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1. WO2022005328 - DEVICE FOR CONVERTING THE VIBRATIONS OF AN AIRCRAFT WING SURFACE INTO ELECTRICAL ENERGY

Publication Number WO/2022/005328
Publication Date 06.01.2022
International Application No. PCT/RU2021/050026
International Filing Date 03.02.2021
IPC
B64D 41/00 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
41Power installations for auxiliary purposes
F03D 9/00 2016.1
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
DWIND MOTORS
9Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
F03D 5/06 2006.1
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
DWIND MOTORS
5Other wind motors
06the wind-engaging parts swinging to-and-fro and not rotating
B64C 3/00 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
3Wings
F03G 7/08 2006.1
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
GSPRING, WEIGHT, INERTIA, OR LIKE MOTORS; MECHANICAL-POWER-PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
7Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
08recovering energy derived from swinging, rolling, pitching, or like movements, e.g. from the vibrations of a machine
Applicants
  • СЕНЧЕНКО, Александр Михайлович SENCHENKO, Aleksandr Mikhailovich [RU]/[RU]
Inventors
  • СЕНЧЕНКО, Александр Михайлович SENCHENKO, Aleksandr Mikhailovich
Agents
  • НЮХОВСКИЙ, Вячеслав Анатольевич NYUHOVSKIJ, Vyacheslav Anatolevich
Priority Data
202012198702.07.2020RU
Publication Language Russian (ru)
Filing Language Russian (RU)
Designated States
Title
(EN) DEVICE FOR CONVERTING THE VIBRATIONS OF AN AIRCRAFT WING SURFACE INTO ELECTRICAL ENERGY
(FR) DISPOSITIF DE CONVERSION DES OSCILLATIONS D'UNE AILE EN ÉNERGIE ÉLECTRIQUE
(RU) УСТРОЙСТВО ДЛЯ ПРЕОБРАЗОВАНИЯ КОЛЕБАНИЙ КРЫЛА В ЭЛЕКТРИЧЕСКУЮ ЭНЕРГИЮ
Abstract
(EN) A device for supplying additional electrical energy to the power system of an aircraft is provided with at least one flexible element arranged along the length of the wing of an aircraft and fastened by one end to said wing, the second end being connected to a drive for rotating the shaft of a generator that generates electrical energy for the power system of the aircraft, wherein the flexible element is arranged along the length of the wing of the aircraft such that the second end is capable of moving as a result of a difference in the bending radius (R1) of the wing and the bending radius (R2) of the flexible element when the wing vibrates during movement of the aircraft.
(FR) L'invention concerne un dispositif de fourniture d'énergie électrique auxiliaire vers un système d'alimentation électrique d'un aéronef, lequel comprend au moins un élément flexible disposé le long de la longueur de l'aile de l'aéronef, qui est fixé par une extrémité à ladite aile et par l'autre extrémité à un actionneur, et qui assure la rotation d'un arbre de générateur d'énergie électrique pour un système d'alimentation électrique de l'aéronef; l'élément flexible est disposé le long de la longueur de l'aile de l'aéronef de manière à déplacer l'autre extrémité du fait de la différence entre le rayon de courbure (R1) de l'aile et le rayon de courbure (R2) de l'élément flexible lors d'une oscillation de l'aile pendant le déplacement de l'aéronef.
(RU) Устройство для подачи дополнительной электрической энергии в систему энергоснабжения летательного аппарата снабжено по меньшей мере одним гибким элементом, расположенным вдоль длины крыла летательного аппарата, прикрепленным одним концом к упомянутому крылу и соединенным другим концом с приводом, обеспечивающему вращение вала генератора электрической энергии для системы энергоснабжения летательного аппарата, при этом гибкий элемент расположен вдоль длины крыла летательного аппарата с возможностью перемещения другого конца из-за разницы в радиуса (R1) изгиба крыла и радиуса (R2) изгиба гибкого элемента при колебаниях крыла во время движения летательного аппарата.
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