Airfoiled engine pylon for aircraft wing

Airfoiled engine pylon for aircraft wing

According to the invention, the suspension pylon (3) comprises a fairing for reducing the local loss in lift (8) and its maximum-width section (7) is located at the front of the concave and set-back rear part (4R) of the pressure face (4) of the wing structure (1). The fairing for reducing the local...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: CAMBON, JEAN-LOUIS
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:According to the invention, the suspension pylon (3) comprises a fairing for reducing the local loss in lift (8) and its maximum-width section (7) is located at the front of the concave and set-back rear part (4R) of the pressure face (4) of the wing structure (1). The fairing for reducing the local loss in lift (8):is housed, at least over most of its height, in the concavity of the rear part (4R) of the pressure face (4) of the wing structure (1), and widens laterally toward the rear; andcomprises a projecting rear part (12) that tapers toward the rear and ends in an aerodynamic trailing edge (16) the length of which is very long by comparison with the maximum width of the fairing.