Udimet 720 Turbine Blade

Udimet 720 Turbine Blade

At our company, the turbine blades we manufacture using isothermal forging technology represent part of our commitment to high quality and innovation. Here is a detailed description of our isothermal forging turbine blades:
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Product Introduction

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At our company, the turbine blades we manufacture using isothermal forging technology represent part of our commitment to high quality and innovation. Here is a detailed description of our isothermal forging turbine blades:

material
Udimet 720 is a high-performance nickel-based superalloy known for its excellent high temperature strength, good weldability, and oxidation resistance at high temperatures. This alloy is ideal for the manufacture of turbine blades because it provides stable performance at high temperatures and pressures, and has excellent fatigue resistance.

technology
During the isothermal forging process, we heat the Udimet 720 to a specific temperature range and keep this temperature constant throughout the forging process. This process allows the material to distribute stress evenly during plastic deformation, thus avoiding cracks and other forms of defects. Isothermal forging can not only form a uniform microstructure, but also improve the dimensional accuracy of turbine blades, reduce the need for subsequent processing, and thus reduce costs.

advantage
Isothermal forged turbine blades have the following significant advantages:

Excellent high temperature performance: Udimet 720 alloys perform well at high temperatures and can withstand the extreme conditions inside aero engines.
High strength and toughness: The uniform microstructure formed in the isothermal forging process makes the turbine blade have higher strength and toughness.
High precision: isothermal forging technology can precisely control the geometry of the blade, reduce the amount of subsequent processing, and improve the yield.
Long life: Through isothermal forging and proper heat treatment process, the turbine blades obtain excellent fatigue resistance and corrosion resistance, thus extending the service life.
Economy: Although the initial cost of isothermal forging is higher, the overall cost effectiveness is improved by reducing the scrap rate and shortening the processing cycle.
Wide applicability: This turbine blade is suitable for a variety of applications, such as aeroengines, industrial gas turbines, etc., to meet the growing demand for high-performance materials.
By using Udimet 720 as a raw material, combined with advanced isothermal forging technology, our company's turbine blade products demonstrate their unique advantages in the market, providing customers with a reliable choice.

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parameter configuration
Product Name
Udimet 720 material constant temperature forging high temperature and high pressure turbine blades
Tolerance
CNC Machining ±0.004mm/Casting ±0.1mm
Place of Origin
Qingdao, Shandong, China
Processing Craft
Constant temperature forging
Material
U720
Manufacturing Method
Constant temperature forging
Surface Coating Technology
sico 1110
Type
OEM; Customized
Certification
ISO9001:2015 Certified, UL Certification,GE,SGS,TUV,etc
Packing
Carton/Wooden box
Inspection
1.Foundry in-house: 100% inspection on critical dimension; 100% on appea rance.
2.Third Party inspection available upon requirement.
3.Optional X-ray detection
4.Fluorescence detection
Service
Drawing Custom
Mainly Testing Facility
Spectrometer,CMM, Tensile testing machine, Impact tester,Hardness tester,X-Ray,Salt spray test box, Pneumatic detection,UV
accelerated weathering tester,dynamic balancing, high-temperature tensile testing,fluorescence test,room temperature mechanical
property testing and other testing.
Quality Guarantee
2 Years
Features & Advantage
1.High machining accuracy, the flatness within 0.001mm
2.High finish appearance, smooth surface roughness is Ra0.6 after machining.
3.The machining precision is high and the assembly structure is seamless.
4.Smooth appearance, corrosion resistance.
5.Pass Salt Spray Test with 144 Hours.
Standard
ISO , DIN, AISI, ASTM, BS, JIS, etc.
GB/T 14992 GJB 5512.1 HB 7763 HB/Z 140
Payment
L/C,D/A,D/P,T/T,Western Union,Money Gram
chemical properties
chemical name
content
Ni
55.16%-59.705%
Cr
15.5%-16.5%
Co
14.0%-15.5%
Ti
4.75%-5.25%
Mo
2.75%-3.25%
Al
2.25%-2.75%
W
1.00%-1.50%
Zr
0.0250%-0.0500%
B
0.0100%-0.0200%
C
0.0100%-0.0200%
Fe
≤0.50%
B
0.01~0.02%
Si
≤0.20%
Mn
≤0.15%
P
≤0.015%
physical properties
The density
8.14g/cm³
Characteristics
alloy non-magnetic
Melting point
1371°C (2500°F)

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