FR3114837B1 - Aeronef avec systeme de stockage d'energie thermique - Google Patents

Aeronef avec systeme de stockage d'energie thermique Download PDF

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Publication number
FR3114837B1
FR3114837B1 FR2110366A FR2110366A FR3114837B1 FR 3114837 B1 FR3114837 B1 FR 3114837B1 FR 2110366 A FR2110366 A FR 2110366A FR 2110366 A FR2110366 A FR 2110366A FR 3114837 B1 FR3114837 B1 FR 3114837B1
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France
Prior art keywords
aircraft
fluid
thermal energy
cooling loop
energy storage
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Active
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FR2110366A
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English (en)
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FR3114837A1 (fr
Inventor
J Douglas Snyder
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Rolls Royce Corp
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Rolls Royce Corp
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Publication date
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Publication of FR3114837A1 publication Critical patent/FR3114837A1/fr
Application granted granted Critical
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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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/224—Heating fuel before feeding to the burner
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
    • B64D33/10—Radiator arrangement
    • 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
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/34—Conditioning fuel, e.g. heating
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • 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
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine 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
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • 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
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/213—Heat transfer, e.g. cooling by the provision of a heat exchanger within the cooling circuit
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/306—Mass flow
    • F05D2270/3062—Mass flow of the auxiliary fluid for heating or cooling purposes
    • 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
    • F05D2270/40—Type of control system
    • F05D2270/44—Type of control system active, predictive, or anticipative
    • 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
    • F05D2270/50—Control logic embodiments
    • F05D2270/56—Control logic embodiments by hydraulic means, e.g. hydraulic valves within a hydraulic circuit
    • 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
    • Y02T50/40—Weight reduction
    • 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)
  • 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)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Supply And Distribution Of Alternating Current (AREA)

Abstract

Système d’énergie thermique (12) pour une utilisation avec un aéronef (10) comprenant une source de chaleur (16), une boucle de refroidissement (20) et un refroidisseur (22). La boucle de refroidissement (20) comprend un conduit de fluide (30) et une pompe (32) configurée pour déplacer un fluide à travers le conduit de fluide (30) pour transférer de la chaleur de la source de chaleur (16) au fluide pour refroidir la source de chaleur (16). Le refroidisseur (22) comprend un échangeur de chaleur à flux d’air (36) situé dans la conduite (34) et en communication thermique avec le fluide dans la boucle de refroidissement (20) pour transférer de la chaleur entre la boucle de refroidissement (20) et l’air conduit à travers la conduite (34). Figure pour l’abrégé : [Fig. 2]
FR2110366A 2020-10-02 2021-09-30 Aeronef avec systeme de stockage d'energie thermique Active FR3114837B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US202063086804P 2020-10-02 2020-10-02
US63/086,804 2020-10-02

Publications (2)

Publication Number Publication Date
FR3114837A1 FR3114837A1 (fr) 2022-04-08
FR3114837B1 true FR3114837B1 (fr) 2023-12-08

Family

ID=80931070

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2110366A Active FR3114837B1 (fr) 2020-10-02 2021-09-30 Aeronef avec systeme de stockage d'energie thermique

Country Status (2)

Country Link
US (3) US11591102B2 (fr)
FR (1) FR3114837B1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11744042B2 (en) * 2020-11-06 2023-08-29 Rolls-Royce North American Technologies Inc. Thermal management system with dual-use serial thermal energy storage for system size reduction
US11525399B1 (en) * 2021-06-17 2022-12-13 Pratt & Whitney Canada Corp. Oil system with flow restrictor
GB2619691A (en) * 2022-03-03 2023-12-20 Rolls Royce Plc Gas turbine engine
GB2622211A (en) 2022-09-06 2024-03-13 Rolls Royce Plc A thermal management system for an aircraft
GB2622208A (en) 2022-09-06 2024-03-13 Rolls Royce Plc A thermal management system for an aircraft
GB2622210A (en) * 2022-09-06 2024-03-13 Rolls Royce Plc A thermal management system for an aircraft
CN115367125A (zh) * 2022-09-08 2022-11-22 北京微焓科技有限公司 混合热管理系统及飞机
GB202214270D0 (en) * 2022-09-29 2022-11-16 Rolls Royce Plc Heat management system for aircraft

Family Cites Families (21)

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Publication number Priority date Publication date Assignee Title
US4263786A (en) * 1979-07-10 1981-04-28 The Boeing Company Fuel conserving air-conditioning apparatus and method for aircraft
US4505124A (en) * 1983-09-22 1985-03-19 The United States Of America As Represented By The Secretary Of The Air Force Heat management system for aircraft
US4614438A (en) * 1984-04-24 1986-09-30 Kabushiki Kaisha Kokusai Technicals Method of mixing fuel oils
US4776536A (en) 1987-05-19 1988-10-11 Rockwell International Corporation Integrated aircraft fuel thermal management system
US6948331B1 (en) 2003-09-12 2005-09-27 Norhrop Grumman Corporation Environmental control system for an aircraft
US20100313591A1 (en) 2009-06-12 2010-12-16 Hamilton Sundstrand Corporation Adaptive heat sink for aircraft environmental control system
US8522572B2 (en) * 2010-07-01 2013-09-03 General Electric Company Adaptive power and thermal management system
EP3392145B1 (fr) 2012-10-31 2022-01-12 Rolls-Royce Corporation Système et procédé de gestion thermique de véhicule d'aéronef
US9561857B2 (en) 2013-02-06 2017-02-07 Raytheon Company Aircraft thermal management system for cooling using expendable coolants
US10081439B1 (en) * 2013-06-20 2018-09-25 The Boeing Company Methods and apparatus to cool a vehicle heat source
US10610712B2 (en) * 2013-12-02 2020-04-07 Aero Systems Consultants LLC Aircraft fuel systems
ES2641956T3 (es) 2013-12-03 2017-11-14 Airbus Defence and Space GmbH Sistema de combustible de aeronave con calentamiento de combustible almacenado
US10260419B2 (en) * 2015-07-31 2019-04-16 General Electric Company Cooling system
US10207809B2 (en) 2015-08-31 2019-02-19 Honeywell International Inc. Integrated air and vapor cycle cooling system
US20210229827A1 (en) * 2015-10-08 2021-07-29 Government Of The United States, As Represented By The Secretary Of The Air Force Thermal management system and method of using same
US10215097B2 (en) 2015-12-08 2019-02-26 General Electric Company Thermal management system
US10752374B1 (en) * 2017-03-15 2020-08-25 Northrop Grumman Systems Corporation Active fuel thermal conditioning for aircraft
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JP6963512B2 (ja) * 2018-01-12 2021-11-10 三菱パワー株式会社 燃料供給システム、ガスタービン、発電プラント、制御方法及びプログラム
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Also Published As

Publication number Publication date
FR3114837A1 (fr) 2022-04-08
US20220106053A1 (en) 2022-04-07
US20220106052A1 (en) 2022-04-07
US20240124150A1 (en) 2024-04-18
US11591102B2 (en) 2023-02-28

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