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1. WO2022097359 - ハイブリッド回転翼航空機

公開番号 WO/2022/097359
公開日 12.05.2022
国際出願番号 PCT/JP2021/032570
国際出願日 06.09.2021
IPC
B64C 27/08 2006.1
B処理操作;運輸
64航空機;飛行;宇宙工学
C飛行機;ヘリコプタ
27回転翼航空機;回転翼航空機特有の回転翼
04ヘリコプタ
08二つ以上の回転翼をもつもの
B64C 39/02 2006.1
B処理操作;運輸
64航空機;飛行;宇宙工学
C飛行機;ヘリコプタ
39他に分類されない航空機
02特殊用途を特徴とするもの
B64D 27/24 2006.1
B処理操作;運輸
64航空機;飛行;宇宙工学
D航空機の装備;飛行服;パラシュート;航空機への動力装置または推進伝達機構の配置または取り付け
27航空機内における動力装置の設備または取り付け;動力装置の設備または取り付けに特徴のある航空機
02動力装置の型または位置に特徴のある航空機
24蒸気,電気またはバネ力を使用するもの
B64D 35/08 2006.1
B処理操作;運輸
64航空機;飛行;宇宙工学
D航空機の装備;飛行服;パラシュート;航空機への動力装置または推進伝達機構の配置または取り付け
35動力装置からプロペラまたは回転翼への動力伝達;伝達装置の配置
08複数の動力装置によって駆動される伝達機構を特徴とするもの
CPC
B60K 6/365
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
6Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units
20the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs
22characterised by apparatus, components or means specially adapted for HEVs
36characterised by the transmission gearings
365with the gears having orbital motion
B60K 6/383
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
6Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units
20the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs
22characterised by apparatus, components or means specially adapted for HEVs
38characterised by the driveline clutches
383One-way clutches or freewheel devices
B60K 6/40
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
6Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units
20the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs
22characterised by apparatus, components or means specially adapted for HEVs
40characterised by the assembly or relative disposition of components
B64C 27/08
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
08with two or more rotors
B64C 39/02
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
B64D 27/04
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
04of piston type
出願人
  • 株式会社FINEMECH FINEMECH CO., LTD. [JP]/[JP]
発明者
  • 平岩 一美 HIRAIWA, Kazuyoshi
代理人
  • 吉田 芳春 YOSHIDA, Yoshiharu
優先権情報
2020-18538405.11.2020JP
公開言語 (言語コード) 日本語 (ja)
出願言語 (言語コード) 日本語 (JA)
指定国 (国コード)
発明の名称
(EN) HYBRID ROTARY-WING AIRCRAFT
(FR) AÉRONEF HYBRIDE À VOILURE TOURNANTE
(JA) ハイブリッド回転翼航空機
要約
(EN) This hybrid rotary-wing aircraft (1) comprises: an internal combustion engine (40); motors (331a, 31b, 32, 33); and a first propelling shaft (11), a second propelling shaft (12), and a third propelling shaft (13) which respectively have rotary wings (21, 21b, 22, 23) to which the motors are respectively connected, and output floating force, the aircraft being configured so that when rotary wings connected to the motors (31a, 32) which can be driven by the internal combustion engine and generate electricity are defined as first propelling wings (21a, 22), and rotary wings other than the first propelling wings are defined as second propelling wings (21b, 23), the two or more first propelling wings and the two or more second propelling wings are distributed and provided to the respective propelling shafts, whereby the floating forces outputted by the respective propelling shafts can be freely controlled.
(FR) Un aéronef hybride à voilure tournante (1) comprend : un moteur à combustion interne (40) ; des moteurs (331a, 31b, 32, 33) ; un premier arbre de propulsion (11), un deuxième arbre de propulsion (12) et un troisième arbre de propulsion (13) qui possèdent respectivement des voilures tournantes (21, 21b, 22, 23) auxquelles les moteurs sont respectivement reliés et qui fournissent une force de flottement, l'aéronef étant conçu de telle sorte que, lorsque des voilures tournantes reliées aux moteurs (31a, 32), qui peuvent être entraînées par le moteur à combustion interne et générer de l'électricité, sont définies en tant que premières ailes de propulsion (21a, 22), et que des voilures tournantes autres que les premières ailes de propulsion sont définies en tant que secondes ailes de propulsion (21b, 23), les deux ou plus de deux premières ailes de propulsion et les deux ou plus de deux secondes ailes de propulsion étant réparties et disposées sur les arbres de propulsion respectifs, moyennant quoi les forces de flottement fournies par les arbres de propulsion respectifs peuvent être commandées librement.
(JA) ハイブリッド回転翼航空機(1)は、内燃機関(40)と、モータ(31a、31b、32、33)と、モータが連結された回転翼(21a、21b、22、23)をそれぞれ有し揚力を発出する第1推進軸(11)、第2推進軸(12)及び第3推進軸(13)とを備え、内燃機関が駆動可能で発電可能なモータ(31a、32)と連結した回転翼を第1推進翼(21a、22)と定義し、第1推進翼以外の回転翼を第2推進翼(21b、23)と定義したとき、2つ以上の第1推進翼と2つ以上の第2推進翼を、各推進軸に分配して設けることにより、各推進軸が発出する揚力をそれぞれ自在に制御可能に構成した。
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