Seal welding device and process for improving yield of thermally induced holes of powder superalloy
Through the process of hydraulic flattening, laser welding and argon arc welding protective sleeve, the problems of low-thermal induced hole yield and poor welding stability during the welding process of powder high-temperature alloy parts are solved, and efficient sealing effect and material performance are achieved promote.
CN119187886AActive Publication Date: 2024-12-27AVIC BEIJING INST OF AERONAUTICAL MATERIALS
Patent Information
- Application Number
- CN202411473364.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-22
- Publication Date
- 2024-12-27
- Estimated Expiration
- 2044-10-22
Smart Images

Figure CN119187886A_ABST
Abstract
The invention relates to a seal welding device and process for improving the yield of thermally induced holes of a powder high-temperature alloy, belongs to the technical field of powder high-temperature alloys, and solves the problem that the yield of the thermally induced holes of the existing powder high-temperature alloy is not high. The sealing and welding process comprises the steps of hydraulic pipe pressing, laser welding, secondary pipe pressing and welding, protective sleeve welding and the like. According to the process, the process of combining hydraulic flattening, laser welding and protective sleeve welding is adopted, the existing process of combining induction heating and air pressure flattening is replaced, the seal welding quality of the powder discharging pipe is guaranteed, the yield is increased to 100% from 95%, and the thermal induction porosity is 0.3% or below.
Need to check novelty before this filing date? Find Prior Art
Citation Information
Patent Citations
Densification method of porous workpiece
CN102189261A
Laser polishing and laser shock peening manufacturing method for welding or additive repairing area
CN111545918A
Powder high-temperature alloy horizontal extrusion integrated sheath and manufacturing method thereof
CN112077324A
Sheath assembling and welding method
CN112453708A
Titanium alloy brazing material and manufacturing method thereof
CN116000502A
