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Title:
COMBINED MAGNET-GAS-DYNAMIC RAMJET ENGINE
Document Type and Number:
WIPO Patent Application WO/1998/037323
Kind Code:
A1
Abstract:
The combined magnet-gas-dynamic ramjet engine is designed for use in hypersonic and aerospace planes. This engine comprises supersonic and hypersonic engine modules as well as magnet-hydro-dynamic (MHD) generators and magnet-hydro-dynamic (MHD) accelerators electrically interconnected and installed on overhead circuits of mixed modules with mutually opposed polarities. The energy exchange chambers of the MHD generators and MHD accelerators are divided by two electrically insulating walls which present windows (fig. 4) on which are mounted controlled panels (fig. 5) allowing for the energy exchange process to be implemented between the MHD converters. Magnet-gas-dynamic means are used to raise the operation speed limitation of the hypersonic statoreactor by increasing the flight Mac numbers from 8-10 to 20-25.

Inventors:
KOROLEV ANATOLY GRIGORIEVICH (RU)
AKSENTY YURY VALENTINOVICH (RU)
Application Number:
PCT/RU1997/000045
Publication Date:
August 27, 1998
Filing Date:
February 25, 1997
Export Citation:
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Assignee:
KOROLEV ANATOLY GRIGORIEVICH (RU)
AKSENTY YURY VALENTINOVICH (RU)
International Classes:
F02K7/10; F03H1/00; H02K44/04; H02K44/08; (IPC1-7): F02K7/10; F03H1/00
Foreign References:
FR2692938A11993-12-31
FR2629873A11989-10-13
GB1303123A1973-01-17
US3436918A1969-04-08
US5211006A1993-05-18
Other References:
A.R.I. KURZINER, "Jet Enginer for High Supersonic Flight Speeds", MOSCOW, MACHINE CONSTRUCTION PUBLISHERS, 1997, pages 119-132.
E. TERIEVA, "A 21st Century Aircraft", SCIENCE AND LIFE, MOSCOW, 1993, No. 8, pages 12-13.
Attorney, Agent or Firm:
Romanov, Vladimir Fedorovich (18-22 Mytischi-5, 5, RU)
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