An aircraft wing element comprises two temperature sensors that are situated on each side of an electrothermal mat, between a structure portion and a shield of said wing element. A shield temperature can be measured more accurately, and a thermal energy flow that is transferred to the shield can be evaluated.
Aircraft wing element
03.04.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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