Improving the efficiency of the powerplant of an unmanned aerial vehicle through the use of cryogenic fuel
- Authors: Kolesnikov A.S.1, Grasko T.V.1, Raznoschikov V.V.2
-
Affiliations:
- Military Educational and Scientific Center of the Air Force Academy named after Professor N.E. Zhukovsky and Yu.A. Gagarin
- Central Institute of Aviation Motors
- Issue: Vol 19, No 3 (2020)
- Pages: 7-17
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/8259
- DOI: https://doi.org/10.18287/2541-7533-2020-19-3-7-17
- ID: 8259
Cite item
Full Text
Abstract
The article is devoted to increasing the efficiency of the power plant of an unmanned aerial vehicle through the use of cryogenic fuel. It has been substantiated that the creation of a power plant is based on an integrated approach to the “Aircraft – Power Plant – Fuel” system and ensures a significant achievement of perfection indicators according to high-level criteria (fuel consumption per hour (kilometer), range, flight duration, etc.) Analysis of energetic properties of some types of aviation fuels showed that gas fuels in their properties are generally superior to liquid ones, except for one thing– low density, which requires a large volume of fuel tanks. An unmanned aerial vehicle Tu-143 “Reis” (Flight) equipped with a pure turbojet engine TR3-117 was chosen as a prototype. The optimization problem of the study was solved. The task was to determine if an engine intended to run on kerosene could operate on propane according to the main parameters of the working process, provided that possible flight conditions were maintained. The obtained altitude and speed characteristics indicate that the conversion of engines from kerosene to cryogenic propane is possible without changing their design by modernizing the combustion chamber and individual elements of the automatic fuel metering system.
Keywords
About the authors
A. S. Kolesnikov
Military Educational and Scientific Center of the Air Force Academy named after Professor N.E. Zhukovsky and Yu.A. Gagarin
Author for correspondence.
Email: sanekkolesnikov1987@rambler.ru
Lecturer of the Department of Aircraft Engines
Russian FederationT. V. Grasko
Military Educational and Scientific Center of the Air Force Academy named after Professor N.E. Zhukovsky and Yu.A. Gagarin
Email: grasko83@mail.ru
Candidate of Science (Engineering), Associate Professor of the Department of Aircraft Engines
Russian FederationV. V. Raznoschikov
Central Institute of Aviation Motors
Email: raznoschikov@mail.ru
Candidate of Science (Engineering), Associate Professor, Leading Researcher
Russian FederationReferences
- Nechaev Yu.N., Kobel'kov V.N., Polev A.S. Aviatsionnye turboreaktivnye dvigateli s izmenyaemym rabochim protsessom dlya mnogorezhimnykh samoletov [Variable-cycle aviation turbojets for multi-mode aircraft]. Moscow: Mashinostroenie Publ., 1988. 175 p.
- Yugov O.K., Selivanov O.D. Soglasovanie kharakteristik samoleta i dvigatelya [Engine/airframe interface]. Moscow: Mashinostroenie Publ., 1975. 204 p.
- Andreev V.A., Borisov V.B., Klimov V.T., Malyshev V.V., Orlov V.N. Vnimanie: gazy. Kriogennoe toplivo dlya aviatsii [Attention: gases. Cryogenic fuel for aviation]. Moscow: Moskovskiy Rabochiy Publ., 2001. 244 p.
- Arkharov A.M., Kunis I.D. Kriogennye zapravochnye sistemy startovykh raketno-kosmicheskikh kompleksov [Cryogenic refueling systems of launch rocket and space complexes]. Moscow: Bauman Moscow State Technical University Publ., 2006. 252 p.
- Raznoschikov V.V., Demskaya I.A. Mathematical model of calculation thermo-physical properties of synthetic liquid fuel. Trudi MAI. 2012. No. 50. (In Russ.). Available at: http://trudymai.ru/published.php?ID=28611
- Demskaya I.A., Raznoschikov V.V. Technique for determination new structures of the alternative fuels. Aerospace MAI Journal. 2012. V. 19, no. 5. P. 72-80. (In Russ.)
