Aerospace turbine blade fir-tree root is a precision-engineered attachment component that secures turbine blades to rotor discs in jet engines using a multi-tooth interlocking design.
| Parameter | Typical range | Notes & selection driver |
|---|---|---|
| Taper Angle | 15-30 degrees | |
| Tooth Count | 3-6 teeth | |
| Fatigue Life | >10,000 cycles at design stress | |
| Surface Finish | Ra 0.4-0.8 μm | |
| Temperature Range | Up to 1000°C | |
| Centrifugal Load Capacity | 50-200 kN per blade |
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
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Manufacturer profiles associated with Fir-Tree Root.
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The fir-tree root provides optimal load distribution across multiple teeth, reduces stress concentrations, accommodates thermal expansion, and offers reliable blade retention under extreme centrifugal forces and temperatures.
Common failures include fretting fatigue at contact surfaces, stress corrosion cracking, creep deformation at high temperatures, and tooth wear from vibrational micro-movements.
Manufacturing typically involves precision machining (broaching, EDM, or grinding), followed by heat treatment, shot peening for compressive stress, and surface coating application for thermal protection.
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