Clamping device for aero-engine blade machining
The utility model discloses a clamping device for aero-engine blade machining, which comprises a bottom plate, a mounting seat is mounted at the center of the outer wall of the top of the bottom plate through a bolt, a double-shaft motor is mounted in the mounting seat through a bolt, a screw is mou...
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Main Authors | , , , |
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Format | Patent |
Language | Chinese English |
Published |
18.06.2024
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Subjects | |
Online Access | Get full text |
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Summary: | The utility model discloses a clamping device for aero-engine blade machining, which comprises a bottom plate, a mounting seat is mounted at the center of the outer wall of the top of the bottom plate through a bolt, a double-shaft motor is mounted in the mounting seat through a bolt, a screw is mounted at the output end of the double-shaft motor through a coupler, and a moving block is in threaded connection with the outer wall of the screw. A lifting plate is slidably connected into the mounting seat, a curved bar movably connected with the lifting plate is movably mounted on the outer wall of the top of the moving block through a rotating shaft, and a lifting seat is mounted on the outer wall of the top of the lifting plate through a bolt. By means of the arranged double-shaft motor, when the double-shaft motor is started, the double-shaft motor can drive a screw to rotate, in the rotating process of the screw, the screw can move through threaded connection with a moving block, the moving block drives a li |
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Bibliography: | Application Number: CN202323077572U |