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Device for Conductive Coatings Quality Control of Rocket and Space Technique Elements

https://doi.org/10.21122/2220-9506-2019-10-1-23-31

Abstract

The widespread use of cryogenic fuels in the aerospace industry necessitates additional thermal insulation of aircraft fuel tanks. At the same time a static charge may occur on the heat insulating layer during operation which can lead to an explosion if fuel leaks. To avoid such situations an antistatic conductive coating is applied to the insulation. The aim of the study is to develop a device for remote control of conductive coatings of aircraft fuel tanks which allows to quick find and mark damaged areas.

The developed method consists in changing the electrical capacitance between the conductive coating of the controlled object and the scanning electrode allowing to identify hazardous in terms of sparking closed shape defects. The basic technical requirements for the device were formed and the required minimum size of the monitored defect were indicated. The design features necessary for the implementation of the device were considered. A block diagram were developed on the basis of which an experimental bench for capacitive control were created which were is based on the bridge measurement method.

The article presents the results of the finite-difference calculation of the electric field in the structure of a capacitive sensor in the presence of a defect, the dependence of the capacitance of the sensor on its displacement over the defective area was also obtained. As the result of experimental studies the experimental data obtained confirmed the theoretical calculations and the correctness of the mathematical model with an accuracy of no worse than 5 %, the absolute error of fixing the defect ± 2 mm at a scanning speed of 0,02 m/s. Was shown that the total error of fixing the coordinates of the defect at different positions of the air gap sensor, temperature and scanning speed lies in the range of 1,5–6,5 mm. The materials presented in the article make it possible to increase flight safety by reducing the likelihood of sparking.

About the Authors

B. V. Skvortsov
Samara National Research University
Russian Federation

Address for correspondence: B.V. Skvortsov – Samara National Research University, Moskovskoye shosse, 34, Samara 443086, Russia.     e-mail: aps@ssau.ru



A. S. Samsonov
Samara National Research University
Russian Federation
Moskovskoye shosse, 34, Samara 443086


S. A. Borminskiy
Samara National Research University
Russian Federation
Moskovskoye shosse, 34, Samara 443086


D. M. Zhivonosnovskaya
Samara National Research University
Russian Federation
Moskovskoye shosse, 34, Samara 443086


References

1. Ovcharenko A.G. EHlektrostaticheskaya bezopasnost' pozharoi vzryvoopasnykh proizvodstv [Electrostatic safety of fire and explosive industries]. Biysk, BTI AltGTU, 2006, 156 p.

2. Vavilov V.D., Timoshenkov S.P., Timoshenkov A.S. Mikrosistemnye datchiki fizicheskikh velichin [Microsystem sensors of physical quantities]. Moscow, Technosphere Publ., 2018, 500 p.

3. Shaternikov V.E., Klyuev S.V. Vikhretokovyj metod nerazrushayushhego kontrolya tonkolistovykh metallicheskikh izdelij [Eddy current method of non-destructive testing of thin sheet metal products]. Moscow, Engineering Publ., 2007, 173 p.

4. Landau L.D., Lifshits E.M. Teoreticheskaya fi Tom II. Teoriya polya [Theoretical physics. Volume II. Field theory]. Moscow, Physmatlit Publ., 2006, 304 p.

5. Hegg M.C., Ogale A., Mescher A., Mamishev A.V., Minaie B. Remote monitoring of resin transfer molding processes by distributed dielectric sensors. Journal of Composite Materials, 2005, no. 39, pp. 1519–1539. DOI: 10.1177/0021998305051083

6. Hegg M.C., Mamishev A.V. Influence of variable plate separation on fringing electric fi in parallel-plate capacitors. Electrical Insulation, Conference Record of the 1988 IEEE International Symposium on, 1998, pp. 384–387. DOI: 10.1109/ELINSL.2004.1380606

7. Batishchev V.I., Melentyev V.S. Izmerenie parametrov emkostnykh datchikov polozheniya i peremeshheniya [Measurement of parameters of capacitive position and displacement sensors]. Moscow, Engineering Publ., 2005, 124 p.

8. Samsonov A.S., Skvortsov B.V. [Monitoring the integrity of the conductive coating of aircraft fuel tanks]. Аviakosmicheskoe priborostroenie [Aerospace Instrumentation], 2015, no. 9, pp. 34–40 (in Russian).

9. Skvortsov B.V., Samsonov A.S., Blinov D.I., Ilmurzina S.F. [Problems of flaw detection of conductive coating of aircraft fuel tanks]. Izvestiya SNTS RАN [News SSC RAS], 2016, vol. 18, no. 1, pp. 114–118 (in Russian).

10. Afonskiy A.A., D'yakonov V.P. EHlektronnye izmereniya v nanotekhnologiyakh i v mikroehlektronike [Electronic measurements in nanotechnology and microelectronics]. Moscow, DMK Press Publ., 2012, 688 p.

11. Tsvetkov E.I. Metrologiya. Modeli. Metrologicheskij analiz. Metrologicheskij sintez [Metrology. Models. Metrological analysis. Metrological synthesis]. Publishing house SPbGETU «LETI», 2014, 293 p.


Review

For citations:


Skvortsov B.V., Samsonov A.S., Borminskiy S.A., Zhivonosnovskaya D.M. Device for Conductive Coatings Quality Control of Rocket and Space Technique Elements. Devices and Methods of Measurements. 2019;10(1):23-31. (In Russ.) https://doi.org/10.21122/2220-9506-2019-10-1-23-31

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ISSN 2220-9506 (Print)
ISSN 2414-0473 (Online)