沉淀处理有关的标准

标准号 & 类别标准名称发布
BS 2HC 101:1989+A3:2013
规范

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)


固溶处理 

1990-02-28
英国标准学会
BS 2HC 102:1989+A3:2013
规范

沉淀硬化铬-镍-铜-钼钢铸件规格(1250 MPa)(Cr 14.0,Ni 4.5,Cu 2.5,Mo 1.5)

Specification for precipitation hardening chromium-nickel-copper-molybdenum steel castings (1250 MPa) (Cr 14. 0, Ni 4.5, Cu 2.5, Mo 1.5)

1990-01-31
英国标准学会
BS 2L 85:1971(2000)
规范

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)


固溶处理 

2000
英国标准学会
BS 2L 95:1971(2000)
规范

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)


固溶处理 

2000
英国标准学会
BS 3B 31:2009
规范

铜-铍合金带材和箔材规范(溶液处理、冷轧:完全硬化和沉淀处理)

Specification for copper-beryllium alloy strip and foil (solution treated, cold rolled: full hard and precipitation treated)


交货状态 

2009-11-30
英国标准学会
BS 3HR 501:2011
规范

耐热镍铬钴钛铝合金冷拔钢丝弹簧和弹簧(镍基Cr19.5-Co18.0-Ti2.5-Al1.5)规格

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


弹簧 

2011-01-31
英国标准学会
BS 3L 63:1971(2011)
规范

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)


固溶处理 

2011
英国标准学会
BS EN 3162:2007
规范

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薄板材和带材.a≤6mm.Rm≥930MPa

Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, sheet and strip a 6 mm, Rm 930 MPa


空气熔炼 

2008-08-29
英国标准学会
BS EN 4315:2007
规范

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


固溶处理 

2008-02-29
英国标准学会
BS EN 4318:2007
规范

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


固溶处理 

2008-02-29
英国标准学会
BS EN 4656:2010
规范

航空航天系列.钢FE-PM1507 (X1CrNiMoAlTi12-11-2).真空感应熔炼和自耗电极重熔.固溶处理和沉淀处理.棒材.a或D≤200 mm.Rm≤1520 MPa

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


真空感应熔炼 

2010-12-31
英国标准学会
EN 4318:2007
规范

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


固溶处理 

2007-08-01
欧洲标准化委员会
LST EN 3160:2007
规范

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


固溶处理 钢 FE-PM3801 

2007-11-15
立陶宛标准局
SS-EN 4315:2007
规范

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


固溶处理 

2007
瑞典标准研究所
SS-EN 4318:2007
规范

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


固溶处理 

2007-10-18
瑞典标准研究所
SS-EN 4376:2016
规范

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


固溶处理 

2016
瑞典标准研究所
UNE-EN 4315:2007
规范

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.)


固溶处理 

2007-11-01
西班牙标准化协会
UNE-EN 4462:2007
规范

航空航天系列 钢 FE-PM1506(X5CrNiMoAl13-8-2)真空感应熔炼和自耗电极重熔 固溶处理和沉淀处理 Bar a 或 D <= 150mm Rm >= 1300 MPa

Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bar - a or D <= 150 mm - Rm >= 1 300 MPa (Endorsed by AENOR in November of 2007.)


真空感应熔炼 

2007-11-01
西班牙标准化协会
UNE-EN 4463:2007
规范

航空航天系列 钢 FE-PM1506(X5CrNiMoAl13-8-2)真空感应熔炼和自耗电极重熔 固溶处理和沉淀处理 Bar a 或 D <= 150mm Rm >= 1400 MPa

Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bar - a or D <= 150 mm - Rm >= 1 400 MPa (Endorsed by AENOR in November of 2007.)


真空感应熔炼 钢 FE-PM1506 

2007-11-01
西班牙标准化协会

 




Copyright ?2007-2026 ANTPEDIA, All Rights Reserved
京ICP备07018254号 京公网安备1101085018 电信与信息服务业务经营许可证:京ICP证110310号
页面更新时间: 2026-09-06 10:01

美利体育(meili)官方网站_美利体育手机版下载