BOPI 05 BR / 2025 REPERTOIRE NUMERIQUE 20 Fig. 2 ________________________________________ (11) 21898 Consulter le mémoire (51) B64C 1/00 (2023.01); B64C 30/00 (2023.01); B64D 33/02 (2023.01); F02C 7/04 (2023.01) (21) 1202400024 - PCT/RU2022/000206 (22) 29/06/2022 (30) RU n° 2021121246 du 19/07/2021 (54) Multi-Functional Supersonic SingleEngine Aircraft. (72) STRELETS, Mikhail Yurievich (RU) BULATOV, Aleksey Sergeevich (RU) NIKITUSHKIN, Mikhail Viktorovich (RU) STEPANOV, Vladimir Dmitrievich (RU) KONONOV, Dmitriy Germanovich (RU) KRYLOV, Leonid Evgenevich (RU) BARABANOV, Aleksandr Vladimirovich (RU) (73) PUBLIC JOINT STOCK COMPANY ‘‘UNITED AIRCRAFT CORPORATION’’ (PJSC ‘‘UAC’’), Ul. B. Pionerskaya, bld. 1 Moscow, MOSCOW 115054, Russian Federation (RU) (74) PAUL T. JING (JING & Partners), 537, Rue AFCODI, Off Texaco Njo-Njo, Bonapriso, P.O. Box 1245, DOUALA (CM). (57) The invention relates to the aviation field. A multifunctional supersonic single-engine aircraft comprises a fuselage, a tapered wing, an allmoving V-shaped empennage, advanced side beams, lower lateral engine air intake located under the fuselage fore section with a duel extending along the aircraft centerline, central and lateral payload bays, a single-engine power plant comprising an engine with a rotatable propulsive nozzle arranged along the aircraft centerline. The aircraft design provides reduced aircraft dimension and lower weight, reduced aerodynamic drag, reduced RCS and radar signature, high aircraft performance and maneuverable characteristics, outstanding stability and controllability characteristics, enlarged payload bays volume, multi-purpose large-sized loads capacity, as well as multi functional capability of aircraft.
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