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Alloy aging treatment
Alloy aging treatment, Total:120 items.
In the international standard classification, Alloy aging treatment involves: Non-ferrous metals, Materials for aerospace construction, Products of non-ferrous metals, Footwear.
European Association of Aerospace Industries, Alloy aging treatment
- AECMA PREN 3462-1988 Titanium Alloy TI-P11 Annealed 540 Less Than or Equal to Rm Less Than or Equal to 770 MPa Bar for Machining De Less Than or Equal to 150 mm
- AECMA PREN 3351-1988 Titanium Alloy TI-P68 Solution Treated and Aged Rm Greater Than or Equal to 1000 MPa Forgings De Less Than or Equal to 150 mm
- AECMA PREN 3314-1988 Titanium Alloy TI-P63 Solution Treated and Aged Rm Greater Than or Equal to 1070 MPA Bar for Machining De Less Than or Equal to 50 mm
- AECMA PREN 3463-1988 Titanium Alloy TI-P11 Solution Treated and Aged 650 Less Than or Equal to Rm Less Than or Equal to 880 MPa Bar for Machining De Less Than or Equal to 75 mm
- AECMA PREN 3555-1988 Aerospace Series Aluminium Alloy (7075) Solution Treated, Controlled Stretched and Artificially Aged (T79510) Extruded Bars and Sections 1,2 Less Than (a or D) Less Than or Equal to 100 mm with Peripheral Coarse Grain Control Issue P 1
- AECMA PREN 3494-1995 Aerospace Series Titanium Alloy TI-P19001 Grade 2 Solution Treated and Aged Forgings De Less Than or Equal to 75 mm Edition P 2
- AECMA PREN 3459-1996 Aerospace Series Titanium Alloy TI-P63001 Solution Treated and Aged Plate 6 mm Less Than a Less Than or Equal to 50 mm Edition P 2 Edition P 2
- AECMA PREN 3125-1988 Aerospace Series Aluminium Alloy AL-C26 Solution Treated and Artificially Aged (T6) Structural Precision Castings Issue P 1
- AECMA PREN 3349-1988 Aerospace Series Magnesium Alloy MG-C92 Solution Treated and Artificially Aged (T6) Casting Issue P 1
- AECMA PREN 3870-1993 Aerospace Series Titanium Alloy TI-P19001 Solution Treated and Aged Sheet and Strip, Hot Rolled a Less Than or Equal to 6 mm Edition P 1
- AECMA PREN 3871-1993 Aerospace Series Titanium Alloy TI-P19001 Solution Treated and Aged Sheet and Strip, Cold Rolled a Less Than or Equal to 6 mm Edition P 1
- AECMA PREN 3466-1994 Aerospace Series Titanium Alloy TI-P63001 Solution Treated and Aged Bar for Machining D Less Than or Equal to 150 mm Edition P 2
- AECMA PREN 3318-1988 Titanium Alloy TI-P64 Not Heat Treated Reference Heat Treatment: Annealed Grade 2 Forging Stock De Less Than or Equal to 360 mm
- AECMA PREN 3319-1988 Titanium Alloy TI-P64 Annealed Rm Greater Than or Equal to 1000 MPa Bar for Machining De Less Than or Equal to 150 mm
- AECMA PREN 3554-1988 Aerospace Series Aluminium Alloy (7010) Solution Treated, Cold Compressed and Artificially Aged (T7652) Hand Forgings a Less Than or Equal to 200 mm Issue P 1
- AECMA PREN 3495-1995 Aerospace Series Titanium Alloy TI-P19001 Grade 2 Annealed Forgings De Less Than or Equal to 150 mm Edition P 2
- AECMA PREN 3459-1988 Aerospace Series Titanium Alloy TI-P68 Solution Treated and Aged Rm Greater Than or Equal to 1030 MPa Plate 6 Less Than a Less Than or Equal to 50 mm Issue P 1
- AECMA PREN 3122-1988 Aerospace Series Aluminium Alloy AL-C27 Solution Treated and Artificially Aged (T6) High Strength Structural Precision Castings Issue P 1
- AECMA PREN 3123-1988 Aerospace Series Aluminium Alloy AL-C27 Solution Treated and Artificially Aged (T6) Structural Precision Castings Issue P 1
- AECMA PREN 3463-1994 Aerospace Series Titanium Alloy TI-P19001 Solution Heat Treated and Aged Bar for Machining D Less Than or Equal to 75 mm Edition P 2
