Impact-reducing separation structure suitable for ignition actuating device

The invention discloses an impact-reducing separation structure suitable for an ignition actuating device. The impact-reducing separation structure comprises a first adapter block, a second adapter block, a base plate, a taper sleeve, a conductive screw and the ignition actuating device, wherein the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	WANG SHUAI, LI CHEN, HU ZHENXING, CHEN KAI, SU HAN, FENG LINA, CHEN DAISONG, WANG XIAOYU, PAN ZHONGWEN, YU BING, ZHANG ZHIFENG, QU ZHANLONG, TANG KE, HE ZHILIANG, LI YAN, SUN JING, HUANG WEI, WU JINTAO
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR
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Beschreibung
Zusammenfassung:	The invention discloses an impact-reducing separation structure suitable for an ignition actuating device. The impact-reducing separation structure comprises a first adapter block, a second adapter block, a base plate, a taper sleeve, a conductive screw and the ignition actuating device, wherein the base plate is connected with the outer end face of the first adapter block through the conductive screw; the inner end face of the first adapter block is attached to the inner end face of the second adapter block; one end of the taper sleeve is arranged in an internal through hole formed in the first adapter block, and the other end of the taper sleeve is arranged in an internal through hole formed in the second adapter block; and the ignition actuating device is arranged in an internal through hole formed in the base plate, an internal through hole formed in the first adapter block, a taper sleeve and an internal through hole formed in the second adapter block in a penetrating manner. The separation structure has