Titanium 1100
Titanium 1100 properties and heat treatment forged piece, Including Titanium 1100 application and specifications, We have all specifications,Including Titanium 1100 steel plate, Titanium 1100 sheet, Titanium 1100 square steel, Titanium 1100 flat bar,Titanium 1100 round bar,Titanium 1100 forgings, we can own production and sales.
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We can produce the Titanium 1100 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 requirement
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Chemical composition % of the ladle analysis of grade Titanium 1100 and Standards
Titanium 1100 Beta Quenched and annealed
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Near Alpha Titanium Alloy
Material Notes:
Key Words: Titanium 1100
Physical Properties | Metric | English | Comments |
---|---|---|---|
Density | 4.50 g/cc | 0.163 lb/in³ | |
Mechanical Properties | Metric | English | Comments |
Tensile Strength, Ultimate | 1010 MPa | 146000 psi | |
750 MPa @Temperature 400 °C |
109000 psi @Temperature 752 °F |
||
Tensile Strength, Yield | 910 MPa | 132000 psi | |
625 MPa @Temperature 400 °C |
90600 psi @Temperature 752 °F |
||
Elongation at Break | 11.0 % | 11.0 % | |
Modulus of Elasticity | 107 - 117 GPa | 15500 - 17000 ksi | |
Poissons Ratio | 0.310 | 0.310 | Typical for alpha titanium alloy. |
Fatigue Strength | 250 MPa @# of Cycles 1.00e+7 |
36300 psi @# of Cycles 1.00e+7 |
notched with Kt = 3.0. |
655 MPa @# of Cycles 1.00e+7 |
95000 psi @# of Cycles 1.00e+7 |
notched with Kt = 1.0. | |
Fracture Toughness | 63.0 MPa-m½ | 57.3 ksi-in½ | K(IC) after 1095ºC anneal |
Shear Modulus | 42.7 GPa | 6190 ksi | Calculated from typical values. |
Electrical Properties | Metric | English | Comments |
Electrical Resistivity | 0.000160 ohm-cm | 0.000160 ohm-cm | Estimated from similar alpha titanium alloys. |
Thermal Properties | Metric | English | Comments |
CTE, linear | 9.00 µm/m-°C @Temperature 20.0 - 100 °C |
5.00 µin/in-°F @Temperature 68.0 - 212 °F |
Typical alpha titanium alloy |
Specific Heat Capacity | 0.525 J/g-°C | 0.125 BTU/lb-°F | Typical value for titanium alloys. |
Thermal Conductivity | 7.00 W/m-K | 48.6 BTU-in/hr-ft²-°F | Estimated from similar titanium alloys. |
Beta Transus | 1015 °C | 1859 °F | |
Component Elements Properties | Metric | English | Comments |
Aluminum, Al | 6.0 % | 6.0 % | |
Molybdenum, Mo | 0.40 % | 0.40 % | |
Silicon, Si | 0.40 % | 0.40 % | |
Tin, Sn | 2.70 % | 2.70 % | |
Titanium, Ti | 87.0 % | 87.0 % | |
Zirconium, Zr | 4.0 % | 4.0 % |
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Machining performance
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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.