Workstation for Integration in an Aircraft, in Particular a Helicopter
First Claim
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1. A workstation for integration in an aircraft, in particular a helicopter, comprising:
- 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;
a manual control unit (82) which is mounted on the first or the second mounting area (18, 36) such that it can pivot.
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Accused Products
Abstract
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.
9 Citations
18 Claims
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1. A workstation for integration in an aircraft, in particular a helicopter, comprising:
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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; a manual control unit (82) which is mounted on the first or the second mounting area (18, 36) such that it can pivot. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18)
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Specification