The present invention thus proposes an inlet cone for an aircraft turbine engine, comprising a frustoconical body and a tip made from elastically deformable material fixed to an end of smaller diameter of said body, the tip comprising a top configured to be situated on an axis of rotation of the cone and a fastening base for attachment on said end of said body. Said base extends in a connecting plane P. Said connecting plane P is inclined relative to said axis of rotation. Said base has a generally circular or oval shape. According to the invention, said connecting plane P is inclined relative to a transverse plane T perpendicular to said axis of rotation.
CÔNE D'ENTRÉE POUR UNE TURBOMACHINE D'AÉRONEF ET TURBOMACHINE D'AÉRONEF ASSOCIÉE
INLET CONE FOR AN AIRCRAFT TURBOMACHINE AND CORRESPONDING AIRCRAFT TURBOMACHINE
EINTRITTSKEGEL FÜR EINE FLUGZEUGSTRÖMUNGSMASCHINE UND ZUGEHÖRIGE FLUGZEUGSTRÖMUNGSMASCHINE
2023-03-01
Patent
Elektronische Ressource
Französisch
IPC: | F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS |
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