HERMETIC FITTING FOR HOLDING THE VERTICAL STABILISER OF THE TAIL UNIT OF AN AIRCRAFT

摘要

The invention relates to a hermetic fitting (41) for holding the vertical stabiliser of the tail unit of an aircraft in a region of the rear fuselage thereof, the basis of the structure being a skin (5) produced using a composite material such as a single part and fuselage frames (7). Said fitting comprises: a first part (43) comprising two bodies (45, 45') including the lugs (47, 47') for holding the vertical stabiliser of the tail unit and vertical walls (49, 49') for connecting the fitting (43) to the fuselage frames (7), and a central tightness profile (51); and two walls of additional parts (55, 55'; 65, 65') with an angular shape, comprising horizontal walls (57, 57'; 67, 67') for connecting to the skin (5) and vertical walls (59, 59'; 69, 69') for connecting to said bodies (45, 45'). All of the parts of the hermetic fitting (41) are produced using a composite material.