Qualitative to Quantitative Non-Destructive Evaluation: A Concept for D-Sight Inspections of Aircraft Structures

Article Preview

Abstract:

Non-destructive evaluation of structures is a key procedure in operation of aircraft structures, necessary to maintain their quality and integrity. Numerous non-destructive testing (NDT) techniques have been adapted to inspect aircraft structures and are currently used according to appropriate protocols. However, many of them provide only qualitative results, such as the D-Sight optical NDT technique used for inspections in aviation. In this study, a concept of improvement of the D-Sight technique is proposed by means of appropriate experimental program and processing procedures applied to the resulting images from inspection. It was demonstrated that appropriately selected processing methods may allow assessing damage quantitatively and improve the overall sensitivity and applicability of a given NDT technique.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

69-74

Citation:

Online since:

September 2022

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2022 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] R.J.H. Wanhill, Milestone case histories in aircraft structural integrity, in: I. Milne, R.O. Ritchie, B. Karihaloo (Eds.), Comprehensive Structural Integrity, Elsevier, Amsterdam, 2003, pp.61-72.

DOI: 10.1016/b0-08-043749-4/01002-8

Google Scholar

[2] S.R. Ignatovich, A. Menou, M.V. Karuskevich, P.O. Maruschak, Fatigue damage and sensor development for aircraft structural health monitoring, Theor. Appl. Fract. Mech. 65 (2013) 23-27.

DOI: 10.1016/j.tafmec.2013.05.004

Google Scholar

[3] S.J. Findlay, N.D. Harrison, Why aircraft fail, Mater. Today 5 (2002) 18-25.

Google Scholar

[4] C. Boller, F.K. Chang, Fujino Y. (Eds.), Encyclopedia of Structural Health Monitoring, Wiley, Chichester, UK, (2009).

Google Scholar

[5] Department Of Transportation U. S., Airman Testing Standards Branch, Federal Aviation Administration, Oklahoma City, OK, Aviation Maintenance Technician Handbook – Airframe, (2018).

Google Scholar

[6] P. Ciężak, A. Rdzanek, Corrosion monitoring of aircraft based on the Corrosion Prognostic Health Management (CPHM) system, J. KONBiN 50 (2020) 205-216.

DOI: 10.2478/jok-2020-0082

Google Scholar

[7] R.L. Reynolds, F. Karpala, D.A. Clarke, O.L. Hegeniers, Theory and applications of a surface inspection technique using double-pass retroreflection, Opt. Eng. 32 (1993) 2122-2129.

DOI: 10.1117/12.143938

Google Scholar

[8] J.P. Komorowski, N.C. Bellinger, R.W. Gould, The role of corrosion pillowing in NDI and in the structural integrity of fuselage joints, Proc. of the 19th Symposium of the International Committee on Aeronautical Fatigue, 16th-20th June 1997, Edinburgh, EMAS Publishing, 251-266.

DOI: 10.2514/6.2005-2023

Google Scholar

[9] J.P. Komorowski, D.S. Forsyth, The role of enhanced visual inspections in the new strategy for corrosion management, Aircr. Eng. Aerosp. Technol. 72 (2000) 5-13.

DOI: 10.1108/00022660010308615

Google Scholar

[10] N.C. Bellinger, J.P. Komorowski, T.J. Benak, Residual life predictions of corroded fuselage lap joints, Int. J. Fatigue 23 (2001) 349-356.

DOI: 10.1016/s0142-1123(01)00148-7

Google Scholar

[11] K. Dragan, S. Klimaszewski, In-service flaw detection and quantification on the MiG-29 composite vertical tail skin, Proc. of the 9th European Conference on Non Destructive Testing, 25th-29th September 2006, Berlin, We.1.1.4.

Google Scholar

[12] G.Y. Tian, R.S. Lu, D. Gledhill, Surface measurement using active vision and light scattering, Opt. Laser. Eng. 45 (2007) 131-139.

Google Scholar

[13] A. Fahr, Aeronautical Applications of Non-destructive Testing, DEStech Publications, Lancaster, PE, (2014).

Google Scholar

[14] A. Katunin, Aircraft Structures: Mechanics, Design, and Maintenance, Silesian University of Technology Press, 810, Gliwice, (2019).

Google Scholar

[15] J.H. Heida, A.J.A. Briunsma, D-Sight technique for rapid impact damage detection on composite aircraft structures, NDT.net Journal 4 (1999) 1-7.

Google Scholar

[16] S. Klimaszewski, A. Leski, K. Dragan, M. Kudelski, M. Wrona, Helicopter structural integrity program of Polish Mi-24 hind helicopters, in: M.J. Bos (Ed.), ICAF 2009, Bridging the Gap Between Theory and Operational Practice, Springer Science & Business Media, Amsterdam, 2009, pp.263-277.

DOI: 10.1007/978-90-481-2746-7_16

Google Scholar

[17] D.J. Willie, O.L. Hageniers, F. Karpala, D Sight for NDE of aging aircraft, in: T.M. Cordell, R.D. Rempt (Eds.), Nondestructive Evaluation of Aging Aircraft, Airports, Aerospace Hardware, and Materials, Proceedings of SPIE 2455 (1995) 1-8.

DOI: 10.1117/12.213532

Google Scholar

[18] K. Dragan, Ageing of composites in the rotorcraft industry, in: R. Martin (Ed.), Ageing of Composites, Woodhead Publishing Series in Composites Science and Engineering, Woodhead Publishing, Cambridge, UK, 2008, pp.311-325.

DOI: 10.1533/9781845694937.2.311

Google Scholar

[19] F. Karpala, O.L. Hegeniers, Development of a D Sight aircraft inspection system: Phase II, Final report DOT/FAA/AR-95/15, Federal Aviation Administration, Washington, D. C., (1996).

Google Scholar

[20] J.P. Komorowski, N.C. Bellinger, R.W. Gould, A. Marincak, R. Reynolds, Quantification of corrosion in aircraft structures with double pass retroreflection, Canadian Aeronaut. Space J. 42 (1996) 76-82.

Google Scholar

[21] Z. Liu, D.S. Forsyth, J.P. Komorowski, Fusion of multimodal NDI images for aircraft corrosion detection and quantification, in: R.S. Blum, Z. Liu (Eds.), Multi-Sensor Image Fusion and Its Applications, CRC Press, Boca Raton, FL, 2006, pp.375-405.

DOI: 10.1201/9781315221069-13

Google Scholar