发明名称 |
Device and method for temperature control in an aircraft cabin |
摘要 |
A device for temperature control in an aircraft cabin includes a first supply control arrangement and a first pressure control arrangement. The first supply control arrangement includes an air duct and a valve arrangement that controls a supply of heated air delivered to a first temperature area of the aircraft cabin such that a first specified temperature for the first temperature zone is achieved. When the valve arrangement fails, the first pressure control arrangement operates to control a pressure of heated air supplied into the first temperature area such that the first specified temperature for the first temperature zone is achieved. |
申请公布号 |
US8336610(B2) |
申请公布日期 |
2012.12.25 |
申请号 |
US20040582701 |
申请日期 |
2004.12.30 |
申请人 |
CENTOFANTE NICO;PETRAC MARKUS;SCHERER THOMAS;BUCHHOLZ UWE;AIRBUS DEUTSCHLAND GMBH |
发明人 |
CENTOFANTE NICO;PETRAC MARKUS;SCHERER THOMAS;BUCHHOLZ UWE |
分类号 |
B64D13/04;B64D11/00;B64D13/00;B64D13/08;G05D15/00;G05D16/00;G05D23/00 |
主分类号 |
B64D13/04 |
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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