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FR3093765B1 - OPTIMIZED TURBOMACHINE AIR-OIL HEAT EXCHANGER SYSTEM - Google Patents

OPTIMIZED TURBOMACHINE AIR-OIL HEAT EXCHANGER SYSTEM
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Publication number
FR3093765B1
FR3093765B1FR1902532AFR1902532AFR3093765B1FR 3093765 B1FR3093765 B1FR 3093765B1FR 1902532 AFR1902532 AFR 1902532AFR 1902532 AFR1902532 AFR 1902532AFR 3093765 B1FR3093765 B1FR 3093765B1
Authority
FR
France
Prior art keywords
heat exchanger
exchanger system
optimized
duct
turbomachine
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
FR1902532A
Other languages
French (fr)
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FR3093765A1 (en
Inventor
Gabriela Philippart
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 SASfiledCriticalSafran Aircraft Engines SAS
Priority to FR1902532ApriorityCriticalpatent/FR3093765B1/en
Publication of FR3093765A1publicationCriticalpatent/FR3093765A1/en
Application grantedgrantedCritical
Publication of FR3093765B1publicationCriticalpatent/FR3093765B1/en
Activelegal-statusCriticalCurrent
Anticipated expirationlegal-statusCritical

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Abstract

Translated fromFrench

L'invention concerne un système échangeur de chaleur (17) d’une turbomachine (1) comprenant un compartiment moteur (14) dans lequel circule de l’huile (H), ce compartiment moteur (14) comprenant un carter (15) délimitant une veine secondaire (13) de la turbomachine (1), caractérisée en ce que le système échangeur de chaleur (17) comporte un conduit (18) qui est ménagé dans le compartiment moteur (14), ce conduit s’étendant depuis une ouverture d’aspiration (19) formée au niveau du carter (15) pour prélever de l’air (Fp) depuis la veine secondaire (13) pour circuler dans le conduit (18), le conduit étant délimité par au moins une paroi (27, 47) séparant l’air prélevée (Fp) de l’huile (H) pour établir un échange thermique entre l’air prélevé (Fp) et l’huile (H) à travers ladite au moins une paroi (27, 47). Figure pour l’abrégé : Figure 2The invention relates to a heat exchanger system (17) for a turbomachine (1) comprising an engine compartment (14) in which oil (H) circulates, this engine compartment (14) comprising a casing (15) delimiting a secondary stream (13) of the turbomachine (1), characterized in that the heat exchanger system (17) comprises a duct (18) which is formed in the engine compartment (14), this duct extending from an opening suction (19) formed at the level of the housing (15) to take air (Fp) from the secondary stream (13) to circulate in the duct (18), the duct being delimited by at least one wall (27 , 47) separating the air taken (Fp) from the oil (H) to establish a heat exchange between the air taken (Fp) and the oil (H) through said at least one wall (27, 47) . Figure for the abstract: Figure 2

FR1902532A2019-03-122019-03-12 OPTIMIZED TURBOMACHINE AIR-OIL HEAT EXCHANGER SYSTEMActiveFR3093765B1 (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
FR1902532AFR3093765B1 (en)2019-03-122019-03-12 OPTIMIZED TURBOMACHINE AIR-OIL HEAT EXCHANGER SYSTEM

Applications Claiming Priority (2)

Application NumberPriority DateFiling DateTitle
FR1902532AFR3093765B1 (en)2019-03-122019-03-12 OPTIMIZED TURBOMACHINE AIR-OIL HEAT EXCHANGER SYSTEM
FR19025322019-03-12

Publications (2)

Publication NumberPublication Date
FR3093765A1 FR3093765A1 (en)2020-09-18
FR3093765B1true FR3093765B1 (en)2021-05-14

Family

ID=66776635

Family Applications (1)

Application NumberTitlePriority DateFiling Date
FR1902532AActiveFR3093765B1 (en)2019-03-122019-03-12 OPTIMIZED TURBOMACHINE AIR-OIL HEAT EXCHANGER SYSTEM

Country Status (1)

CountryLink
FR (1)FR3093765B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
FR3146165A1 (en)2023-02-232024-08-30Safran HEAT EXCHANGE SYSTEM FOR AN AIRCRAFT TURBOMACHINE

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
EP2336525B1 (en)*2009-12-212015-08-26Techspace Aero S.A.Integration of an air-liquid heat exchanger on an engine
EP2472067B1 (en)*2010-12-312013-09-25Techspace Aero S.A.Integration of a surface heat exchanger with controlled air flow in an airplane engine
US10323540B2 (en)*2015-12-072019-06-18General Electric CompanyGas turbine engine fluid cooling systems and methods of assembling the same
FR3044636B1 (en)*2015-12-082019-08-30Safran Aircraft Engines AIRCRAFT TURBOMACHINE EQUIPPED WITH AIR-OIL SURFACE HEAT EXCHANGER

Also Published As

Publication numberPublication date
FR3093765A1 (en)2020-09-18

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