|
标准编号 |
标准名称 |
发布部门 |
发布日期 |
状态 |
|
SAE AMS 7904:2015 |
Beryllium Bars, Rods, Tubing, And Shapes, High Ductility Grade |
SAE Intern.. |
2015-01-07 |
现行 |
|
SAE AMS 7908:2015 |
Beryllium Near-Net Preforms, Standard Grade, Hot Isostatic Pressed |
SAE Intern.. |
2015-01-07 |
现行 |
|
SAE AMS 7910:2015 |
Beryllium Near-Net Preforms, Standard Grade, Cold Isostatic Pressed, Sintered |
SAE Intern.. |
2015-01-07 |
现行 |
|
SAE AMS 5878:2015 |
Nickel Alloy, Corrosion And Heat-Resistant, Sheet, Strip, And Plate, 59Ni - 22Cr - 2Mo - 14W - 0.35Ai - 0.03La, Solution Heat Treated |
SAE Intern.. |
2015-01-05 |
现行 |
|
SAE AMS 4535:2015 |
Copper-Beryllium Alloy, Mechanical Tubing 98Cu - 1.9Be Solution And Precipitation Heat Treated (Tf00, Formerly At) |
SAE Intern.. |
2015-01-05 |
现行 |
|
SAE AMS 5766:2014 |
Alloy, Corrosion And Heat-Resistant, Bars And Forgings, 21Cr - 32.5Ni - 0.38Ti - 0.38Al - 45Fe, Solution Heat Treated |
SAE Intern.. |
2014-12-29 |
现行 |
|
SAE AMS 5873:2014 |
Nickel Alloy, Corrosion And Heat-Resistant, Sheet, Strip, And Plate, 65Ni - 15.8Cr - 15.2Mo - 0.30Ai - 0.05La, Consumable Electrode Remelted, Solution Heat Treated |
SAE Intern.. |
2014-12-29 |
现行 |
|
SAE AMS 4783:2014 |
Cobalt Alloy, High Temperature Brazing Filler Metal, 50Co - 8.0Si - 19Cr - 17Ni - 4.0W - 0.80B, 2050 To 2100 Degrees F (1121 To 1149 Degrees C) Solidus-Liquidus Range |
SAE Intern.. |
2014-12-11 |
现行 |
|
SAE AMS 5544:2014 |
Nickel Alloy, Corrosion And Heat-Resistant, Sheet, Strip, And Plate, 57Ni - 19.5Cr - 13.5Co - 4.2Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B, Consumable Electrode Or Vacuum Induction Melted, Annealed |
SAE Intern.. |
2014-12-11 |
现行 |
|
SAE AMS 4700:2009 (R2014) |
Copper Wire, Bare, High Purity |
SAE Intern.. |
2014-12-03 |
现行 |
|
ASTM F1110-09(2014) |
Standard Test Method for Sandwich Corrosion Test |
American S.. |
2014-12-01 |
现行 |
|
ASTM D2532-14 |
Standard Test Method for Viscosity and Viscosity Change After Standing at Low Temperature of Aircraft Turbine Lubricants |
American S.. |
2014-12-01 |
被替代 |
|
ASTM D3115-95(2014) |
Standard Test Method for Explosive Reactivity of Lubricants with Aerospace Alloys Under High Shear |
American S.. |
2014-12-01 |
现行 |
|
SAE AMS 5769:2003 (R2014) |
Alloy, Corrosion And Heat-Resistant, Bars, Forgings, And Rings, 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0(Cb+Ta) - 0.15N - 32Fe Solution Heat Treated |
SAE Intern.. |
2014-10-14 |
现行 |
|
SAE AMS 5717:2003 (R2014) |
Nickel Alloy, Corrosion And Heat-Resistant, Bars, Forgings, And Rings 45.5Ni - 25.5Cr - 3.2Co - 3.2Mo - 3.2W - 18.5Fe Solution Heat Treated |
SAE Intern.. |
2014-10-13 |
现行 |
|
SAE AMS 4505:2009 (R2014) |
Copper Alloy (Brass), Sheet, Strip, And Plate, 70Cu - 30Zn, Annealed (Os035) |
SAE Intern.. |
2014-10-01 |
现行 |
|
SAE AMS 4554:2009 (R2014) |
Brass Tubing, Seamless, 66.5Cu - 33Zn - 0.45Pb, Annealed |
SAE Intern.. |
2014-10-01 |
现行 |
|
SAE AMS 3898/8:1994 (R2014) |
Interleaf Carrier Material, Composite Tape/Broadgoods, Kraft, Differentially Coated Paper, Unperforated, 0.0038 Inch +/- 0.0004 (0.097 Mm +/- 0.010) |
SAE Intern.. |
2014-08-18 |
现行 |
|
SAE AMS 3898/2:1994 (R2014) |
Interleaf Carrier Material, Composite Tape Polyethylene Film, 0.0018 Inch (0.046 Mm), Unperforated |
SAE Intern.. |
2014-08-18 |
现行 |
|
SAE AMS 3898/3:1994 (R2014) |
Interleaf Carrier Material, Composite Tape, Polyethylene Coated Paper, Unperforated, 0.0035 Inch (0.089 Mm) |
SAE Intern.. |
2014-08-18 |
现行 |
