FR2995497B1 - Turbomachine d'aeronef comprenant au moins un systeme de refroidissement d'au moins un dispositif electronique - Google Patents

Turbomachine d'aeronef comprenant au moins un systeme de refroidissement d'au moins un dispositif electronique

Info

Publication number
FR2995497B1
FR2995497B1 FR1258455A FR1258455A FR2995497B1 FR 2995497 B1 FR2995497 B1 FR 2995497B1 FR 1258455 A FR1258455 A FR 1258455A FR 1258455 A FR1258455 A FR 1258455A FR 2995497 B1 FR2995497 B1 FR 2995497B1
Authority
FR
France
Prior art keywords
electronic device
cooling system
aircraft turbomachine
turbomachine
aircraft
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.)
Expired - Fee Related
Application number
FR1258455A
Other languages
English (en)
Other versions
FR2995497A1 (fr
Inventor
Olivier Verseux
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations 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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1258455A priority Critical patent/FR2995497B1/fr
Publication of FR2995497A1 publication Critical patent/FR2995497A1/fr
Application granted granted Critical
Publication of FR2995497B1 publication Critical patent/FR2995497B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • H05K7/20009—Modifications to facilitate cooling, ventilating, or heating using a gaseous coolant in electronic enclosures
    • H05K7/20136—Forced ventilation, e.g. by fans
    • H05K7/20154—Heat dissipaters coupled to components
    • H05K7/20163—Heat dissipaters coupled to components the components being isolated from air flow, e.g. hollow heat sinks, wind tunnels or funnels

Landscapes

  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1258455A 2012-09-10 2012-09-10 Turbomachine d'aeronef comprenant au moins un systeme de refroidissement d'au moins un dispositif electronique Expired - Fee Related FR2995497B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1258455A FR2995497B1 (fr) 2012-09-10 2012-09-10 Turbomachine d'aeronef comprenant au moins un systeme de refroidissement d'au moins un dispositif electronique

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1258455A FR2995497B1 (fr) 2012-09-10 2012-09-10 Turbomachine d'aeronef comprenant au moins un systeme de refroidissement d'au moins un dispositif electronique

Publications (2)

Publication Number Publication Date
FR2995497A1 FR2995497A1 (fr) 2014-03-14
FR2995497B1 true FR2995497B1 (fr) 2016-06-10

Family

ID=47022932

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1258455A Expired - Fee Related FR2995497B1 (fr) 2012-09-10 2012-09-10 Turbomachine d'aeronef comprenant au moins un systeme de refroidissement d'au moins un dispositif electronique

Country Status (1)

Country Link
FR (1) FR2995497B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150034278A1 (en) * 2013-07-30 2015-02-05 Hamilton Sundstrand Corporation Heat pipe matrix for electronics cooling
US20170184026A1 (en) * 2015-12-28 2017-06-29 General Electric Company System and method of soakback mitigation through passive cooling
FR3072649B1 (fr) 2017-10-20 2019-11-08 Airbus Operations Systeme de protection contre le givre pour nacelle de moteur d'aeronef
GB201800778D0 (en) * 2018-01-18 2018-03-07 Rolls Royce Plc Mount for a gas turbine engine unit

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090175718A1 (en) * 2007-12-31 2009-07-09 Carlos Diaz System and method for passive cooling of gas turbine engine control components
US8235096B1 (en) * 2009-04-07 2012-08-07 University Of Central Florida Research Foundation, Inc. Hydrophilic particle enhanced phase change-based heat exchange
TWI437951B (zh) * 2009-09-08 2014-05-11 Sunonwealth Electr Mach Ind Co 散熱裝置

Also Published As

Publication number Publication date
FR2995497A1 (fr) 2014-03-14

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