Rocket interface integrated automatic closing covering cap with built-in torsional spring

The invention provides a rocket interface integrated automatic closing covering cap with a built-in torsional spring. The rocket interface integrated automatic closing covering cap comprises a covering frame, a cover plate, a first rotating shaft, a second rotating shaft, the torsional spring and a...

Full description

Saved in:
Bibliographic Details
Main Authors LIU LIMING, XUE XILONG, LUO HONGZHI, OU YANGXING, SUN HAIXIA, XIA HUI, CHEN YOUWEI, LI ZHIWEI, BAO YUBING, YAO RUIJUAN, REN DONGHONG, YIN JIANHUA, CAO JINGLE, LIU CHANGZHI, ZHANG DONG, ZHANG DENGYU, WANG KANGKANG, LI TIANJIAO
Format Patent
LanguageChinese
English
Published 09.05.2023
Subjects
Online AccessGet full text

Cover

Loading…
More Information
Summary:The invention provides a rocket interface integrated automatic closing covering cap with a built-in torsional spring. The rocket interface integrated automatic closing covering cap comprises a covering frame, a cover plate, a first rotating shaft, a second rotating shaft, the torsional spring and a locking assembly. A lock catch and a torsional spring cavity are arranged on the opening frame; a first rotating shaft cavity, a second rotating shaft cavity and a lock cavity are formed in the cover plate; the locking assembly is installed in the lock cavity. The torsion spring is installed in the torsion spring cavity, the first rotating shaft penetrates through the first rotating shaft cavity and penetrates into the torsion spring cavity to be connected with one end of the torsion spring, and the second rotating shaft penetrates through the second rotating shaft cavity and penetrates into the torsion spring cavity to be connected with the other end of the torsion spring. The first rotating shaft is fixedly conne
Bibliography:Application Number: CN202211351471