FR3023587B1 - Turbomachine a systeme de refroidissement autonome d'equipements. - Google Patents

Turbomachine a systeme de refroidissement autonome d'equipements.

Info

Publication number
FR3023587B1
FR3023587B1 FR1456682A FR1456682A FR3023587B1 FR 3023587 B1 FR3023587 B1 FR 3023587B1 FR 1456682 A FR1456682 A FR 1456682A FR 1456682 A FR1456682 A FR 1456682A FR 3023587 B1 FR3023587 B1 FR 3023587B1
Authority
FR
France
Prior art keywords
turbomachine
equipment
cooling system
autonomous cooling
autonomous
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
FR1456682A
Other languages
English (en)
Other versions
FR3023587A1 (fr
Inventor
Olivier Lafargue
Stephen Langford
Sebastien Combebias
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 Helicopter Engines SAS
Original Assignee
Turbomeca SA
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 Turbomeca SA filed Critical Turbomeca SA
Priority to FR1456682A priority Critical patent/FR3023587B1/fr
Publication of FR3023587A1 publication Critical patent/FR3023587A1/fr
Application granted granted Critical
Publication of FR3023587B1 publication Critical patent/FR3023587B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
    • F02C7/055—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with intake grids, screens or guards
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/329—Application in turbines in gas turbines in helicopters
    • 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
    • F05D2260/60—Fluid transfer
    • F05D2260/607—Preventing clogging or obstruction of flow paths by dirt, dust, or foreign particles
    • 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)
FR1456682A 2014-07-10 2014-07-10 Turbomachine a systeme de refroidissement autonome d'equipements. Active FR3023587B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1456682A FR3023587B1 (fr) 2014-07-10 2014-07-10 Turbomachine a systeme de refroidissement autonome d'equipements.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1456682A FR3023587B1 (fr) 2014-07-10 2014-07-10 Turbomachine a systeme de refroidissement autonome d'equipements.

Publications (2)

Publication Number Publication Date
FR3023587A1 FR3023587A1 (fr) 2016-01-15
FR3023587B1 true FR3023587B1 (fr) 2016-07-15

Family

ID=51688246

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1456682A Active FR3023587B1 (fr) 2014-07-10 2014-07-10 Turbomachine a systeme de refroidissement autonome d'equipements.

Country Status (1)

Country Link
FR (1) FR3023587B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2995556B1 (fr) * 2014-09-12 2018-11-07 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Avion avec une prise d'air pour un moteur à propulsion

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3859785A (en) * 1973-12-17 1975-01-14 Curtiss Wright Corp Turbine engine with integral compressor and alternator rotor
DE3828834C1 (fr) * 1988-08-25 1989-11-02 Mtu Muenchen Gmbh
FR2788308A1 (fr) * 1999-01-07 2000-07-13 Snecma Dispositif de refroidissement d'un reducteur de vitesse de turbomachine
FR2955617B1 (fr) * 2010-01-26 2012-10-26 Airbus Operations Sas Propulseur a turbomachine pour aeronef
EP2712805B1 (fr) * 2012-09-28 2016-03-02 AGUSTAWESTLAND S.p.A. Système et procédé de refroidissement d'une transmission d'aéronef capable d'effectuer du vol stationnaire

Also Published As

Publication number Publication date
FR3023587A1 (fr) 2016-01-15

Similar Documents

Publication Publication Date Title
GB201619987D0 (en) Fluid cooling system
DK3167234T3 (da) Kølesystem
DE112015004508A5 (de) Fluidführungssystem
GB201409991D0 (en) Turbine case cooling system
FR3017658B1 (fr) Boitier d'entrainement d'equipements pour turbomachine
FR3026717B1 (fr) Atterrisseur d'aeronef.
FR3021993B1 (fr) Procede de dimensionnement d'une turbomachine
FR3030748B1 (fr) Systeme d'observation d'objets
FR3022281B1 (fr) Systeme d'habillage d'un grillage
FR3021531B1 (fr) Systeme de conservation
FR3020172B1 (fr) Procede de guidage d'un aeronef
DK3168555T3 (da) Køleanlæg
FR3046749B1 (fr) Systeme de gonflage-degonflage d'un pneumatique
ES1148633Y (es) Equipo autonomo para suministro de biomasa.
GB2530736B (en) Engine cooling system
FR3027015B1 (fr) Atterrisseur d'aeronef.
GB2548835B (en) A cooling system
FR3030161B1 (fr) Systeme de communication d'un aeronef
FR3023587B1 (fr) Turbomachine a systeme de refroidissement autonome d'equipements.
FR3018771B1 (fr) Aeronef muni d'un systeme avionique
FR3020170B1 (fr) Procede de guidage d'un aeronef
FR3026718B1 (fr) Systeme de roulage d'un aeronef.
FR3029019B3 (fr) Systeme d'eclairage
ES1145708Y (es) Equipo autónomo de buceo con umbilical
FR3040452B1 (fr) Systeme d'accouplement etanche

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20160115

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

CD Change of name or company name

Owner name: SAFRAN HELICOPTER ENGINES, FR

Effective date: 20170727

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10