Combined jet engine with RAM jet and turbojet

Power plants – Reaction motor – Interrelated reaction motors

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Details

60244, 137 151, F02K 716

Patent

active

053478070

ABSTRACT:
A jet engine includes a gas turbine, peripheral ramjet channels located oide the gas turbine and including burners wherein a gas circulation stream in the engine is subdivided over part of its length into a central turbojet stream which flows through the gas turbine, the peripheral ramjet channels and peripheral discharge channels terminating by flowing into a part of the gas circulation stream downstream of the turbine. A plurality of flaps are provided for opening and closing the central stream. A ring surrounds the central stream and extends in front of part of the peripheral discharge channels and ramjet channels. A motor is also provided for rotating the ring wherein the ring has a plurality of slots formed therein, the channels being arranged such that the slots successfully pass, during rotation of the ring in a continuous direction, in front of the discharge channels only, then in front of none of the channels and then in front of the ramjet channels only.

REFERENCES:
patent: 3153904 (1964-10-01), Ellis et al.
patent: 3938328 (1976-02-01), Klees
patent: 4909031 (1990-03-01), Grieb
patent: 4919364 (1990-04-01), John et al.
patent: 5058378 (1991-10-01), Enderle
patent: 5105615 (1992-04-01), Herzog
patent: 5148673 (1992-09-01), Enderle

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