发布时间:2024-05-27 17:49:26 - 更新时间:2024年06月29日 15:22
点击量:0
Titanium materials for surgical implant applications Part 4: Wrought titanium 15-zirconium 4-niobium 4-tantalum alloy (Erratum 1)
Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Sheet and strip, hot rolled - a Less than or equal to 6 mm
Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in titanium alloy, aluminium IVD coated - Classification : 1 100 MPa (at ambient temperature)/425 oC.
This standard specifies requirements for titanium-aluminiummolybdenum-tin-silicon alloy forging stock with a tensile strength of 1 000 to 1 200 MPa
Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 MPa) (limiting ruling section over 100 mm up to and including 150 mm)
This standard specifies requirements for titanium-aluminiumvanadium alloy plate with a tensile strength of 895 to 1 150 MPa
Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)
This British Standard specifies requirements for commercially pure titanium sheet and strip with a tensile strength of 390 MPa to 540 MPa
Specification for sheet and strip of commercially pure titanium (tensile strength 390-540 MPa)
This British Standard specifies requirements for commercially pure titanium bar and section with a tensile strength of 540 MPa to 740 MPa
Specification for bar and section for machining of commercially pure titanium (tensile strength 540-740 MPa)
This British Standard specifies requirements for nickel-cobaltchromium-molybdenum-titanium-aluminium heat-resisting alloy plate, sheet and strip
Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)
This British Standard specifies requirements for titanium-aluminiummolybdenum-tin-silicon-carbon alloy forging stock with a tensile strength of 1 205
Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 MPa) (limiting ruling section over 25 mm up to and including 75 mm)
This British Standard specifies requirements for commercially pure titanium sheet and strip with a tensile strength of 290 MPa to 420 MPa
Specification for sheet and strip of commercially pure titanium (tensile strength 290-420 MPa)
This British Standard specifies requirements for commercially pure titanium sheet and strip with a tensile strength of 570 MPa to 730 MPa
Specification for sheet and strip of commercially pure titanium (tensile strength 570-730 MPa)
This standard specifies requirements for titanium-aluminiummolybdenum-tin-silicon alloy bar and section with a tensile strength of 1 000 MPa to 1 200
Specification for bar and section for machining of titanium-aluminium- molybdenum-tin-silicon-carbon alloy (Tensile strength 1000-1200 MPa) (Limiting ruling section over 100 mm up to and including 150 mm)
This British Standard specifies requirements for titanium-aluminiumvanadium alloy sheet with a tensile strength of 960 MPa to 1 270 MPa
Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 960-1270 MPa)
This British Standard specifies requirements for titanium-aluminiummolybdenum-tin-silicon-carbon alloy forging stock with a tensile strength of 1 250
Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 MPa) (limiting ruling section 25 mm)
This standard specifies requirements for titanium-aluminiummolybdenum-tin-silicon alloy forging stock with a tensile strength of 1 050 MPa to 1 220
Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 MPa) (limiting ruling section 100 mm)
Titanium materials for surgical implant applications Part 4: Wrought titanium 15-zirconium 4-niobium 4-tantalum alloy (Erratum 1)
Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Sheet and strip, hot rolled - a Less than or equal to 6 mm
Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in titanium alloy, aluminium IVD coated - Classification : 1 100 MPa (at ambient temperature)/425 oC.
This standard specifies requirements for titanium-aluminiummolybdenum-tin-silicon alloy forging stock with a tensile strength of 1 000 to 1 200 MPa
Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon alloy (tensile strength 1000-1200 MPa) (limiting ruling section over 100 mm up to and including 150 mm)
This standard specifies requirements for titanium-aluminiumvanadium alloy plate with a tensile strength of 895 to 1 150 MPa
Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)
This British Standard specifies requirements for commercially pure titanium sheet and strip with a tensile strength of 390 MPa to 540 MPa
Specification for sheet and strip of commercially pure titanium (tensile strength 390-540 MPa)
This British Standard specifies requirements for commercially pure titanium bar and section with a tensile strength of 540 MPa to 740 MPa
Specification for bar and section for machining of commercially pure titanium (tensile strength 540-740 MPa)
This British Standard specifies requirements for nickel-cobaltchromium-molybdenum-titanium-aluminium heat-resisting alloy plate, sheet and strip
Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy plate, sheet and strip (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)
This British Standard specifies requirements for titanium-aluminiummolybdenum-tin-silicon-carbon alloy forging stock with a tensile strength of 1 205
Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 MPa) (limiting ruling section over 25 mm up to and including 75 mm)
This British Standard specifies requirements for commercially pure titanium sheet and strip with a tensile strength of 290 MPa to 420 MPa
Specification for sheet and strip of commercially pure titanium (tensile strength 290-420 MPa)
This British Standard specifies requirements for commercially pure titanium sheet and strip with a tensile strength of 570 MPa to 730 MPa
Specification for sheet and strip of commercially pure titanium (tensile strength 570-730 MPa)
This standard specifies requirements for titanium-aluminiummolybdenum-tin-silicon alloy bar and section with a tensile strength of 1 000 MPa to 1 200
Specification for bar and section for machining of titanium-aluminium- molybdenum-tin-silicon-carbon alloy (Tensile strength 1000-1200 MPa) (Limiting ruling section over 100 mm up to and including 150 mm)
This British Standard specifies requirements for titanium-aluminiumvanadium alloy sheet with a tensile strength of 960 MPa to 1 270 MPa
Specification for sheet of titanium-aluminium-vanadium alloy (tensile strength 960-1270 MPa)
This British Standard specifies requirements for titanium-aluminiummolybdenum-tin-silicon-carbon alloy forging stock with a tensile strength of 1 250
Specification for forging stock of titanium-aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1250-1420 MPa) (limiting ruling section 25 mm)
This standard specifies requirements for titanium-aluminiummolybdenum-tin-silicon alloy forging stock with a tensile strength of 1 050 MPa to 1 220
Specification for forging stock of titanium- aluminium-molybdenum-tin-silicon alloy (tensile strength 1050-1220 MPa) (limiting ruling section 100 mm)