Monitoring of inner regions of an aircraft
First Claim
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1. A monitoring system in an aircraft for monitoring at least one first inner region from a second inner region, particularly for detecting or observing fire or smoke, wherein the monitoring system comprises:
- a first sensor device; and
a user interface;
wherein the first sensor device is adapted for measuring first physical data and is disposed in the first inner region;
wherein the user interface is disposed in the second inner region; and
wherein the user interface has an output unit for outputting first information to a user on the basis of the first physical data and a control unit for controlling at least one of the output unit and the first sensor device.
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Abstract
The present invention includes a monitoring system in an aircraft for monitoring inner regions, such as cargo chambers, comprising a user interface by means of which the crew on board in a simple manner may obtain detailed information concerning the present or past state of the inner region. In this respect, the access to these information may be controlled remotely so that a fast and precise analysis of the dangerous situation may be carried out.
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Citations
17 Claims
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1. A monitoring system in an aircraft for monitoring at least one first inner region from a second inner region, particularly for detecting or observing fire or smoke, wherein the monitoring system comprises:
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a first sensor device; and
a user interface;
wherein the first sensor device is adapted for measuring first physical data and is disposed in the first inner region;
wherein the user interface is disposed in the second inner region; and
wherein the user interface has an output unit for outputting first information to a user on the basis of the first physical data and a control unit for controlling at least one of the output unit and the first sensor device. - View Dependent Claims (2, 3, 4, 5, 6, 7, 17)
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8. A user interface for a monitoring system in an aircraft, the monitoring system being adapted for monitoring at least one first inner region from out of a second inner region, particularly for detecting or observing fire or smoke, wherein the user interface comprises:
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an output unit; and
a control unit;
wherein the output unit is adapted for outputting information to a user on the basis of first physical data; and
wherein the control unit is adapted for controlling the output unit or a first sensor device for measuring the first physical data. - View Dependent Claims (9, 10, 11, 12)
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13. A method for monitoring at least one first inner region of an aircraft from out of a second inner region of an aircraft, particularly for detecting or observing fire or smoke, wherein the first inner region and the second inner region are situated inside an aircraft, wherein the method comprises the following steps:
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outputting first information to a user on the basis of first physical data by means of an output unit; and
controlling the output unit or a first sensor device for measuring the first physical data by means of a control unit, wherein the first sensor device is disposed in the first inner region, and wherein the output unit and the control unit are disposed in the second inner region. - View Dependent Claims (14, 15, 16)
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Specification