Lead sealing tool and lead sealing method for engine parts
Patent Information
- Application Number
- CN202211567644.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2022-12-07
- Publication Date
- 2025-01-07
- Estimated Expiration
- 2042-12-07
AI Technical Summary
Aero engine parts are prone to cracks and breakage of lead seals during the lead sealing process. The prior art is difficult to effectively protect lead seals, resulting in damage caused by the lock wires being wound.
A lead seal tool for engine parts is designed, using a clamping head and a stop pin structure, and the two lock wires are penetrated through the opening of the lead sealing block, and the lock wires are avoided from being wound through the blocking effect of the stop pin, and the bonding limit is limited. The positioning pin and guide pin are used to precisely control the thickness and position of the lead seal block.
It effectively improves the protective performance of the lead seal block, avoids cracks and breakage caused by the entanglement of the lock wire inside the lead seal block, and ensures the integrity of the lead seal block and the efficient quality of the lead seal.
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Figure CN116092373B_ABST
Abstract
Citation Information
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