FLEXIBLE-USE DISPLAY AND CONTROL ELEMENT PANEL FOR CONTROLLING CABIN FUNCTIONS
First Claim
Patent Images
1. A display- and control element panel for controlling cabin functions in an aircraft, comprising:
- a bi-stable display element having at least one subregion; and
a control element;
whereinthe bi-stable display element and the control element arranged so as to be essentially congruent;
whereinthe bi-stable display element is adapted to reproduce information at least in one sub-region;
whereinan event is triggerable by activating the control element, wherein the display- and control element panel is decouplable from at least one element from the group consisting of a display-control element, image-rendering element and energy supply element, associated with the display- and control element panel; and
wherein the display- and control element panel is operable in the operating state in the aircraft without the at least one element.
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Abstract
A display- and control element panel for controlling cabin functions in an aircraft, comprising a bi-stable display element and a control elements wherein the bi-stable display element and the control element are arranged so as to be essentially congruent, wherein the bi-stable display element is adapted to reproduce information at least in one sub-region, and wherein an event is triggerable by activating the control element.
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Citations
16 Claims
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1. A display- and control element panel for controlling cabin functions in an aircraft, comprising:
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a bi-stable display element having at least one subregion; and a control element;
whereinthe bi-stable display element and the control element arranged so as to be essentially congruent;
whereinthe bi-stable display element is adapted to reproduce information at least in one sub-region;
whereinan event is triggerable by activating the control element, wherein the display- and control element panel is decouplable from at least one element from the group consisting of a display-control element, image-rendering element and energy supply element, associated with the display- and control element panel; and wherein the display- and control element panel is operable in the operating state in the aircraft without the at least one element. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16)
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Specification