INDUSTRY COMPONENT

Blade Attachment Slots

Precision-engineered slots on rotor disks for secure blade attachment in turbomachinery.

Component Specifications

Definition
Blade attachment slots are precisely machined grooves or recesses on the periphery of a rotor disk in turbomachinery (such as gas turbines, steam turbines, or compressors). These slots are designed to securely hold and position turbine or compressor blades, transferring centrifugal and aerodynamic loads from the blades to the disk while maintaining precise alignment and allowing for thermal expansion. They are critical for rotor assembly integrity and aerodynamic performance.
Working Principle
The slots mechanically interlock with the blade roots (e.g., fir-tree, dovetail, or T-root designs) to transfer loads. During operation, centrifugal forces push the blade roots into the slot, creating a tight fit that distributes stress. The slot geometry ensures proper blade angle and spacing for optimal fluid dynamics, while allowing for differential thermal expansion between the disk and blades to prevent binding or excessive stress.
Materials
Typically forged or machined from high-strength, heat-resistant alloys such as nickel-based superalloys (e.g., Inconel 718, Waspaloy) or titanium alloys (e.g., Ti-6Al-4V), matching or complementing the rotor disk material. Surface treatments like shot peening or coatings may be applied to enhance fatigue resistance.
Technical Parameters
  • Hardness 30-50 HRC
  • Slot Type Fir-tree, Dovetail, T-slot, or Axial Entry
  • Tolerance ±0.025 mm to ±0.1 mm
  • Load Capacity Designed for centrifugal loads up to 100-500 MPa
  • Surface Finish Ra 0.8 μm to 3.2 μm
Standards
ISO 12107, DIN EN 10204, ASME B46.1

Industry Taxonomies & Aliases

Commonly used trade names and technical identifiers for Blade Attachment Slots.

Parent Products

This component is used in the following industrial products

Engineering Analysis

Risks & Mitigation
  • Fatigue cracking due to cyclic loads
  • Wear or fretting at slot interfaces
  • Misalignment causing vibration or efficiency loss
  • Thermal stress-induced deformation
FMEA Triads
Trigger: High cyclic centrifugal and thermal stresses
Failure: Crack initiation and propagation in the slot, leading to disk failure
Mitigation: Use fatigue-resistant materials, optimize slot geometry with finite element analysis (FEA), apply surface treatments, and implement regular NDT inspections.
Trigger: Improper machining or tolerances
Failure: Blade looseness or excessive stress concentrations
Mitigation: Adhere to strict machining standards, use precision tooling, and conduct thorough quality control checks.

Industrial Ecosystem

Compatible With

Interchangeable Parts

Compliance & Inspection

Tolerance
Meets ISO 2768-mK for general tolerances and specific design standards for slot geometry
Test Method
Dimensional verification via CMM, fatigue testing per ISO 12107, and NDT per ASME BPVC Section V

Buyer Feedback

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Frequently Asked Questions

What are the common types of blade attachment slots?

Common types include fir-tree slots (for high-stress applications like gas turbines), dovetail slots (common in steam turbines and compressors), T-slots (for axial retention), and axial entry slots (for easier assembly). The choice depends on load, temperature, and assembly requirements.

How are blade attachment slots inspected for quality?

Inspection methods include coordinate measuring machines (CMM) for dimensional accuracy, non-destructive testing (NDT) like dye penetrant or ultrasonic testing for cracks, surface roughness measurement, and visual checks for wear or damage during maintenance.

Can I contact factories directly?

Yes, each factory profile provides direct contact information.

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