ADAPTATEUR DESTINE A ETRE INTERPOSE ENTRE UNE STRUCTURE RIGIDE DE MAT D'ACCROCHAGE DE TURBOMOTEUR D'AERONEF ET UN ELEMENT DE VOILURE

The adapter (20) has a first binding interface cooperating with a second binding interface that is secured to a rigid structure (10) of a connecting strut (4) of a turboshaft engine i.e. jet engine (2), where the turboshaft engine is arranged in front of a fan casing (12). Configuration of a third b...

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Bibliographische Detailangaben

Hauptverfasser:	KIERBEL DANIEL, HARAMBURU ERIC, SIMONDIN FLORENT
Format:	Patent
Sprache:	fre
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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