COMPLIANCES IN A TURBOMACHINE WITH A SPEED REDUCER

COMPLIANCES IN A TURBOMACHINE WITH A SPEED REDUCER

Disclosed is an assembly for a turbomachine, comprising: *-a first connection element (9) having a first radial compliance (SRI); *-a second connection element (10) having a second radial compliance (SR2); *-a third connection element (11) having a third radial compliance (SR3); and *-a fourth conne...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: TAN-KIM, Alexandre Jean-Marie, GIVERT, Maxime Paul Numa, BECOULET, Julien Fabien Patrick
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Beschreibung
Zusammenfassung:Disclosed is an assembly for a turbomachine, comprising: *-a first connection element (9) having a first radial compliance (SRI); *-a second connection element (10) having a second radial compliance (SR2); *-a third connection element (11) having a third radial compliance (SR3); and *-a fourth connection element (12) having a fourth radial compliance (SR4), wherein a ratio of the first radial compliance (SRI) to the third radial compliance (SR3) is strictly lower than 10%, and/or a ratio of the first radial compliance (SRI) to the second radial compliance (SR2) is strictly lower than 4%, and/or a ratio of the first radial compliance (SRI) to the fourth radial compliance (SR4) is strictly lower than 50%.