FR3129435B1 - Ensemble pour aéronef muni d’au moins un système d’actionnement d’inversion de poussée fonctionnant à l’hydrogène. - Google Patents

Ensemble pour aéronef muni d’au moins un système d’actionnement d’inversion de poussée fonctionnant à l’hydrogène. Download PDF

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Publication number
FR3129435B1
FR3129435B1 FR2112526A FR2112526A FR3129435B1 FR 3129435 B1 FR3129435 B1 FR 3129435B1 FR 2112526 A FR2112526 A FR 2112526A FR 2112526 A FR2112526 A FR 2112526A FR 3129435 B1 FR3129435 B1 FR 3129435B1
Authority
FR
France
Prior art keywords
hydrogen
thrust reverser
actuation system
reverser actuation
aircraft assembly
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
FR2112526A
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English (en)
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FR3129435A1 (fr
Inventor
Jihane Bellahbib
Hakim Maalioune
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.)
Safran Nacelles SAS
Original Assignee
Safran Nacelles 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 Safran Nacelles SAS filed Critical Safran Nacelles SAS
Priority to FR2112526A priority Critical patent/FR3129435B1/fr
Priority to US18/058,483 priority patent/US20230174248A1/en
Publication of FR3129435A1 publication Critical patent/FR3129435A1/fr
Application granted granted Critical
Publication of FR3129435B1 publication Critical patent/FR3129435B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/30—Fuel systems for specific fuels
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
    • 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
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • B64D2041/005—Fuel cells
    • 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
    • F05D2220/00—Application
    • F05D2220/70—Application in combination with
    • F05D2220/76—Application in combination with an electrical generator
    • 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
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/40—Application of hydrogen technology to transportation, e.g. using fuel cells

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Fuel Cell (AREA)

Abstract

Aéronef (1a) muni d’au moins un propulseur alimenté en hydrogène par au moins un réservoir d’hydrogène, muni d’au moins un système d’inversion de poussée comprenant au moins un actionneur, caractérisé par le fait que l’aéronef comprend : au moins un moyen de stockage ou d’acheminement de l’hydrogène résiduel du propulseur (9), une pile à combustible disposée dans la source de puissance à hydrogène (2a) et alimentée en hydrogène par le au moins un moyen de stockage de l’hydrogène résiduel (9), etun système d’actionnement d’inversion de poussée à hydrogène (3a) comprenant un contrôleur de système d’actionnement d’inversion de poussée à hydrogène (5a), et une unité de puissance primaire à hydrogène (7a) munie d’une pile à combustible alimentée en hydrogène et alimentant le au moins un actionneur d’inversion de poussée. Figure pour l’abrégé : Fig 2
FR2112526A 2021-11-25 2021-11-25 Ensemble pour aéronef muni d’au moins un système d’actionnement d’inversion de poussée fonctionnant à l’hydrogène. Active FR3129435B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR2112526A FR3129435B1 (fr) 2021-11-25 2021-11-25 Ensemble pour aéronef muni d’au moins un système d’actionnement d’inversion de poussée fonctionnant à l’hydrogène.
US18/058,483 US20230174248A1 (en) 2021-11-25 2022-11-23 Aircraft assembly fitted with at least one hydrogen-powered thrust reverser actuation system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2112526 2021-11-25
FR2112526A FR3129435B1 (fr) 2021-11-25 2021-11-25 Ensemble pour aéronef muni d’au moins un système d’actionnement d’inversion de poussée fonctionnant à l’hydrogène.

Publications (2)

Publication Number Publication Date
FR3129435A1 FR3129435A1 (fr) 2023-05-26
FR3129435B1 true FR3129435B1 (fr) 2024-03-08

Family

ID=79602003

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2112526A Active FR3129435B1 (fr) 2021-11-25 2021-11-25 Ensemble pour aéronef muni d’au moins un système d’actionnement d’inversion de poussée fonctionnant à l’hydrogène.

Country Status (2)

Country Link
US (1) US20230174248A1 (fr)
FR (1) FR3129435B1 (fr)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0313456D0 (en) * 2003-06-11 2003-07-16 Rolls Royce Plc Propulsion arrangement
FR2990248B1 (fr) 2012-05-04 2015-09-25 Aircelle Sa Systeme de commande pour inverseur de poussee
FR3009544B1 (fr) 2013-08-06 2017-06-23 Aircelle Sa Systemes electriques de la nacelle energetiquement autonomes
GB2556092B (en) * 2016-11-18 2019-03-06 Ge Aviat Systems Ltd Electrical power system for aircraft using fuel cells and an energy storage device
CN113232869A (zh) * 2021-05-13 2021-08-10 中电科芜湖通用航空产业技术研究院有限公司 一种集成式氢能源飞行器动力系统和电动飞行器

Also Published As

Publication number Publication date
US20230174248A1 (en) 2023-06-08
FR3129435A1 (fr) 2023-05-26

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