FR3016956B1 - Echangeur de chaleur d'une turbomachine - Google Patents
Echangeur de chaleur d'une turbomachine Download PDFInfo
- Publication number
- FR3016956B1 FR3016956B1 FR1400220A FR1400220A FR3016956B1 FR 3016956 B1 FR3016956 B1 FR 3016956B1 FR 1400220 A FR1400220 A FR 1400220A FR 1400220 A FR1400220 A FR 1400220A FR 3016956 B1 FR3016956 B1 FR 3016956B1
- Authority
- FR
- France
- Prior art keywords
- heat exchanger
- turbomachine
- central body
- leading edge
- trailing edge
- 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
Links
- 239000012530 fluid Substances 0.000 abstract 1
Classifications
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- 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
- F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M5/00—Heating, cooling, or controlling temperature of lubricant; Lubrication means facilitating engine starting
- F01M5/002—Cooling
-
- 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
- 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
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F13/00—Arrangements for modifying heat-transfer, e.g. increasing, decreasing
- F28F13/06—Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
- F28F3/02—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M5/00—Heating, cooling, or controlling temperature of lubricant; Lubrication means facilitating engine starting
- F01M5/002—Cooling
- F01M2005/004—Oil-cooled 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/129—Cascades, i.e. assemblies of similar profiles acting in parallel
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
- F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2215/00—Fins
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2250/00—Arrangements for modifying the flow of the heat exchange media, e.g. flow guiding means; Particular flow patterns
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Geometry (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
L'invention concerne un échangeur de chaleur pour un canal de circulation d'air d'une turbomachine, l'échangeur de chaleur étant configuré pour être traversé par un fluide à refroidir et comprend une pluralité d'ailettes faisant saillie par rapport à une surface support, chaque ailette s'étend axialement sur une longueur dans le sens de circulation d'air et comprend un bord d'attaque et un bord de fuite, l'échangeur de chaleur étant caractérisé en ce que chaque ailette comprend en outre un corps central, entre le bord d'attaque et le bord de fuite, le corps central présentant dans un plan parallèle à la surface support un profil central courbe.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1400220A FR3016956B1 (fr) | 2014-01-29 | 2014-01-29 | Echangeur de chaleur d'une turbomachine |
GB1501092.9A GB2524623B (en) | 2014-01-29 | 2015-01-22 | Heat exchanger of a turbomachine |
US14/605,223 US10066875B2 (en) | 2014-01-29 | 2015-01-26 | Heat exchanger of a turbomachine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1400220 | 2014-01-29 | ||
FR1400220A FR3016956B1 (fr) | 2014-01-29 | 2014-01-29 | Echangeur de chaleur d'une turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3016956A1 FR3016956A1 (fr) | 2015-07-31 |
FR3016956B1 true FR3016956B1 (fr) | 2019-04-19 |
Family
ID=50639683
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1400220A Active FR3016956B1 (fr) | 2014-01-29 | 2014-01-29 | Echangeur de chaleur d'une turbomachine |
Country Status (3)
Country | Link |
---|---|
US (1) | US10066875B2 (fr) |
FR (1) | FR3016956B1 (fr) |
GB (1) | GB2524623B (fr) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20170009118A1 (en) * | 2015-07-10 | 2017-01-12 | General Electric Company | Method and apparatus for generating latent heat at low temperatures using exothermic salt crystallization |
