High-pressure compressor first-stage rectifier inner ring machining tool
CN224373425UActive Publication Date: 2026-06-19CHENGDU HAOYU AVIATION EQUIP MFG CO LTD
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- CHENGDU HAOYU AVIATION EQUIP MFG CO LTD
- Filing Date
- 2025-06-12
- Publication Date
- 2026-06-19
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Figure CN224373425U_ABST
Abstract
The utility model discloses: high pressure compressor first stage rectifier inner ring processing frock, including the chassis, be equipped with the placing groove on the chassis, be equipped with the fixed assembly on the chassis, be equipped with the adjusting assembly on the chassis, be equipped with the limiting assembly on the adjusting assembly, the utility model discloses as high pressure compressor first stage rectifier inner ring processing frock, through fixed assembly, this clamping scheme realizes the high -efficient accurate fixation of high pressure compressor first stage rectifier inner ring through mechanical linkage mechanism, and its core advantage lies in that gear -threaded rod transmission system is used to convert rotary motion into linear clamping force, and the synchronous movement of the abutting block along the guide rod is driven through the double -end threaded rod symmetric distribution, ensures the even force and center positioning of rectifier inner ring inner side wall surface. The transmission design of rotating shaft and gear set makes the operation process more labor-saving and controllable, and the cooperation mechanism of rotating plate and limiting shaft realizes the quick locking and stable keeping of processing position.
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