BR112023016760A2 - Arquitetura flexível para um sistema híbrido de aeroespaço e componentes otimizados da mesma - Google Patents

Arquitetura flexível para um sistema híbrido de aeroespaço e componentes otimizados da mesma

Info

Publication number
BR112023016760A2
BR112023016760A2 BR112023016760A BR112023016760A BR112023016760A2 BR 112023016760 A2 BR112023016760 A2 BR 112023016760A2 BR 112023016760 A BR112023016760 A BR 112023016760A BR 112023016760 A BR112023016760 A BR 112023016760A BR 112023016760 A2 BR112023016760 A2 BR 112023016760A2
Authority
BR
Brazil
Prior art keywords
electrical machine
flexible architecture
hybrid
engine
optimized components
Prior art date
Application number
BR112023016760A
Other languages
English (en)
Portuguese (pt)
Inventor
Austin Cassels
David Eichstedt
N Spitzer David
Richard Bartsch Eric
Patrick Currier
Pat Anderson Richard
Gerardo Santacruz Xavier
Original Assignee
Verdego Aero Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Verdego Aero Inc filed Critical Verdego Aero Inc
Publication of BR112023016760A2 publication Critical patent/BR112023016760A2/pt

Links

Classifications

    • 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)
BR112023016760A 2021-02-21 2022-02-22 Arquitetura flexível para um sistema híbrido de aeroespaço e componentes otimizados da mesma BR112023016760A2 (pt)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US202163151760P 2021-02-21 2021-02-21
US202163163165P 2021-03-19 2021-03-19
US202163280543P 2021-11-17 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 (1)

Publication Number Publication Date
BR112023016760A2 true BR112023016760A2 (pt) 2023-10-31

Family

ID=83155614

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112023016760A BR112023016760A2 (pt) 2021-02-21 2022-02-22 Arquitetura flexível para um sistema híbrido de aeroespaço e componentes otimizados da mesma

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

Also Published As

Publication number Publication date
EP4294727A4 (en) 2025-02-12
WO2022187032A2 (en) 2022-09-09
JP2024507365A (ja) 2024-02-19
EP4294727A2 (en) 2023-12-27
US20230391463A1 (en) 2023-12-07
WO2022187032A3 (en) 2022-11-10

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Legal Events

Date Code Title Description
B25G Requested change of headquarter approved

Owner name: VERDEGO AERO, INC. (US)