AGENCEMENT D'AILE D'AERONEF COMPORTANT UN MAT D'ACCROCHAGE DE MOTEUR DEFINISSANT EN ZONE AVANT UN CANAL LATERAL D'ECOULEMENT D'AIR

The arrangement (1) has a wing (2) including proximal and distal ends, and a hooking pylon (4) of an engine (6) e.g. turbojet engine, suspended under the wing. The wing has a front zone (8) e.g. aerodynamic zone, situated toward the front with respect to a wing`s leading edge (10). The zone has a la...

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Bibliographische Detailangaben
Hauptverfasser:	DANTIN STEPHANIE, FOL THIERRY, JIMENEZ PHILIPPE, GERARD LUDOVIC
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 arrangement (1) has a wing (2) including proximal and distal ends, and a hooking pylon (4) of an engine (6) e.g. turbojet engine, suspended under the wing. The wing has a front zone (8) e.g. aerodynamic zone, situated toward the front with respect to a wing`s leading edge (10). The zone has a lateral projection (12) delimiting an air flowing lateral channel (14) by projecting toward the proximal end of the wing, where air flow is accelerated through the channel and is evacuated in a direction privileged under the wing, between a lower surface of the wing and a nacelle of the engine.