49.025.30 钛 标准查询与下载

SAE AMS4917H-2012 溶液热处理的钛合金薄板材、带材和板材13.5V 11Cr 3.0Al

This specification covers a titanium alloy in the form of sheet, strip, and plate through 4.00 inches (101.6 mm).. This material has been used typically for parts to be formed 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 conditions, but usage is not limited to such applications. This alloy may have poor crack propagation resistance in the precipitation heat treated condition. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP982 reco

Titanium Alloy Sheet, Strip, and Plate 13.5V 11Cr 3.0Al Solution Heat Treated

DIN EN 3456:2012 航空航天系列. TI-P64001 (Ti-6Al-4V)型钛合金. 退火. 热轧板材和带材. <小于 => 6 mm; 德文和英文版本EN 3456-2012

Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Sheet and strip, hot rolled - a 6 mm; German and English version EN 3456:2012

BS EN 3464:2012 航天航空系列.钛合金(TI-6AI-4V).煅烧.板材.6 mm

SAE AMS4979G-2012 溶解和沉淀热处理钛合金棒材,线材,锻件和环材6A1 6V 2Sn

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 high strength- to-weight ratio up to 750 °F (399 °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, Forgings, and Rings 6A1 6V 2Sn Solution and Precipitation Heat Treated

SAE AMS4970J-2012 溶解和沉淀热处理7A1 4Mo钛合金棒材,线材和铸件

This specification covers a titanium alloy in the form of bars, wire, forgings, and forging stock. This alloy has been used typically for parts requiring strength up to 900 °F (482 °C), but usage is not limited to such application. 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 Forgings 7A1 4Mo Solution and Precipitation Heat Treated

SAE AMS4940B-2012 退火25.0 ksi屈服强度(172 MPa)工业纯钛金属片材,带板和板材

This specification covers one grade (Grade 1) of commercially-pure titanium in the form of sheet, strip, and plate up through a thickness of 1.000 inch (25.40 mm). This material has been used typically for parts requiring the properties of titanium and good formability but not high strength, but usage is not limited to such applications.

Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 25.0 ksi (172 MPa) Yield Strength

SAE AMS2636-2012 优质级钛和钛合金铸件的浸入式超声波检查

This specification covers procedures for ultrasonic immersion inspection of premium grade wrought titanium and titanium alloy forgings. Premium grade is a term used to describe titanium alloys used for critical rotating components in turbine engines. For details, see SAE AMS 2380, the specification that covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products.

Ultrasonic Immersion Inspection Titanium and Titanium Alloy Forgings Premium Grade

SAE AMS4910P-2012 退火5Al 2.5Sn钛合金片材,带材和板材

This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring strength up to 800 °F (427 °C) and where such parts may require welding during fabrication, 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 5Al 2.5Sn Annealed

SAE AMS2643E-2012 钛合金结构检查,化学腐蚀检查规程

This specification covers a procedure for revealing the macrostructure and microstructure of titanium alloys. This inspection procedure has been used typically for detecting defects and segregation in titanium alloys. This procedure should not be used on finished parts.

Structural Examination of Titanium Alloys, Chemical Etch Inspection Procedure

SAE AMS4976H-2012 溶解和沉淀热处理6.0Al 2.0Sn 4.0Zr 2.0Mo钛合金铸件

This specification covers a titanium alloy in the form of forgings and forging stock. 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 procedure and service conditions may cause these forgings to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.

Titanium Alloy, Forgings 6.0Al 2.0Sn 4.0Zr 2.0Mo Solution and Precipitation Heat Treated

SAE AMS4981F-2012 融解和沉积热处理6.0Al 2.0Sn 4.0Zr 6.0Mo钛合金棒材,线材和铸件

This specification covers a titanium alloy in the form of bars, wire, forgings, and forging stock. This alloy has been used typically for parts requiring high strength 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. SAE ARP 982 recommends practices to minimize such conditions.

Titanium Alloy Bars, Wire, and Forgings 6.0Al 2.0Sn 4.0Zr 6.0Mo Solution and Precipitation Heat Treated

DS/EN 3464:2012 航空航天系列 钛合金 Ti-6Al-4V 退火 板材 6 mm < a <= 100 mm

This European Standard specifies the requirements relating to:Titanium alloy Ti-6Al-4VAnnealedPlate6 mm < a

Aerospace series - Titanium alloy Ti-6Al-4V - Annealed - Plate - 6 mm < a <= 100 mm

SAE AMS4975L-2012 溶解和沉淀热处理6.0Al 2.0Sn 4.0Zr 2.0Mo 0.08Si钛合金棒材,线材和环材

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

SAE AMS4963C-2012 改进强度热处理退火6.0Al 4.0V钛合金棒材,线材,锻件和环材

This specification covera a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging, flash welded rings, or heading. These products have been used typically for parts to be rough machined prior to solution and precipitation heat treatment and for parts 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; SAE ARP 983 recommends practices to minimize such conditions.

Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Annealed, Heat Treatable, Modified Strength

SAE AMS4973G-2012 溶解热处理和稳定钛合金锻件8Al 1Mo 1V

This specificaiton covers a titanium alloy in the form of forgings and forging stock. This alloy has been used typically for parts requiring strength up to 800 degree F (427 degree C), but usage is not limited to such applications.

Titanium Alloy Forgings 8Al 1Mo 1V Solution Heat Treated and Stabilized

SAE AMS4909J-2012 超低间隙退火,5Al 2.5Sn板材,带材和片材钛合金

This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring a combination of weldability, ductility, and good notch-toughness down to -423 °F (-253 °C), but usage is not limited to such applications. Certain processing procedures and service conditions may cause those products to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.

Titanium Alloy, Sheet, Strip, and Plate 5Al 2.5Sn, Extra Low Interstitial Annealed

DS/EN 3456:2012 航空航天系列 钛合金 TI-P64001（Ti-6Al-4V） 退火 板材和钢带，热轧 a <= 6 mm

This standard specifies the requirements relating to:Titanium alloy TI-P64001 (Ti-6Al-4V)AnnealedSheet and strip, hot rolleda

Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Sheet and strip, hot rolled - a <= 6 mm

EN 3464:2012 航天航空系列.钛合金(TI-6AI-4V).煅烧.板材.6 mm

This European Standard specifies the requirements relating to: Titanium alloy Ti-6Al-4V Annealed Plate 6 mm < a 100 mm for aerospace applications.

Aerospace series - Titanium alloy Ti-6Al-4V - Annealed - Plate - 6 mm < a ≤ 100 mm

BS EN 3456:2012 航空航天系列.TI-P64001(Ti-6Al-4V)型钛合金.退火.热轧薄板材和带材.a 6 mm

Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Sheet and strip, hot rolled - a 6 mm

SAE AMS7498P-2012 钛和钛合金闪焊环材

This specification covers flash welded rings made of titanium and selected titanium alloys. These rings have been used typically for parts such as flanges and rings, but usage is not limited to such applications.

Rings, Flash Welded Titanium and Titanium Alloys