PROPULSION ASSEMBLY FOR AN AIRCRAFT, COMPRISING AN INTERMEDIATE COWL OF THE STATIONARY, REMOVABLE TYPE, MOUNTED ON A HINGE SYSTEM

Abstract: an aircraft propulsion unit including a nacelle comprising a fan compartment, a front cowling forming an air inlet, and an intermediate section having at least one removable fixed intermediate cowling, externally delimiting the fan compartment, and attached to another structure of the propulsion unit by removable through fasteners. the intermediate cowling is connected to another element of the propulsion unit by means of a hinge system which, as a result of removing the removable through fasteners, is designed to allow the intermediate cowling to be moved between a closed position, in which it extends continuously with the front cowling, and an open position, in which the intermediate cowling is shifted upstream or downstream so as to open the fan compartment

Inventor(s): Patrick GONIDEC, Patrick André BOILEAU, Albin LAFONT, Jérémie SARTORI, Caroline GERARD, Frédéric BOUDEHEN

CPC Classification: F02K7/00 (Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof (rocket-engine plants ))

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