CENTRAL SUPPORT FOR AUXILIARY TUBES WITH ELASTIC RETURN

The invention relates to a turbomachine assembly comprising: -a casing comprising: -an internal hub (10), -an external ferrule (20) extending around and at a distance from the internal hub (10), -a hollow arm (30), provided with a longitudinal cavity (40) and connecting the internal hub (10) and the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: RENON, Olivier, SULTANA, Patrick Jean Laurent, PRESTEL, Sebastien Jean Laurent
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:The invention relates to a turbomachine assembly comprising: -a casing comprising: -an internal hub (10), -an external ferrule (20) extending around and at a distance from the internal hub (10), -a hollow arm (30), provided with a longitudinal cavity (40) and connecting the internal hub (10) and the external ferrule (20), -a tube (50) configured to extend in the interior of the longitudinal cavity (40) of the hollow arm (30) of the casing and comprising a central support (60) comprising two elastic blades (61) and configured to exert a pressure on the wall (42) of the longitudinal cavity (40) when the tube (50) is extended in the interior of the longitudinal cavity (40); characterized in that the material(s) of the elastic blades (61) is (are) such that said elastic blades (61) have a stress curve between the minimum and maximum stress curves of table A.