49.025.30 钛 标准查询与下载
共找到 620 条与 钛 相关的标准，共 42 页
Aerospace series - Titanium Ti10V2Fe3Al - Bars - D < 110 mm - Rm > or = 1 240 MPa.
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2012-02-01
- 实施
- 2012-02-25
This European Standard specifies the requirements relating to: Titanium alloy TI-P64003; Cold worked and stress relieved; Seamless tube for pressure systems; 4 mm
Aerospace series - Titanium alloy TI-P64003 - Cold worked and stress relieved - Seamless tube for pressure systems - 4 mm ��D ��51 mm - 690 MPa ��Rm ��1 030 MPa
- ICS
- 49.025.30
- CCS
- 发布
- 2012-02-01
- 实施
This European Standard specifies the requirements relating to: 1) Titanium alloy Ti-6Al-4V Annealed Forgings De 150 mm for aerospace applications.
Aerospace series - Titanium alloy Ti-6Al-4V - Annealed - Forgings - De <= 150 mm
- ICS
- 49.025.30
- CCS
- 发布
- 2012-02-01
- 实施
Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Not heat treated - Forging stock, for annealed forgings - De
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2012-01
- 实施
This European Standard specifies the requirements relating to: 1) Titanium alloy Ti-4Al-4Mo-2Sn Solution treated and aged Forgings De
Aerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De ≤ 150 mm
- ICS
- 49.025.30
- CCS
- 发布
- 2012
- 实施
This European Standard specifies the requirements relating to: )Titanium alloy TI P64001 (Ti 6Al 4V)Not heat treatedForging stock, for annealed forgingsDe
Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Not heat treated - Forging stock, for annealed forgings - De <= 360 mm
- ICS
- 49.025.30
- CCS
- 发布
- 2011-12-09
- 实施
- 2011-12-09
Aerospace series - Titanium Ti10V2Fe3Al - Bars - D
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-12-01
- 实施
Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Not heat treated. Forging stock, for annealed forgings. De
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-11-30
- 实施
- 2011-11-30
This specification covers a titanium alloy in the form of round bar and wire, 0.625 inch (15.88 mm) and under in nominal diameter or thickness. These products have been used typically for coil springs requiring high tensile strength and corrosion resistance, but usage is not limited to such application.
Titanium Alloy, Round Bar and Wire 3Al 8V 6Cr 4Mo 4Zr Consumable Electrode Melted Solution Heat Treated and Cold Drawn
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-10-21
- 实施
Aerospace series - Titanium Ti10V2Fe3Al - Bars - D < 110 mm - Rm ? 1 240 MPa
- ICS
- 49.025.30
- CCS
- 发布
- 2011-10-17
- 实施
- 2011-10-17
Aerospace series - Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe) - Rm ? 1 300 MPa - Bars - De < 110 mm
- ICS
- 49.025.30
- CCS
- 发布
- 2011-10-17
- 实施
- 2011-10-17
This specification covers a titanium alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring a combination of high tensile strength up to 750 °F (399 °C) and high fracture toughness, but usage is not limited to such applications.
Titanium Alloy Bars, Forgings, and Rings 6Al 4V Extra Low Interstitial (ELI) Duplex Annealed, Fracture Toughness
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-09-23
- 实施
This specification covers a titanium alloy in the form of bars, wire, flash welded rings, and stock for flash welded rings. These products have been used typically for parts requiring strength up to 800 °F (427 °C) and which may be welded during fabrication, but usage is not limited to such applications.
Titanium Alloy, Bars, Wire, and Rings, 5Al 2.5Sn, Annealed, 110 ksi (758 MPa) Yield Strength
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-09-13
- 实施
This specification covers a titanium alloy in the form of bars, wire, forging, flash welded rings, and stock for forging or flash welded rings. Primarily for parts requiring good weldability and high strength-to-weight ratio operating from -250 to -423 °F (-155 to -255 °C), but usage is not limited to such applications. The room and elevated temperature strengths of this alloy are lower than those of AMS 4926 and AMS 4966.
Titanium Alloy Bars, Forgings, and Rings 5A1 2.5Sn, Extra Low Interstitial, Annealed
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-09-13
- 实施
This specification covers a titanium alloy in the form of sheet and strip. These products have been used typically for parts to be formed in the solution heat treated condition and subsequently precipitation heat treated to obtain high strength-to-weight ratio or stability up to 1100 °F (593 °C), but usage is not limited to such applications.
Titanium Alloy, Sheet and Strip 15Mo 3.0Al 2.8Cb 0.20Si
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-09-13
- 实施
This specification covers a titanium alloy in the form of forgings 3.0 inches (76 mm) and under in nominal cross-sectional thickness and of stock for forging. These products have been used typically for parts in high stress and stress-corrosion-resistant applications, but usage is not limited to such applications.
Titanium Alloy Forgings 10V 2Fe 3Al Consumable Electrode Melted, Solution Heat Treated and Aged, 173 ksi (1193 MPa) Tensile Strength
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-09-13
- 实施
This specification covers a titanium alloy in the form of bars, wire, flash welded rings, and stock or flash welded rings or heading. This alloy has been used typically for parts requiring strength up to 800 °F (427 °C), but usage is not limited to such applications. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.
Titanium Alloy Bars, Wire, and Rings 8A1 1Mo 1V Solution Heat Treated and Stabilized
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-09-13
- 实施
This standard specifies the requirements relating to: Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0,4Fe) Rm >= 1300 MPa Bars De
Aerospace series - Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe) - Rm
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-09-01
- 实施
This European Standard specifies the requirements relating to: Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe) Rm ≥ 1 300 MPa Bars De ＜ 100 mm for aerospace applications.
Aerospace series. Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe). Rm≥1300 MPa. Bars. De＜110 mm
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-08-31
- 实施
- 2011-08-31
This standard specifies the requirements relating to:Titanium Ti10V2Fe3AlBarsD < 110 mmRm >or= 1 240 MPafor aerospace applications.
Aerospace series - Titanium Ti10V2Fe3Al - Bars - D < 110 mm - Rm + 1 240 MPa
- ICS
- 49.025.30
- CCS
- 发布
- 2011-07-31
- 实施
- 2011-07-31
