B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 3/50 (2006.01) B64C 13/30 (2006.01)
Patent
CA 2656442
Adjusting device for adjusting a high-lift flap (2; 102) and airfoil wing provided with the same, comprising at lest one flap drive (20) for operating the flap (2; 102), and comprising several drive stations (3, 4, 5) which movably connect the high-lift flap (2; 102) to the airfoil wing (1) for guiding the flap (2; 102) by means of tension/compression elements (7; 107), the flap drive (20) being connected to several drive stations (3, 4, 5) for adjusting the high-lift flap (2; 102). According to the invention, at least one compensation element (10; 110) is provided at least at one drive station (4) for compensation of constraining forces occurring in the drive links comprising the tension/compression elements (7; 107) due to relative movements in wing chord direction between the flap (2; 102) and the wing (1).
Dispositif d'ajustement pour ajuster un volet hypersustentateur (2 ; 102) et aile portante dotée de celui-ci, comprenant au moins un entraînement de volets (20) pour commander le volet (2 ; 102), et plusieurs stations d'entraînement (3, 4, 5) qui relient de manière mobile le volet hypersustentateur (2 ; 102) à l'aile portante (1) pour guider le volet (2 ; 102) au moyen d'éléments de tension/compression (7 ; 107), l'entraînement de volets (20) étant relié à plusieurs stations d'entraînement (3, 4, 5) pour ajuster le volet hypersustentateur (2 ; 102). Selon l'invention, au moins un élément de compensation (10 ; 110) est prévu au moins sur une station d'entraînement (4) pour compenser les forces de liaison apparaissant dans les maillons d'entraînement comprenant les éléments de tension/compression (7 ; 107) en raison des mouvements relatifs dans la direction de la corde d'aile entre le volet (2 ; 102) et l'aile (1).
Airbus Deutschland Gmbh
Airbus Operations Gmbh
Mcfadden Fincham
LandOfFree
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