Diagnosis and Repair Technology of Damaged Elements of Casa Aircraft

• Autorzy: Salacinski M. , Synaszko P. , Olszak R.

Identyfikatory

DOI

10.2478/v10164-010-0030-x

• Języki publikacji: EN

Abstrakty

EN

Recently Polish Air Force has been equipped with new types of aircraft. New aircraft have many elements made of composites. Composites enable increasing performance but also pose new challenges. One of these challenges is the necessity of repairing after damage. This paper presents the results of the non-destructive inspection (MIA, conductivity, optical measurement ) of the C-295 plane after damage. Some parts made of composites and metal were damaged. In this paper, the authors propose a technology of repairing damaged parts.

• Wydawca: Wydawnictwa Naukowe Sieci Badawczej Łukasiewicz - Instytutu Lotnictwa
• Czasopismo: Fatigue of Aircraft Structures
• Rocznik: 2010
• Tom: Iss. 2
• Strony: 98--105
• Opis fizyczny: Bibliogr. 4 poz., rys., wykr.

Twórcy

autor

Salacinski M.

• Air Force Institute of Technology, Warsaw, Poland

autor

Synaszko P.

• Air Force Institute of Technology, Warsaw, Poland

autor

Olszak R.

• Military Aviation Works No. 3, Deblin, Poland

Bibliografia

• [1] Dragan, K. & Klimaszewski, S. (2006). In-service Flaw Detection and Quantification on the MiG-29 Composite Vertical Tail Skin, ECNDT.
• [2] Roach, D., Moore, D., Walkington, P. (1996). Nondestructive Inspection of Bonded Composite Doublers for Aircraft, Sandia National Labs, FAA Airworthiness Assurance NDI Validation Center.
• [3] Technical Manual. (2005). Nondestructive Inspection Methods, Basic Theory, T.O. 33B-1-1, NAVAIR 01-1A-16, TM 1-1500-335-23.
• [4] Baker, A., Rose, F., Jones, R. (2002). Advances in the Bonded Composite Repair of Metallic Aircraft Structure. Oxford. ISBN 0-008-042699-9.