FR2960912B1 - Dispositif de protection d'un calculateur de turbo-machine d'aeronef en cas de feu - Google Patents

Dispositif de protection d'un calculateur de turbo-machine d'aeronef en cas de feu

Info

Publication number
FR2960912B1
FR2960912B1 FR1054488A FR1054488A FR2960912B1 FR 2960912 B1 FR2960912 B1 FR 2960912B1 FR 1054488 A FR1054488 A FR 1054488A FR 1054488 A FR1054488 A FR 1054488A FR 2960912 B1 FR2960912 B1 FR 2960912B1
Authority
FR
France
Prior art keywords
fire
protecting
cases
aircraft turbo
machine calculator
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
FR1054488A
Other languages
English (en)
Other versions
FR2960912A1 (fr
Inventor
Bruno Robert Gaully
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
SNECMA 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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1054488A priority Critical patent/FR2960912B1/fr
Publication of FR2960912A1 publication Critical patent/FR2960912A1/fr
Application granted granted Critical
Publication of FR2960912B1 publication Critical patent/FR2960912B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F1/00Details not covered by groups G06F3/00 - G06F13/00 and G06F21/00
    • G06F1/16Constructional details or arrangements
    • G06F1/20Cooling means
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00Constructional details common to different types of electric apparatus
    • H05K7/20Modifications to facilitate cooling, ventilating, or heating
    • H05K7/20009Modifications to facilitate cooling, ventilating, or heating using a gaseous coolant in electronic enclosures
    • H05K7/20136Forced ventilation, e.g. by fans

Landscapes

  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Thermal Sciences (AREA)
  • Human Computer Interaction (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1054488A 2010-06-08 2010-06-08 Dispositif de protection d'un calculateur de turbo-machine d'aeronef en cas de feu Active FR2960912B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1054488A FR2960912B1 (fr) 2010-06-08 2010-06-08 Dispositif de protection d'un calculateur de turbo-machine d'aeronef en cas de feu

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1054488A FR2960912B1 (fr) 2010-06-08 2010-06-08 Dispositif de protection d'un calculateur de turbo-machine d'aeronef en cas de feu

Publications (2)

Publication Number Publication Date
FR2960912A1 FR2960912A1 (fr) 2011-12-09
FR2960912B1 true FR2960912B1 (fr) 2012-06-08

Family

ID=43585646

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1054488A Active FR2960912B1 (fr) 2010-06-08 2010-06-08 Dispositif de protection d'un calculateur de turbo-machine d'aeronef en cas de feu

Country Status (1)

Country Link
FR (1) FR2960912B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015097391A1 (fr) 2013-12-24 2015-07-02 Snecma Ensemble propulsif d'aeronef avec systeme d'extinction de feu

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2998128B1 (fr) * 2012-11-13 2016-10-07 Microturbo Calculateur de turbo-machine d'aeronef
FR3009340B1 (fr) * 2013-08-01 2018-03-09 Safran Aircraft Engines Ventilation d'un equipement de turbomachine
FR3029569B1 (fr) * 2014-12-08 2017-01-13 Snecma Installation pour turbomachine comportant un connecteur de harnais relie a une cloison pare-feu
FR3044865B1 (fr) * 2015-12-08 2017-12-01 Snecma Calculateur electronique d'une turbomachine d'aeronef
US10047676B2 (en) * 2016-04-25 2018-08-14 United Technologies Corporation Electronic module mounting to vibration isolating structure
US10267236B2 (en) 2016-04-25 2019-04-23 United Technologies Corporation Electronic module mounting to vibration isolating structure

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4351150A (en) * 1980-02-25 1982-09-28 General Electric Company Auxiliary air system for gas turbine engine
US4504030A (en) * 1982-12-06 1985-03-12 United Technologies Corporation Cooling means
US7448219B2 (en) * 2004-06-21 2008-11-11 Boeing Co Hingeless flapper valve for flow control
TWI246395B (en) * 2004-11-18 2005-12-21 Delta Electronics Inc Electronic device having heat-dissipating structure for socket
US7180737B2 (en) * 2004-12-20 2007-02-20 Harris Corporation Heat exchanger system for circuit card assemblies
US7307840B2 (en) * 2005-10-14 2007-12-11 Smiths Aerospace Llc Cross-flow redundant air cooling method for high reliability electronics

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015097391A1 (fr) 2013-12-24 2015-07-02 Snecma Ensemble propulsif d'aeronef avec systeme d'extinction de feu

Also Published As

Publication number Publication date
FR2960912A1 (fr) 2011-12-09

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