An aircraft propulsion unit comprising a motor, a system for supplying fuel to the motor, a fairing inside which the motor and at least part of the fuel supplying system are positioned, and at least one pressure relief device configured to establish communication between the inner and outer zones of the fairing when the pressure in the inner zone is greater than or equal to a given threshold or when a leak is detected. Also an aircraft comprising at least one such propulsion unit.
ENSEMBLE DE PROPULSION D AÉRONEF COMPRENANT AU MOINS UN DISPOSITIF DE SURPRESSION ET AÉRONEF COMPORTANT AU MOINS UN TEL ENSEMBLE DE PROPULSION
AIRCRAFT PROPULSION ASSEMBLY COMPRISING AT LEAST ONE BOOSTER DEVICE AND AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION ASSEMBLY
FLUGZEUGANTRIEBSANORDNUNG MIT MINDESTENS EINER ÜBERDRUCKVORRICHTUNG UND FLUGZEUG MIT MINDESTENS EINER SOLCHEN ANTRIEBSEINHEIT
2025-04-16
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2024
|European Patent Office | 2024
|ENSEMBLE DE PROPULSION D'UN AERONEF COMPORTANT AU MOINS DEUX SOUFFLANTES DEPORTEES
European Patent Office | 2017
|