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RESIDUAL STRENGTH AND ENDURANCE OF ROD CONSTRUCTION ELEMENTS OF AIRCRAFT AFTER THE DAMAGE BY LIGHTNING-LIKE ELECTRICAL DISCHARGES

Abstract

Caused by lightning damage to the external elements of construction of the aircraft, in the form of deformities, burn-through and erosive craters and also hidden defects in the affected area can cause a reduction in the strength of damaged parts. Fatigue tests of samples of rod construction elements damaged by lightning-like electrical discharges showed that for a symmetric cycle of variable loading at an amplitude of 100 kPa and a frequency of 50 Hz supply of fatigue strength decreased in 1,5-1,7 times, and fatigue life decreased in 25 times at local burns and in 70 times at annular burns. The main reason is education on the details of micro cracks in the area of erosive craters formed by discharge.

About the Authors

S. K. Kamzolov
МГТУ ГА
Russian Federation


S. M. Novikov
МГТУ ГА
Russian Federation


A. N. Razumovsky
МГТУ ГА
Russian Federation


References

1. Kamzolov S.K., Samohin A.V. Ob opasnosti polyotov v grozu (versii dvuh katastrof) // Nauchnyy vestnik MGTU GA. 2012. № 180. S. 102-105.

2. E.M. Bazelyan, YU.P. Rayzer. Fizika molnii i molniezashchity. M., FIZMATLIT, 2001. – 320 s.

3. Clifford D.W. Characteristics of Lightning Strikes to Aircraft. / Proc. of the International Conference on Lightning and Static Electricity. – Oxford, 25-30 March 1982. – P. A9-1 – A9-11.

4. Birger I.A., Mavlyutov R.R. Soprotivlenie materialov: Uchebnoe posobie.- M.: Nauka. 1986. – 560 s.


Review

For citations:


Kamzolov S.K., Novikov S.M., Razumovsky A.N. RESIDUAL STRENGTH AND ENDURANCE OF ROD CONSTRUCTION ELEMENTS OF AIRCRAFT AFTER THE DAMAGE BY LIGHTNING-LIKE ELECTRICAL DISCHARGES. Civil Aviation High Technologies. 2015;(222):195-200. (In Russ.)

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ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)