A propulsion unit includes a nacelle, a turbojet engine, and a thrust reverser having gratings provided with movable thrust reversal gratings arranged around an annular duct for fresh air from the turbojet engine. The propulsion unit further includes actuators arranged around the annular duct and each actuator has a front end attached to the turbojet engine and a rear end which translates movable rear covers and gratings for opening, in the annular duct, radial passages which receive said gratings. The propulsion unit further has lifting points that are arranged around the annular duct for lifting the turbojet engine. At least one of the lifting points is formed on a beam for attaching an front end of an actuator.
ENSEMBLE PROPULSIF COMPORTANT DES POINTS DE LEVAGE DISPOSÉS SUR DES SUPPORTS DE VÉRINS D'INVERSEUR DE POUSSÉE
PROPULSION UNIT HAVING LIFTING POINTS ARRANGED ON BEAMS FOR THRUST REVERSER ACTUATORS
ANTRIEBSEINHEIT MIT AN BALKEN ANGEORDNETEN HUBPUNKTEN FÜR SCHUBUMKEHRSTELLGLIEDER
07.08.2024
Patent
Elektronische Ressource
Französisch
IPC: | F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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