共找到 169 条与 黑色金属合金综合 相关的标准,共 12 页
This standard specifies the requirements relating to: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15)- Non heat treated, forging stock a or D ≤200 mm for aerospace applications.
Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D
This standard specifies the requirements relating to: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) -- Solution treated and precipitation treated, bar and section De ≤ 100 mm, Rm ≥ 960 MPa for aerospace applications.
Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De
This standard specifies the requirements relating to: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) — Solution treated and precipitation treated, bar and section De ≤ 100 mm, Rm ≥ 960 MPa for aerospace applications.
Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De ≤ 100 mm, Rm ≥ 960 MPa
This standard specifies the requirements relating to: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) — Solution treated and precipitation treated, bar and section a or D ≤ 100 mm, Rm ≥ 900 MPa for aerospace applications.
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 series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Non heat treated, forging stock a or D ? 250 mm
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 series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D ? 200 mm
Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De ? 100 mm, Rm ? 960 MPa
This standard specifies the requirements relating to:Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D = 900 MPa for aerospace applications.
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
This standard specifies the requirements relating to:Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Non heat treated, forging stock a or D
Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Non heat treated, forging stock a or D <= 250 mm
This standard specifies the requirements relating to:Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar andsection De = 960 MPafor aerospace applications.
Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De <= 100 mm, Rm >= 960 MPa
This standard specifies the requirements relating to:Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D
Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D <= 200 mm
This specification covers a series of iron-nickel, iron-nickel-cobalt, and iron-nickel-chromium alloys used for sealing to glasses and ceramics in electronic applications (see 6.1).
Iron-Nickel Alloys for Sealing to Glasses and Ceramics
This standard specifies the requirements relating to: Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15)-Non heat treated, forging stock a or D 250 mm for aerospace applications.
Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Non heat treated, forging stock a or D <= 250 mm
This standard specifies the requirements relating to:Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15)-Solution treated and precipitation treated, bar and section a or D 100 mm, Rm 900 MPa for aerospace applications.
Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D <= 100 mm Rm a >= 900 MPa
This standard specifies the requirements relating to:Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15)-Solution treated and precipitation treated, bar and section De 100 mm, Rm 960 MPa for aerospace applications.
Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De <= 100 mm, Rm >= 960 MPa
This standard specifies the requirements relating to: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15)-Non heat treated, forging stock a or D 200 mm for aerospace applications.
Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D <= 200 mm
This standard specifies the requirements relating to: Heat resisting alloy FE-PA2601(X6NiCrTiMoV26-15) Consumable electrode remelted Solution and precipitation treated Sheet, strip and plate Sheet,strip and plate 0,5 mm≤a≤10 mm for aerospace applications.
Aerospace series - Heat resisting alloy FE-PA2601(X6NiCrTiMoV26-15) - Consumable electrode remelted - Solution and precipitation treated - Sheet, strip and plate - 0,5 mm
Aerospace series - Steel FE-PL1507 (40CrMoV12) - Air melted - Annealed - Forging stock - a or D ? 350 mm
Polarizing/Coding Key Overstress Test Procedure for Electrical Connectors and Sockets To be published as ANSI/EIA/ECA-364-86
Polarizing/Coding Key Overstress Test Procedure for Electrical Connectors and Sockets To be published as ANSI/EIA/ECA-364-86
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