An arrangement is provided that includes a thrust reverser flap link rod on an internal fixed structure of a turbojet engine nacelle. The link rod is connected to the internal fixed structure by an elastic means that is a spring.
AGENCEMENT DE BIELLES DE VOLETS D'INVERSION DE POUSSÉE SUR LA STRUCTURE INTERNE FIXE D'UNE NACELLE DE TURBORÉACTEUR
ANORDNUNG EINER PLEUELSTANGE FÜR SCHUBUMKEHRER AUF DIE INNERE STRUKTUR EINER TRIEBWERKSGONDEL
THRUST REVERSER DOOR ASSEMBLY ON THE INNER PART OF AN ENGINE NACELLE
2016-04-27
Patent
Electronic Resource
French
TURBORÉACTEUR D'AÉRONEF COMPORTANT DEUX MODULES D'INVERSION DE POUSSÉE
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