Multifunctional aircraft with reduced radar visibility

The invention relates to the aircraft industry field, in particular to tactical aviation aircraft providing for the detection and striking of air, above-water and land-based targets. The technical result to which the invention is directed consists in reducing the radar visibility size of an aircraft...

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Hauptverfasser: LEBEDEV ROMAN STANISLAVOVICH, DAVIDENKO ALEKSANDR NIKOLAEVICH, GAVRIKOV ANDREY YUR EVICH, RUNISCHEV VLADIMIR ALEKSANDROVICH, KONONOV DMITRY GERMANOVICH, LOG ARKOV ANDREY NIKOLAEVICH, STRELETS MIHAIL YURIEVICH, POLYAKOVA NATAL YA BORISOVNA, BOYKO MIHAIL ALEKSEEVICH, EROFEEV VASILY SERGEEVICH, FEDORENKO ANATOLY IVNOVICH, BIBIKOV SERGEY YURIEVICH, VASIL EV MIHAIL BORISOVICH
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:The invention relates to the aircraft industry field, in particular to tactical aviation aircraft providing for the detection and striking of air, above-water and land-based targets. The technical result to which the invention is directed consists in reducing the radar visibility size of an aircraft to an average size of the order of 0.1-1 m2. The aircraft comprises a fuselage (1), wings (2), all-flying vertical fin (AFVF) panels (3), all-flying horizontal fin (AFHF) panels (4), a cockpit light (5), horizontal lips of engine air intakes (6), fine-meshed screens closing air exhausts (7), lateral inclined lips of engine air intakes (8), a device reducing the effective scattering surface (ESS) of the power plant (9), and compartment flaps for a probe for in-flight refuelling (10). To provide for specified levels of an effective scattering surface (ESS) on the aircraft, a set of measures is carried out in relation to the airframe; to the power plant; to optical and antenna systems of a set of onboard equipment; and to equipment which is suspended and is extendible during flight.