APPLICATION OF POWDER CHARGES IN THE EMERGENCY SYSTEM OF AN AIRCRAFT LANDING GEAR
https://doi.org/10.51955/2312-1327_2024_3_117
Abstract
Problematic issues related to the operation of the landing gear system of modern aircraft are considered. Some specific requirements for similar systems used on military aircraft are indicated. A constructive solution is proposed in the form of an original development for the use of the energy of powder gases in the emergency landing gear system using the example of the Yak-130 aircraft. The author carried out an analysis of the additional equipment necessary for the operation of the proposed method of extending the landing gear, as well as its impact on the flight performance of the aircraft related to a possible increase in weight as well as changes in the dimensions of the aircraft.
Based on the results of the study, a conclusion was made about the possibility of using powder charges in the emergency system of an aircraft landing gear.
About the Author
A. F. PennoRussian Federation
Anatoly F. Penno, Candidate of Pedagogic sciences
References
1. Aircraft chassis (2022). Available at: https://ru.ruwiki.ru/wiki/Aircraftchassis# (accessed 2 April 2024). (in Russian).
2. Aircraft hydraulic system // [Electronic resource] 2015. URL: https://avia.pro/blog/gidravlicheskaya-sistema-samoleta (access date: 06/19/2024). (in Russian).
3. An Ts., Bobkov A. V. (2021). Analysis of the reliability of the aircraft landing gear retraction and release system. Collection: Youth and science: current problems of fundamental and applied research: Materials of the IV All-Russian National Scientific Conference of Students, Postgraduate Students and Young Scientists. In 4 parts, Komsomolsk-on-Amur, April 12–16, 2021. Komsomolsk-on-Amur: KNAGU. 1: 192-193. (in Russian).
4. Bekishev S. A. (2019). Improving the operation of the control system for retracting and extending the landing gear of an aircraft during landing. Current problems and prospects for the development of civil aviation. Collection of proceedings of the VIII All-Russian scientific and practical conference with international participation. Irkutsk branch of MSTU GA. Irkutsk: 14-20. (in Russian).
5. Currey N. S. (1988). Aircraft Landing Gear Design: Principles and Practice. Washington: AIAA Education Series. 373 p.
6. Frolov G. K., Godovets V. K. (2023). Modern circuit solutions for emergency landing gear retraction drives. Youth Bulletin of UGATU. 28(2): 132-138. (in Russian).
7. Kuzmin Yu. V. (2021). History of the creation of a retractable landing gear. Available at: https://cyberleninka.ru/article/n/istoriya-sozdaniya-ubirayuschegosya-shassi (accessed 2 April 2024). (in Russian).
8. How the landing gear and brake system of a passenger aircraft works (2021). Available at: https://habr.com/ru/companies/etmc_exponenta/articles/564046/ (accessed 2 April 2024). (in Russian).
9. Kondratyeva M. A., Kuznetsov S. N. (2022). Constructive improvement of the aircraft landing gear emergency release system based on the use of powder gas energy. Current problems and prospects for the development of civil aviation. Collection of proceedings of the XI International Scientific and Practical Conference. dedicated to the celebration of the 100th anniversary of the Tupolev design bureau, the 55th anniversary of the Irkutsk branch of MSTU GA, the 75th anniversary of the Irkutsk Aviation Technical College. Irkutsk: 68-73. (in Russian).
10. Patent No. 2780009 C1 Russian Federation, IPC B64C 25/22, B64C 25/30. emergency landing gear extension drive: No. 2022101851: app. 01/27/2022: publ. 09.19.2022 / R. R. Kalimullin, N. A. Polyakov, G. K. Frolov, V. A. Tselishchev; applicant: Federal State Budgetary Educational Institution of Higher Education "Ufa State Aviation Technical University". EDN WKWJEX. (in Russian).
11. Penno A. F. (2021). Increasing the reliability of the hydraulic system of a combat training aircraft Yak-130. Interuniversity collection of scientific papers. Ministry of Defense of the Russian Federation; Ministry of Education and Science of the Russian Federation Krasnodar Higher Military Aviation School of Pilots. 25: 19-23. (in Russian).
12. Penno A. F., Belovodsky Yu. P. (2022). Some proposals for increasing the reliability of the hydraulic system of an aircraft. Interuniversity collection of scientific papers. Digest of articles. 26: 65-71. (in Russian).
13. Superjet aircraft landing gear (2014). Available at: https. http://repo.ssau.ru/bitstream/Uchebnyeposobiya/Shassi-samoleta-Superjet-Elektronnyi-resurs-elektron-ucheb-posobie-po-napravleniupodgot-bakalavrov-162300-Tehn-ekspluataciya-letat-apparatov-i-aviac-dvigatelei-54502/1/Kisilev%20YU.V.%20Chassis%20aircraft.pdf (accessed 2 April 2024). (in Russian).
14. Zhang W. G., Lin. G. (2014). Analysis of Aircraft Hydraulic System Failures. Engineering Advanced Materials Research. 989-994. 2947-2950. DOI: 10.4028/WWW.SCIENTIFIC.NET/AMR.989994.2947.
15. Zhitomirsky G. I. (2005). Aircraft design. Moscow: Mashinostroenie, 406 p. (in Russian).
Review
For citations:
Penno A.F. APPLICATION OF POWDER CHARGES IN THE EMERGENCY SYSTEM OF AN AIRCRAFT LANDING GEAR. Crede Experto: transport, society, education, language. 2024;(3):117-133. (In Russ.) https://doi.org/10.51955/2312-1327_2024_3_117
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