Научная электронная библиотека ULRICH'S Periodicals Directory

Сибирский государственный университет
науки и технологий имени академика М.Ф. Решетнева

Сибирский аэрокосмический журнал
ISSN 2712-8970 (Print) ISSN 2782-5760 (on-line)

Сведения об образовательной организации

UDK 621.182.233
INFLUENCE OF DESIGN PARAMETERS OF A FLOW REGULATOR ON ITS STATIC AND DYNAMIC CHARACTERISTICS
E. N. Beliaev [1], A. I. Kolomentsev [1], L. B. Nascimento [2], V. P. Nasarov [3]
[1]Moscow Aviation Institute (national research university) 4, Volokolamskoe sh., Moscow, 125993, Russian Federation E-mail: kaf202@mai.ru [2]Technological Institute of Aeronautics 50, Marechal Eduardo Gomes sq., Sao Jose dos Campos, 12228-900, Brazil E-mail: ips@ita br [3] Siberian State Aerospace University named after academician M. F. Reshetnev 31, Krasnoyarsky Rabochy Av., Krasnoyarsk, 660014, Russian Federation, Е-mail: dla@sibsau.ru
This article is dedicated to a theoretical analysis of the influence of geometrical and mechanical parameters of the direct action flow regulator used in LRE on its static and dynamic characteristics. The investigation was conducted using a lumped-parameter mathematical model. It was showed, that the region dependently of the pressure drop in flow regulator, which the static characteristic is positive, is expanded when using the triangular geometry for the orifices of regulation, which is very important, specially, for multi-regimes LRE. For this geometric form orifice, the hydraulic force, which depends of the flow rate and the pressure drop in these orifices, and the thickness of the slide valve, have less influence in the positive behavior of the static characteristic of the regulator. The dynamic characteristics of the flow regulator, calculated in the technical system, are widely defined by the area of the piston and the area of the damping orifices.
regulator, static characteristic, hydraulic force, slide valve.
References

1. Belyaev E. N., Chervakov V. V. Matematicheskoe modelirovanie ZhRD (Mathematical modeling of LPRE). Moscow, MAI-PRINT Publ., 2009, 280 p.

2. Belyaev E. N, Chvanov V. K., Chervakov V. V. Matematicheskoe modelirovanie rabochego processa zhidkostnyh raketnyh dvigatej (Mathematical modeling of the work process in liquid-propellant rocket engine), edited V. K. Chvanova. Moscow, MAI Publ., 1999, 228 p.

3. Glikman B. F. Avtomaticheskoe regulirovanie zhidkostnyh raketnyh dvigatelej (Automatic regulation of liquid-propellant rocket engine). Moscow, Mashinostroenie Publ., 1974, 396 p.

4. Zenin E. S., Men'shikova O. M., Fedotchev V. A. [Mathematical model of regulators of LPRE]. Polet. 2013,
no. 5, p. 20–24.

5. Lebedinsky E. V., Mosolov S. V., Kalmykov G. P. et al. Komp'juternye modeli zhidkostnyh raketnyh dvigatelej (Computer models of liquid-propellant rocket engine). Moscow, Mashinostroenie Publ., 2009, 375 p.

6. Sheviakov A. A., Kalnin V. M., Naumenkova N. V. et al. Avtomaticheskoe upravlenie raketnymi dvigatejami (Automatic control of rocket engines). Moscow, Mashinostroenie Publ., 1978, 290 p.


Belyaev Evgeny Nikolaevich – Candidate of Engineering Science, associate professor, Moscow Aviation Institute. E-mail: kaf202@mail.ru

Kolomentsev Alexander Ivanovich – Candidate of Engineering Science, professor of Moscow Aviation Institute. E-mail: kaf202@mail.ru

Nascimento Leonardo – Master’s degree student, Moscow Aviation Institute. E-mail: kaf202@mail.ru

Nazarov Vladimir Pavlovich – Candidate of Engineering Sciences, professor, head of the Department of Flying vehicles, Siberian State Aerospace University named after academician M. F. Reshetnev. E-mail: dla@sibsau.ru