TWO-LOOP TURBOJET ENGINE Russian patent published in 1995 - IPC

Abstract RU 2029881 C1

FIELD: aircraft engineering. SUBSTANCE: inlet fairing and fairing positioned downstream of the turbine are mounted for rotation and provided with curved blades. The periphery ends of the blades follow profile of corresponding fairing. EFFECT: improved design. 1 dwg

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RU 2 029 881 C1

Authors

Sheremeev Evgenij Ivanovich

Dates

1995-02-27—Published

1992-01-03—Filed