Heating system for an aircraft or spacecraft
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Accused Products
Abstract
A heating system for an aircraft or spacecraft with a control device which includes at least one power line data transmission transceiver and one sensor controller, and at least one remote component which has a sensor element and a heating element, the at least one power line data transmission transceiver being connected to the at least one remote component via a connecting cable, the control device being designed to supply the at least one heating element with power via the connecting cable and the sensor controller being designed to exchange first control signals with the sensor element via the connecting cable.
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Citations
23 Claims
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1-10. -10. (canceled)
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11. A heating system for an aircraft or spacecraft, comprising:
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a control device, which comprises at least one power line data transmission transceiver and a sensor controller; and at least one remote component, which comprises a sensor element and a heating element, wherein the at least one power line data transmission transceiver is connected to the at least one remote component via a connecting cable, wherein the control device is designed to supply the at least one heating element with power via the connecting cable, and wherein the sensor controller is designed to exchange first control signals with the sensor element via the connecting cable. - View Dependent Claims (12, 13, 14, 15)
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16. A method for operating a heating system for an aircraft or spacecraft, comprising:
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supplying a first remote component, which comprises a heating element, with power by a control device via a first connecting cable; and exchanging control signals between the control device and a sensor element of the first remote component via the first connecting cable. - View Dependent Claims (17, 18)
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19. An aircraft or spacecraft comprising a heating system, the heating system comprising:
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a control device, which comprises at least one power line data transmission transceiver and a sensor controller; and at least one remote component, which comprises a sensor element and a heating element, wherein the at least one power line data transmission transceiver is connected to the at least one remote component via a connecting cable, wherein the control device is designed to supply the at least one heating element with power via the connecting cable, and wherein the sensor controller is designed to exchange first control signals with the sensor element via the connecting cable. - View Dependent Claims (20, 21, 22, 23)
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Specification