Processing

Please wait...

Settings

Settings

Goto Application

1. WO2020141567 - MANNED AIRCRAFT

Publication Number WO/2020/141567
Publication Date 09.07.2020
International Application No. PCT/JP2019/000001
International Filing Date 01.01.2019
IPC
B64C 27/08 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
08with two or more rotors
B64C 29/02 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
29Aircraft capable of landing or taking-off vertically
02having its flight directional axis vertical when grounded
B64C 39/02 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
CPC
B64C 27/08
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
08with two or more rotors
B64C 27/28
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
22Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
28with forward-propulsion propellers pivotable to act as lifting rotors
B64C 29/02
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
29Aircraft capable of landing or taking-off vertically
02having its flight directional axis vertical when grounded
B64C 39/02
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
Applicants
  • 株式会社エアロネクスト AERONEXT INC. [JP]/[JP]
Inventors
  • 鈴木 陽一 SUZUKI Yoichi
Agents
  • 特許業務法人iPLAB Startups PATENT FIRM IPLAB STARTUPS
Priority Data
Publication Language Japanese (JA)
Filing Language Japanese (JA)
Designated States
Title
(EN) MANNED AIRCRAFT
(FR) AÉRONEF PILOTÉ
(JA) 有人飛行体
Abstract
(EN)
[Problem] To provide an aircraft that can safely and efficiently transition from hovering to horizontal flight. [Solution] This aircraft comprises: a lift generation part such as a main wing; a thrust generation part that makes it possible to achieve flight and hovering; and a connection part that displaceably connects the lift generation part and the thrust generation part such that the lift generation part can maintain a positive angle of attack relative to a flight direction, at least during hovering. Said configuration makes it possible to transition safely from hovering to horizontal flight.
(FR)
Le problème décrit par la présente invention est de fournir un aéronef qui peut effectuer une transition sûre et efficace d'un vol stationnaire à un vol horizontal. La solution selon l'invention porte sur un aéronef comprenant : une partie de génération de portance telle qu'une aile principale ; une partie de génération de poussée qui permet d'obtenir un vol et un vol stationnaire ; et une partie de liaison qui relie de manière mobile la partie de génération de portance et la partie de génération de poussée de telle sorte que la partie de génération de portance peut maintenir un angle d'attaque positif par rapport à une direction de vol, au moins pendant le vol stationnaire. Cette configuration permet d'effectuer une transition en toute sécurité d'un vol stationnaire à un vol horizontal.
(JA)
【課題】ホバリングから水平飛行への効率的かつ安全な移行を可能にした飛行体を提供する。 【解決手段】本発明による飛行体は、主翼などの揚力発生部と、飛行及びホバリング可能な推力発生部と、少なくともホバリング時において揚力発生部が飛行方向に対して正の迎角を維持可能となるように、記揚力発生部及び前記推力発生部を変位可能に接続する接続部とを備えている。かかる構成により、ホバリング時から水平飛行移行へと安全に移行することができる。
Related patent documents
EP2019907452This application is not viewable in PATENTSCOPE because the national phase entry has not been published yet or the national entry is issued from a country that does not share data with WIPO or there is a formatting issue or an unavailability of the application.
Latest bibliographic data on file with the International Bureau