Integral suspended structure of propelling system

The invention relates to the technical field of aircraft structural design, and provides an integral suspended structure of propelling system. One end of the suspended structure is connected to an aircraft wing and the other end of the suspended structure is connected to an aero-engine. The suspende...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LI XIAONAN, ZHOU LIANGDAO, HU YINYIN, WU GUANGHUI, YAN MINGPENG, YU QIFENG, PENG SEN, WENG HAOJIE, ZHANG PENGFEI, MA SHIWEI, LIN GUOZHENG, GUO HAISHA, TANG HONGGANG, HAN KECEN, ZHANG SHIBIAO, ZHANG HONGJIE
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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