Stable and reliable military aviation part clamp
The stable and reliable military aviation part clamp comprises a main body frame, a two-way threaded rod and a clamping block, the two-way threaded rod is rotationally connected to the interior of the main body frame, and the outer side wall of the two-way threaded rod is in threaded connection with...
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Main Authors | , , |
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Format | Patent |
Language | Chinese English |
Published |
08.07.2022
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Subjects | |
Online Access | Get full text |
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Summary: | The stable and reliable military aviation part clamp comprises a main body frame, a two-way threaded rod and a clamping block, the two-way threaded rod is rotationally connected to the interior of the main body frame, and the outer side wall of the two-way threaded rod is in threaded connection with an auxiliary clamping structure; one side of the two-way threaded rod penetrates to the outer side of the main body frame and is fixedly connected with the reinforcing structure, the other side of the two-way threaded rod penetrates to the outer side of the main body frame and is fixedly connected with one side of the adjusting handle, and an anti-skid structure is installed on the inner side of the clamping block. Due to the fact that the anti-skidding structure is arranged, the anti-skidding protruding teeth are prone to abrasion after the clamp is used for a long time, the clamping effect of the clamp is greatly reduced, and due to the fact that the clamping blocks are of a clamping structure, the anti-skidding |
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Bibliography: | Application Number: CN202220774102U |