JP2024507365A - 航空宇宙ハイブリッドシステム及びその最適化した構成要素の柔軟なアーキテクチャ - Google Patents

航空宇宙ハイブリッドシステム及びその最適化した構成要素の柔軟なアーキテクチャ Download PDF

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Publication number
JP2024507365A
JP2024507365A JP2023550176A JP2023550176A JP2024507365A JP 2024507365 A JP2024507365 A JP 2024507365A JP 2023550176 A JP2023550176 A JP 2023550176A JP 2023550176 A JP2023550176 A JP 2023550176A JP 2024507365 A JP2024507365 A JP 2024507365A
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JP
Japan
Prior art keywords
power
output
engine
power shaft
electrical
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
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JP2023550176A
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English (en)
Japanese (ja)
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JP2024507365A5 (https=
Inventor
リチャード バーチュ，エリック
パット アンダーソン，リチャード
アイヒシュテット，デイヴィッド
エヌ． スピッツァー，デイヴィッド
カッセルズ，オースティン
ヘラルド サンタクルズ，グザヴィエ
キュリアー，パトリック
Original Assignee
ヴェルデゴ エアロ，インコーポレイテッド
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Application filed by ヴェルデゴ エアロ，インコーポレイテッド filed Critical ヴェルデゴ エアロ，インコーポレイテッド
Publication of JP2024507365A publication Critical patent/JP2024507365A/ja
Publication of JP2024507365A5 publication Critical patent/JP2024507365A5/ja
Pending legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/04—Aircraft characterised by the type or position of power plants of piston type
    • B64D27/08—Aircraft characterised by the type or position of power plants of piston type within, or attached to, fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/30—Aircraft characterised by electric power plants
    • B64D27/33—Hybrid electric aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/30—Aircraft characterised by electric power plants
    • B64D27/35—Arrangements for on-board electric energy production, distribution, recovery or storage
    • B64D27/357—Arrangements for on-board electric energy production, distribution, recovery or storage using batteries
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/16—Power plant control systems; Arrangement of power plant control systems in aircraft for electric power plants
    • B64D31/18—Power plant control systems; Arrangement of power plant control systems in aircraft for electric power plants for hybrid-electric power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • B64D35/02—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants
    • B64D35/021—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants for electric power plants
    • B64D35/022—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants for electric power plants of hybrid-electric type
    • B64D35/023—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants for electric power plants of hybrid-electric type of series-parallel type
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Auxiliary Drives, Propulsion Controls, And Safety Devices (AREA)
JP2023550176A 2021-02-21 2022-02-22 航空宇宙ハイブリッドシステム及びその最適化した構成要素の柔軟なアーキテクチャ Pending JP2024507365A (ja)

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
US202163151760P 2021-02-21 2021-02-21
US63/151,760 2021-02-21
US202163163165P 2021-03-19 2021-03-19
US63/163,165 2021-03-19
US202163280543P 2021-11-17 2021-11-17
US63/280,543 2021-11-17
PCT/US2022/017383 WO2022187032A2 (en) 2021-02-21 2022-02-22 Flexible architecture for an aerospace hybrid system and optimized components thereof

Publications (2)

Publication Number Publication Date
JP2024507365A true JP2024507365A (ja) 2024-02-19
JP2024507365A5 JP2024507365A5 (https=) 2025-03-04

Family

ID=83155614

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2023550176A Pending JP2024507365A (ja) 2021-02-21 2022-02-22 航空宇宙ハイブリッドシステム及びその最適化した構成要素の柔軟なアーキテクチャ

Country Status (5)

Country Link
US (1) US20230391463A1 (https=)
EP (1) EP4294727A4 (https=)
JP (1) JP2024507365A (https=)
BR (1) BR112023016760A2 (https=)
WO (1) WO2022187032A2 (https=)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN121752968A (zh) * 2023-07-10 2026-03-27 阿切尔航空公司 用于航空器的飞行控制的系统和方法

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004048866A (ja) * 2002-07-10 2004-02-12 Nissan Motor Co Ltd ハイブリッド車両のトルク制御装置
JP2018140767A (ja) * 2016-12-13 2018-09-13 ゼネラル・エレクトリック・カンパニイ ハイブリッド電気駆動システム
US20190344898A1 (en) * 2018-05-14 2019-11-14 Rolls-Royce Plc Hybrid Aircraft Propulsion System
JP2019534665A (ja) * 2016-10-20 2019-11-28 トップ フライト テクノロジーズ， インコーポレイテッド ハイブリッド電力システム特性評価
WO2020079369A1 (fr) * 2018-10-17 2020-04-23 Voltaero Engin comprenant un groupe motopropulseur hybride et procede de pilotage correspondant
WO2020096254A1 (ko) * 2018-11-07 2020-05-14 문창모 하이브리드 전기 추진시스템을 이용하는 수직이착륙 항공기 및 그 제어 방법

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5045027A (en) * 1989-08-07 1991-09-03 Caterpillar Inc. Torsionally tuned spring coupling and drive mechanism including same
CA2820254C (en) * 2012-07-09 2020-02-18 Mcmaster University Hybrid powertrain system
US10384765B2 (en) * 2014-02-06 2019-08-20 Bell Helicopter Textron Inc. Interconnect drive system
US9869240B2 (en) * 2015-02-20 2018-01-16 Pratt & Whitney Canada Corp. Compound engine assembly with cantilevered compressor and turbine
DE102016216461A1 (de) * 2016-08-31 2018-03-01 Continental Automotive Gmbh Elektrisches Drehschwingungsberuhigungssystem für Mild Hybrid Fahrzeuge
US11970062B2 (en) * 2017-04-05 2024-04-30 Ge Aviation Systems Llc Systems and methods of power allocation for hybrid electric architecture
FR3096659B1 (fr) * 2019-05-29 2021-05-07 Voltaero Engin comprenant un groupe motopropulseur hybride et procédé de pilotage correspondant
US11679891B2 (en) * 2019-06-06 2023-06-20 Beta Air, Llc Integrated electric propulsion assembly

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004048866A (ja) * 2002-07-10 2004-02-12 Nissan Motor Co Ltd ハイブリッド車両のトルク制御装置
JP2019534665A (ja) * 2016-10-20 2019-11-28 トップ フライト テクノロジーズ， インコーポレイテッド ハイブリッド電力システム特性評価
JP2018140767A (ja) * 2016-12-13 2018-09-13 ゼネラル・エレクトリック・カンパニイ ハイブリッド電気駆動システム
US20190344898A1 (en) * 2018-05-14 2019-11-14 Rolls-Royce Plc Hybrid Aircraft Propulsion System
WO2020079369A1 (fr) * 2018-10-17 2020-04-23 Voltaero Engin comprenant un groupe motopropulseur hybride et procede de pilotage correspondant
WO2020096254A1 (ko) * 2018-11-07 2020-05-14 문창모 하이브리드 전기 추진시스템을 이용하는 수직이착륙 항공기 및 그 제어 방법

Also Published As

Publication number Publication date
BR112023016760A2 (pt) 2023-10-31
EP4294727A4 (en) 2025-02-12
WO2022187032A2 (en) 2022-09-09
EP4294727A2 (en) 2023-12-27
US20230391463A1 (en) 2023-12-07
WO2022187032A3 (en) 2022-11-10

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