FLYING VEHICLE

FIELD: aeronautical engineering.SUBSTANCE: proposed flying vehicle has fuselage, wing with extensions-vortex generators with swept-forward and swept-back edges and additional vortex generator mounted in nose section of fuselage and high-lift devices for wing leading edge.EFFECT: extended range of an...

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Hauptverfasser:	Andreev Jurij Vasil'evich, Demidov Boris Fedorovich, Lebed' Nina Klement'evna, Val'denberg Mikhail Romanovich, Chernigovskij Valentin Iovich, Golovkin Mikhail Alekseevich, Vozhdaev Evgenij Semenovich, Bjushgens Georgij Sergeevich, Mikeladze Vitalij Georgievich, Dolzhenko Nikolaj Nikolaevich, Golovkin Vladimir Alekseevich, Pjatakhin Valentin Ivanovich, Sedov Grigorij Aleksandrovich
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COSMONAUTICS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HELICOPTERS PERFORMING OPERATIONS TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE TRANSPORTING
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Beschreibung
Zusammenfassung:	FIELD: aeronautical engineering.SUBSTANCE: proposed flying vehicle has fuselage, wing with extensions-vortex generators with swept-forward and swept-back edges and additional vortex generator mounted in nose section of fuselage and high-lift devices for wing leading edge.EFFECT: extended range of angles of attack.3 dwg Изобретение относится к области авиационной техники. Летательный аппарат содержит корпус, крыло с наплывами-генераторами вихрей с кромками прямой и обратной стреловидности, а также дополнительный генератор вихрей, установленный в носовой части корпуса, и механизацией по передней кромке крыла. Технический результат - расширение эксплуатационного диапазона углов атаки. 3 ил.