Fittings for attaching the vertical tail stabilizer of an...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/26 (2006.01)

Patent

CA 2759753

The invention relates to metal fittings (41, 71) for engaging the vertical tailplane of an aircraft in an area of the rear fuselage, which are made fully from a composite material and comprise: a) a first part (43, 73) including lugs (45, 45'; 75, 75') for engaging the vertical tailplane and vertical walls (47, 47'; 77, 77') joining the metal fittings (41, 71) to the ring frames (7); and b) at least one pair of additional parts (49, 49'; 79, 79') including horizontal walls (51, 51'; 81, 81') joining the metal fittings (41, 71) to the skin (5). The metal fitting (71) for engagement with an inclined load also includes a second pair of angle parts (90, 90') including vertical walls (93, 93') joining to the lugs (75, 75'). The invention also relates to methods for mounting said metal fittings (41, 71).

La présente invention concerne des ferrures (41, 71) pour la prise du stabilisateur vertical de la queue d'un aéronef dans une zone transversale de son fuselage intégralement fabriqués avec un matériau composite, lesquelles ferrures comprennent: a) une première pièce (43, 73) qui comprend les pattes (45, 45'; 75, 75') de prise du stabilisateur vertical de la queue et les parois verticales (47, 47'; 77, 77') de raccordement de la ferrure (41, 71) aux cadres (7); b) au moins une paire de pièces supplémentaires (49, 49'; 79, 79') qui comprennent des parois horizontales (51, 51'; 81, 81') de raccordement de la ferrure (41, 71) au revêtement (5). La ferrure (71) permettant une prise avec une charge inclinée comprend également une seconde paire de pièces (90, 90') ayant une forme angulaire, lesquelles comprennent des parois verticales (93, 93') de raccordement aux pattes (75, 75'). La présente invention concerne également des procédés de montage desdites ferrures (41, 71).

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