Processing

Please wait...

Settings

Settings

Goto Application

1. JP2020108997 - MANNED FLIGHT VEHICLE

Office
Japan
Application Number 2019175460
Application Date 26.09.2019
Publication Number 2020108997
Publication Date 16.07.2020
Publication Kind A
IPC
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 27/08
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
08with two or more rotors
B64C 27/26
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
26characterised by provision of fixed wings
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
Applicants AERONEXT INC
株式会社エアロネクスト
Inventors SUZUKI YOICHI
鈴木 陽一
Title
(EN) MANNED FLIGHT VEHICLE
(JA) 有人飛行体
Abstract
(EN)

PROBLEM TO BE SOLVED: To provide a flight vehicle which is allowed to efficiently and safely transfer from hovering to horizontal flight.

SOLUTION: A flight vehicle 1 is equipped with lift generation parts 100 such as main wings, thrust generation parts 104 that enable the vehicle to fly and hover, and a connection part that connects the lift generation parts to the thrust generation parts in a manner of capable of displacing, so that the lift generation parts can keep positive angles of attack with respect to a flight direction at least during hovering. This configuration enables the vehicle to safely transfer from hovering to horizontal flight.

SELECTED DRAWING: Figure 1

COPYRIGHT: (C)2020,JPO&INPIT

(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】飛行体1は、主翼などの揚力発生部100と、飛行及びホバリング可能な推力発生部104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。
【選択図】図1

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.