Coaxial powder feeding and laser forging compound additive-subtractive manufacturing method and device
A technology of coaxial powder feeding and manufacturing method, applied in the field of adding and subtracting materials manufacturing, can solve the problems of internal quality problems of parts, low dimensional accuracy efficiency, etc., to solve the air holes, ensure the contour and surface accuracy of the parts, and improve the residual stress distribution state. Effect
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Embodiment 1
[0033] Such as figure 1 Shown is an embodiment of the manufacturing method of coaxial powder feeding and laser forging composite addition and subtraction of the present invention, including the following steps:
[0034] S1. Based on the 3D model of the part, slice the part into several layers, generate the laser cladding path, impact forging path, plane and profiling milling path code of each layer, and preliminarily design the laser cladding process parameters of the manufacturing device ;
[0035] S2. Start the continuous laser generator 18, and the cladding robot 14 drives the coaxial powder feeding cladding laser head 13 to perform cladding and forming according to the laser cladding process parameters in step S1;
[0036] S3. According to the laser cladding process parameters in step S2 and the temperature data of the infrared temperature sensor 12, analyze and obtain the laser forging process parameters, and carry out laser forging on the formed area of each layer thr...
Embodiment 2
[0046] Such as figure 2 Shown is the first embodiment of the coaxial powder feeding and laser forging composite addition and subtraction material manufacturing device, including the central control system 2 and the workbench power system 3 connected to the central control system 2, cladding system, and laser forging system , milling system, computer 1, workbench power system 3 is connected with five-axis workbench 5, cladding system, laser forging system, milling system are connected with support frame 20, workpiece 15 is set on five-axis workbench 5; The power system 3 , the cladding system, the laser forging system, and the milling system are provided with an outer casing 19 , and a tool magazine 4 connected with the central control system 2 is also arranged in the outer casing 19 .
[0047] During implementation of this embodiment, the central control system 2 is provided with three control modules for respectively controlling the cladding system, the laser forging system,...
Embodiment 3
[0052] This embodiment is the application of the method of Embodiment 1 in the manufacture of an aircraft engine blisk, including the following steps:
[0053] S1. Determine the three-dimensional model of the overall blisk through the computer 1, slice the parts of the disk body and the blade, respectively plan the laser cladding path, impact forging path, and milling path of each layer, and generate a milling and cladding robot 14 The motion code of the forging robot 10, the milling code of the milling robot 6, and the motion code of the five-axis worktable 5 preliminarily determine the laser cladding process parameters;
[0054] S2. Manufacture of the disk body: According to the planned path of the disk body, the laser beam is generated by the continuous laser generator 18 and transmitted to the coaxial powder feeding and cladding laser head 13 through the optical path, while the powder storage tank 16 and the gas storage tank 17 are sent to the The powder / air pipe transport...
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