Aero-engine film hole laser high-efficiency combined machining method

An aero-engine and composite processing technology, applied in laser welding equipment, metal processing equipment, manufacturing tools, etc., can solve the problems of low ultra-fast laser power, impact on hole-making efficiency, hole wall burrs, etc., to achieve no spatter, improve Process quality, effect of low heat affected zone

Inactive Publication Date: 2018-05-25
AECC AVIATION POWER CO LTD
View PDF3 Cites 7 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, the air film holes of aero-engine parts are mostly processed by EDM, laser, electro-hydraulic beam and other methods. The hole making methods of EDM and laser will cause burrs, remelted layers, heat-affected zones, microcracks, etc. on the hole wall. Defects; Although the hole-making method of electro-hydraulic beam can avoid the above defects, the efficiency is low; with the development of laser technology, ultra-fast laser hole-making technology is more and more used in hole-making, and the above defects can also be avoided. However, the power of ultrafast lasers is generally small, and the efficiency of hole making is also greatly affected.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Aero-engine film hole laser high-efficiency combined machining method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0021] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. The embodiments described herein are only part of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0022] refer to figure 1 As shown, the laser high-efficiency composite processing method for air film holes of aero-engines of the present invention is specifically supplemented as follows:

[0023] 1. Move the laser head 1 to the processing position of the air film hole of the workpiece 2;

[0024] 2. Switch the laser head to long-pulse laser, adopt the method of helical hole making, the initial aperture is 0, the end aperture is 0.2-0.3mm smaller than th...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention discloses an aero-engine film hole laser high-efficiency combined machining method. A long-pulse laser and ultrafast laser combined hole forming method is adopted. According to the method, firstly, a preformed hole is formed through nanosecond laser; secondly, the preformed hole is processed into the hole meeting the requirement through the ultrafast laser; the machining efficiency and machining quality are both considered, and the film hole machining efficiency is improved. As the preformed hole of a film hole is machined through long-pulse laser (rough machining), the next stepof the machining amount of ultrafast laser (finish machining) is greatly reduced. The machining efficiency is improved. The requirements for the machining efficiency during engineering machining aremet. Through the combined hole forming method, the film hole can be free of a remelting layer, burrs and splashes, and high-quality and high-efficiency machining of a low-heat influence area can be achieved.

Description

technical field [0001] The invention belongs to the technical field of laser hole making, and relates to a high-efficiency laser composite processing technology for an air film hole of an aero-engine part, in particular to a high-efficiency laser composite processing method for an air-film hole of an aero-engine. Background technique [0002] At present, most of the gas film holes of aero-engine parts are processed by EDM, laser, electro-hydraulic beam and other methods. The hole making methods of EDM and laser will cause burrs, remelted layers, heat-affected zones, microcracks, etc. on the hole wall. Defects; Although the hole-making method of electro-hydraulic beam can avoid the above defects, the efficiency is low; with the development of laser technology, ultra-fast laser hole-making technology is more and more used in hole-making, and the above defects can also be avoided. However, the power of ultrafast lasers is generally small, and the efficiency of hole making is al...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): B23K26/36
CPCB23K26/36
Inventor 梁养民谢国印王琦杨小君吴晓锋耿军儒王琼波侯春梅
Owner AECC AVIATION POWER CO LTD
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products