Acceleration heavy landing indicator

The invention provides an acceleration heavy landing indicator, wherein a box body is composed of a front cover plate, a rear cover plate, a left side cover plate, a right side cover plate, an upper cover plate and a lower cover plate, an induction mechanism, a locking mechanism, a reset mechanism a...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CHEN LIGEN, DENG WENWEN, XU HUANYU, GUO WEI, LI CANSHAN, PENG RUI, WANG ZHIZHU, DUAN XINXING, WANG BIN, ZHANG DANDAN
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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