A system for heating an aircraft surface having a thermally disadvantageous zone includes a carbon nanotube (CNT) sheet heating element having a power inlet configured to receive power from an external power source and provide it to the CNT sheet heating element extending across the thermally disadvantageous zone. The CNT sheet heating element is configured and arranged such that upon application of power from the external power source to the CNT sheet heating element, the CNT sheet heating element generates a first heat output in a first zone and a second heat output in the heat disadvantageous zone, where the second heat output is greater than the first heat output.
一种用于加热具有热不利区的飞机表面的系统包括碳纳米管(CNT)片状加热元件,所述碳纳米管片状加热元件具有电力入口,所述电力入口被配置成从外部电源接收电力并且将其提供给延伸跨过所述热不利区的所述CNT片状加热元件。所述CNT片状加热元件被配置和布置成使得在从所述外部电源向所述CNT片状加热元件施加电力时,所述CNT片状加热元件在第一区中产生第一热输出,并且在所述热不利区中产生第二热输出,其中所述第二热输出大于所述第一热输出。
Aircraft heating system for thermally disadvantageous zones
用于热不利区的飞机加热系统
2023-04-18
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AIRCRAFT HEATING SYSTEM FOR THERMALLY DISADVANTAGED ZONES
Europäisches Patentamt | 2023
|AIRCRAFT HEATING SYSTEM FOR THERMALLY DISADVANTAGED ZONES
Europäisches Patentamt | 2023
|Europäisches Patentamt | 2023
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