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2 461 494

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IPC

B64C39/10(2006-01-01)

(21) (22)

Application

2010142153/11, 2010-10-15

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Start date

2010-10-15

(22)

Actual filing date

2010-10-15

(45)

Published

2012-09-20

(72)

Inventor

Barkovskij Vladimir IvanovichFedorenko Gennadij AndreevichPavlenko Aleksandr AlekseevichPavlovets Gennadij AndreevichKul'Tin Viktor GeorgievichNilov Viktor AleksandrovichSidorov Vladimir Alekseevich

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Aehrogidrodinamicheskij Institut Imeni Professora N.E. Zhukovskogo"Otkrytoe Aktsionernoe Obshchestvo Samoletostroitel'Naja Korporatsija

DRONE AIRCRAFT Russian patent published in 2012 - IPC B64C39/10

Abstract RU 2461494 C2

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering. Proposed drone comprises wing with integral high-sweep leading edge and low-sweep trailing edge, twin-finned tail, rudders on the latter and tail elevens. Fins are dropped to drone mirror plane at angle Ψ to vertical exceeding 45° are jointed at tail cross-section. Tail trailing edge makes with wing leading edge the angle φ≈92-95°. Rudders and elevens are used as controls.

EFFECT: higher efficiency of controls.

8 dwg

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RU 2 461 494 C2

Authors

Barkovskij Vladimir Ivanovich

Fedorenko Gennadij Andreevich

Pavlenko Aleksandr Alekseevich

Pavlovets Gennadij Andreevich

Kul'Tin Viktor Georgievich

Nilov Viktor Aleksandrovich

Sidorov Vladimir Alekseevich

Dates

2012-09-20—Published

2010-10-15—Filed