THRUST FORMING METHOD AND DEVICE Russian patent published in 2003 - IPC

Abstract RU 2215890 C2

FIELD: mechanical engineering. SUBSTANCE: invention can be used in design of engines of different application. According to proposed method first of all separate resonance activation of fuel components is carried out and then detonation process is effected by sequential reflections detonation wave from at least two optically intercoupled surfaces. Device is essentially electromagnetic gravity-controlled jet engine in which energy of chemical fuel (propellant and oxidizer) is converted in periodical detonation processes directly into energy of time and space quantized electromagnetic gravity waves. EFFECT: improved possibilities of detonation processes and provision of effective transformation of chemical energy into thrust. 9 cl, 3 dwg

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RU 2 215 890 C2

Authors

Gorjachko I.G.

Dobrosotskij A.V.

Dates

2003-11-10Published

2001-08-13Filed