Heating system for an aircraft or spacecraft

Patent metadata

Field	Value
Publication number	US-9380648-B2
Application number	US-201214362250-A
Country	US
Kind code	B2
Filing date	Nov 27, 2012
Priority date	Dec 7, 2011
Publication date	Jun 28, 2016
Grant date	Jun 28, 2016

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.

First claim

The invention claimed is:

1. A heating system for an aircraft or spacecraft, comprising:
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.

2. The heating system according to claim 1 , wherein the sensor controller is designed to communicate with the sensor element by means of a power line data transmission system.

3. The heating system according to claim 1 , wherein the control device comprises a heating controller which is designed to exchange second control signals with the heating element via the connecting cable.

4. The heating system according to claim 1 , wherein the sensor element is a temperature sensor and wherein the first control signals comprise temperature measurement values in the vicinity of the remote components.

5. The heating system according to claim 4 , wherein the remote component comprises an evaluation circuit which is configured to evaluate the temperature measurement values recorded by the temperature sensor.

6. A method for operating a heating system for an aircraft or spacecraft, comprising:
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.

7. The method according to claim 6 , further comprising:
supplying a second remote component, which comprises a heating element, with power by the control device via a second connecting cable; and
exchanging control signals between the control device and a sensor element of the second remote component via the second connecting cable.

8. The method according to claim 6 , wherein the sensor element comprises a temperature sensor and wherein exchanging control signals entails exchanging temperature measurement values.

9. An aircraft or spacecraft comprising a heating system, the heating system comprising:
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.

10. The aircraft or spacecraft according to claim 9 , wherein the at least one remote component is a pipe heating component of the aircraft or spacecraft.

11. The aircraft or spacecraft according to claim 9 , wherein the at least one remote component is an underfloor heating component of the aircraft or spacecraft.

12. The aircraft or spacecraft according to claim 9 , wherein the at least one remote component is a drainage heating component of the aircraft or spacecraft.

13. The aircraft or spacecraft according to claim 9 , wherein the at least one remote component is a waste water pipe heating component of the aircraft or spacecraft.

Assignees

• Airbus Operations Gmbh

Inventors

• Altay Mehmet

Classifications

• B64G1/428

  Power distribution and management · CPC title

• B64D2221/00

  Electric power distribution systems onboard aircraft · CPC title

• H04B2203/5458

  Monitor sensor; Alarm systems · CPC title

• B64C1/18

  Floors · CPC title

• H04B3/548

  the power on the line being DC (arrangements for feeding power H04L12/10; extracting feeding power from signals H04L25/02) · CPC title