A strut for an aircraft landing gear is provided. The strut includes a casing configured to absorb landing forces applied to the aircraft landing gear. The casing includes a cavity in which an energy accumulator is housed. The energy accumulator can be a removable cartridge which can be inserted in the cavity. An aircraft landing gear comprising such a strut is also provided. An aircraft comprising at least one such landing gear having such a strut is also provided. A method for emergency deployment of such a landing gear, using energy stored in the energy accumulator integrated in the strut of the landing gear to deploy the landing gear is also provided.
JAMBE POUR ATTERRISSEUR D'AERONEF EQUIPE D'UN ACCUMULATEUR, ATTERRISSEUR COMPRENANT UNE TELLE JAMBE ET AERONEF COMPRENANT AU MOINS UN TEL ATTERRISSEUR
STRUT FOR AIRCRAFT LANDING GEAR EQUIPPED WITH AN ACCUMULATOR, LANDING GEAR COMPRISING SUCH A STRUT, AND AIRCRAFT COMPRISING AT LEAST ONE SUCH LANDING GEAR
STREBE FÜR EIN FLUGZEUGFAHRWERK MIT EINEM AKKUMULATOR, FAHRWERK MIT SOLCH EINER STREBE UND FLUGZEUG MIT MINDESTENS EINEM SOLCHEN FAHRWERK
2024-12-18
Patent
Electronic Resource
French
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