In view of the current development problems of the introduced heavy-duty gas turbine compressor cylinder,such as poor positioning effect of the positioning structure of the surface flange,large processing deformation,unstable processing accuracy,and difficulty in ensuring assembly accuracy,the optimization of the positioning structure of the surface flange and the improvement of the manufac-turing process were proposed to improve the design quality and ensure the manufacturing accuracy.
关键词
重型燃机/压气机缸/定位结构优化/制造工艺完善
Key words
heavy-duty gas turbine/compressor cylinder/positioning structure optimization/manufacturing process improvement
维普
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