TWO-LOOP TURBO-JET ENGINE Russian patent published in 1995 - IPC

Abstract RU 2033550 C1

FIELD: aircraft engineering. SUBSTANCE: engine has outer and internal housings 1,5 with inlet and outlet units 2,3. Fan 3 is positioned inside inlet unit 2. Compressor 6, combustion chamber 7, and gas turbine 9 are positioned inside the internal housing. The heat-exchanger-evaporator is positioned above the gas turbine whereto the inlet of the steam turbine is connected. The condenser of turbine 9 is constructed as an air condenser made up as a space interposed between the wall of outer housing 1 and corrugated baffle. EFFECT: enhanced efficiency. 2 dwg

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RU 2 033 550 C1

Authors

Boboed Nikolaj Timofeevich[By]

Dates

1995-04-20—Published

1991-10-08—Filed