ENSEMBLE PROPULSIF LATERAL POUR AERONEF COMPRENANT UN ARCEAU DE SUPPORT D'UN TURBOMOTEUR

The unit has an arch (64) including a proximal end (66a) and a distal end (66b) extending on sides of a longitudinal plane (V) with a longitudinal axis (17) and extending vertically when the unit is fit on an aircraft on ground. A half line (D1) starting from the axis and passing through the distal...

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Bibliographische Detailangaben
Hauptverfasser:	TERRAL ROMAIN, BROCHARD WOLFGANG
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 unit has an arch (64) including a proximal end (66a) and a distal end (66b) extending on sides of a longitudinal plane (V) with a longitudinal axis (17) and extending vertically when the unit is fit on an aircraft on ground. A half line (D1) starting from the axis and passing through the distal end defines an angular sector of angle (theta 1) ranging between 45 degree and 120 degree, along with another half line (D2) that starts from the axis and is contained in the plane, and intercepts the arch when the arch is seen in a sectional view on a transverse plane orthogonal to the axis.