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1 1 2 6435 2 6435 u u u 9 0 0 0 0 5 0 0 0 0 I 0 0 0 0 0 6 0 0 0 u 0 0 0 Multi frequency eddy current inspection of multilayered structures in aircrafts Student Name Fu Yu Classu110813 Supervisor Fu Yuewen Abstract With the rapid development of aviation industry in recent years the aviation safety is more and more important to us In both military aviation and civil aviation field how to make the preventive maintenance and prevent mechanical failure in operation of aircrafts is particularly important Especially those overage aircrafts beyond the original design life 20 to 25 years are still in service they are vulnerable to the influence of corrosion damage and fatigue crack How to be efficiently and make accurate detection of these defects which endanger the property and safety of life on board One of the methods is multi frequency eddy current testing method It s easy to produce fatigue crack near the rivets in riveting multi layer structures prone to corrosion defects between the layers Firstly this paper introduces the principle of multi frequency eddy current inspection technology According to the questions mentioned above we build the experimental platform to simulate multi level structure in aircrafts Secondly Using double frequency eddy current detector to detect the simulated multilayer structure discusses the differences and characteristics of single and multi frequency eddy current testing analyzes the advantages of multi frequency eddy current testing in multilayer structure detection Equipment produce current in different frequency and detect by one eddy current probe various frequency signals can detect defects in different depth of multilayer structure The results show that multi frequency eddy current testing realize the effective defects Multi frequency eddy current testing eliminates noisy signal caused by fasteners interlayer and air gap enhance the flaw signal It has great advantages in detection of interior of the aircraft skin The testing practice and the conclusion of this article can be used for multi frequency eddy current testing technology in the actual detection Keyword Multi frequency eddy current Corrosion defects Riveting multi layer structures Crack defects Signature of Supervisor q r q r 9 9 2 2 9 9 2 2 2 Phasec2200 I 2 11 0 21 0 31 0 0 41 51 0 9 9 2 2 11 0 0 2015 3 0932015 4 10 2 0 2015 4 1132015 4 20 31 0 2015 4 2132015 4 25 41 2015 4 2632015 5 16 51 0 2015 5 1732015 5 31 61 0 2015 6 0132015 6 06 71 9 0 2015 6 0732015 6 26 2 2 1 J A Bieber S K Shaligram J H Rose J C Moulder Time gating of Pulsed Eddy Current Signals for Defect Characterization and Discrimination in Aircraft Lap Joints J Review of Progress in QNDE 1997 16B 1915 1921 2 SMITH R A HUGO G R Deep corrosion and crack detection in aging aircraft using transient eddy current NDE J Insight 2001 43 1 u14 24 3 J A Bieber S K Shaligram J H Rose et al Time gating of pulsed eddy current signals for defect characterization and discrimination in aircraft lap joints Review of progress in QNDE 1997 16B 1915 1921 4 B A Lepine B P Wallace D S Forsyth Pulsed eddy current method developments forbidden corrosion detection in aircraft structures NDT E International 1999 4 1 1 10 5 S Giguere B A Lepine J M S Dubois Pulsed eddy current technology Characterizing material loss with gap and lift off variations Research in Nondestructive Evaluation 2001 13 119 129 6 Ali Sohpian Gui Yun Tian et al A feature extraction technique based on principal component analysis for pulsed Eddy current NDT J NDT E International 2002 36 37 41 7 LIBBY H LtIntroduction to electromagnetic nondestructive test methodswMx t New York John WileypSons Inc 