Heat storage type skin heat exchange system

The invention belongs to the technical field of aircraft heat management, and particularly relates to a heat storage type skin heat exchange system. A temperature control object and a power unit are mounted on a fluid pipeline; the inlet end of the skin heat exchanger is connected with the outlet en...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	FU YUNHAN, LIANG XINGZHUANG, LI ZHENGHONG, LIANG HONGBO
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS COSMONAUTICS ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY HELICOPTERS MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS PERFORMING OPERATIONS PRINTED CIRCUITS TRANSPORTING
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Beschreibung
Zusammenfassung:	The invention belongs to the technical field of aircraft heat management, and particularly relates to a heat storage type skin heat exchange system. A temperature control object and a power unit are mounted on a fluid pipeline; the inlet end of the skin heat exchanger is connected with the outlet end of the fluid pipeline, and the outlet end of the skin heat exchanger is connected with the inlet end of the fluid pipeline; the heat storage unit is connected with the skin heat exchanger; the skin is connected with the skin heat exchanger and/or the heat storage unit; the temperature detection unit is mounted at an inlet of a temperature control object; the control unit is connected with the temperature control object, the power unit and the temperature detection unit and used for controlling starting and stopping of the power unit according to the operation signal of the temperature control object and controlling the rotating speed of the power unit according to the temperature signal of the temperature detecti