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...
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Main Authors | , , , , , , , , , , , , , , , , , |
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Format | Patent |
Language | Chinese English |
Published |
09.05.2023
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Subjects | |
Online Access | Get full text |
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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 |
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Bibliography: | Application Number: CN202211351471 |