US10697371B2 (en) | 2015-12-28 | 2020-06-30 | General Electric Company | Method and system for a combined air-oil cooler and fuel-oil cooler heat exchanger |
US11519295B2 (en) | 2018-12-03 | 2022-12-06 | Raytheon Technologies Corporation | Thermal management system for gas turbine engine |
DE102020001564A1 (de) * | 2019-04-10 | 2020-10-15 | Sew-Eurodrive Gmbh & Co Kg | Elektrogerät mit Gehäuseteil |
FR3096444B1 (fr) * | 2019-05-20 | 2021-05-07 | Safran | Systeme d’echange de chaleur optimise |
US11519368B2 (en) | 2020-01-07 | 2022-12-06 | Raytheon Technologies Corporation | Heat exchanger supply plenum |
US11852024B2 (en) * | 2020-12-18 | 2023-12-26 | Ge Aviation Systems Llc | Electrical strut for a turbine engine |
EP4374056A1 (fr) * | 2021-07-22 | 2024-05-29 | Safran Aero Boosters | Système pour refroidir de l'huile dans une turbomachine d'aéronef |
BE1029619B1 (fr) * | 2021-07-22 | 2023-02-20 | Safran Aero Boosters | Système pour refroidir de l'huile dans une turbomachine d'aéronef |
FR3140122A1 (fr) | 2022-09-26 | 2024-03-29 | Safran Aircraft Engines | Ensemble pour turbomachine d’aeronef comprenant un echangeur de chaleur du type sacoc, de conception ameliore |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1775041A (en) * | 1925-02-21 | 1930-09-02 | Karmazin John | Radiator |
US3886639A (en) * | 1975-02-01 | 1975-06-03 | Peerless Of America | Method of making a finned heat exchanger |
DD244191A1 (de) * | 1985-12-23 | 1987-03-25 | Kyffhaeuserhuette Maschf | Profilierte waermeuebertragungsplatten |
US4974413A (en) * | 1989-08-11 | 1990-12-04 | Szego Peter F | Recuperative heat exchanger |
FI974293A0 (fi) * | 1997-11-21 | 1997-11-21 | Muuntolaite Oy | Kylelement foer ojaemnt foerdelad vaermebelastning |
US5984636A (en) | 1997-12-17 | 1999-11-16 | Pratt & Whitney Canada Inc. | Cooling arrangement for turbine rotor |
US6698511B2 (en) * | 2001-05-18 | 2004-03-02 | Incep Technologies, Inc. | Vortex heatsink for high performance thermal applications |
DE20205200U1 (de) * | 2002-03-22 | 2002-08-08 | Erbsloeh Aluminium Gmbh | Hohlkammerprofil aus Metall insbesondere für Wärmetauscher und Verformungsvorrichtung |
US7079390B2 (en) * | 2003-06-05 | 2006-07-18 | Hewlett-Packard Development, L.P. | System and method for heat dissipation and air flow redirection in a chassis |
US20070051502A1 (en) * | 2004-05-19 | 2007-03-08 | Showa Denko K.K. | Heat exchanger fin, heat exchanger, condensers, and evaporators |
JP4677891B2 (ja) * | 2005-12-01 | 2011-04-27 | トヨタ自動車株式会社 | 伝熱部品 |
FR2946089B1 (fr) | 2009-05-27 | 2012-05-04 | Airbus France | Dispositif de refroidissement de fluides pour propulseur a turbomachine |
US8662150B2 (en) * | 2010-08-09 | 2014-03-04 | General Electric Company | Heat exchanger media pad for a gas turbine |
US8784047B2 (en) * | 2010-11-04 | 2014-07-22 | Hamilton Sundstrand Corporation | Gas turbine engine heat exchanger with tapered fins |
GB201121754D0 (en) | 2011-12-19 | 2012-02-01 | Rolls Royce Plc | A heat exchanger |
US9238284B2 (en) * | 2011-12-20 | 2016-01-19 | Unison Industries, Llc | Methods for forming a heat exchanger and portions thereof |
US10145253B2 (en) * | 2012-04-05 | 2018-12-04 | Safran Aircraft Engines | Stator vane formed by a set of vane parts |
-
2014
- 2014-01-29 FR FR1400220A patent/FR3016956B1/fr active Active
-
2015
- 2015-01-22 GB GB1501092.9A patent/GB2524623B/en active Active
- 2015-01-26 US US14/605,223 patent/US10066875B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
GB2524623B (en) | 2020-05-06 |
FR3016956A1 (fr) | 2015-07-31 |
GB201501092D0 (en) | 2015-03-11 |
GB2524623A (en) | 2015-09-30 |
US20150211801A1 (en) | 2015-07-30 |
US10066875B2 (en) | 2018-09-04 |
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