Method for composite machining of blisk flow passage
An integral blisk and composite machining technology, applied in the field of aero-engines, can solve the problems of narrow tool space in the flow channel area, unsuitable control of the machining process, serious tool wear, etc. The effect of increased durability
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[0063] Such as image 3 with Figure 4 As shown, a compressor blisk is processed, the blisk is composed of a disc and blades, the material is titanium alloy, the blade length = 60mm, the blade width = 50mm, the minimum blade distance = 10mm, and the minimum machining allowance is 1mm.
[0064] According to a method for compound processing of the overall blisk flow channel of the present invention, the specific processing steps are as follows:
[0065] Step 1: Division of processing areas:
[0066] 1. Tool diameter D=10×2=20mm.
[0067] 2. Airfoil safety distance=1+0.2=1.2mm.
[0068] 3. Airfoil safety clearance = 1mm.
[0069] 4. Determine the triangular area: such as figure 1 As shown, using the CAD model, on the vertical projection plane,
[0070] (1) Determine the edge projection contour line of the leaf back of the adjacent blade and the leaf pot;
[0071] (2) Considering the machining allowance of the rough opening channel, the most edge contour line area is offset...
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