ASTM B265 Gr1 Ti Alloy Chemical composition and Mechanical properties
ASTM B265 Gr1 Ti Alloy
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ASTM B265 Gr1 properties and heat treatment forged piece, Including ASTM B265 Gr1 application and specifications, We have all specifications，Including ASTM B265 Gr1 steel plate, ASTM B265 Gr1 sheet, ASTM B265 Gr1 square steel, ASTM B265 Gr1 flat bar,ASTM B265 Gr1 round bar,ASTM B265 Gr1 forgings, we can own production and sales.
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Specialized high quality steel
We have the advantages of equipment, technologies and price
forged/hot rolling/ extrusion of steel
We can produce the ASTM B265 Gr1 has the following specifications:
Round bar steel: 1mm to 3000mm
Square-shape steel: 1mm to 2000mm
Plate steel:0.1mm to 2500mm
Width: 10mm to 2500mm
Lenth: We can supply any lenth based on the customer's requirement.
Forging: Shafts with flanks/pipes/tubes/slugs/donuts/cubes/other shapes
Tubings: OD: φ6-219 mm, with wall thickness ranging from 1-35 mm.
Finished goods condition: hot forging/hot rolling + annealing/normalizing + tempering/quenching + tempering/any conditions based on the customer's requirement
Surface conditions: scaled (hot working finish)/ground/rough machining/fine machining/based on the customer's requirement
Furnaces for metallurgical processing: electrode arc + LF/VD/VOD/ESR/Vacuum consumable electrode.
Ultrasonic inspection: 100% ultrasonic inspection for any inperfections or based on the customer's requirementExcellent service for all kinds of industries,with advantages of technologies, equipment and price.
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Chemical composition % of the ladle analysis of grade ASTM B265 Gr1 and Standards
230.4~60mm
Brief description:
Titanium sheet/plate
Specification: T（0.4-60mm）*WT(400-3000mm)*L(1000-3000mm)
Material: Gr1 Gr2 Gr3 Gr4 Gr5 Gr7 Gr9 Gr12 Gr23
Standard: ASTM B265 BSW AMS JIS ISO9001:2000
Detailed description:
Titanium sheet/plate, titanium alloy sheet, mirror surface titanium sheet, titanium clad sheet
CP grade 1 can be used in the deep drawing parts for its good elongation and excellent corrosion-resistance.
CP grade 2 is used the most widely in the commercially pure titanium.
CP grade 3 is almost only used in pressure vessel.
CP grade 4 can be use in some fittings parts and fastening pieces, but for complex shape need 300 degree celsius to form.
Alloy grade 5, Ti-6Al-4V, is the most widely used in the titanium alloys because of its comprehensive mechanical, physical and chemical properties.
Alloy grade 7, add little palladium in cp titanium and it has the most excellent corrosion-resistance. Of course it costs higher.
Alloy grade 9, Ti-3Al-2.5V, is the most widely used in the golf clubs and bicycle girders.
Alloy grade 12, it has the similar properties with the grade 7 but costs lesser.
Alloy grade 23, Ti-6Al-4V ELI (Extra Low Interstitial) can be use in the medical appliance
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Mark |
Production method |
Processing technical |
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TA1(GR1) TA2(GR2) TA9(GR7) TC4(GR5) TA18(GR9) TC4ELI(GR23) |
Hot rolled |
R＆M |
CB/T3621-94 GB/T14845-2007 |
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Y＆M |
ASTM B265 ASTM F67 ASTM F136 MIL |
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Cold rolled |
C |
BWS |
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C |
JIS |
Machining performance
Download ASTM B265 Gr1 the mechanical properties of the report, the report provides detailed performance analysis and application. Download >>
Principal Design Features
One of the most widely used precipitation hardening grades in the business. While soft and ductile in the solution annealed condition, it is capable of high properties with a single precipitation or aging treatment. Characterized by good corrosion resistance, high harness, toughness and strength.
Machinability
Long, gummy chips characterize this alloys machinability. It can be machined in the annealed condition, however condition H1150M will yield best results. Post machining solution treatment of parts will be required prior to final hardening if machining in this condition.
Heat Treatment
CONDITION A--Soak at 1900 F (1038 C) for 30 minutes and cool below 60 F (16 C) for complete martensite transformation. CONDITION H 950- Treat Condition A material at 900 F(482 C) for 1 hour, air cool.. CONDITION H925, H1025, H1075, H1100, H1150- Soak solution treated material for 4 hours at specified temperature, air cool, CONDITION H1150M- Soak solution treated material at 1400 F (760 C) for 2 hours, air cool, then re-heat to 1150 F (620 C) for 4 hours and air cool.
Welding
Successfully welded by common fusion and resistance methods, this alloy should not be joined by oxyacetylene welding. AWS E/ER630 filler metal is recommended if required.
Forging
Soak for 1 hour at 2150 F (1177 C) prior to forging. Do not work below 1850 F (1010 C). Post-work solution treatment is required prior to final hardening.
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