SUSPENSION D'UN TURBOREACTEUR A UN AERONEF

The suspension has a front attachment (10) with a beam transversal with respect to an axis connected to an external ferrule of an intermediate case (3) by two rods of the front attachment. A rear attachment (11) has two rods connected to another external ferrule of an exhaust case (8). A thrust tran...

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Bibliographische Detailangaben
Hauptverfasser:	LEFORT GUILLAUME, CHOUARD PIERRE ALAIN JEAN MARIE, TROHEL MATHIEU JEAN PIERRE, FAUVELET BENOIT MARC MICHEL
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 suspension has a front attachment (10) with a beam transversal with respect to an axis connected to an external ferrule of an intermediate case (3) by two rods of the front attachment. A rear attachment (11) has two rods connected to another external ferrule of an exhaust case (8). A thrust transmission rod (12) connects the hub of the case (3) to the rear attachment. A plane formed by the rods of front attachment and the transmission rod are convergent in a point on the axis of a motor or near the axis.