The invention relates to a propulsion (100) assembly for an aircraft (50), said propulsion assembly (100) having:- a jet engine (102),- an attachment pylon (104) having a rigid structure (106), and- an extinguishing system (2),According to the invention, the extinguishing system is located in a front position relative to said rigid structure, the extinguishing system being positioned between said rigid structure and said jet engine.With such an arrangement, the length of the piping of the extinguishing agent between the extinguishing bottle and the nozzle can be reduced, which reduces the overall weight of the extinguishing system.
AIRCRAFT PROPULSION ASSEMBLY HAVING A JET ENGINE, A PYLON AND AN EXTINGUISHING SYSTEM
FLUGZEUGANTRIEBSANORDNUNG MIT STRAHLTRIEBWERK, PYLON UND LÖSCHSYSTEM
ENSEMBLE PROPULSIF D'AÉRONEF COMPRENANT UN TURBORÉACTEUR, UN MÂT ET UN SYSTÈME D'EXTINCTION
2024-12-25
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AIRCRAFT PROPULSION ASSEMBLY HAVING A JET ENGINE, A PYLON AND AN EXTINGUISHING SYSTEM
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