Integrated controller applied to aircraft and aircraft

The embodiment of the invention provides an integrated controller applied to an aircraft and the aircraft, and the integrated controller comprises: a shell, wherein an air inlet is formed in the firstend face of the shell, an air outlet is formed in the second end face opposite to the first end face...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CHANG XINYUE, YANG CHUNLEI, NIAN YONGSHANG, WEI MIN, JIANG KAI, LI XUESI, WANG JINING, FAN JIAORONG, CHEN KUN, SHI RUOCHONG, CONG ENBO, CHEN JUNJIE, WAN GUIBIN, WANG RUOFAN, SU ZHONGWEI, REN XINYU, WANG HAIYANG, SUN RUNYU
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS PRINTED CIRCUITS
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