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High Temperature Alloy in Gas Turbines

We provide one-stop vacuum casting and post-processing services for key gas turbine high-temperature parts, including turbine blades, turbine disks, turbine segments, combustion chambers, gas turbine stators, turbine nozzles, turbine impellers and other precision accessories.

High Temperature Alloy in Gas Turbines Introduction

Gas turbines operate under extreme high-temperature, high-pressure and corrosive working conditions, requiring high-performance alloys with exceptional creep resistance, thermal fatigue strength, oxidation resistance and structural stability. Qihang Bida focuses on custom vacuum casting of high-temperature alloys specifically designed for gas turbine components, addressing the core performance demands of gas turbine power generation, aerospace propulsion and marine power systems.

Nickel-based superalloys (Inconel Series, Nimonic alloy, Rene Alloys), cobalt-based superalloys, MAR-M alloys, single crystal alloys (CMSX Series) and nickel-chromium alloys are the most widely adopted materials for gas turbines. These alloys maintain excellent mechanical properties and dimensional stability even under long-term high-temperature service up to 1000°C, effectively resisting creep deformation, oxidation and hot corrosion.

We provide one-stop vacuum casting and post-processing services for key gas turbine high-temperature parts, including turbine blades, turbine disks, turbine segments, combustion chambers, gas turbine stators, turbine nozzles, turbine impellers and other precision accessories. Our vacuum casting process eliminates internal porosity and impurities, ensuring high dimensional accuracy and structural integrity for every gas turbine component, meeting strict industrial quality standards and long service life requirements.

Nickel-Based Superalloys

STEP 1

Inconel X-750(GH4145)

Designed for high-load environments above 700℃, mainly used for turbine blades and guide vanes. It boasts ultra-high strength, exceptional creep resistance and fatigue resistance, ensuring stable performance under harsh thermal-mechanical coupling conditions.

STEP 2

Hastelloy X (GH3536)

Capable of long-term service at up to 1200℃, specially developed for combustion chambers, flame tubes and other high-temperature components. It features superior oxidation resistance and excellent weldability, adapting to extreme thermal cycling environments.

STEP 3

‌Incoloy 901‌(GH1035)

Suitable for hot-end components operating below 700℃, such as combustion chambers and turbine diaphragms. It delivers high toughness and outstanding thermal fatigue resistance, prolonging the service life of key parts.

STEP 4

Inconel 718(GH4169)

One of the most widely used wrought superalloys, primarily applied to compressor disks, bolts and other structural parts. It features a yield strength of up to 1000 MPa at 650℃, with outstanding structural stability and mechanical properties.

Cobalt-based Superalloys

UMCo50(Co150B): Ideal for high-temperature wear-resistant environments ranging from 600℃ to 950℃, widely used for guide vanes, seals, nozzles and other components. It features high hardness (HRC≥35 at 950℃), excellent erosion resistance and hot corrosion resistance.

Cobalt-based Superalloys Specifications

PartGradesKey Performance
Combustio ChamberGH3536,Inconel 617,Hastelloy XHigh temperature oxidation resistance, thermal fatigue resistance, easy welding
Guide VaneInconel 718, GH4169,IN738,Mar M247,FSX414High temperature endurance strength, thermal corrosion resistance
Rotor BladeIN792,IN939,Single Crystal CMSX-4High creep resistance, fatigue resistance, hot corrosion resistance
Turbine DiskInconel 718,GH4169, A286, GH2132, GH2903High yield strength, low expansion, stable microstructure
Seal/Ring ComponentGH2903Low thermal expansion, high dimensional stability

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