This page explains how Turbine Blades/Rotor is classified within Machinery and Equipment Manufacturing. Technical values and manufacturer relationships are research references; confirm the current specification and supplier evidence for each order.
The rotating assembly that extracts energy from fluid flow to drive a turbine shaft.
Technical details and manufacturing context for Turbine Blades/Rotor
| Parameter | Typical range | Notes & selection driver |
|---|---|---|
| Rotor Diameter | 500–2000 mm | Determines turbine size and power output |
| Blade Length | 100–800 mm | Affects aerodynamic performance and efficiency |
| Operating Speed | 3000–15000 rpm | Higher speeds require stronger materials |
| Max Operating Temperature | 600–1100 °C | Exceeding limit causes creep and oxidation |
| Blade Material | Inconel 718 | Nickel-based superalloy for high-temperature strengthASTM B637 |
| Rotor Material | AISI 4140 | Alloy steel for toughness and fatigue resistanceASTM A29 |
| Surface Finish | Ra 0.4–0.8 µm | Smoother finish reduces friction and stress concentrationISO 1302 |
| Balancing Grade | G2.5 | Ensures vibration within acceptable limitsISO 1940-1 |
| Dynamic Balancing Accuracy | ≤1.0 g·mm | Higher accuracy reduces vibration and noiseISO 1940-1 |
| Weight | 50–500 kg | Affects handling and installation |
| Max Overspeed | 120 % | Must withstand 120% of rated speed without failureAPI 611 |
Ranges are indicative industry figures for RFQ preparation, not a supplier commitment. Confirm every value and standard with the legal manufacturer before ordering.
Commonly used trade names and technical identifiers for Turbine Blades/Rotor.
This component is essential for the following industrial systems and equipment:
| pressure: | Up to 250 bar (dependent on design and material) |
| flow rate: | 5-500 m³/s (dependent on turbine size and application) |
| temperature: | -50°C to 650°C (dependent on material grade) |
| slurry concentration: | Not applicable for slurry; maximum solid particle size < 0.1 mm for clean fluids |
Indicative industry ranges for design and RFQ preparation. Confirm the exact figures and applicable standard with the manufacturer before specifying.
Quoted from the published standard.
Manufacturer profiles associated with Turbine Blades/Rotor.
Manufacturer listings support early research and capability understanding. They are not certification, ranking, or transaction guarantees.
A practical evidence checklist for RFQ preparation and supplier evaluation.
CNFX does not score or rank suppliers. Buyers must verify all claims and documents with the legal manufacturer before ordering.
Blades are often made from nickel-based superalloys like Inconel 718, while the rotor is commonly forged from alloy steel such as AISI 4140. These materials provide high-temperature strength, toughness, and fatigue resistance. Always verify the exact material grade with the manufacturer for your specific application.
Key parameters include rotor diameter (500–2000 mm), blade length (100–800 mm), operating speed (3000–15000 rpm), maximum operating temperature (600–1100°C), and operating pressure (1.0–1.6 MPa). These values are reference ranges; confirm the exact specifications for your model.
Balancing grade is typically specified as G2.5 per ISO 1940-1, with dynamic balancing accuracy of ≤1.0 g·mm. This ensures vibration remains within acceptable limits. The manufacturer should provide balancing reports to confirm compliance.
Relevant standards include ISO 1302 for surface finish, ISO 1940-1 for balancing, and API 611 for overspeed protection. These are verification references; the manufacturer must confirm that the product meets all applicable standards.
Editorial classification, named public sources where available, and source-reviewed manufacturer records.
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