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...
Gespeichert in:
Hauptverfasser: | , , |
---|---|
Format: | Patent |
Sprache: | eng ; fre |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Schreiben Sie den ersten Kommentar!