Combined processing-type electrode used for machining sealing grooves of aero-engine guide blades
A technology for aero-engines and guide vanes, applied in electrode manufacturing, electric processing equipment, metal processing equipment, etc., can solve the problems of difficulty in ensuring the position of sealing grooves, fluctuations in electrode positions, and affecting machining accuracy, and achieve machining accuracy and position The effect of high degree of guarantee, reducing the frequency of electrode replacement, and improving the processing pass rate
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Embodiment 1
[0027] In this embodiment, the structural schematic diagram of the combined machining electrode used for machining the sealing groove of the guide vane of the aeroengine is as follows figure 1 as shown, figure 1 The A-direction view is as figure 2 As shown, the combined processing electrode includes an electrode base 1, a chuck 2, a first copper-tungsten alloy block 3, a second copper-tungsten alloy block 4, a first electrode 5 for processing a large edge plate sealing groove and a Process the second electrode 6 of the sealing groove of the small edge plate,
[0028] The first electrode 5 is located at the end of the first copper-tungsten alloy block 3 and is an integral structure with the first copper-tungsten alloy block, and the second electrode 6 is located at the end of the second copper-tungsten alloy block 4 and is integrated with the second copper-tungsten alloy block. The block is an integrated structure, and the first copper-tungsten alloy block and the second cop...
Embodiment 2
[0031] In this embodiment, the structural schematic diagram of the combined machining electrode used for machining the sealing groove of the guide vane of the aeroengine is as follows figure 1 as shown, figure 1 The A-direction view is as figure 2 As shown, the combined processing electrode includes an electrode base 1, a chuck 2, a first copper-tungsten alloy block 3, a second copper-tungsten alloy block 4, a first electrode 5 for processing a large edge plate sealing groove and a Process the second electrode 6 of the sealing groove of the small edge plate,
[0032]The first electrode 5 is located at the end of the first copper-tungsten alloy block 3 and is an integral structure with the first copper-tungsten alloy block, and the second electrode 6 is located at the end of the second copper-tungsten alloy block 4 and is integrated with the second copper-tungsten alloy block. The block is an integrated structure, and the first copper-tungsten alloy block and the second copp...
Embodiment 3
[0035] In this embodiment, the method for using the combined processing electrode described in the present invention is provided, and the combined processing electrode provided in Example 1 or Example 2 is used to process such as image 3 The radial surface 10 of the large edge plate basin and the radial surface 11 of the small edge plate basin of the shown aeroengine power turbine multi-connected guide vane, the four sides on the back radial surface 12 of the large edge plate and the back radial surface 13 of the small edge plate A sealing groove, wherein, the structural schematic diagram of the sealing groove 14 on the radial surface and the back radial surface of the large edge plate basin of the multi-connected guide vane is as follows Figure 4 As shown, the structural schematic diagram of the sealing groove 15 on the radial surface and back radial surface of the small edge plate basin of the multi-connected guide vane is as follows Figure 5 as shown, Figure 6 yes Fi...
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