Aircraft Skin Corrosion and Structural Safety Considerations

• Authors: Pila Jan , Kozuba Jarosław , Martinec Franciszek
• Languages of publication: EN

Abstracts

PL

Korozja pokrycia samolotu i względy bezpieczeństwa konstrukcyjnego

Keywords

EN

aircraft structure; aircraft safety; non-destructive inspection; corrosion; maintenance; load; fatigue

PL

konstrukcja statku powietrznego; bezpieczeństwo statku powietrznego; inspekcja nieniszcząca; korozja; konserwacja; obciążenie; zmęczenie

• Publisher: Instytut Nauk Społecznych i Bezpieczeństwa Uniwersytetu Przyrodniczo-Humanistycznego w Siedlcach
• Journal: De Securitate et Defensione. O Bezpieczeństwie i Obronności
• Year: 2021
• Issue: 2(7)
• Pages: 149-163

Dates

published

2021-12-17

Contributors

author

Pila Jan

• Silesian University of Technology, Katowice, Poland

author

Kozuba Jarosław

• Silesian University of Technology, Katowice, Poland

author

Martinec Franciszek

• University College of Business in Prague, Prague, Czech Republic

References

• 1. Advisory Circular. 1997. AC No: 43-204, FAA, U.S. Department of Transportation. In https://www.faa.gov/documentLibrary/media/Advisory_Circular/43-204.pdf.
• 2. Craig Benjamin D., Lane Richard A., Rose David H. 2006. Corrosion Prevention and Control, A Program Management Guide for Selecting Materials. In http://www.acqnotes.com/At-tachments/Corrosion%20Prevention%20and%20Control%20A%20Program%20Man-agement%20Guide%20for%20Selecting%20Materials.pdf.
• 3. Federal Aviation Regulations: Airworthiness standards, transport ..., Part 25, § 25.571 Dam-age - tolerance and fatigue evaluation of structure. In https://www.law.cor-nell.edu/cfr/text/14/25.571.
• 4. Greer, Jr. James M., Brown Molly, and others. 2020. Fatigue and residual strength effects of exfoliation corrosion damage. In https://saf-engineering.com/wp-content/up-loads/2020/05/Aging2005-FATIGUE-AND-RESIDUAL-STRENGTH-EFFECTS-OF-EXFOLIATION-CORROSION-DAMAGE.pdf.
• 5. Jaya Aditya, Tiong Ung Hing, Mohammed Reza, Bil Cees, Clark Graham. 2010. Corrosion treatments and the fatigue of aerospace structural joints. Australia. In https://core.ac.uk/download/pdf/82351243.pdf.
• 6. Komorowski Jerzy P., and others. 1998. Probability of detection of corrosion in aircraft struc-tures. Ottawa, Canada. In https://www.researchgate.net/publication/44076249_Probabi-lity_of_Detection_of_Corrosion_in_Aircraft_Structures.
• 7. Mirkin I.I., Mikhalev A.V., Feigenbaum Yu. M. Improvement of the system of providing and maintaining the airworthiness of aircraft under corrosion safety. In https://cyber-leninka.ru/article/n/sovershenstvovanie-sistemy-obespecheniya-i-podderzhaniya-letnoy-godnosti-samoletov-po-usloviyam-bezopasnosti-ot-korrozii/viewer.
• 8. Niu Michael C.Y. 1999. Airframe stress analysis and sizing. Hong Kong.
• 9. Siegel Mel, Gunatilake Priyan. 1997. Remote Inspection Technologies for Aircraft Skin Inspec-tion. IEEE Workshop on Emergent Technologies and Virtual Systems for Instrumentation and Measurement Niagara Falls, Ontario, Canada, May 15-17. In https://www.re-searchgate.net/publication/2314728_Remote_Inspection_Technologies_of_Air-craft_Skin_Inspection.
• 10. Whaley P.W. 1999. Corrosion damage tolerance methodology for C/KC-135 fuselage structure. Oklahoma City, USA. In https://dokumen.tips/documents/corrosion-damage-tolerance-methodology-for-corrosion-damage-tolerance-methodology.html.
• 11. Особенности коррозионной повреждаемости авиационных конструкций [Osobennosti korrozionnoy povrezhdayemosti aviatsionnykh konstruktsiy]. In https://helpiks.org/6-19149.html.

Identifiers

DOI

https://doi.org/10.34739/dsd.2021.02.10