Rene 41 Seal Segment Tooling for Honeycomb Pocket and Feather Edges

Plan five-axis carbide tooling for a Rene 41 turbine seal segment with a honeycomb braze pocket, thin feather edges, angled cooling holes and gas-path profile inspection.

Rene 41 Seal Segment Tooling for Honeycomb Pocket and Feather Edges

English: Rene 41 Seal Segment Tooling for Honeycomb Pocket and Feather Edges

This case begins at the thin feather edge, because a toolpath that is safe in the pocket can still pull the edge or consume braze stock. Five-axis access and wear trends drive each cutter decision.

Drawing feature-to-tool decisions

Drawing feature Tool, geometry and holder Decision and rejected alternative
Forging skin and datum pads Ø32 high-positive PVD carbide shoulder mill, strong micro-hone Survives interrupted skin while avoiding a heavily negative heat-generating edge.
Honeycomb braze pocket Ø10 5-flute AlTiN variable-helix rougher, then Ø6 reduced-neck finisher Separates metal removal from corner access and protects braze-wall stock.
Curved gas-path surface Ø12 carbide barrel cutter, AlTiN, shrink-fit holder Large effective radius reduces passes; a long small ball mill is rejected for deflection.
Feather edges Ø4 sharp corner-radius carbide, light alternating passes Balances cutting force across the thin edge and leaves controlled braze allowance.
Angled cooling holes Carbide spot drill plus Ø1.2 coated micro drill, short pilot and guided 5-axis entry Prevents skating and work-hardened entry; peck dwell is rejected.

Fixture and cutting sequence

Use a 3+2 roughing orientation for the pocket, leave 0.30 mm braze stock, then use continuous five-axis barrel finishing on the gas path. Support the feather edge with a removable nest and alternate sides before microdrilling.

Material, chip and tool-life controls

Rene 41 work-hardens after rubbing. Keep radial engagement constant, use high-pressure coolant aimed below the edge, index tool life by cutting minutes and stop when scallop height or spindle load trends upward.

Tolerance and surface verification

Blue-light scan compares the gas-path profile, CMM verifies datum-pad relation and feather-edge stock, and borescope inspection checks cooling-hole breakout. Braze-pocket walls retain 0.30 ±0.03 mm and the finished surface targets Ra 1.6 µm before coating.

Search questions answered

Why use a barrel cutter on the gas path?

Its large effective radius reduces passes and deflection while preserving five-axis contact control.

When is a micro drill changed?

Change it on thrust or breakout trend, not only after breakage; a worn edge creates a hardened entrance.

Why support the feather edge?

The nest converts a bending problem into a light cutting problem and makes alternating passes repeatable.

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