SELF-ADJUSTABLE AIR INTAKE

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...

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Bibliographische Detailangaben
1. Verfasser:	MEDVEDEV V.T
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	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