| 摘要 |
The method involves installing the hinge shafts (12,14,16) in the ball joints after blockage of an adjustment unit. The adjustment unit is used to actuate the ball joints so that their centers are brought into their theoretical positions. <??>Independent claims are also included for the following: <??>(a) an aircraft; <??>(b) a device for installing the hinge shaft; and <??>(c) an adjustable ball joint. |
