Processing

Please wait...

Settings

Settings

Goto Application

1. WO2022211406 - UNMANNED FLIGHT DEVICE USING HYBRID PROPULSION DEVICE AND HYBRID PROPULSION DEVICE

Publication Number WO/2022/211406
Publication Date 06.10.2022
International Application No. PCT/KR2022/004307
International Filing Date 28.03.2022
IPC
B64D 27/16 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
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
02Aircraft characterised by the type or position of power plant
16of jet type
B64C 39/02 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
B64C 29/00 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
29Aircraft capable of landing or taking-off vertically
B64D 27/02 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
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
02Aircraft characterised by the type or position of power plant
CPC
B64C 29/00
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
29Aircraft capable of landing or taking-off vertically
B64C 39/02
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
B64D 27/02
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
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
02Aircraft characterised by the type or position of power plant
B64D 27/16
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
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
02Aircraft characterised by the type or position of power plant
16of jet type
Applicants
  • 탁승호 TAK, Seung-Ho [KR]/[KR]
Inventors
  • 탁승호 TAK, Seung-Ho
Agents
  • 특허법인 신지 SINJI PATENT FIRM
Priority Data
10-2021-004004328.03.2021KR
10-2021-004308402.04.2021KR
10-2021-004684611.04.2021KR
Publication Language Korean (ko)
Filing Language Korean (KO)
Designated States
Title
(EN) UNMANNED FLIGHT DEVICE USING HYBRID PROPULSION DEVICE AND HYBRID PROPULSION DEVICE
(FR) DISPOSITIF DE VOL SANS PILOTE UTILISANT UN DISPOSITIF DE PROPULSION HYBRIDE ET DISPOSITIF DE PROPULSION HYBRIDE
(KO) 하이브리드 추진장치를 이용한 무인비행장치와 하이브리드 추진장치
Abstract
(EN) An unmanned non-stop flight device according to an aspect of the present invention comprises: a cold jet propulsion device; one or more hybrid propulsion devices including a jet engine propulsion device; and a flight control device. The flight control device vertically takes off and lands by operating the cold jet propulsion device, and flies at a high speed for a long time by operating the jet engine propulsion device. The cold jet propulsion device is a propulsion device that utilizes a disc interface traction effect. The cold jet propulsion device is propelled by discharging compressed high-speed air by rotating a plurality of disks spaced apart from each other at regular intervals. The jet engine propulsion device propels an engine by discharging a high-temperature gas generated by burning fuel inside the engine.
(FR) Un dispositif de vol sans escale sans pilote selon un aspect de la présente invention comprend : un dispositif de propulsion à jet froid ; un ou plusieurs dispositifs de propulsion hybride comprenant un dispositif de propulsion de moteur à réaction ; et un dispositif de commande de vol. Le dispositif de commande de vol décolle et atterrit verticalement en actionnant le dispositif de propulsion à jet froid, et vole à grande vitesse pendant une longue période en actionnant le dispositif de propulsion de moteur à réaction. Le dispositif de propulsion à jet froid est un dispositif de propulsion qui utilise un effet de traction d'interface de disque. Le dispositif de propulsion à jet froid est propulsé par évacuation d'air comprimé à grande vitesse par rotation d'une pluralité de disques espacés les uns des autres à des intervalles réguliers. Le dispositif de propulsion de moteur à réaction propulse un moteur par évacuation d'un gaz à haute température généré par combustion de carburant à l'intérieur du moteur.
(KO) 본 발명의 일 양상에 따른 무인무정지비행장치는 콜드제트 추진장치와, 제트엔진 추진장치를 포함하는 하나 이상의 하이브리드 추진장치와, 비행제어 장치를 포함한다. 비행제어 장치는 콜드제트 추진장치를 가동시켜 수직으로 이착륙하며, 제트엔진 추진장치를 가동시켜 장시간 고속 비행한다. 콜드제트 추진장치는 디스크 경계면 견인효과를 이용하는 추진장치이다. 콜드제트 추진장치는 일정한 간격으로 서로 이격된 복수의 디스크를 회전시켜 압축된 고속의 공기를 배출하여 추진한다. 제트엔진 추진장치는 엔진 내부에서 연료를 연소시켜 발생된 고온의 가스를 배출하여 추진한다.
Latest bibliographic data on file with the International Bureau