- Raznoschikov V.V., Demskaya I.A. Technique of optimum structure aviation condensed fuel formation. Alternative Fuel Transport. 2011. No. 5 (23). P. 16-19. (In Russ.)
- Raznoschikov V.V., Zagumennov V.V., Demskaya I.A. Thermohydraulic optimization of the aero-derivative cryogenic fuel supply system running on supercooled propane. Alternative Fuel Transport. 2014. No. 4 (40). P. 26-36. (In Russ.)
- Raznoschikov V.V., Stashkiv M.S. Computational research of parameters of cryogenic propellant system for high-speed aircraft. Journal of Physics: Conference Series. 2019. V. 1147, Iss. 1. doi: 10.1088/1742-6596/1147/1/012056
- Yanovskii L.S., Lempert D.B., Raznoschikov V.V., Aver’kov I.S. Evaluation of effectiveness of solid fuels based on high enthalpy dispersants for rocket ramjet engines. Russian Journal of Applied Chemistry. 2019. V. 92, Iss. 3. P. 367-388. doi: 10.1134/S1070427219030078
- Yanovskii L.S., Lempert D.B., Raznoschikov V.V., Averkov I.S, Zyuzin I.N., Zholudev A.F., Kislov M.B. Prospects for the use of diethynylbenzene as a fuel dispersant for rocket ramjet engines. Russian Chemical Bulletin. 2019. V. 68, Iss. 10. P. 1848-1855. doi: 10.1007/s11172-019-2634-9
- Lempert D.B., Raznoschikov V.V., Aver'kov I.S., Yanovskiy L.S. High-enthalpy organic components as dispersants of solid fuel ducted rockets. Proceedings of the 23rd Seminar on New Trends in Research of Energetic Materials (April, 1-3, 2020, Czech Republic, Pardubice). P. 156-163.
- Raznoschikov V.V. Systematic analysis of fuel consumption in aviation power plants. All-Russian Scientific-Technical Journal «Polyot». 2008. No. 4. P. 28-32. (In Russ.)
- Antonov A.V. Sistemnyy analiz [System analysis]. Moscow: Vysshaya Shkola Publ., 2004. 454 p.
- Raznoschikov V.V., Yanovskiy L.S., Zagumennov V.V. Khimmotologicheskiy analiz i metodika proektirovaniya aviatsionnykh kriogennykh toplivnykh sistem samoletov. V kn.: «Mezhdunarodnaya entsiklopediya CALS-tekhnologiy. Aviatsionno-kosmicheskoe mashinostroenie». Moscow: NITs ASK Publ., 2015. P. 471-475. (In Russ.)
- Reznikov M.E. Aviatsionnye topliva i smazoshnye materialy (aviatsionnaya khimmotologiya): uchebnoe posobie [Aviation fuels and lubricants (aviation chemmotology): tutorial]. Moscow: Voennoe Izdatel’stvo Ministerstva Oborony Rossii Publ., 2003. 234 p.
- Dubovkin N.F., Yanovskiy L.S., Kharin A.A., Shevchenko I.V., Verkholomov V.K., Surikov E.V. Topliva dlya vozdushno-reaktivnykh dvigateley [Fuels for air-jet engines]. Moscow: MATI – Russian State Technological University Publ., 2005. 443 p.
- Butov A.M., Kozarev L.A. Matematicheskoe modelirovanie rabochego protsessa aviatsionnykh dvigateley: uchebnoe posobie [Mathematical modeling of working process of aircraft engines. Tutorial]. Moscow: Voenno-vozdushnaya Inzhenernaya Akademiya imeni N.E. Zhukovskogo Publ., 1993. 143 p.
- Egorov I.N., Kretinin G.V., Leshchenko I.A., Kuptsov S.V. Stochastic optimization of aviation gas turbine engines using mathematical models based on artificial neural networks. Vestnik Akademii Nauk Aviatsii i Vozdukhoplavaniya. 2002. No. 1. P. 44-48. (In Russ.)
- Egorov I.N., Tyulenev V.P., Pavlenko V.F. Methods of indirect statistical optimization based on self-organization and their use in the optimization tasks of aviation GTE. No. 2622-V89, 1989. (In Russ., unpubished)
Supplementary files
