LEADING EDGE SHIELD

The invention relates to the field of turbomachine blades, and more specifically to a leading edge shield (32) for a turbomachine blade (16), which comprises a lower canopy fin (34) and an upper canopy fin (36), each extending in the height and length direction and connected together along their hei...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: RUF, THIBAULT, DIOGO, GERALD, BASSOT, ALAIN JACQUES MICHEL, GUIVARC'H, JEREMY, ROMERO, JEAN-LOUIS
Format: Patent
Sprache:eng ; fre
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