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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

Inactive Publication Date: 2016-03-16
AECC AERO SCI & TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since the processing electrodes of the sealing grooves of the large and small edge plates are in the shape of thin sheets and made of red copper, the wear and tear in the process of processing is very fast. On average, a new electrode needs to be replaced every time a guide vane is processed. Due to the processing position of the sealing groove High precision and machining accuracy are required, so the assembly accuracy of the electrode is very high, and it is difficult to ensure that the relative position of the electrode and the electrode base is consistent during each assembly when the electrode is frequently replaced, which will easily cause fluctuations in the position of the electrode, which in turn will lead to the position of the sealing groove degree is difficult to guarantee
Moreover, the separate processing of the sealing grooves on the large and small edge plates also has the problem of low processing efficiency
At the same time, because the electrode is made of red copper and is in a thin sheet shape, there is a problem of insufficient strength. During the processing of the sealing groove, the electrode is easily deformed, which affects the processing accuracy, and the processing pass rate of the sealing groove is extremely low.

Method used

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  • Combined processing-type electrode used for machining sealing grooves of aero-engine guide blades
  • Combined processing-type electrode used for machining sealing grooves of aero-engine guide blades
  • Combined processing-type electrode used for machining sealing grooves of aero-engine guide blades

Examples

Experimental program
Comparison scheme
Effect test

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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Abstract

The invention provides a combined processing-type electrode used for machining sealing grooves of aero-engine guide blades. The combined processing-type electrode comprises an electrode body, an electrode base, a clamping head, a first copper-tungsten alloy block, a second copper-tungsten alloy block, first electrode bodies and second electrode bodies. The first electrode bodies are located at the end of the first copper-tungsten alloy block and integrated with the first copper-tungsten alloy block. The second electrode bodies are located at the end of the second copper-tungsten alloy block and integrated with the second copper-tungsten alloy block. The first copper-tungsten alloy block and the second copper-tungsten alloy block are fixed to the two ends of the bottom surface of the electrode base respectively. The shapes of the first electrode bodies and the shapes of the second electrode bodies are consistent with the shapes of sealing grooves to be machined in large margin plates of the guide blades and the shapes of sealing grooves to be machined in small margin plates of the guide blades respectively, and the positions of the first electrode bodies and the positions of the second electrode bodies are matched with the positions of the sealing grooves to be machined in the large margin plates of the guide blades and the positions of the sealing grooves to be machined in the small margin plates of the guide blades respectively. The clamping head comprises a main shaft connecting part and a base connecting part, wherein the shape of the main shaft connecting part is matched with a main shaft head of an electro-discharge machine tool, and the base connecting part is provided with a threaded hole. The main shaft connecting part penetrates through a clamping head installing through hole formed in the electrode base, and the base connecting part is in threaded connection with the electrode base.

Description

technical field [0001] The invention belongs to the technical field of manufacturing guide vanes of aero-engines, and in particular relates to a combined processing electrode used for machining sealing grooves of guide vanes of aero-engines. Background technique [0002] The guide vane is the part that bears the most high temperature and thermal shock in the aero-engine components, and its working conditions are very harsh. In addition to being subjected to large aerodynamic work and unstable pulsating load, the guide vane is also surrounded by high-temperature gas. The temperature of the working environment is high and the temperature changes greatly, and the heating of the guide vane is seriously uneven. In order to reduce the air leakage loss of the aero-engine and improve the sealing effect, it is necessary to process sealing grooves on the guide vanes. The sealing grooves are respectively distributed on the large and small edge plates of the guide vanes. Due to the dee...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23H7/24B23H7/22
CPCB23H7/24B23H7/22
Inventor 任凤英刘建朱冰玉裴聪周林夏艳罗培真王春笋李惠苏展弘李成刚
Owner AECC AERO SCI & TECH CO LTD
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