Patent ID: 11958598
Assignee: AIRBUS OPERATIONS LIMITED
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 8:
9. The wing according to claim 8, wherein the drive system is configured such that during synchronous rotation of the first and second output wheels alternatingly a) one of the projections of the first output wheel engages one of the recesses of the first sync wheel, rotates the first sync wheel by 90°, and then disengages from the said recess of the first sync wheel, and b) one of the projections of the second output wheel engages one of the recesses of the second sync wheel, rotates the second sync wheel by 90°, and then disengages from the said recess of the second sync wheel, when the first and second output wheels rotate synchronously,
while upon asynchronous rotation of the first and second output wheels a) one of the projections of the first output wheel runs against the first sync wheel without properly engaging one of the recesses of the first sync wheel, thereby blocking or obstructing rotation of the first output wheel, and/or b) one of the projections of the second output wheel runs against the second sync wheel without properly engaging one of the recesses of the second sync wheel, thereby blocking or obstructing rotation of the second output wheel.