LUGGAGE HOLD OR FREIGHT TO AERODYNAMIC LINES ADAPTED TO A REDUCTION OF TRAINE 'CX' FORMING FAIRING OF THE MAIN LANDING COMPARTMENT UNDER FUSELATION OF AIRCRAFT.

摘要

Baggage or freight hold device for an aircraft with landing gear under the fuselage, the device combines the volume necessary for a fairing by extending the aerodynamic lines of the gear bay (1) with a part of the volume available under the cabin floor, obtained by a reduction in the curvature of the fuselage bottom frames (7), the fairing hold assembly (2) is stiffened longitudinally by a central panel forming a beam (9). Preformed panels (11) each incorporating an access with a shield-shaped door (12) are fixed onto the main frames (3) (4) (5) on the central panel (9) and along a ledge (10) which longitudinally fixes the upper shape of the hold (2), a flap (15) loaded by a spring sets the pressure level in the fairing hold which is temperature-controlled by a flow of cabin air calibrated through an orifice. This device is particularly suitable for releasing baggage hold space in the cabin of aircraft equipped with a landing gear under the fuselage and requiring an aerodynamic fairing. IMAGE