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1. WO2020107091 - AIRCRAFT

Publication Number WO/2020/107091
Publication Date 04.06.2020
International Application No. PCT/BY2019/000017
International Filing Date 25.11.2019
IPC
B64C 31/036 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
31Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
028Hang-glider-type aircraft; Microlight-type aircraft
036having parachute-type wing
B64D 17/78 2006.01
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
17Parachutes
78in association with other load-retarding apparatus
CPC
B64C 31/036
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
31Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
028Hang-glider-type aircraft; Microlight-type aircraft
036having parachute-type wing
B64D 17/78
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
17Parachutes
78in association with other load-retarding apparatus
Applicants
  • ДАВЫДОВ, Владимир Александрович DAVIDOFF, Vladimir Aleksandrovich [BY]/[BY]
Inventors
  • ДАВЫДОВ, Владимир Александрович DAVIDOFF, Vladimir Aleksandrovich
Priority Data
a 2018049330.11.2018BY
Publication Language Russian (RU)
Filing Language Russian (RU)
Designated States
Title
(EN) AIRCRAFT
(FR) AÉRONEF
(RU) ЛЕТАТЕЛЬНЫЙ АППАРАТ
Abstract
(EN)
The invention relates to the field of heavier-than-air aircraft, aeroplanes and unmanned aircraft, and more particularly to emergency rescue systems. The aim of the invention is achieved by means of an aircraft consisting of a propulsion system, a parachute, and a body, wherein the parachute is configured in a fixed form in a permanently open state and is connected to the body by rigid struts. In addition, the centre of gravity of the aircraft is lower than the aerodynamic centre of the aircraft.
(FR)
L’invention concerne le domaine des aéronefs plus lourds que l’air, des avions, des drones, et notamment des systèmes de sauvetage d’urgence. L’objectif technique est réalisé en ce qu’on connaît un aéronef constitué d’un groupe moteur, d’un parachute, d’un corps. Le parachute est réalisé avec une forme fixe à l’état ouvert en permanence, est relié au corps au moyen de haubans rigides. Le centre de gravité de l’aéronef se trouve plus base que le foyer aérodynamique de l’aéronef.
(RU)
Изобретение относится к области летательных аппаратов тяжелее воздуха, к самолетам и беспилотным летательным аппаратам, в частности системам аварийного спасения. Поставленная техническая задача достигается тем, что известен ледательный аппарат, состоящим из силовой установки, парашюта, корпуса. При этом парашют выполнен фиксированной формы в перманентно раскрытом состоянии, соединен с корпусом жесткими подкосами. при этом центр тяжести летательного аппарата находится ниже аэродинамического фокуса летательного аппарата
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