FIELD: aircraft industry; ramjet engines.
SUBSTANCE: proposed method of organization of combustion hypersonic ramjet engine comes to delivery of fuel into combustion chamber before air intake in zone formed between fuel nozzle, pylons and air intake. For this purpose fuel nozzle is arranged in nose part of engine before air intake along its axis and is connected with air intake by pylons.
EFFECT: improved mixing of fuel components providing in its turn complete combustion of fuel, improved stabilization of process of combustion in combustion chamber of hypersonic ramjet engine.
4 cl, 1 dwg
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Authors
Dates
2005-10-10—Published
2003-10-20—Filed