FIELD: transport.
SUBSTANCE: set of invention relates to aircraft surface anti-icing and/or anti-misting system, method of control over said system and aircraft with said system. Temperature transducer is arranged nearby protected surface to generate temperature data. There is a computer to generate control data proceeding from said temperature data and transfer it into aircraft computer network. Electric power supply system is arranged in aircraft central electric system to receive control data via computer network and incorporates switch operated depending upon control data. Heating element is located nearby protected surface and receives power supply via said switch. In control effected by said system, control data is determined received from temperature transducer. Control data is transmitted into aircraft computer network and received by electric power supply system. Depending upon control data, switched in switched to feed power supply to said heating element.
EFFECT: optimised aircraft anti-icing and anti-misting.
17 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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|
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|
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| CYBERPHYSICAL SYSTEM FOR SYNTHESIS OF DIGITAL TWIN OF AIRCRAFT | 2023 |
|
RU2809462C1 |