- AECMA PREN 3737-1995 Aerospace Series Titanium Alloy TI-P65002 Not Heat Treated Grade 2 Forging Stock, for Solution Treated and Aged Forgings a or D Less Than or Equal to 360 mm Edition P 1
- AECMA PREN 3735-1994 Aerospace Series Titanium Alloy TI-P65002 Solution Treated and Aged Bar for Machining D is Less Than or Equal to 75 mm Edition P 1
- AECMA PREN 3736-1995 Aerospace Series Titanium Alloy TI-P65002 Grade 2 Solution Treated and Aged Forgings De Less Than or Equal to 75 mm Edition P 1
- AECMA PREN 3494-1988 Titanium Alloy TI-P11 Solution Treated and Aged 650 Less Than or Equal to Rm Less Than or Equal to 880 MPa Forgings De Less Than or Equal to 75 mm
- AECMA PREN 3495-1988 Titanium alloy TI-P11 Annealed 540 Less Than or Equal to Rm Less Than or Equal to 770 MPa Forgings De Less Than or Equal to 150 mm
- AECMA PREN 3457-2002 Aerospace Series Titanium Alloy TI-P63 Not Heat Treated Reference Heat Treatment: Solution Treated and Aged Grade 2 Forging Stock for Fasteners D Less Than or Equal to 25 mm Issue P 2 [Refer To: ASD-STAN PREN 3813]
- AECMA PREN 3552-1988 Aerospace Series Aluminium Alloy (2618A) Solution Treated, Straightened and Artificially Aged (T6) Clad Sheet and Strip 0,4 Less Than or Equal to a Less Than or Equal to 6 mm Issue P 1
- AECMA PREN 3466-1988 Titanium Alloy TI-P68 Solution Treated and Aged Rm Greater Than or Equal to 1000 MPa Bar for Machining De Less Than or Equal to 150 mm
- AECMA PREN 3345-1988 Aerospace Series Aluminium Alloy (7150) Solution Treated, Water Quenched Controlled Stretched and Artificially Aged (T6511) Extruded Bar and Section (a or D) Less Than or Equal to 90 mm with Peripheral Coarse Grain Control Issue P 1
- AECMA PREN 3550-1988 Aerospace Series Aluminium Alloy (2024) Solution Treated, Stretched and Artificially Aged (T8511) Extruded Bars and Sections (a or D) Less Than or Equal to 150 mm Issue P 1
- AECMA PREN 3551-1988 Aerospace Series Aluminium Alloy (7150) Solution Treated, Straightened and Artificially Aged (T6511) Extruded Bars and Sections (a or D) Less Than or Equal to 90 mm Issue P 1
- AECMA PREN 3465-1988 Titanium Alloy TI-P68 Not Heat Treated Reference Heat Treatment: Solution Treated and Aged Grade 2 Forging Stock De Less Than or Equal to 360 mm
- AECMA PREN 3313-1988 Titanium Alloy TI-P63 Not Heat Treated Reference Heat Treatment: Solution Treated and Aged Grade 2 Forging Stock De Less Than or Equal to360 mm
- AECMA PREN 3553-1988 Aerospace Series Aluminium Alloy (2618A) Solution Treated, Stretched and Artificially Aged (T6511) Extruded Bars and Sections 1,2 Less Than or Equal to (a or D) Less Than or Equal to 100 mm Issue P 1
- AECMA PREN 3310-1995 Aerospace Series Titanium Alloy TI-P64001 not Heat Treated Grade 2 Forging Stock, for Annealed Forgings a or D Less Than or Equal to 360 mm Edition P 2
- AECMA PREN 3313-1995 Aerospace Series Titanium Alloy TI-P64001 not Heat Treated Grade 2 Forging Stock, for Solution Treated and Aged Forgings a or D Less Than or Equal to 360 mm Edition P 2
- AECMA PREN 3353-2002 Aerospace Series Titanium Alloy TI-P63 Solution Treated and Aged Rm Greater Than or Equal to 1100 MPa Bar and Wire for Fasteners Machined De Less Than or Equal to 25 mm Issue P 2 [Refer To: ASD-STAN PREN 3813]
European Committee for Standardization (CEN), Alloy aging treatment
- EN 3459:2010 Aerospace series - Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn) - Solution treated and aged - Plate - 6 mm < a <= 50 mm
Society of Automotive Engineers (SAE), Alloy aging treatment
