FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to load slat release mechanism. Proposed mechanism comprises first drive element connected with slat at first swivel point and second drive element connected with slat at second swivel point shifted relative to said first swivel point. First rack is fitted at said first drive element while first gear is fitted on drive shaft. Said first gear serves to transmit power to said first drive element via said rack. Second rack is fitted at said second drive element while second gear is fitted on drive shaft. Second gear features radius other than that of the first gear. Said second gear serves to transmit power to said second drive element via said rack so that second drive element displaced at speed other than that of the first drive element.
EFFECT: simplified mechanism.
11 cl, 10 dwg
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