The invention relates to a turbomachine (1) extending along an axis (X), comprising a high-pressure body with a high-pressure compressor (4) coupled in rotation to a high-pressure turbine (6), and a low-pressure body including a low-pressure compressor (3) coupled in rotation to a low-pressure turbine (7), an upstream casing (14) located upstream of the high-pressure compressor (4), and means of suspension (12, 13) for the turbomachine (1), intended for attaching the turbomachine (1) to an aircraft pylon (11).
TURBOMACHINE COMPORTANT DES MOYENS DE SUSPENSION
TURBOMACHINE COMPRISING SUSPENSION MEANS
TURBOSTRAHLTRIEBWERK MIT MITTEL ZUR AUFHÄNGUNG DES TRIEBWERKS
30.11.2022
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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