JP2024507365A5 - - Google Patents

Info

Publication number
JP2024507365A5
JP2024507365A5 JP2023550176A JP2023550176A JP2024507365A5 JP 2024507365 A5 JP2024507365 A5 JP 2024507365A5 JP 2023550176 A JP2023550176 A JP 2023550176A JP 2023550176 A JP2023550176 A JP 2023550176A JP 2024507365 A5 JP2024507365 A5 JP 2024507365A5
Authority
JP
Japan
Prior art keywords
power
power shaft
engine
output
hybrid powertrain
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
Application number
JP2023550176A
Other languages
English (en)
Japanese (ja)
Other versions
JP2024507365A (ja
Filing date
Publication date
Application filed filed Critical
Priority claimed from PCT/US2022/017383 external-priority patent/WO2022187032A2/en
Publication of JP2024507365A publication Critical patent/JP2024507365A/ja
Publication of JP2024507365A5 publication Critical patent/JP2024507365A5/ja
Pending legal-status Critical Current

Links

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 JP2024507365A (ja) 2024-02-19
JP2024507365A5 true 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

Family Cites Families (14)

* 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
JP3901041B2 (ja) * 2002-07-10 2007-04-04 日産自動車株式会社 ハイブリッド車両のトルク制御装置
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
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
US10837304B2 (en) * 2016-12-13 2020-11-17 General Electric Company Hybrid-electric drive system
US11970062B2 (en) * 2017-04-05 2024-04-30 Ge Aviation Systems Llc Systems and methods of power allocation for hybrid electric architecture
GB201807774D0 (en) * 2018-05-14 2018-06-27 Rolls Royce Plc Hybrid aircraft propulsion system
FR3087421B1 (fr) * 2018-10-17 2022-03-04 Voltaero Engin comprenant un groupe motopropulseur hybride et procede de pilotage correspondant
CN113056422B (zh) * 2018-11-07 2024-05-14 昌仁航空株式会社 使用混合电力推进系统的垂直起降航空器及其控制方法
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

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