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2 811 754

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IPC

B64C13/00(2006-01-01)

B64C19/00(2006-01-01)

G06F11/16(2006-01-01)

G05D1/00(2006-01-01)

(21) (22)

Application

2023112654, 2023-05-16

(24)

Start date

2023-05-16

(22)

Actual filing date

2023-05-16

(45)

Published

2024-01-16

(72)

Inventor

Popov Aleksandr SergeevichMaltsev Aleksandr MikhajlovichElizarov Aleksandr ViktorovichFetisov Evgenij Vyacheslavovich

(73)

Holder

Federalnoe Gosudarstvennoe Kazennoe Voennoe Obrazovatelnoe Uchrezhdenie Vysshego Obrazovaniya Uchebno-Nauchnyj Tsentr Voenno-Vozdushnykh Sil Akademiya Imeni Professora N.E. Zhukovskogo I Yu.A. Gagarina" Voronezh) Ministerstva Oborony Rossijskoj Federatsii

CONTROL DEVICE FOR MULTI-SECTION AIRCRAFT RUDDER DRIVES Russian patent published in 2024 - IPC B64C13/00 B64C19/00 G06F11/16 G05D1/00

Abstract RU 2811754 C1

FIELD: aircraft engineering.

SUBSTANCE: control device for multi-section rudder drives of an aircraft contains K sensors for monitoring aircraft parameters, connected by a common data bus to N rudder section servo units, each containing a rudder section drive with a rudder section angular position sensor and a computer, including a control module, a control command generation module, and a majority sampling control module connected in a certain way.

EFFECT: improved stability and controllability of the aircraft in case of failure/jamming of the rudder section is ensured by generating individual control commands for each serviceable section of the multi-section rudder, taking into account the angular position of the failed section.

1 cl, 1 dwg

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RU 2 811 754 C1

Authors

Popov Aleksandr Sergeevich

Maltsev Aleksandr Mikhajlovich

Elizarov Aleksandr Viktorovich

Fetisov Evgenij Vyacheslavovich

Dates

2024-01-16—Published

2023-05-16—Filed