- SAE AMS4437E-2003 Magnesium Alloy Castings, Sand 8.7Al - 0.70Zn (AZ91C-T6) Solution Heat Treated and Aged UNS M11914
- SAE AMS6930C-2011 Titanium Alloy Bars, Forgings and Forging Stock 6.0Al 4.0V Solution Heat Treated and Aged
- SAE AMS4303A-2000 Aluminum Alloy Plate, 2.7Cu 2.2Li 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged
- SAE AMS4458-2010 Aluminum Alloy, Plate (2.7 Cu - 1.8 Li - 0.7 Zn) 2099-T86 Solution Heat Treated, Cold Worked and Artificially Aged
- SAE AMS6921A-2011 Titanium Alloy Bars, Forgings and Forging Stock 3Al 8V 6Cr 4Mo 4Zr Solution Heat Treated and Aged
- SAE AMS6930D-2012 Titanium Alloy Bars, Forgings and Forging Stock 6.0Al 4.0V Solution Heat Treated and Aged
- SAE AMS6930E-2014 Titanium Alloy Bars, Forgings and Forging Stock, 6.0Al - 4.0V, Solution Heat Treated and Aged
- SAE AMS4437F-2014 Magnesium Alloy Castings, Sand 8.7Al - 0.70Zn (AZ91C-T6) Solution Heat Treated and Aged
- SAE AMS4904B-2011 Titanium Alloy Sheet, Strip, and Plate 6Al 4V Solution Heat Treated and Aged
- SAE AMS4934E-2007 Titanium Alloy, Extrusions and Flash Welded Rings 6Al - 4V Solution Heat Treated and Aged
- SAE AMS4085B-1986 Aluminum Alloy, Sheet 5.7Zn 2.2Mg 1.6Cu 0.22Cr Solution Heat Treated and Overaged
- SAE AMS4107F-2005 Aluminum Alloy Die Forgings (7050-T74) Solution Heat Treated and Overaged UNS A97050
- SAE AMS4085C-2006 Aluminum Alloy Sheet 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T761) Solution Heat Treated and Overaged UNS A9747
- SAE AMS4934D-2002 Titanium Alloy, Extrusions and Flash Welded Rings, 6Al 4V, Solution Heat Treated and Aged
- SAE AMS4078G-2007 Aluminum Alloy Plate (7075-T7351) Solution Heat Treated, Stress Relieved, and Overaged UNS A97075
- SAE AMS4085D-2011 Aluminum Alloy Sheet 5.7Zn 2.2Mg 1.6Cu 0.22Cr (7475-T761) Solution Heat Treated and Overaged
- SAE AMS4236C-2013 Aluminum Alloy Castings 4.6Cu 0.35Mn 0.25Mg 0.22Ti (A206.0-T4) Solution Heat Treated and Naturally Aged
- SAE AMS6906-2004 Titanium Alloy Bars, Forgings and Forging Stock 6.0Al 2.0Sn 4.0Zr 6.0Mo Solution Heat Treated and Aged
- SAE AMS6926-2004 Titanium Alloy Bars, Forgings and Forging Stock 13V 11Cr 3Al Solution Heat Treated and Aged
- SAE AMS4306A-1993 Aluminum Alloy, Plate 6.4Zn 2.4Mg 2.2Cu 0.12Zr, Solution Heat Treated, Stress Relieved, and Aged
- SAE AMS4242B-2007 Aluminum Alloy, Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged
- SAE AMS4303B-2007 Aluminum Alloy Plate, 2.7Cu - 2.2Li - 0.12Zr (2090-T81), Solution Heat Treated, Cold Worked, and Aged
- SAE AMS4904A-2007 Titanium Alloy Sheet, Strip, and Plate 6Al 4V Solution Heat Treated and Aged
- SAE AMS4236A-1987 Aluminum Alloy, Castings 4.6Cu 0.35Mn 0.25Mg 0.22Ti (A206.0-T4) Solution Heat Treated and Naturally Aged
- SAE AMS6906A-2011 Titanium Alloy Bars, Forgings and Forging Stock 6.0Al 2.0Sn 4.0Zr 6.0Mo Solution Heat Treated and Aged
- SAE AMS4478-2013 Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu 1.5Mg 0.60Mn (Alclad 2024, -T81 Sheet, -T851 Plate) Solution Heat Treated, Cold Worked and Artificially Aged
- SAE AMS4166F-2003 Aluminum Alloy, Extrusions 5.6Zn 2.5Mg 1.6Cu 0.23Cr (7075-T73) Solution Heat Treated and Overaged
- SAE AMS4934F-2011 Titanium Alloy, Extrusions and Flash Welded Rings, 6Al 4V, Solution Heat Treated and Aged
- SAE AMS4161G-2002 Aluminum Alloy, Extrusions 1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T4) Solution Heat Treated and Naturally Aged
- SAE AMS4223D-2007 Aluminum Alloy, Castings 4.5Cu - 0.70Ag - 0.30Mn - 0.25Mg - 0.25Ti (A201.0-T4) Solution Heat Treated and Naturally Aged
