发明名称 |
ELECTRIC DE-ICING DEVICE FOR TURBOJET ENGINE NACELLE |
摘要 |
The present disclosure provides an electric de-icing/anti-icing device for a turbojet engine or turbo-prop nacelle element to be protected from icing. The device includes: a heating assembly including first and second heating stages positioned in the nacelle element; an electricity supply circuit delivering a primary voltage to the first heating stage of the heating assembly. In particular, the electricity supply circuit includes an electricity source, and a de-icing/anti-icing circuit which is connected to the heating assembly and supplied voltage by the electricity source. Furthermore, the de-icing/anti-icing device includes components to supply a complementary voltage to the second heating stage of the heating assembly. |
申请公布号 |
EP2941382(A1) |
申请公布日期 |
2015.11.11 |
申请号 |
EP20140701814 |
申请日期 |
2014.01.07 |
申请人 |
AIRCELLE |
发明人 |
PEREIRA, DAVID;MAALIOUNE, HAKIM;COAT-LENZOTTI, CAROLINE |
分类号 |
B64D15/12;B64D33/02 |
主分类号 |
B64D15/12 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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