FR3084988B1 - Echangeur de chaleur avionique - Google Patents

Echangeur de chaleur avionique Download PDF

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Publication number
FR3084988B1
FR3084988B1 FR1909058A FR1909058A FR3084988B1 FR 3084988 B1 FR3084988 B1 FR 3084988B1 FR 1909058 A FR1909058 A FR 1909058A FR 1909058 A FR1909058 A FR 1909058A FR 3084988 B1 FR3084988 B1 FR 3084988B1
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FR
France
Prior art keywords
avionics
exterior
heat exchanger
conduit
rear face
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
FR1909058A
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English (en)
Other versions
FR3084988A1 (fr
Inventor
Michael Ralph Storage
Dennis Alan Mcqueen
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.)
Unison Industries LLC
Original Assignee
Unison Industries LLC
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 Unison Industries LLC filed Critical Unison Industries LLC
Publication of FR3084988A1 publication Critical patent/FR3084988A1/fr
Application granted granted Critical
Publication of FR3084988B1 publication Critical patent/FR3084988B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00—Constructional details common to different types of electric apparatus
    • H05K7/20—Modifications to facilitate cooling, ventilating, or heating
    • H05K7/20218—Modifications to facilitate cooling, ventilating, or heating using a liquid coolant without phase change in electronic enclosures
    • H05K7/20254—Cold plates transferring heat from heat source to coolant
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D39/00—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders
    • B21D39/04—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders of tubes with tubes; of tubes with rods
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/06—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of high energy impulses, e.g. magnetic energy
    • B23K20/08—Explosive welding
    • 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
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
    • F25D9/00—Devices not associated with refrigerating machinery and not covered by groups F25D1/00 - F25D7/00; Combinations of devices covered by two or more of the groups F25D1/00 - F25D7/00
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D1/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
    • F28D1/02—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
    • F28D1/04—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits
    • F28D1/047—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being bent, e.g. in a serpentine or zig-zag
    • F28D1/0477—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being bent, e.g. in a serpentine or zig-zag the conduits being bent in a serpentine or zig-zag
    • 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
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/024—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising cooling means
    • 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
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0021—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for aircrafts or cosmonautics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0028—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for cooling heat generating elements, e.g. for cooling electronic components or electric devices
    • F28D2021/0029—Heat sinks
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2280/00—Mounting arrangements; Arrangements for facilitating assembling or disassembling of heat exchanger parts
    • F28F2280/06—Adapter frames, e.g. for mounting heat exchanger cores on other structure and for allowing fluidic connections

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

Les moteurs à turbine d'avion sont commandés par des dispositifs électroniques complexes tels que le FADEC et les unités PSS. Ces dispositifs peuvent être affectés par l'environnement du moteur, y compris la condensation de l'eau évaporée. Les aspects de la présente divulgation comprennent des échangeurs de chaleur uniques destinés à contrôler la température de ces appareils électroniques afin d'assurer leur bon fonctionnement. La présente invention propose un ensemble de commande avionique qui comprend un dispositif de commande de moteur comportant un boîtier avionique définissant un extérieur et un intérieur, avec au moins un connecteur (60), s'étendant depuis l'extérieur du boîtier avionique, et au moins un capteur (62) situé à l'intérieur. L’ensemble de commande avionique comprend également un échangeur de chaleur (52) comportant un conduit (64) définissant une voie de circulation de fluide avec au moins un passage de fluide menant d'un orifice d'entrée (68) de l'échangeur de chaleur (52) à un orifice de sortie (70) de l'échangeur de chaleur (52). Le conduit (64) définit une longueur avec une face arrière, et lorsque le conduit (64) est relié sur le plan fonctionnel à l'extérieur du boîtier avionique, au moins une première partie de la face arrière est espacée de l'extérieur du boîtier avionique, et au moins une deuxième partie de la face arrière est en contact avec l'extérieur du boîtier avionique, et la chaleur du liquide s’écoulant dans la voie de circulation de fluide est transmise au boîtier avionique. Figure pour l’abrégé : Fig 2
FR1909058A 2018-08-10 2019-08-07 Echangeur de chaleur avionique Active FR3084988B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201862717021P 2018-08-10 2018-08-10
US62/717.021 2018-08-10

