AIRCRAFT TURBOSHAFT ENGINE COMPRESSOR COMPRISING A DEVICE FOR IMMOBILISING A RETAINING ANNULUS

Disclosed is a compressor of a dual-flow aircraft turboshaft engine extending longitudinally along an axis X, the compressor comprising a low-pressure compressor, a high-pressure compressor and an intermediate casing axially connecting the low-pressure compressor and the high-pressure compressor, th...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Dumas, Lilian Yann, Robin, Noël Joseph Camille, Sevi, Guillaume, Bergon, Blaise, Van De Kerckhove, Thomas Etienne Camille Marie, Delahaye, Thomas Nolwenn Emmanuel, Jablonski, Laurent
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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