DISPOSITIF DE LIAISON DESTINE A RELIER UN PREMIER CORPS A UN SECOND CORPS, NOTAMMENT POUR ENSEMBLE MOTEUR D'AERONEF

The device (2) has first and second elements including connecting ends (21, 31) connected to bodies e.g. engine mounting structure and turbojet engine, respectively. The elements have respective tubular portions (22, 32) extending along a longitudinal axis (X). The tubular portions are integrated by...

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Bibliographische Detailangaben
Hauptverfasser:	VALERY BENOIT, BONNET MATHIEU
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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Beschreibung
Zusammenfassung:	The device (2) has first and second elements including connecting ends (21, 31) connected to bodies e.g. engine mounting structure and turbojet engine, respectively. The elements have respective tubular portions (22, 32) extending along a longitudinal axis (X). The tubular portions are integrated by complementary tubular portions (41-43) extending along the axis, from one of the tubular portions of the corresponding element and around the other tubular portion. Each portion has a surface having identical value, in a cross-section of the longitudinal axis. An independent claim is also included for an assembly comprising bodies and a connecting device.