PL4032812T3 - Sposoby i układy zarządzania zasilaniem hybrydowego elektrycznego zespołu napędowego - Google Patents

Sposoby i układy zarządzania zasilaniem hybrydowego elektrycznego zespołu napędowego

Info

Publication number
PL4032812T3
PL4032812T3 PL22153036.3T PL22153036T PL4032812T3 PL 4032812 T3 PL4032812 T3 PL 4032812T3 PL 22153036 T PL22153036 T PL 22153036T PL 4032812 T3 PL4032812 T3 PL 4032812T3
Authority
PL
Poland
Prior art keywords
systems
methods
power management
hybrid electric
electric powerplant
Prior art date
Application number
PL22153036.3T
Other languages
English (en)
Inventor
Michael R. MARK
Leonid Guerchkovitch
Original Assignee
Pratt & Whitney Canada Corp.
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 Pratt & Whitney Canada Corp. filed Critical Pratt & Whitney Canada Corp.
Publication of PL4032812T3 publication Critical patent/PL4032812T3/pl

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • B64D31/09—Initiating means actuated automatically in response to power plant failure
    • 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
    • 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
    • B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/053—Explicitly mentioned power

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Hybrid Electric Vehicles (AREA)
PL22153036.3T 2021-01-22 2022-01-24 Sposoby i układy zarządzania zasilaniem hybrydowego elektrycznego zespołu napędowego PL4032812T3 (pl)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US17/155,582 US11685540B2 (en) 2021-01-22 2021-01-22 Methods and systems for power management of a hybrid electric powerplant

Publications (1)

Publication Number Publication Date
PL4032812T3 true PL4032812T3 (pl) 2025-10-27

Family

ID=80001554

Family Applications (1)

Application Number Title Priority Date Filing Date
PL22153036.3T PL4032812T3 (pl) 2021-01-22 2022-01-24 Sposoby i układy zarządzania zasilaniem hybrydowego elektrycznego zespołu napędowego

Country Status (4)

Country Link
US (1) US11685540B2 (pl)
EP (1) EP4032812B1 (pl)
CA (1) CA3146041A1 (pl)
PL (1) PL4032812T3 (pl)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20230257128A1 (en) * 2022-02-11 2023-08-17 Pratt & Whitney Canada Corp. Hybrid-Electric Aircraft Propulsion System and Method for Operating the Same
IT202200016215A1 (it) * 2022-07-29 2024-01-29 Gen Electric Controllo di sistemi di propulsione e trasmissione completamente elettrici o ibridi-elettrici
US12091182B1 (en) * 2023-02-28 2024-09-17 Rtx Corporation Aircraft hybrid electric propulsion architecture with generator-motor fail mode
US12263953B2 (en) * 2023-05-02 2025-04-01 Pratt & Whitney Canada Corp. System and method for operating a hybrid aircraft power plant
US20240426708A1 (en) * 2023-06-26 2024-12-26 Pratt & Whitney Canada Corp. Testing secondary power system of aircraft powerplant
US20240425188A1 (en) * 2023-06-26 2024-12-26 Pratt & Whitney Canada Corp. Testing secondary power system of aircraft powerplant
FR3154455B1 (fr) * 2023-10-18 2025-09-05 Safran Aircraft Engines Systeme de commande d’une turbomachine hybridee par observateur a reconfiguration par detection de saturation de commande
US12030657B1 (en) * 2023-10-27 2024-07-09 Rtx Corporation System and methods for power split algorithm design for aircraft hybrid electric propulsion based on combined actor-critic RL agent and control barrier function filter
US20260001653A1 (en) * 2024-06-28 2026-01-01 Pratt & Whitney Canada Corp. Systems and methods for controlling an electric motor of an aircraft propulsion system
US12509236B1 (en) 2024-06-28 2025-12-30 Pratt & Whitney Canada Corp. Control assembly for aircraft propulsion systems

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7313470B2 (en) 2004-08-19 2007-12-25 Ford Global Technologies, Llc Vehicle torque monitoring system
DE102005040778A1 (de) 2005-08-29 2007-03-08 Robert Bosch Gmbh Verfahren zur Begrenzung von Sollmomenten bei der Motorsteuerung
DE102010047016A1 (de) 2010-09-30 2012-04-05 Voith Patent Gmbh Drehmomentsteuerung für Hybridantriebe
FR2997382B1 (fr) 2012-10-29 2014-11-21 Eurocopter France Procede de gestion d'une panne moteur sur un aeronef multimoteur muni d'une installation motrice hybride
US10800536B2 (en) * 2017-06-09 2020-10-13 General Electric Company Propulsion system for an aircraft
FR3090576B1 (fr) * 2018-12-20 2021-09-10 Airbus Helicopters Procédé d’assistance pour aéronef monomoteur à voilure tournante lors d’une panne moteur.
WO2020180372A2 (en) 2019-03-01 2020-09-10 United Technologies Advanced Projects, Inc. Degraded mode operation of hybrid electric propulsion systems
US10907494B2 (en) 2019-04-30 2021-02-02 Rolls-Royce North American Technologies Inc. Parallel hybrid propulsion system
FR3114077B1 (fr) * 2020-09-14 2024-01-19 Airbus Helicopters Procédé et dispositif de gestion de l’énergie fournie par une installation motrice hybride pour giravion

Also Published As

Publication number Publication date
EP4032812B1 (en) 2025-07-16
CA3146041A1 (en) 2022-07-22
EP4032812A1 (en) 2022-07-27
US20220234748A1 (en) 2022-07-28
US11685540B2 (en) 2023-06-27

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