SUPERSONIC MULTI-PURPOSE AIRCRAFT

FIELD: aviation. ^ SUBSTANCE: proposed aircraft has fuselage, wing, main power plant with two turbo-jet engines 1, auxiliary power plant 2, fin assembly and side air intakes. Power plant 2 includes two supersonic turbo-jet engines 1 which are mounted in widened tail section of fuselage for placing f...

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Bibliographische Detailangaben
Hauptverfasser:	MATVEEV ANDREJ IVANOVICH, GURTOVOJ ARKADIJ IOSIFOVICH, DEMCHENKO OLEG FEDOROVICH, POPOVICH KONSTANTIN FEDOROVICH, SHKOLIN VLADIMIR PETROVICH, KODOLA VALERIJ GRIGOR'EVICH, DOLZHENKOV NIKOLAJ NIKOLAEVICH, AGAPOV SERGEJ STEPANOVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	FIELD: aviation. ^ SUBSTANCE: proposed aircraft has fuselage, wing, main power plant with two turbo-jet engines 1, auxiliary power plant 2, fin assembly and side air intakes. Power plant 2 includes two supersonic turbo-jet engines 1 which are mounted in widened tail section of fuselage for placing fin assembly root in between them. Auxiliary power plant 2 is located at the bottom of center section of fuselage behind pilot cabin. Inlet openings of air intakes are made under wing and are bounded by fuselage in lower parts. Wing is provided with controllable slotted louvres in upper part of air intakes for air replenishment. Boundary layer drainage slots are made between upper edge of air intakes and lower surface of wing. ^ EFFECT: enhanced efficiency of multi-purpose supersonic aircraft. ^ 3 cl, 4 dwg