Incoloy 20 Turbocharger Spare Parts For Core Cartridge GT20 Turbo Turbine Wheel
Incoloy 20 Turbocharger Spare Parts For Core Cartridge GT20 Turbo Turbine Wheel
Incoloy 20 Turbocharger Spare Parts For Core Cartridge GT20 Turbo Turbine Wheel
Incoloy 20 Turbocharger Spare Parts For Core Cartridge GT20 Turbo Turbine Wheel
Incoloy 20 Turbocharger Spare Parts For Core Cartridge GT20 Turbo Turbine Wheel
Incoloy 20 Turbocharger Spare Parts For Core Cartridge GT20 Turbo Turbine Wheel
Incoloy 20 Turbocharger Spare Parts For Core Cartridge GT20 Turbo Turbine Wheel
Incoloy 20 Turbocharger Spare Parts For Core Cartridge GT20 Turbo Turbine Wheel
Turbo Turbine Wheel
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Product Name |
Custom Vacuum Forging Micro Turbocharger Inconel 625 713 Titanium Alloy Gas Steam Rc Jet Engine Turbine Impller Wheel For UAV |
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Tolerance |
0.004mm |
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Place of Origin |
Qingdao, Shandong, China |
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Processing Craft |
Drawing→ Mold design→ Mold manufacturing→ Wax pressing→ Wax Repairing→ Tree Grouping→ Shell Making (paste)→ Dewaxing→ Shell |
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Surface Treatment |
Electroplating, Chrome Plating, Zinc Plating, Nickel plating, Electrophoresis, Anodization, Polishing, Powder coating, |
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Type |
Precision casting, lost Wax Casting, investment casting, plaster casting, ceramic mold casting, metal mold casting,vauucm casting |
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OEM; Customized |
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Certification |
ISO9001:2015 Certified, UL Certification |
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Packing |
Carton/Wooden box |
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Inspection |
1.Foundry in-house: 100% inspection on critical dimension; 100% on appea rance. |
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2.Third Party inspection available upon requirement. |
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3.Optional X-ray detection |
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4.Fluorescence detection |
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Service |
Drawing Custom |
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Mainly Testing Facility |
Three-dimensional measuring instrument (CMM), Salt spray test box, Dynamic balance detector, Pneumatic detection |
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Quality Guarantee |
2 Years |
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Features & Advantage |
1.High machining accuracy, the flatness within 0.1mm |
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2.High finish appearance, smooth surface roughness is Ra1.6 after machining. |
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3.The machining precision is high and the assembly structure is seamless. |
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4.Smooth appearance, corrosion resistance. |
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5.Pass Salt Spray Test with 144 Hours. |
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Standard |
ISO , DIN, AISI, ASTM, BS, JIS, etc. |
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GB/T 14992 GJB 5512.1 HB 7763 HB/Z 140 |
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Payment |
L/C,D/A,D/P,T/T,Western Union,Money Gram |
Manufacturing Process
The manufacturing of nickel alloy turbine blades involves several sophisticated steps:
Investment Casting: The most common method, where a wax pattern of the blade is coated with a ceramic shell, which is then removed after the metal is poured and solidified.
Directional Solidification (DS) and Single Crystal (SC) Techniques: These advanced casting techniques align the grain structure of the metal, resulting in blades with superior mechanical properties and longer life spans. SC blades, in particular, have no grain boundaries, significantly reducing the likelihood of creep and fatigue.
Coating
To further protect against high temperatures and oxidation, turbine blades often receive a thermal barrier coating (TBC), typically composed of ceramic materials. These coatings can include:
Yttria-Stabilized Zirconia (YSZ): A common TBC material that provides excellent thermal insulation.
Bond Coats: Intermediate layers that improve the adhesion of the TBC to the metal substrate and protect against oxidation.
Advantages
High-Temperature Strength: Maintains mechanical properties at elevated temperatures.
Corrosion and Oxidation Resistance: Withstands harsh environments.
Creep Resistance: Resists deformation under long-term stress at high temperatures.
Fatigue Resistance: Withstands repeated thermal and mechanical loading cycles.
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