FR2990001B1 - Assemblage d'un echangeur thermique au sein d'un carter intermediaire de turboreacteur - Google Patents

Assemblage d'un echangeur thermique au sein d'un carter intermediaire de turboreacteur

Info

Publication number
FR2990001B1
FR2990001B1 FR1253937A FR1253937A FR2990001B1 FR 2990001 B1 FR2990001 B1 FR 2990001B1 FR 1253937 A FR1253937 A FR 1253937A FR 1253937 A FR1253937 A FR 1253937A FR 2990001 B1 FR2990001 B1 FR 2990001B1
Authority
FR
France
Prior art keywords
assembling
heat exchanger
core case
turbo
intermediate turbo
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
FR1253937A
Other languages
English (en)
Other versions
FR2990001A1 (fr
Inventor
Frederic Paul Eichstadt
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 FR1253937A priority Critical patent/FR2990001B1/fr
Publication of FR2990001A1 publication Critical patent/FR2990001A1/fr
Application granted granted Critical
Publication of FR2990001B1 publication Critical patent/FR2990001B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • 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
    • 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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/766—Control or regulation of thrust reversers with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
    • 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
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • 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
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1253937A 2012-04-27 2012-04-27 Assemblage d'un echangeur thermique au sein d'un carter intermediaire de turboreacteur Active FR2990001B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1253937A FR2990001B1 (fr) 2012-04-27 2012-04-27 Assemblage d'un echangeur thermique au sein d'un carter intermediaire de turboreacteur

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1253937A FR2990001B1 (fr) 2012-04-27 2012-04-27 Assemblage d'un echangeur thermique au sein d'un carter intermediaire de turboreacteur

Publications (2)

Publication Number Publication Date
FR2990001A1 FR2990001A1 (fr) 2013-11-01
FR2990001B1 true FR2990001B1 (fr) 2016-01-08

Family

ID=46506504

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1253937A Active FR2990001B1 (fr) 2012-04-27 2012-04-27 Assemblage d'un echangeur thermique au sein d'un carter intermediaire de turboreacteur

Country Status (1)

Country Link
FR (1) FR2990001B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109154254A (zh) * 2016-05-18 2019-01-04 和谐工业有限责任公司 涡轮发动机冷却器组合件

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2994216B1 (fr) * 2012-08-02 2014-09-05 Snecma Partie de revolution de carter intermediaire comportant un insert dispose dans une rainure annulaire
US9677474B2 (en) * 2013-11-18 2017-06-13 Unison Industries, Llc Surface cooler support mechanism
US10393147B2 (en) * 2015-07-23 2019-08-27 Unison Industries, Llc Fan casing assemblies and method of mounting a cooler to a fan casing
GB201712242D0 (en) 2017-07-31 2017-09-13 Rolls Royce Plc A mount assembly

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8387362B2 (en) * 2006-10-19 2013-03-05 Michael Ralph Storage Method and apparatus for operating gas turbine engine heat exchangers
FR2925120B1 (fr) * 2007-12-18 2010-02-19 Snecma Extension de carter intermediaire pour turboreacteur d'aeronef, comprenant une rainure annulaire sectorisee de reception des capots de nacelle
US8181443B2 (en) * 2008-12-10 2012-05-22 Pratt & Whitney Canada Corp. Heat exchanger to cool turbine air cooling flow
US8510945B2 (en) * 2009-12-22 2013-08-20 Unison Industries, Llc Method of mounting a heat exchanger in a gas turbine engine assembly
EP2339123B1 (fr) * 2009-12-23 2013-07-10 Techspace Aero S.A. Paroi intérieure annulaire de la veine secondaire d'un turboréacteur et procédé d'assemblage d'une telle paroi

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109154254A (zh) * 2016-05-18 2019-01-04 和谐工业有限责任公司 涡轮发动机冷却器组合件
CN109154254B (zh) * 2016-05-18 2020-12-22 和谐工业有限责任公司 涡轮发动机冷却器组合件

Also Published As

Publication number Publication date
FR2990001A1 (fr) 2013-11-01

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