A soldered structure of a rocket head of a damascene alloy and a method of manufacturing the same

By using an inlaid alloy rocket head manufacturing method, and employing induction welding technology to connect wear-resistant and corrosion-resistant alloy blocks to the rocket head cone, the problems of rocket head wear and corrosion were solved, achieving wear-resistant and corrosion-resistant effects while reducing costs.

CN115740713BActive Publication Date: 2026-07-10KUNSHAN SERGEANT EQUIP IND

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
KUNSHAN SERGEANT EQUIP IND
Filing Date
2022-12-02
Publication Date
2026-07-10

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Abstract

The application discloses an inlaying alloy rocket head, a welding structure and a manufacturing method thereof. The manufacturing method of the inlaying alloy rocket head comprises the following steps: inverting the rocket head, and automatically loading wear-resistant and corrosion-resistant alloy blocks at symmetrical positions of a cone part of the rocket head; lifting an inductive fusion welding coil to a position where the wear-resistant and corrosion-resistant alloy blocks are contained in the rocket head; loading an anti-sticking porcelain net close to the position of the wear-resistant and corrosion-resistant alloy blocks, so as to prevent the welding coil from being stuck to the wear-resistant and corrosion-resistant alloy blocks; and inductively heating the welding coil, and then locally fusing and connecting the alloy blocks and the rocket head to be welded together. Through the above method, the application has the advantages of simple structure, wear-resistant material and a rocket head body.
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