DRIVE SHAFT COMPRISING A FUSIBLE SECTION AND METHOD FOR PROTECTING SUCH A DRIVE SHAFT AGAINST AN OVERTORQUE

A drive shaft of an aircraft turbine engine includes a first portion and a second portion, and connecting means connecting the first and second portions and being configured to transmit a torque from the second portion to the first portion. The connecting means has at least one bellows with a first...

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Bibliographische Detailangaben

Hauptverfasser:	NEGRI, Arnaud, Nicolas, BECOULET, Julien, Fabien, Patrick, BRAULT, Michel, Gilbert, Roland, CUVILLIER, Romain, Guillaume
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING BRAKES CLUTCHES COUPLINGS FOR TRANSMITTING ROTATION ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MECHANICAL ENGINEERING THERMAL INSULATION IN GENERAL WEAPONS
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