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Ti11Sn5Zr2.25Al1Mo0.25Si

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Ti11Sn5Zr2.25Al1Mo0.25Si properties and heat treatment forged piece, Including Ti11Sn5Zr2.25Al1Mo0.25Si application and specifications, We have all specifications,Including Ti11Sn5Zr2.25Al1Mo0.25Si steel plate, Ti11Sn5Zr2.25Al1Mo0.25Si sheet, Ti11Sn5Zr2.25Al1Mo0.25Si square steel, Ti11Sn5Zr2.25Al1Mo0.25Si flat bar,Ti11Sn5Zr2.25Al1Mo0.25Si round bar,Ti11Sn5Zr2.25Al1Mo0.25Si forgings, we can own production and sales.


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We have the advantages of equipment, technologies and price

forged/hot rolling/ extrusion of steel


We can produce the Ti11Sn5Zr2.25Al1Mo0.25Si 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 Ti11Sn5Zr2.25Al1Mo0.25Si and Standards

Titanium IMI 679 (Ti-11Sn-5Zr-2.25Al-1Mo-0.25Si), Oil-Quenched and Aged
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Near Alpha Titanium Alloy

Material Notes: Alpha Prime Transus 880ºC. Tensile Properties below after oil quench/aged heat treatment: 900°C/OQ, 500°C/24hr/AC.

Key Words: Ti11Sn5Zr2.25Al1Mo0.25Si

Physical Properties Metric English Comments
Density  4.84 g/cc 0.175 lb/in³
 
Mechanical Properties Metric English Comments
Tensile Strength, Ultimate  1110 MPa 161000 psi
Tensile Strength, Yield  970 MPa 141000 psi
Elongation at Break  8.00 % 8.00 %
Reduction of Area  25.0 % 25.0 %
Modulus of Elasticity  115 GPa 16700 ksi Typical value for an alpha titanium alloy
Poissons Ratio  0.310 0.310 Typical for alpha titanium alloy.
Fatigue Strength   110 MPa
@# of Cycles 1.00e+7
16000 psi
@# of Cycles 1.00e+7
Kt = 3.0; R = -1.0 (air-cooled and aged sample)
  200 MPa
@# of Cycles 50000
29000 psi
@# of Cycles 50000
Kt = 3.0; R = -1.0 (air-cooled and aged sample)
  390 MPa
@# of Cycles 1.00e+7
56600 psi
@# of Cycles 1.00e+7
(air-cooled and aged sample)
  590 MPa
@# of Cycles 50000
85600 psi
@# of Cycles 50000
(air-cooled and aged sample)
Shear Modulus  43.9 GPa 6370 ksi Calculated from typical values.
 
Electrical Properties Metric English Comments
Electrical Resistivity  0.000160 ohm-cm 0.000160 ohm-cm
 
Thermal Properties Metric English Comments
CTE, linear   8.60 µm/m-°C
@Temperature 20.0 °C
4.78 µin/in-°F
@Temperature 68.0 °F
  9.30 µm/m-°C
@Temperature 250 °C
5.17 µin/in-°F
@Temperature 482 °F
  10.0 µm/m-°C
@Temperature 500 °C
5.56 µin/in-°F
@Temperature 932 °F
Specific Heat Capacity  0.500 J/g-°C 0.120 BTU/lb-°F
Thermal Conductivity  8.30 W/m-K 57.6 BTU-in/hr-ft²-°F
Maximum Service Temperature, Air  450 °C 842 °F
Beta Transus  880 °C 1620 °F
 
Component Elements Properties Metric English Comments
Aluminum, Al  2.25 % 2.25 %
Molybdenum, Mo  1.0 % 1.0 %
Silicon, Si  0.25 % 0.25 %
Tin, Sn  11.0 % 11.0 %
Titanium, Ti  81.0 % 81.0 %
Zirconium, Zr  5.0 % 5.0 %

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MTA670 / 14134
 




Machining performance

Download Ti11Sn5Zr2.25Al1Mo0.25Si 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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