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FR3074532B1 - Echangeur de chaleur gaz-liquide pour turbomachine, comprenant une surface aval au moins partiellement aerodynamique - Google Patents

Echangeur de chaleur gaz-liquide pour turbomachine, comprenant une surface aval au moins partiellement aerodynamique Download PDF

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Publication number
FR3074532B1
FR3074532B1 FR1761540A FR1761540A FR3074532B1 FR 3074532 B1 FR3074532 B1 FR 3074532B1 FR 1761540 A FR1761540 A FR 1761540A FR 1761540 A FR1761540 A FR 1761540A FR 3074532 B1 FR3074532 B1 FR 3074532B1
Authority
FR
France
Prior art keywords
gas
downstream
turbomachine
heat exchanger
liquid heat
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
FR1761540A
Other languages
English (en)
Other versions
FR3074532A1 (fr
Inventor
Stephane Louis Lucien Auberger
Romain Jean-Claude FERRIER
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 Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines 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 Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1761540A priority Critical patent/FR3074532B1/fr
Publication of FR3074532A1 publication Critical patent/FR3074532A1/fr
Application granted granted Critical
Publication of FR3074532B1 publication Critical patent/FR3074532B1/fr
Active legal-status Critical Current
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105—Heating the by-pass flow
    • F02K3/115—Heating the by-pass flow by means of indirect heat exchange
    • 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
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • 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
    • 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)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

L'invention concerne un échangeur de chaleur gaz-liquide (20) pour un conduit d'écoulement (16) de gaz dans une turbomachine. L'échangeur (20) comprend une partie aval (23). La partie aval (23) comprend des étages (22) comprenant chacun au moins un passage d'écoulement du gaz (30) et au moins un passage d'écoulement de liquide (46). Au moins certains des passages d'écoulement du gaz (30) et/ou de liquide (46) participent à la délimitation d'une surface externe aval (S2) qui délimite l'échangeur (20, 220) vers l'aval et qui est destinée à être en contact du gaz s'écoulant dans le conduit (16). Les étages (22) étant de longueurs (l1, l2) variables vers l'aval, de sorte que la surface externe aval (S2) est au moins partiellement aérodynamique.
FR1761540A 2017-12-01 2017-12-01 Echangeur de chaleur gaz-liquide pour turbomachine, comprenant une surface aval au moins partiellement aerodynamique Active FR3074532B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1761540A FR3074532B1 (fr) 2017-12-01 2017-12-01 Echangeur de chaleur gaz-liquide pour turbomachine, comprenant une surface aval au moins partiellement aerodynamique

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1761540 2017-12-01
FR1761540A FR3074532B1 (fr) 2017-12-01 2017-12-01 Echangeur de chaleur gaz-liquide pour turbomachine, comprenant une surface aval au moins partiellement aerodynamique

Publications (2)

Publication Number Publication Date
FR3074532A1 FR3074532A1 (fr) 2019-06-07
FR3074532B1 true FR3074532B1 (fr) 2020-03-27

Family

ID=61027979

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1761540A Active FR3074532B1 (fr) 2017-12-01 2017-12-01 Echangeur de chaleur gaz-liquide pour turbomachine, comprenant une surface aval au moins partiellement aerodynamique

Country Status (1)

Country Link
FR (1) FR3074532B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB202218535D0 (en) 2022-12-09 2023-01-25 Rolls Royce Plc A propulsion system comprising a heat exchanger

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8763363B2 (en) * 2007-07-06 2014-07-01 General Electric Company Method and system for cooling fluid in a turbine engine
US20120227949A1 (en) * 2011-03-11 2012-09-13 Weber Richard M Aerodynamic heat exchange structure
GB2500871B (en) * 2012-04-05 2017-03-01 Ford Global Tech Llc An Air to Liquid Heat Exchanger
US10450956B2 (en) * 2014-10-21 2019-10-22 United Technologies Corporation Additive manufactured ducted heat exchanger system with additively manufactured fairing

Also Published As

Publication number Publication date
FR3074532A1 (fr) 2019-06-07

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