A Force Sensorless Method for CFRP/Ti Stack Interface Detection during Robotic Orbital Drilling Operations

Drilling carbon fiber reinforced plastics and titanium (CFRP/Ti) stacks is one of the most important activities in aircraft assembly. It is favorable to use different drilling parameters for each layer due to their dissimilar machining properties. However, large aircraft parts with changing profiles...

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Main Authors: Qiang Fang, Ze-Min Pan, Bing Han, Shao-Hua Fei, Guan-Hua Xu, Ying-Lin Ke
Format: Article
Language:English
Published: Hindawi Limited 2015-01-01
Series:Mathematical Problems in Engineering
Online Access:http://dx.doi.org/10.1155/2015/952049
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spelling doaj-f70d9fb3a39c4444837cdf64011e653c2020-11-24T22:38:09ZengHindawi LimitedMathematical Problems in Engineering1024-123X1563-51472015-01-01201510.1155/2015/952049952049A Force Sensorless Method for CFRP/Ti Stack Interface Detection during Robotic Orbital Drilling OperationsQiang Fang0Ze-Min Pan1Bing Han2Shao-Hua Fei3Guan-Hua Xu4Ying-Lin Ke5The State Key Laboratory of Fluid Power Transmission and Control, College of Mechanical Engineering, Zhejiang University, Hangzhou 310027, ChinaThe State Key Laboratory of Fluid Power Transmission and Control, College of Mechanical Engineering, Zhejiang University, Hangzhou 310027, ChinaAVIC Xi’an Aircraft Industry (Group) Company Ltd., Xi’an 710089, ChinaThe State Key Laboratory of Fluid Power Transmission and Control, College of Mechanical Engineering, Zhejiang University, Hangzhou 310027, ChinaThe State Key Laboratory of Fluid Power Transmission and Control, College of Mechanical Engineering, Zhejiang University, Hangzhou 310027, ChinaThe State Key Laboratory of Fluid Power Transmission and Control, College of Mechanical Engineering, Zhejiang University, Hangzhou 310027, ChinaDrilling carbon fiber reinforced plastics and titanium (CFRP/Ti) stacks is one of the most important activities in aircraft assembly. It is favorable to use different drilling parameters for each layer due to their dissimilar machining properties. However, large aircraft parts with changing profiles lead to variation of thickness along the profiles, which makes it challenging to adapt the cutting parameters for different materials being drilled. This paper proposes a force sensorless method based on cutting force observer for monitoring the thrust force and identifying the drilling material during the drilling process. The cutting force observer, which is the combination of an adaptive disturbance observer and friction force model, is used to estimate the thrust force. An in-process algorithm is developed to monitor the variation of the thrust force for detecting the stack interface between the CFRP and titanium materials. Robotic orbital drilling experiments have been conducted on CFRP/Ti stacks. The estimate error of the cutting force observer was less than 13%, and the stack interface was detected in 0.25 s (or 0.05 mm) before or after the tool transited it. The results show that the proposed method can successfully detect the CFRP/Ti stack interface for the cutting parameters adaptation.http://dx.doi.org/10.1155/2015/952049
collection DOAJ
language English
format Article
sources DOAJ
author Qiang Fang
Ze-Min Pan
Bing Han
Shao-Hua Fei
Guan-Hua Xu
Ying-Lin Ke
spellingShingle Qiang Fang
Ze-Min Pan
Bing Han
Shao-Hua Fei
Guan-Hua Xu
Ying-Lin Ke
A Force Sensorless Method for CFRP/Ti Stack Interface Detection during Robotic Orbital Drilling Operations
Mathematical Problems in Engineering
author_facet Qiang Fang
Ze-Min Pan
Bing Han
Shao-Hua Fei
Guan-Hua Xu
Ying-Lin Ke
author_sort Qiang Fang
title A Force Sensorless Method for CFRP/Ti Stack Interface Detection during Robotic Orbital Drilling Operations
title_short A Force Sensorless Method for CFRP/Ti Stack Interface Detection during Robotic Orbital Drilling Operations
title_full A Force Sensorless Method for CFRP/Ti Stack Interface Detection during Robotic Orbital Drilling Operations
title_fullStr A Force Sensorless Method for CFRP/Ti Stack Interface Detection during Robotic Orbital Drilling Operations
title_full_unstemmed A Force Sensorless Method for CFRP/Ti Stack Interface Detection during Robotic Orbital Drilling Operations
title_sort force sensorless method for cfrp/ti stack interface detection during robotic orbital drilling operations
publisher Hindawi Limited
series Mathematical Problems in Engineering
issn 1024-123X
1563-5147
publishDate 2015-01-01
description Drilling carbon fiber reinforced plastics and titanium (CFRP/Ti) stacks is one of the most important activities in aircraft assembly. It is favorable to use different drilling parameters for each layer due to their dissimilar machining properties. However, large aircraft parts with changing profiles lead to variation of thickness along the profiles, which makes it challenging to adapt the cutting parameters for different materials being drilled. This paper proposes a force sensorless method based on cutting force observer for monitoring the thrust force and identifying the drilling material during the drilling process. The cutting force observer, which is the combination of an adaptive disturbance observer and friction force model, is used to estimate the thrust force. An in-process algorithm is developed to monitor the variation of the thrust force for detecting the stack interface between the CFRP and titanium materials. Robotic orbital drilling experiments have been conducted on CFRP/Ti stacks. The estimate error of the cutting force observer was less than 13%, and the stack interface was detected in 0.25 s (or 0.05 mm) before or after the tool transited it. The results show that the proposed method can successfully detect the CFRP/Ti stack interface for the cutting parameters adaptation.
url http://dx.doi.org/10.1155/2015/952049
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