Fairing device for nacelle of an aircraft propulsion power unit

Details Fairing device for nacelle of an aircraft propulsion power unit Fairing device for nacelle of an aircraft propulsion power unit

B - Operations, Transporting

64

D

B64D 29/06 (2006.01)

Patent

CA 2728700

A nacelle, a part of which is the fairing device, surrounds a gas turbine engine (4) and a support pylon (7) on an aircraft fuselage (15). The pylon extends into a substantially horizontal plane of symmetry containing the longitudinal axis of the propulsion power unit (1), and comprises a central compartment (7b) that is open on the top and on the bottom and provided for housing devices. The pylon is attached to the fuselage (5) by a distal edge (7d) extending parallel to the longitudinal axis of the propulsion power unit (1). The fairing device consists of an upper half-cowl (2) and a lower half-cowl (3) substantially symmetrical relative to said plane of symmetry, and lockable therebetween, in a closed position. The upper half-cowl (2) and lower half-cowl (3) are individually pivotably mounted on the distal edge (7d) of the pylon (7) such that, in an open position, access is provided at the same time to the engine (4) and to the central compartment (7b) of the pylon (7).

Une nacelle, dont fait partie le dispositif de capotage entoure un moteur à turbine à gaz (4) et un pylône (7) de maintien à un fuselage (15) d'un aéronef. Le pylône s'étend dans un plan de symétrie sensiblement horizontal contenant l'axe longitudinal de l'unité de puissance propulsive (1), et comporte un compartiment central (7b) ouvert par en dessus et par en dessous, et prévu pour loger des équipements. Le pylône est rattaché au fuselage (15) par un bord distal (7d) s'étendant parallèlement à l'axe longitudinal de l'unité de puissance propulsive (1), Le dispositif de capotage est constitué d'un demi-capot supérieur (2) et d'un demi-capot inférieur (3) sensiblement symétriques par rapport audit plan de symétrie, et verrouillables entre eux, en position fermée. Les demi-capots supérieur (2) et inférieur (3) sont montés pivotant individuellement sur le bord distal (7d) du pylône (7) de manière à, en position ouverte, donner accès à la fois au moteur (4) et au compartiment central (7b) du pylône (7).

Affiliated with

Also associated with

Rating

Fairing device for nacelle of an aircraft propulsion power unit does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Fairing device for nacelle of an aircraft propulsion power unit, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Fairing device for nacelle of an aircraft propulsion power unit will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1511117