LABYRINTH SEALING DEVICE FOR AN AIRCRAFT TURBOMACHINE

The invention relates to a labyrinth-type sealing device for an aircraft turbomachine, this device having: - a rotor comprising at least one external annular lip (12a, 12b), and - a stator comprising an annular coating (16) made of abradable material with extends around the lip (12a, 12b) and which...

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Bibliographische Detailangaben
Hauptverfasser: BRUNET, Antoine Robert Alain, BAUMAS, Olivier Jean-Daniel, HANSOM, Michael Piers
Format: Patent
Sprache:eng ; fre
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