| 摘要 |
A flap support structure (6) for an aircraft wing (3) having a trailing edge flap (5), the flap support structure comprising: a flap support beam (10) including an aerodynamic fairing (17); and a drive unit (13) including a universal support structure (18) which rotatably receives a drive shaft (25) connected to a drive arm (14a) for moving the trailing edge flap, wherein the universal support structure also forms part of the flap support beam and supports the aerodynamic fairing. |
