Corrosion of aircraft structures made of aluminum alloys

Materials Science

Volumn 39, Issue 6, 2003, Pages 889-894

  Abolikhina, E V ^a   Molyar, A G ^a  

^a Antonov Aircraft Scientific and Technical Complex   (Ukraine)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CORROSION; MATERIALS SCIENCE; REMOVAL; STRUCTURAL ANALYSIS;

AIRCRAFT STRUCTURES; CORROSION DAMAGES; LOAD-BEARING UNITS;

ALUMINUM ALLOYS;

ALLOY; ALUMINUM;

AIRCRAFT; ARTICLE; CORROSION; MATERIAL COATING;

EID: 3442888087     PISSN: 1068820X     EISSN: None     Source Type: Journal    
DOI: 10.1023/B:MASC.0000031656.94285.4c     Document Type: Article

References (8)

1. B. E. Aizenberg, Evaluation and Prediction of the Durability of Skins of Airframe Panels Having Corrosion Damages [in Russian], Abstract of Candidate-Degree Thesis (Engineering), Kiev (1992).
2. An Investigation into the Mechanism of Exfoliation Corrosion of Aluminum Alloys [in Russian], UDI Report on the Project 05-550-079 (1983).
3. Detection and Removal of Corrosion. Recovery and Strengthening of the Rust Protection of Structural Elements of the Airframe of An-24, An-24T, An-26, An-30, and An-32 Items in Operation and Overhaul [in Russian], OPI Production Manual 472-87, 2nd ed. (1987).
4. Determination of the Crack Growth Rate in V93pchT1 Aluminum Alloy in Different Media under Long-Term Static Loading [in Russian], VIAM Technical Report (1991).
5. I. N. Fridlyander, Aluminum Deformable Structural Alloys [in Russian], Metallurgiya, Moscow (1979).
6. Common Standards of the Airworthiness of Civil Transport Airplanes [in Russian] (1985).
7. G. I. Nesterenko, Determination of the Principal Load-Bearing Elements of an Airframe [in Russian], TsAGI Report No. 4935 (1991).
8. V. S. Dubinskii, A Procedure of Taking into Account Possible Reduction of the Strength Characteristics of Aircraft Structures due to Corrosion in Establishing the Service Life for an Airframe [in Russian], TsAGI Report No. 5004 (1972).