| 摘要 |
The invention relates to fittings (41, 71) for fixing the vertical tail stabilizer of an aircraft in an area of its rear fuselage integrally manufactured with a composite material comprising: a) a first piece (43, 73) comprising lugs (45, 45′; 75, 75′) for fixing the vertical tail stabilizer and vertical walls (47, 47′; 77, 77′) for fixing the fitting (41, 71) to the frames (7); b) at least one pair of additional pieces (49, 49′; 79, 79′) comprising horizontal walls (51, 51′; 81, 81′) for fixing the fitting (41, 71) to the skin (5). The fitting (71) for fixing with an inclined load also comprises a second pair of pieces (90, 90′) having an angular shape comprising vertical walls (93, 93′) for the fixing with the lugs (75, 75′). The invention also relates to processes for assembling these fittings (41, 71).
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