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1. JPWO2020141567 - 有人飛行体

Office
Japan
Application Number 2019540129
Application Date 01.01.2019
Publication Number WO2020141567
Publication Date 15.11.2019
Grant Number 6613423
Grant Date 15.11.2019
Publication Kind B1
IPC
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
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
Inventors 鈴木 陽一
Title
(JA) 有人飛行体
Abstract
(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。
【選択図】図1

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