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。
| 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
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
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 |
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