Aero engine flame tube

Aero engine flame tube

航空发动机火焰筒

Description

Multi-structure composite integrated molding enables one-shot printing of dense film cooling holes, ensuring high consistency and uniformity. Additive optimization iterations shorten manufacturing cycles, reduce development costs, and effectively improve efficiency. The minimum film cooling hole diameter is 0.5mm, with precision controlled within ±0.1mm, ensuring high consistency and uniformity. Wall thickness is <2mm, and overall dimensional accuracy is ≤±0.3mm.

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