1971t 8 Gui Yun Tian Ali Sophian Defect classification using a new feature for pulsed eddy current Sensors J NDT E International 2005 38 77 82 9 Ali Sophian Characterization of Surface and Sub surface Discontinuities in Metals Using Pulsed Eddy Current Sensors C Thesis the University of Huddersfield in partial fulfilment of the requirements for the degree of Doctor of Philosophy The United Kingdom 2003 10 G Y Tian Y Li and C Mandache Study of Lift Off Invariance for Pulsed Eddy Current Signals J IEEE Transaction on Magnetics 2009 45 1 184 191 I I 8989 2 2 2 2 2 2 22 I I 2 2 s o s o s o o u u n s s o s n o u u u u 1 2 3 4 5 6 2015 1 1 1 s s s o s o n s s o s o s s o s s o n s s o z n s s o z zo s o z s o s o 1 2 1 2 1 1970 s Libby H L s sz q r I Jo s 2015 2 o s s n n I Jo s o 1983 s IBG qPreventive Multi Frequency Eddy current TechnologysPMFTr 8 s 1 1000 s 8 o s s n n s 8 s s I Jo 1993 s Thompson J G s I Jo 2002 s Edward P s s s s I Jo2003 sBos B V D SAAB 2000 s n s I Jo 2006 s TMT eddyMax 4U Airbus A340 600 s I Jo 1 2 2 o 1992 s ZETEC MIZ 18A I Jo1995 ET 255A I Jo1998 I Jo2000 s EEC 39 4 8 s I Jo2002 s I Jo 2009 s s n I Jo s s z hhMFE 1 s 2015 3 s s s I Jo s z s o 1 3 q r s n n s s o u t s o t s o t Phasec2200 s o t n s s o t o 1 4 s o s s o s n o s n o z s o 1 5 s s o 2015 4 2 1 s s o o s s s o s o q r s o o 2015 5 s EP u drdz drdztzrV V p f q r dSB t Vp 1 dSA t 1 c dl t A q r sE k o s s 3 s s o s s o z s o 3 s s o 2 2 o s s s z o o s s o s o s s s s s s o o G9 s s s 2015 6 s s4825G s s I Jo 2 3 s s n s o s s o u q r hh Phh ehh 8 V ghh B V q r s Pneng o n n s s o s s o z s s o z s O q r s O q r s o Oq r ds s fx xeJJ 0 2015 7 q2 r d od s o d o I Jo 2 4 z s o 4 s u sc dSB dt d dlE q r 4 s s s u scs dSD dt d dSJdlH q r B s u SV qdvdSD q r B s u s dSB0 q r s8n5n6n3 n n f Z o ED 0 q r 0 B H q r EJ q r q r q r s q r q r f 1 2015 8 o z s z o u t B E q r t D JH q r D q r 0 B q r 2 5 s n s o 2015 9 3 1 s o u n n n o s u n s o s o s o s n o s u t o t t hh o t o 2015 10 3 2 3 2 1 Phasec 2200 76 CRO 8XMTS RK OM s n s s o s o s o RK OM u s o o 3 2 2 u n n n n o z s n n n o sz o o s o z q r s 2015 11 o z o o s o s s o s o z o s n s o s o CRO 8XMTS 2 s s VVs VVs s 8b Rbo 2 s z s o s OVX s o 2 2015 12 3 3 3 3 1 o VVc VVc VVq c c r s VVs o s o z o k s o 3 3 2 s o n n n VVs n n n n VVo s VVc VVs VVc VVs VVc VVs VVc VVs VVc VVs VVc VVo VV y VV o 2015 13 3 4 s s o 2015 14 4 1 4 1 1 s z s n s n q r o l m o s s m o 2015 15 s VVn VVn VVn VVo s o 4 1 2 XNOuAOPUOM SX 4R s5S YUKau GsESO u4R s s s s q VV VVr s q l m r s s 4 2 XNO0 AOPU 4Rs5S YUKau GsESO u4R 4R s O S u O V i 2015 16 s 32 4UOK o A64 s s s A64 o 6 7C8 s BM XUU s 2 X o A64 YO K SX s 5S YUKau GsESO uB Vo B V B V RK O B V 7KS s o 4 3 s CRO 8XMTS RK OM o 2015 17 5 1 s o u q VV VVr s s o z 8bn 8bn VV o K 8b L 8b 2015 18 M VV s s o s s s o s BD 729 k s s s o qKr qLr 8b 8b VV 2015 19 s o n s s o s s s s s o o s s s s VV o s s z o 5 2 n s u zs s zo s 8b Rb o uzn s s o n s o qKr Rb 2015 20 qLr Rb l qKr Rb qLr Rb m s Rb Rbo 2015 21 qKr Rb qLr Rb l qKr Rb 2015 22 qKr Rb m s z o s s o s s s o n o qKr Rb qLr Rb 2015 23 qMr m qKr 8b qLr 8b 2015 24 qMr m s o s s s s z o s s s s s o l s s s s o 5 3 n n s s o 2015 25 6 1 s o s s s z o s o s z s o s z s o s o z o s s s s o 6 2 zn s s zo s s n n s o s s z o z s n o s s s o s s s s s 2015 26 o s n s o s o s s o 6 2 s o s s n n o n s o s z o s s o z s s o s s o 2015 27 I J LIBBY H L Introduction to electromagnetic nondestructive test methodwMx New York John WileypSons Inc 1971t I J I J I J z I J I J I J I J Thompson J G Subsurface Corrosion Detection in Aircraft Lap Splices Using a Dual Frequency Eddy Current Inspection Technique

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