| 摘要 |
A workstation for integration in an aircraft, in particular a helicopter, comprises a floor anchoring area (14) for anchoring the workstation (10) on an aircraft floor, a first mounting area (18) which is essentially fixed on the floor anchoring area (14), a second mounting area (36) which is supported on the first mounting area (18) such that it can pivot, a monitor unit (60) which is mounted on the second mounting area (36) such that it can pivot, and a manual control unit (82) which is mounted on the first or the second mounting area (18; 36) such that it can pivot. |
