Afterburner operating on detonative combustion of liquid jet propulsion fuel

Мұқаба

Дәйексөз келтіру

Толық мәтін

Ашық рұқсат Ашық рұқсат
Рұқсат жабық Рұқсат берілді
Рұқсат жабық Тек жазылушылар үшін

Аннотация

The results of a new series of test fires of a detonation afterburner as part of a small-size turbojet are presented. In contrast to previous tests with a sequential arrangement of turbojet and afterburner, the new series provides for gasdynamic separation of airflows: air was supplied to the afterburner separately using an auxiliary power unit. The separation of airflows made it possible to ensure the stable operation of the combined power plant in different modes of operation of the turbojet when the afterburner was turned on. In the test fires, a stable mode of spinning detonation of aviation kerosene with single detonation wave was registered and the detonative combustion of kerosene in the afterburner did not affect turbojet operation.

Толық мәтін

Рұқсат жабық

Авторлар туралы

Sergey Frolov

N. N. Semenov Federal Research Center for Chemical Physics of the Russian Academy of Sciences

Хат алмасуға жауапты Автор.
Email: smfrol@chph.ras.ru

Doctor of Science in physics and mathematics, head of department, head of laboratory

Ресей, 4 Kosygin Str., Moscow 119991

Vladislav Ivanov

N. N. Semenov Federal Research Center for Chemical Physics of the Russian Academy of Sciences

Email: ivanov.vls@gmail.com

Doctor of Science in physics and mathematics, leading research scientist

Ресей, 4 Kosygin Str., Moscow 119991

Igor Shamshin

N. N. Semenov Federal Research Center for Chemical Physics of the Russian Academy of Sciences

Email: igor_shamshin@mail.ru

Candidate of Science in physics and mathematics, leading research scientist

Ресей, 4 Kosygin Str., Moscow 119991

Victor Aksenov

N. N. Semenov Federal Research Center for Chemical Physics of the Russian Academy of Sciences

Email: v.aksenov@mail.ru

Candidate of Science in physics and mathematics, senior research scientist

Ресей, 4 Kosygin Str., Moscow 119991

Mikhail Vovk

A. Lyulka Design Bureau

Email: mihail.vovk@okb.umpo.ru

Candidate of Science in technology, deputy chief designer, head of department, PJSC UEC-UMPO

Ресей, 13 Kasatkina Str., Moscow 129301

Igor Mokrynskij

A. Lyulka Design Bureau

Email: igor.mokrynskij@okb.umpo.ru

head of department, PJSC UEC-UMPO

Ресей, 13 Kasatkina Str., Moscow 129301

Vladislav Bruskov

MU 15650-16

Email: smfrol@chph.ras.ru

Candidate of Science in technology, head of directorate

Ресей, Shchelkovo-10, Moscow Region 141110

Dmitry Igonkin

MU 15650-16

Email: smfrol@chph.ras.ru

senior test engineer

Ресей, Shchelkovo-10, Moscow Region 141110

Sergei Moskvitin

MU 15650-16

Email: smfrol@chph.ras.ru

senior test engineer

Ресей, Shchelkovo-10, Moscow Region 141110

Anatoly Illarionov

MU 15650-16

Email: smfrol@chph.ras.ru

head of department

Ресей, Shchelkovo-10, Moscow Region 141110

Evgenii Marchukov

Moscow Aviation Institute (National Research University)

Email: okb@okb.umpo.ru

Doctor of Science in technology, professor, head of department

Ресей, 4 Volokolamskoe Sh., Moscow 125993

Әдебиет тізімі

  1. Frolov, S. M., V. S. Ivanov, I. O. Shamshin, V. S. Aksenov, M. Yu. Vovk, I. V. Mokrynskij, V. A. Bruskov, D. V. Igonkin, S. N. Moskvitin, A. A. Illarionov, and Marchukov E. Yu. 2020. A detonation afterburner. Dokl. Phys. 65(1):36–39. doi: 10.1134/S1028335820010061.
  2. Frolov, S. M., V. S. Aksenov, P. A. Gusev, V. S. Ivanov, S. N. Medvedev, and I. O. Shamshin. 2014. Experimental proof of the energy efficiency of the Zel’dovich thermodynamic cycle. Dokl. Phys. Chem. 459(2):207–211. doi: 10.1134/S0012501614120057.
  3. Dubrovskii, A. V., V. S. Ivanov, A. E. Zangiev, and S. M. Frolov. 2016. Three-dimensional numerical simulation of the characteristics of a ramjet power plant with a continuous-detonation combustor in supersonic flight. Russ. J. Phys. Chem. B 10(3):469–482. doi: 10.1134/S1990793116030179.
  4. Ivanov, V. S., S. S. Sergeev, S. M. Frolov, Yu. M. Mironov, A. E. Novikov, and I. I. Schulz. 2020. Izmerenie davleniya v netpreryvno-detonatsionnykh kamerakh sgoraniya [On pressure measurements in continuous-detonation combustors]. Goren. Vzryv (Mosk.) — Combustion and Explosion 13(1):55–65. doi: 10.30826/CE20130106.
  5. Frolov, S. M., V. S. Aksenov, A. V. Dubrovskii, A. E. Zangiev, V. S. Ivanov, S. N. Medvedev, and I. O. Shamshin. 2015. Chemiionization and acoustic diagnostics of the process in continuous- and pulse-detonation combustors. Dokl. Phys. Chem. 465(1):273–278. doi: 10.1134/S0012501615110019.

Қосымша файлдар

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Әрекет
1. JATS XML
2. Figure 1 Photograph of the turbojet–detonation afterburner assembly in one of the test fires

Жүктеу (130KB)
3. Figure 2 Records of pressure pulsation sensor in a test fire

Жүктеу (70KB)

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