- SAE AMS4161H-2013 Aluminum Alloy, Extrusions 1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T4) Solution Heat Treated and Naturally Aged
- SAE AMS6921-2004 Titanium Alloy Bars, Forgings and Forging Stock 3Al 8V 6Cr 4Mo 4Zr Solution Heat Treated and Aged
- SAE AMS4965J-2007 Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Solution Heat Treated and Aged
- SAE AMS4990B-2013 Titanium Alloy Sheet, Strip, and Plate, 6Al - 6V - 2Sn, Solution Heat Treated and Aged
- SAE AMS4303B-2000 Aluminum Alloy Plate, 2.7Cu 2.2Li 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged
- SAE AMS4280J-2008 Aluminum Alloy Castings, Permanent Mold, 5.0Si 1.2Cu 0.5Mg (355.0-T71) Solution Heat Treated and Overaged
- SAE AMS4407-2007 Aluminum Alloy, Plate (7056-T7651) 9.1Zn - 1.6Cu - 1.9Mg Solution Heat Treated, Stress Relieved, and Overaged UNS A97056
- SAE AMS4347C-2007 Aluminum Alloy Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.5Mn (6013-T4) Solution Heat Treated and Naturally Aged UNS A96013
- SAE AMS4026L-2005 Aluminum Alloy, Sheet and Plate 1.0Mg 0.60Si 0.28Cu 0.20Cr Solution Heat Treated and Naturally Aged
- SAE AMS4339A-2004 Aluminum Alloy, Rolled or Cold Finished Bars and Rods 4.4Cu - 1.5Mg - 0.60Mn (2024-T851) Solution Heat Treated, Cold Worked, and Artificially Aged UNS A92024 [Superseded: SAE AMS 4112D]
- SAE AMS4237A-1987 Aluminum Alloy, Castings, Sand, 4.6Cu 0.35Mn 0.25Mg 0.22Ti (206.0-T71), Solution Heat Treated and Naturally Aged
- SAE AMS4470-2009 Aluminum Alloy, Plate (7085-T7451) 7.5Zn 1.6Cu 1.5Mg 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
- SAE AMS4473-2011 Aluminum Alloy Plate (2624-T39) 4.1Cu 1.4Mg 0.6Mn Solution Heat Treated, Cold Worked and Naturally Aged
- SAE AMS4211B-2007 Alluminum Alloy, Plate 6.2Zn - 1.9Cu - 2.1Mg - 0.10Zr (7040-T7451) Solution Heat Treated, Stress Relieved, and Overaged UNS A97040
- SAE AMS6930B-2011 Titanium Alloy Bars, Forgings and Forging Stock 6.0Al 4.0V Solution Heat Treated and Aged
- SAE AMS6935A-2011 Titanium Alloy Bars, Forgings and Forging Stock 6.0Al 6.0V 2.0Sn Solution Heat Treated and Aged
- SAE AMS6926A-2011 Titanium Alloy Bars, Forgings and Forging Stock 13V 11Cr 3Al Solution Heat Treated and Aged
- SAE AMS4965H-2002 Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Solution Heat Treated and Aged
- SAE AMS4306B-2007 Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T6151) Solution Heat Treated, Stress Relieved, and Aged UNS A97150
- SAE AMS4342D-2000 Aluminum Alloy, Extrusions 6.2Zn 2.3Cu 2.2Mg 0.12Zr (7050-T74511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged
- SAE AMS4401-2006 Aluminum Alloy Plate (7140-T7451) 6.6Zn - 1.8Cu - 2.0Mg - 0.10Zr Solution Heat Treated, Stress Relieved and Overaged
British Standards Institution (BSI), Alloy aging treatment
- BS EN 3459:2010 Aerospace series - Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn) - Solution treated and aged - Plate - 6 mm a 50 mm
- BS EN 3315:2018 Aerospace series. Titanium alloy TI-P64001. Solution treated and aged. Forgings. De ≤ 75 mm
- BS EN 3314:2019 Aerospace series. Titanium alloy TI-P64001. Solution treated and aged. Bar for machining. D ≤ 75 mm
- BS L 103:1971 Specification for forging stock and forgings of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0. 8)
- BS L 158:1978 Specification for close toleranced sheet and strip of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0. 8)
- BS L 164:1978 Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0. 8)
- BS 2L 169:2002 Ingots (as cast) and castings (solution treated and artificially aged) of aluminium-silicon-magnesium alloy (Si 7, Mg 0. 6)
