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Frontiers of Mechanical Engineering

ISSN 2095-0233

ISSN 2095-0241(Online)

CN 11-5984/TH

邮发代号 80-975

2019 Impact Factor: 2.448

Frontiers of Mechanical Engineering  2020, Vol. 15 Issue (2): 240-255   https://doi.org/10.1007/s11465-019-0581-7
  本期目录
Two-sided ultrasonic surface rolling process of aeroengine blades based on on-machine noncontact measurement
Shulei YAO1, Xian CAO1, Shuang LIU1(), Congyang GONG2, Kaiming ZHANG1, Chengcheng ZHANG2, Xiancheng ZHANG1()
1. Key Laboratory of Pressure Systems and Safety (Ministry of Education), East China University of Science and Technology, Shanghai 200237, China
2. AECC Commercial Aircraft Engine Co., Ltd., Shanghai Engineering Research Center for Commercial Aircraft Engine, Shanghai 201108, China
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Abstract

As crucial parts of an aeroengine, blades are vulnerable to damage from long-term operation in harsh environments. The ultrasonic surface rolling process (USRP) is a novel surface treatment technique that can highly improve the mechanical behavior of blades. During secondary machining, the nominal blade model cannot be used for secondary machining path generation due to the deviation between the actual and nominal blades. The clamping error of the blade also affects the precision of secondary machining. This study presents a two-sided USRP (TS-USRP) machining for aeroengine blades on the basis of on-machine noncontact measurement. First, a TS-USRP machining system for blade is developed. Second, a 3D scanning system is used to obtain the point cloud of the blade, and a series of point cloud processing steps is performed. A local point cloud automatic extraction algorithm is introduced to extract the point cloud of the strengthened region of the blade. Then, the tool path is designed on the basis of the extracted point cloud. Finally, an experiment is conducted on an actual blade, with results showing that the proposed method is effective and efficient.

Key wordsaeroengine blades    on-machine noncontact measurement    point cloud processing    path planning    surface strengthening
收稿日期: 2019-09-17      出版日期: 2020-05-25
Corresponding Author(s): Shuang LIU,Xiancheng ZHANG   
 引用本文:   
. [J]. Frontiers of Mechanical Engineering, 2020, 15(2): 240-255.
Shulei YAO, Xian CAO, Shuang LIU, Congyang GONG, Kaiming ZHANG, Chengcheng ZHANG, Xiancheng ZHANG. Two-sided ultrasonic surface rolling process of aeroengine blades based on on-machine noncontact measurement. Front. Mech. Eng., 2020, 15(2): 240-255.
 链接本文:  
https://academic.hep.com.cn/fme/CN/10.1007/s11465-019-0581-7
https://academic.hep.com.cn/fme/CN/Y2020/V15/I2/240
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>= Min <Max Points %
−35.6999 −30.0474 7 0.0007
−30.0474 −24.3949 14 0.0014
−24.3949 −18.7424 23 0.0022
−18.7424 −13.0900 12 0.0012
−13.0900 −7.4375 19 0.0018
−7.4375 −1.7850 1215 0.1175
−1.7850 1.7850 1032822 99.8744
1.7850 7.4375 6 0.0006
7.4375 13.0900 1 0.0001
13.0900 18.7424 0 0.0000
18.7424 24.3949 0 0.0000
24.3949 30.0474 0 0.0000
30.0474 35.6999 2 0.0002
Tab.1  
Best fit alignment deviation index Deviation/mm
Max. upper deviation 32.4411
Max. lower deviation −35.6999
Average deviation (?0.1954, 0.1954)
Standard deviation 0.3321
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