Electric spark processing method for sealing grooves of aero engine guide vane

A technology for aero-engines and guide vanes, applied in electric processing equipment, metal processing equipment, circuits, etc., can solve the problems of difficulty in ensuring the position of sealing grooves, fluctuations in electrode positions, and affecting processing accuracy, so as to ensure processing accuracy and position The effect of 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 electrode is made of red copper, it wears out quickly during the processing process. On average, a new electrode needs to be replaced every time a guide vane is processed. Due to the high requirements for the processing position and processing accuracy of the sealing groove, the assembly accuracy of the electrode is required. Very high, and frequent electrode replacement is difficult to ensure that the relative position of the electrode and the electrode base is consistent during each assembly, which will easily cause fluctuations in the elec

Method used

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  • Electric spark processing method for sealing grooves of aero engine guide vane
  • Electric spark processing method for sealing grooves of aero engine guide vane
  • Electric spark processing method for sealing grooves of aero engine guide vane

Examples

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Embodiment 1

[0033] In this embodiment, adopt the method described in the present invention to process such as figure 1 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 2 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 image 3 as shown, Figure 4 yes figure 2 The K1-K1 view and image 3 The view of K2-K2, the multi-connected guide vanes are made of superalloy K438, the processing re...

Embodiment 2

[0040] In this embodiment, adopt the method described in the present invention to process such as figure 1 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 2 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 image 3 as shown, Figure 4 yes figure 2 The K1-K1 view and image 3 The view of K2-K2, the multi-connected guide vanes are made of superalloy K438, the processing re...

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Abstract

This invention provides an electric spark processing method for sealing grooves of an aero engine guide vane. The method comprises the following steps: (1) two copper-tungsten alloy blocks are fixed on an electrode pedestal and are processed into two electrodes by adopting a milling mode, wherein the two electrodes have the shapes same as and the positions matching with those of the sealing grooves, formed in large and small margin plates of the guide vane, to be processed respectively; and (2) the two electrodes are placed aligning to the parts, to be processed, of big and small margin plates of the guide vane respectively, an electric spark processing machine is started to ensure that the two electrodes carries out electric spark processing on the parts to be processed in the depth direction of the sealing grooves; the two electrodes are aligned to a next part to be processed after processing of the sealing groove of the processed surface is finished, and processing continues according to the process conditions until all the sealing grooves, in the same type, formed in the guide vane are processed; and after the electrodes wears, the two copper-tungsten alloy blocks which are fixed on the electrode pedestal are reprocessed into electrodes by using the milling mode, and then the sealing grooves are continuously processed.

Description

technical field [0001] The invention belongs to the technical field of manufacturing guide blades of aero-engines, in particular to an electric spark machining method for sealing grooves of guide blades 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. Because superalloys have excellent high-temperature strength and hardness, they are often used as the first choice for making guide vanes. [0003] In order to reduce air leakage loss of aero-engines and improve the sealing effect, it is necessary to process sealing grooves on the guide vanes....

Claims

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Application Information

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IPC IPC(8): B23H9/00B23H1/04B23H1/06B23H1/02
CPCB23H9/006B23H1/02B23H1/04B23H1/06
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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