(U.S.) Ford Automotive Standards, Alloy aging treatment
- FORD WSS-M2A176-A1-2013 ALUMINUM ALLOY, SHEET, NON-HEAT TREATABLE, REDUCED L脺DERING ***TO BE USED WITH FORD WSS-M99P1111-A***
Aerospace, Security and Defence Industries Association of Europe (ASD), Alloy aging treatment
- ASD-STAN PREN 3322-1996 Aerospace Series Titanium Alloy TI-P65001 Solution Treated and Aged Grade 1 - Forgings De Less Than or Equal to 75 mm (Edition P 2)
- ASD-STAN PREN 3340-1988 Aerospace Series Aluminium Alloy (7050) Solution Treated and Artificially Aged (T76) Die Forgings a Less Than or Equal to 200 mm (Issue P 1)
- ASD-STAN PREN 3314-1994 Aerospace Series Titanium Alloy TI-P64001 Solution Treated and Aged Bar for Machining D Less Than or Equal to 75 mm (Edition P 2)
- ASD-STAN PREN 3735-1994 Aerospace Series Titanium Alloy TI-P65002 Solution Treated and Aged Bar for Machining D is Less Than or Equal to 75 mm (Edition P 1)
- ASD-STAN PREN 3348-1988 Aerospace Series Aluminium Alloy (2024) Solution Treated and Artificially Aged (T62) Plate 6 Less Than or Equal to a Less Than or Equal to 50 mm (Issue P 1)
- ASD-STAN PREN 3119-1995 Aerospace Series Titanium Alloy TI-P46001 not Heat Treated Grade 2 Forging Stock, for Solution Treated and Aged Forgings a or D Less Than or Equal to 360 mm (Edition P 2)
- ASD-STAN PREN 3123-1988 Aerospace Series Aluminium Alloy AL-C27 Solution Treated and Artificially Aged (T6) Structural Precision Castings (Issue P 1)
- ASD-STAN PREN 3122-1988 Aerospace Series Aluminium Alloy AL-C27 Solution Treated and Artificially Aged (T6) High Strength Structural Precision Castings (Issue P 1)
- ASD-STAN PREN 3550-1988 Aerospace Series Aluminium Alloy (2024) Solution Treated, Stretched and Artificially Aged (T8511) Extruded Bars and Sections (a or D) Less Than or Equal to 150 mm (Issue P 1)
- ASD-STAN PREN 3343-1988 Aerospace Series Aluminium Alloy (7010) Solution Treated and Artificially Aged (T76511) Extruded Bars and Sections 1 Less Than (a or D) Less Than or Equal to 130 mm with Peripheral Coarse Grain Control (Issue P 1)
- ASD-STAN PREN 3466-1988 Titanium Alloy TI-P68 Solution Treated and Aged Rm Greater Than or Equal to 1000 MPa Bar for Machining De Less Than or Equal to 150 mm
- ASD-STAN PREN 3494-1995 Aerospace Series Titanium Alloy TI-P19001 Grade 2 Solution Treated and Aged Forgings De Less Than or Equal to 75 mm (Edition P 2)
- ASD-STAN PREN 3736-1995 Aerospace Series Titanium Alloy TI-P65002 Grade 2 Solution Treated and Aged Forgings De Less Than or Equal to 75 mm (Edition P 1)
- ASD-STAN PREN 3737-1995 Aerospace Series Titanium Alloy TI-P65002 Not Heat Treated Grade 2 Forging Stock, for Solution Treated and Aged Forgings a or D Less Than or Equal to 360 mm (Edition P 1)
- ASD-STAN PREN 3554-1988 Aerospace Series Aluminium Alloy (7010) Solution Treated, Cold Compressed and Artificially Aged (T7652) Hand Forgings a Less Than or Equal to 200 mm (Issue P 1)
Association Francaise de Normalisation, Alloy aging treatment
- NF L14-648*NF EN 3351:2013 Aerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De < ou = 150 mm
- PR EN 3871:1994 Aerospace series. Titanium alloy ti-P19001. Solution treated and aged. Sheet and strip, cold rolled a inferior or equal to 6 mm.
- PR EN 3870:1994 Aerospace series. Titanium alloy ti-P19001. Solution treated and aged. Sheet and strip, hot rolled a inferior or equal to 6 mm.
Korean Agency for Technology and Standards (KATS), Alloy aging treatment
KR-KS, Alloy aging treatment
Professional Standard-Ships, Alloy aging treatment