Turbine Blade 0962E740P0002

The Turbine Blade 0962E740P0002 is a high-performance rotating hot-section component designed for use in gas turbine and aero-derivative turbine systems. Turbine blades operate in one of the most demanding environments within a turbine engine, converting thermal energy from high-temperature combustion gases into mechanical rotational power. Modern turbine blades are typically manufactured from advanced nickel-based superalloys capable of withstanding extreme temperatures, centrifugal forces, oxidation, and thermal fatigue.

As a critical component in power generation, oil & gas compression, marine propulsion, and aerospace engines, turbine blade reliability directly affects turbine efficiency, fuel consumption, maintenance intervals, and operational safety.

At Dawopu, we manufacture OEM-quality turbine blades and precision turbine components using advanced casting, CNC machining, heat treatment, and inspection technologies.

Material Specifications

Nickel-Based Superalloy (Typical)

Inconel 718

• Tensile Strength: 1240–1380 MPa
• Yield Strength: ≥1030 MPa
• Hardness: 35–45 HRC
• Operating Temperature: up to 700°C+
• Excellent fatigue resistance

High-Temperature Turbine Alloys

Inconel 738

• Outstanding creep resistance
• Excellent oxidation resistance
• Suitable for turbine hot sections

Directionally Solidified (DS) Superalloys

• Improved grain structure
• Enhanced fatigue life
• Better thermal stability

Single Crystal Superalloys (Optional)

• Superior creep resistance
• Extended turbine service life
• High-temperature aerospace applications

Modern turbine blades are commonly produced from high-strength superalloys specifically engineered for extreme temperature and stress conditions.