Publications (2)

Publication Number Publication Date
FR3084988A1 FR3084988A1 (fr) 2020-02-14
FR3084988B1 true FR3084988B1 (fr) 2022-10-07

Family

ID=69457780

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1909058A Active FR3084988B1 (fr) 2018-08-10 2019-08-07 Echangeur de chaleur avionique

Country Status (2)

Country Link
US (1) US11480069B2 (fr)
FR (1) FR3084988B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20210000397A (ko) * 2019-06-25 2021-01-05 삼성전자주식회사 로봇 청소기, 스테이션 및 청소 시스템

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5553461A (en) 1995-01-11 1996-09-10 Grumman Aerospace Corporation Anti-icing heat exchanger for aircraft air cycle performance enhancement
MXPA02010588A (es) 2000-04-26 2003-05-14 Cosma Int Inc Hidroconformacion de una estructura tubular de diametro variable a partir de una pieza preformada tubular, usando soldadura de impulsos electromagneticos.
US7131612B2 (en) 2003-07-29 2006-11-07 Pratt & Whitney Canada Corp. Nacelle inlet lip anti-icing with engine oil
US7946806B2 (en) 2007-10-10 2011-05-24 United Technologies Corporation Gas turbine engine systems and related methods involving heat exchange
US8867210B2 (en) * 2012-10-31 2014-10-21 Deere & Company Cooling apparatus for an electrical substrate
FR3028133B1 (fr) 2014-11-04 2018-02-16 Safran Electrical & Power Baie avionique
US20170010046A1 (en) 2015-07-08 2017-01-12 Thermolift, Inc. Heat Exchanger
GB2544979A (en) 2015-12-01 2017-06-07 Rolls Royce Plc A heat sink of source apparatus and method
US11002290B2 (en) * 2016-01-08 2021-05-11 General Electric Company Heat exchanger for embedded engine applications: curvilinear plate
US11306974B2 (en) * 2016-06-15 2022-04-19 Delta Electronics, Inc. Temperature plate and heat dissipation device
US11168583B2 (en) * 2016-07-22 2021-11-09 General Electric Company Systems and methods for cooling components within a gas turbine engine
US20180051946A1 (en) * 2016-08-17 2018-02-22 Hamilton Sundstrand Corporation Heat exchanger arrangements and related methods
US10450957B2 (en) * 2017-01-23 2019-10-22 United Technologies Corporation Gas turbine engine with heat pipe system
US11320211B2 (en) * 2017-04-11 2022-05-03 Cooler Master Co., Ltd. Heat transfer device
US10842044B2 (en) * 2017-07-10 2020-11-17 Rolls-Royce North American Technologies, Inc. Cooling system in hybrid electric propulsion gas turbine engine
FR3071008B1 (fr) * 2017-09-11 2019-09-13 Safran Aircraft Engines Aube directrice de sortie pour turbomachine, comprenant un passage de refroidissement de lubrifiant equipe d'une matrice de conduction thermique comprimee entre les parois d'intrados et d'extrados
JP7058538B2 (ja) * 2018-04-05 2022-04-22 東京エレクトロン株式会社 流量制御方法、温度制御方法及び処理装置
US20200011455A1 (en) * 2018-07-05 2020-01-09 Unison Industries, Llc Duct assembly and method of forming
US10690422B2 (en) * 2018-08-03 2020-06-23 General Electric Company Thermal management system
US20200200040A1 (en) * 2018-12-19 2020-06-25 Unison Industries, Llc Aircraft surface cooler assembly
US11143105B2 (en) * 2018-12-19 2021-10-12 Unison Industries, Llc Mounting assembly and fan casing assembly

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Publication number Publication date
FR3084988A1 (fr) 2020-02-14
US11480069B2 (en) 2022-10-25
US20200224553A1 (en) 2020-07-16

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