Airplane canard liquid cooling heat dissipation device

The utility model discloses an airplane canard liquid cooling heat dissipation device which comprises a right canard, a left canard and an electronic device, the electronic device is provided with a liquid cooling pipeline, and the liquid cooling pipeline comprises an outlet connector and an inlet c...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BAO YONG, ZHANG JIE, WANG ZHENHUA, AN SUYANG, HAN SEUNG-RIM, FAN FENGYING, WANG YI, PENG YUE, LIU YIHUA
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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