RAMJET ENGINE Russian patent published in 2018 - IPC F02K7/10 

Abstract RU 2647919 C1

FIELD: engines.

SUBSTANCE: ramjet engine, consisting of input block, diffuser, combustion chamber, output device. At hypersonic speeds of flight (M>5), water is supplied to flow channel. Water is fed through samplers, which are located inside the diffuser, temperature of air-steam mixture is not more than 2,000 K. Increase in the flight speed of the ramjet to seven or eight Mach numbers is achieved.

EFFECT: ramjet can be used to create hypersonic aircraft.

4 cl, 2 dwg

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RU 2 647 919 C1

Authors

Pismennyj Vladimir Leonidovich

Dates

2018-03-21Published

2016-06-20Filed