FR3128200B1 - Dispositif volant hybride - Google Patents

Dispositif volant hybride Download PDF

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Publication number
FR3128200B1
FR3128200B1 FR2111127A FR2111127A FR3128200B1 FR 3128200 B1 FR3128200 B1 FR 3128200B1 FR 2111127 A FR2111127 A FR 2111127A FR 2111127 A FR2111127 A FR 2111127A FR 3128200 B1 FR3128200 B1 FR 3128200B1
Authority
FR
France
Prior art keywords
electric
combustion engine
transfer circuit
energy transfer
electric motor
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.)
Active
Application number
FR2111127A
Other languages
English (en)
Other versions
FR3128200A1 (fr
Inventor
Frankie Zapata
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zipair SAS
Original Assignee
Zipair SAS
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 Zipair SAS filed Critical Zipair SAS
Priority to FR2111127A priority Critical patent/FR3128200B1/fr
Priority to PCT/FR2022/051459 priority patent/WO2023067253A1/fr
Priority to US18/701,755 priority patent/US12434834B2/en
Publication of FR3128200A1 publication Critical patent/FR3128200A1/fr
Application granted granted Critical
Publication of FR3128200B1 publication Critical patent/FR3128200B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64C29/0083—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 several motors of different type
    • 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
    • B60—VEHICLES IN GENERAL
    • B60Y—INDEXING SCHEME RELATING TO ASPECTS CROSS-CUTTING VEHICLE TECHNOLOGY
    • B60Y2200/00—Type of vehicle
    • B60Y2200/90—Vehicles comprising electric prime movers
    • B60Y2200/92—Hybrid vehicles
    • 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
    • B64D2221/00—Electric power distribution systems onboard aircraft
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—ELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2105/00—Networks for supplying or distributing electric power characterised by their spatial reach or by the load
    • H02J2105/30—Networks for supplying or distributing electric power characterised by their spatial reach or by the load the load networks being external to vehicles, i.e. exchanging power with vehicles
    • H02J2105/32—Networks for supplying or distributing electric power characterised by their spatial reach or by the load the load networks being external to vehicles, i.e. exchanging power with vehicles for aircrafts

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Hybrid Electric Vehicles (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

L’invention concerne un dispositif volant comportant un corps principal sur lequel est fixé un moteur à combustion (MC) et un moteur électrique (ME), un générateur électrique (GE) et un circuit de transfert d’énergie électrique (300). Les moteurs à combustion (MC) et électrique (ME) sont agencés pour créer des vecteurs de poussée et sont placés de part et d’autre du corps principal afin de créer des vecteurs de poussée de chaque côté d’un plan de séparation dudit corps. Le générateur électrique (GE) est couplé mécaniquement au moteur à combustion (MC) afin d’être entrainé par ce dernier. Le circuit de transfert d’énergie électrique (300) est connecté entre le générateur électrique (GE) et le moteur électrique (ME), le circuit de transfert d’énergie (300) étant configuré pour créer une résistance mécanique ralentissant le moteur à combustion (MC) et pour produire de l’énergie électrique afin d’alimenter le moteur électrique (ME). Figure pour l’abrégé : Fig.3
FR2111127A 2021-10-20 2021-10-20 Dispositif volant hybride Active FR3128200B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR2111127A FR3128200B1 (fr) 2021-10-20 2021-10-20 Dispositif volant hybride
PCT/FR2022/051459 WO2023067253A1 (fr) 2021-10-20 2022-07-21 Dispositif volant hybride
US18/701,755 US12434834B2 (en) 2021-10-20 2022-07-21 Hybrid flying device

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2111127A FR3128200B1 (fr) 2021-10-20 2021-10-20 Dispositif volant hybride
FR2111127 2021-10-20

Publications (2)

Publication Number Publication Date
FR3128200A1 FR3128200A1 (fr) 2023-04-21
FR3128200B1 true FR3128200B1 (fr) 2024-06-21

Family

ID=80735527

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2111127A Active FR3128200B1 (fr) 2021-10-20 2021-10-20 Dispositif volant hybride

Country Status (3)

Country Link
US (1) US12434834B2 (fr)
FR (1) FR3128200B1 (fr)
WO (1) WO2023067253A1 (fr)

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013109392A1 (de) * 2013-08-29 2015-03-05 Airbus Defence and Space GmbH Schnellfliegendes, senkrechtstartfähiges Fluggerät
US9481471B2 (en) * 2013-11-11 2016-11-01 The Boeing Company Autonomous propulsion apparatus and methods
KR101615486B1 (ko) * 2015-07-17 2016-04-26 주식회사 한국카본 하이브리드 전기 추진시스템을 이용하는 수직이착륙 항공기
FR3049931B1 (fr) 2016-04-08 2018-05-18 Zipair Dispositif de propulsion d'un passager
CA2958375C (fr) * 2016-05-06 2025-01-07 Rolls-Royce North American Technologies, Inc. Systeme d'alimentation facultativement hybride
US10689082B2 (en) * 2017-04-12 2020-06-23 Rolls-Royce North American Technologies, Inc. Mechanically and electrically distributed propulsion
CN207120892U (zh) * 2017-04-14 2018-03-20 深圳市轻准科技有限公司 混动无人机
EP3630601A4 (fr) * 2017-06-01 2021-02-24 Moog Inc. Système d'alimentation auxiliaire pour giravion avec bras d'hélice pliants et train d'atterrissage à zone déformable
CN107628241A (zh) * 2017-09-25 2018-01-26 安徽瓦尔特机械贸易有限公司 一种无人机混合动力系统
CN109263878A (zh) * 2018-10-30 2019-01-25 佛山市神风航空科技有限公司 八旋翼载人飞行器
WO2020096254A1 (fr) * 2018-11-07 2020-05-14 문창모 Aéronef à décollage et à atterrissage verticaux utilisant un système de propulsion électrique hybride et procédé de commande associé
DE102022205488A1 (de) * 2022-05-31 2023-11-30 Rolls-Royce Deutschland Ltd & Co Kg Dimensionierung des Spaltes zwischen Substrat und Kühlkörper in Hochspannungs-Leistungswandlern

Also Published As

Publication number Publication date
US12434834B2 (en) 2025-10-07
WO2023067253A1 (fr) 2023-04-27
FR3128200A1 (fr) 2023-04-21
US20250136287A1 (en) 2025-05-01

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