| 摘要 |
The invention provides a deployment mechanism 60 for deploying an auxiliary wing surface device 30 from an aircraft wing body 20, the deployment mechanism providing a first connector portion 75, 576 for connecting the deployment mechanism to the aircraft wing body, a second connector portion 65 for connecting the deployment mechanism to the auxiliary wing surface device, and a telescopic rod 61 linking the first and second connector portions, the telescopic rod comprising an inner rod 64 extendable from inside of an outer rod 63 to increase the length of the telescopic rod, such that the distance between the first and second connector portions can be increased. The invention also provides an aircraft wing 10, 510, an aircraft and a method of operating an aircraft. |
