SELF-ADJUSTABLE AIR INTAKE Russian patent published in 2001 - IPC

Abstract RU 2171211 C2

FIELD: air intakes for air-jet engines of flying vehicles at extended range of flight speeds. SUBSTANCE: supersonic air intake includes additional passage having inlet in supersonic zone and outlet in subsonic zone. Additional passage has swivel panel with axis of rotation located in front of flow. Swivel panel is mounted on far side of air intake from center of cross section. EFFECT: possibility of self-adjusting of flow section to present velocity of incoming flow and amount of back pressure. 4 cl, 7 dwg

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RU 2 171 211 C2

Authors

Medvedev V.T.

Dates

2001-07-27—Published

1997-12-29—Filed