49.025.30 钛 标准查询与下载
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This European Standard specifies the requirements relating to: Titanium Ti-10V-2Fe-3Al Bars D ＜ 110 mm Rm ≥ 1 240 MPa for aerospace applications.
Aerospace series. Titanium Ti10V2Fe3Al. Bars. D＜110 mm. Rm≥1240 MPa
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-07-31
- 实施
- 2011-07-31
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
This specification covers the procedure for ultrasonic inspection of wrought titanium and titanium alloy products 0.25 inch (6.4 mm) and over in cross-sectional (thickness) or diameter. When specifically requested by purchaser, this specification may be used for metals other than titanium. This procedure has been used typically for locating internal defects, such as cracks, voids, spongy areas, and other structural discontinuities, which may or may not be exposed to the surface, but usage is not limited to such applications.
Ultrasonic Inspection, Titanium and Titanium Alloy Bar, Billet and Plate
- ICS
- 49.025.30
- CCS
- H26
- 发布
- 2011-07-22
- 实施
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, drawn shapes, and stock for forging or flash welded rings. These products have been used typically for parts requiring a combination of moderate strength and good ductility with a maximum service temperature up to 750 °F (400 °C) depending on time at temperature where the product is to be used in the annealed condition, but usage is not limited to such applications.
Titanium Alloy Bars, Wire, Forgings, Rings and Drawn Shapes 4Al 2.3V 1.5Fe Annealed
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-07-08
- 实施
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, drawn shapes, and stock for forging, heading, or flash welded rings. These products have been used typically for parts to be rough machined prior to solution and precipitation heat treatment and for parts, such as pressure vessels and other aerospace structures, requiring high strength-to-weight ratios at or near room temperature, 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; ARP982 recommends practices to minimize such conditions.
Titanium Alloy, Bars, Wire, Forgings, Rings, and Drawn Shapes 4Al 2.5V 1.5Fe Annealed, Heat Treatable
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-07-08
- 实施
This specification covers a titanium alloy in the form of bars, wire, forgings, and flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and of stock for forging and flash welded rings. These products have been used typically for parts which are machined after solution and precipitation heat treatment and aging and are suitable for parts requiring high strength-to-weight ratios up to moderately elevated temperatures, but usage is not limited to such applications.
Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Solution Heat Treated and Aged
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-06-23
- 实施
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring good weldability and ductility, combined with good notch-toughness down to -320 °F (-196 °C), but usage is not limited to such applications.
Titanium Alloy Bars, Wire, Forgings, and Rings 6Al 4V, Extra Low Interstitials Annealed
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-06-23
- 实施
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging, heading, or flash welded rings. These products have been used typically for parts to be rough machined prior to solution and precipitation heat treatment and for parts, such as pressure vessels and other aerospace structures, requiring high strength-to- weight ratios at or near room temperature, but usage is not limited to such applications.
Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Annealed, Heat Treatable
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-06-23
- 实施
This specification covers a titanium alloy in the form of bars, wire, forgings, and flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and of stock for foging or flash welded rings. These products have been used typically for parts which are machined after being solution heat treated and aged, and are suitable for parts requiring high strength-to-weight ratios at or near room temperature, but usage is not limited to such applications.
Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Solution Heat Treated and Aged Modified Strength
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-06-23
- 实施
This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate. These products have been used typically for parts requiring moderate, sustained strength up to 400 °F (204 °C) and oxidation resistance up to 600 °F (316 °C), but usage is not limited to such applications.
Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70 ksi (485 MPa)
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-06-23
- 实施
This specification covers a titanium alloy in the form of seamless tubing. This tubing has been used typically for parts, such as hydraulic lines, requiring strength and oxidation resistance up to 600 °F (316 °C) and weldability, but usage is not limited to such applications.
Titanium Alloy Tubing, Seamless, Hydraulic 3Al 2.5V, Controlled Contractile Strain Ratio Cold Worked, Stress Relieved
- ICS
- 49.025.30
- CCS
- V21
- 发布
- 2011-06-23
- 实施
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts which require high mechanical properties in the annealed condition and a high strength to weight ratio up to 750 °F (399 °C), but usage it not limited to such applications.
Titanium Alloy, Bars, Wire, Forgings and Rings, 6Al 6V 2Sn, Annealed
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-06-23
- 实施
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded ring. These products have been used typically for parts requiring good fatigue strength, formability, and strength up to 480 °F (249 °C), but usage is not limited to such applications. The alloy is superplastic below 1520 °F (827 °C) and hot formable from 1200 to 1560 °F (649 to 849 °C).
Titanium Alloys Bars, Wire, Forgings, and Rings 4.5Al 3V 2Fe 2Mo Annealed
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-06-23
- 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 high strength and toughness and good creep resistance up to 1000 °F (538 °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. ARP 982 recommends practices to minimize such conditions.
Titanium Alloy, Bars, Wire and Rings, 6.0Al 2.0Sn 4.0Zr 2.0Mo 0.08Si, Solution and Precipitation Heat Treated
- ICS
- 49.025.30
- CCS
- 发布
- 2011-06-23
- 实施
This specification covers a titanium alloy in the form of sheet, strip, and plate. This material has been used typically for parts to be formed or machined in the solution heat treated condition and subsequently precipitation heat treated requiring high strength-to-weight ratio and stability up to 550 °F (288 °C) in the precipitation heat treated condition, 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 Sheet, Strip, and Plate 6Al 4V Solution Heat Treated
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-06-07
- 实施
This specification covers a titanium alloy in the form of sheet, strip, and plate. This material has been typically requiring high strength-to-weight ratio and stability up to 550 °F (288 °C) in the precipitation heat treated condition, 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 Sheet, Strip, and Plate 6Al 4V Solution Heat Treated and Aged
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-06-07
- 实施
This European Standard specifies the requirements relating to: Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe) Rm 1300 MPa Bars De < 110 mm for aerospace applications.
Aerospace series - Titanium Ti-P63002 (Ti5Al5Mo5V3Cr0.4Fe) - Rm 1300 MPa - Bars - De < 110 mm
- ICS
- 49.025.30
- CCS
- 发布
- 2011-06-01
- 实施
This European Standard specifies the requirements relating to: Titanium Ti-10V-2Fe-3Al; Bars; D < 110 mm; Rm >= 1240 MPa for aerospace applications.
Aerospace series - Titanium Ti10V2Fe3Al - Bars - D < 110 mm - Rm >= 1240 MPa
- ICS
- 49.025.30
- CCS
- 发布
- 2011-06-01
- 实施
This standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy pre-production and production castings. It shall be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
Aerospace series - Titanium and titanium alloys - Technical specification - Part 008: Pre-production and production castings; German and English version EN 4800-008:2010
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-06
- 实施
This standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy remelting stock. It shall be applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
Aerospace series - Titanium and titanium alloys - Technical specification - Part 007: Remelting stock; German and English version EN 4800-007:2010
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2011-06
- 实施
