49.025.30 钛 标准查询与下载

SAE AMS4971K-2014 退火热处理6Al - 6V - 2Sn钛合金棒,线材,锻件和环材

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 diameter or least distance between parallel sides and stock for forging or flash welded rings of any size.

Titanium Alloy, Bars, Wire, Forgings, and Rings, 6Al - 6V - 2Sn, Annealed, Heat Treatable

SAE AMS4978G-2014 退火的钛合金棒材、线材、锻材和环材6Al - 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.

Titanium Alloy Bars, Wire, Forgings, and Rings, 6Al - 6V - 2Sn, Annealed

SAE AMS4945F-2014 受控收缩的应变比冷作应力消失的液压无缝钛合金管3Al - 2.5V

This specification covers a titanium alloy in the form of seamless tubing.

Titanium Alloy Tubing, Seamless, Hydraulic, 3Al - 2.5V, Controlled Contractile Strain Ratio, Cold Worked, Stress Relieved

SAE AMS4935K-2014 β处理的淬火6Al - 4V钛合金挤压件和闪速对焊环

This specification covers a titanium alloy in the form of extruded bars and shapes, flash welded rings, and stock for flash welded rings. These products have been used typically for parts that do not require heat treatment but require high mechanical properties in the annealed condition and for which processing above the beta transus is permissible, but usage is not limited to such applications. This alloy exhibits high strength-to-weight ratios up to 750 °F (399 °C).

Titanium Alloy Extrusions and Flash Welded Rings, 6Al - 4V, Annealed, Beta Processed

SAE AMS4898D-2014 退火6Al - 2Sn - 2Zr - 2Mo - 2Cr - 0.15Si钛合金板材

This specification covers a titanium alloy in the form of sheet in nominal thicknesses 0.016 through 0.1874 inch (0.41 through 4.760 mm).

Titanium Alloy, Sheet, 6Al - 2Sn - 2Zr - 2Mo - 2Cr - 0.15Si, Annealed

NF L14-644*NF EN 3813:2013 航空航天系列.钛合金TI-P64001 (Ti-6Al-4V).退火的.锻造紧固件棒材和线材.De≤50 mm

Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar and wire for forged fasteners - De < or = to 50 mm

SAE AMS4993E-2013 6Al-4V烧结的混合粉末钛铝合金压块

This specification covers a titanium alloy in the form of compacts produced by pressing and sintering a blend of elemental titanium powder and aluminum vanadium alloy powder. These compacts have been used typically for light weight nuts (""B-nuts"") used for connecting fluid lines to fittings and to equipment, and for other small high-quantity miscellaneous hardware, 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, Blended Powder Compacts, Sintered, 6Al - 4V

SAE AMS4990B-2013 溶液热处理的和老化的6Al-6V-2Sn钛合金片材、带材和板材

This specification covers a titanium alloy in the form of sheet, strip, and plate. This material is typically used for parts requiring high strength-to-weight ratio and stability up to 550 °F (288 °C), but usage is not limited to such applications.

Titanium Alloy Sheet, Strip, and Plate, 6Al - 6V - 2Sn, Solution Heat Treated and Aged

SAE AMS4907K-2013 退火超低间隙钛合金片材、带材和板材

Titanium Alloy, Sheet, Strip, and Plate, 6.0Al - 4.0V, Extra Low Interstitial, Annealed

SAE AMS4902K-2013 屈服强度40.0 ksi(276 MPa)纯商业退火的钛薄板材、带材和厚板材

This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate up through 1.000 inch (25.40 mm). This material typically has been used for parts requiring aqueous corrosion resistance, moderate 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 40.0 ksi (276 MPa) Yield Strength

SAE AMS4958D-2013 3Al 8V 6Cr 4Mo 4Zr自耗电极熔炼、溶液热处理和无中心接地的钛合金棒材和杆材

This specification covers a titanium alloy in the form of bars and rod 1.000 inch (25.40 mm) and under in nominal diameter. These products have been used typically for coil springs requiring low solid height, high tensile strength, and corrosion resistance, but usage is not limited to such applications.

Titanium Alloy, Bars and Rod, 3Al 8V 6Cr 4Mo 4Zr, Consumable Electrode Melted, Solution Heat Treated and Centerless Ground or Peeled and Polished

SAE AMS4949A-2013 表面粘结的层压钛片材

This specifocation covers titanium in the form of laminated sheet. This materials has been used typically for shims in which thickness is adjusted by removal of laminations as required, but usage is not limited to such applications.

Titanium, Sheet, Laminated, Surface Bonded

DS/EN 4632-006:2013 航空航天系列 航空航天结构材料的焊接性和钎焊性 第006部分：钛合金的均质组件

This European Standard defines degrees of weldability and brazeability for materials or families of materials used in the aerospace applications. It comprises a series of sheets, by materials or by material family, which: - indicate the main titles, the t

Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys

DIN EN 3813:2013 航空航天系列.钛合金TI-P64001(Ti-6Al-4V).退火.锻造紧固件的棒材和线材.D_e 50 mm.德文和英文版本EN 3813-2013

Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar and wire for forged fasteners - D_e 50 mm; German and English version EN 3813:2013

DIN EN 3354:2013 航空航天系列.钛合金Ti-6Al-4V.退火.超塑性成形片材.a < kleiner => 6 mm.德文和英文版本EN 3354-2013

Aerospace series - Titanium alloy Ti-6Al-4V - Annealed - Sheet for superplastic forming - a 6 mm; German and English version EN 3354:2013

SAE AMS4998E-2013 6Al 4V钛合金粉末

This specification covers a titanium alloy in the for of prealloyed powder. This powder has been used typically for compaction into net or near net shapes and into forgings stock in the form of billets or preforms, but usage is not limited to such applications.

Titanium Alloy Powder 6Al 4V

NF L14-648*NF EN 3351:2013 航空航天系列.钛合金Ti-4Al-4Mo-2Sn.溶液处理和老化.锻件. De 150 mm

Aerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De < ou = 150 mm

SAE AMS4915L-2013 单退火8Al 1V 1Mo钛合金薄板材、带材和厚板材

This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm). These products have been used typically for parts requiring strength up to 800 °F (427 °C) where fracture toughness is not critical. 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 8Al 1V 1Mo Single Annealed

SAE AMS4966P-2013 屈服强度为110 ksi(758 MPa)的退火钛合金锻件5Al 2.5Sn

This specification covers a titanium alloy in the form of forgings and forging stock. These forgings 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, Forgings 5Al 2.5Sn Annealed, 110 ksi (758 MPa) Yield Strength

SAE AMS4939B-2013 经溶液热处理的钛合金3Al 8V 6Cr 4Mo 4Zr薄板材、带材和厚板材

This specification covers a titanium alloy in the form of sheet, strip, and plate through 4.000 inches (101.60 mm).. 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 treatment 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 3Al 8V 6Cr 4Mo 4Zr Solution Heat treated