Stationary airfoil-shaped components in turbines/expanders that direct and accelerate fluid flow onto rotating blades.
| Parameter | Typical range | Notes & selection driver |
|---|---|---|
| Solidity | 1.2-2.0 | |
| Aspect Ratio | 1.5-4.0 | |
| Chord Length | 50-300 mm | |
| Stagger Angle | 20-45° | |
| Leading Edge Radius | 0.5-2.0 mm | |
| Trailing Edge Thickness | 0.3-1.2 mm |
Ranges are indicative industry figures for RFQ preparation, not a supplier commitment. Confirm every value and standard with the legal manufacturer before ordering.
This component is used in the following industrial products
A practical evidence checklist for RFQ preparation and supplier evaluation.
Compare the published product scope and source details, then include your specifications and quantity in an enquiry.
Manufacturer profiles associated with Stator Vanes.
Explore company information and manufacturing capabilities, then discuss the scope of your project with a relevant supplier.
Stator vanes is the general term for stationary airfoils in turbomachinery. Nozzle guide vanes specifically refer to the first stator row immediately upstream of turbine rotors in gas turbines, where they function as convergent nozzles.
They optimize efficiency by: 1) Minimizing incidence losses through proper flow angle alignment, 2) Reducing secondary flow losses with endwall contouring, 3) Controlling wake interactions between blade rows, typically contributing 2-8% to stage efficiency.
Editorial classification, named public sources where available, and source-reviewed manufacturer records. See the editorial policy.