FR2976975B1 - Ventilation de relais d'accessoires, turboreacteur comportant un tel relais - Google Patents

Ventilation de relais d'accessoires, turboreacteur comportant un tel relais

Info

Publication number
FR2976975B1
FR2976975B1 FR1155520A FR1155520A FR2976975B1 FR 2976975 B1 FR2976975 B1 FR 2976975B1 FR 1155520 A FR1155520 A FR 1155520A FR 1155520 A FR1155520 A FR 1155520A FR 2976975 B1 FR2976975 B1 FR 2976975B1
Authority
FR
France
Prior art keywords
relay
accessories
vent
turbojet engine
turbojet
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
FR1155520A
Other languages
English (en)
Other versions
FR2976975A1 (fr
Inventor
Pierrick Charlemagne
Gerard Philippe Gauthier
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 FR1155520A priority Critical patent/FR2976975B1/fr
Priority to US14/127,387 priority patent/US9599023B2/en
Priority to GB1322868.9A priority patent/GB2506543B/en
Priority to PCT/FR2012/051422 priority patent/WO2012175883A1/fr
Publication of FR2976975A1 publication Critical patent/FR2976975A1/fr
Application granted granted Critical
Publication of FR2976975B1 publication Critical patent/FR2976975B1/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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • 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
    • F05D2260/40—Transmission of power
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
    • 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)
FR1155520A 2011-06-22 2011-06-22 Ventilation de relais d'accessoires, turboreacteur comportant un tel relais Active FR2976975B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1155520A FR2976975B1 (fr) 2011-06-22 2011-06-22 Ventilation de relais d'accessoires, turboreacteur comportant un tel relais
US14/127,387 US9599023B2 (en) 2011-06-22 2012-06-21 Ventilation of an accessory gear box, and turbojet engine comprising such a gear box
GB1322868.9A GB2506543B (en) 2011-06-22 2012-06-21 Ventilation of an accessory gear box, and a multi-flow turbojet engine comprising such a gear box
PCT/FR2012/051422 WO2012175883A1 (fr) 2011-06-22 2012-06-21 Ventilation de relais d'accessoires, turboreacteur comportant un tel relais

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1155520A FR2976975B1 (fr) 2011-06-22 2011-06-22 Ventilation de relais d'accessoires, turboreacteur comportant un tel relais

Publications (2)

Publication Number Publication Date
FR2976975A1 FR2976975A1 (fr) 2012-12-28
FR2976975B1 true FR2976975B1 (fr) 2013-06-28

Family

ID=46456915

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1155520A Active FR2976975B1 (fr) 2011-06-22 2011-06-22 Ventilation de relais d'accessoires, turboreacteur comportant un tel relais

Country Status (4)

Country Link
US (1) US9599023B2 (fr)
FR (1) FR2976975B1 (fr)
GB (1) GB2506543B (fr)
WO (1) WO2012175883A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3366385A1 (fr) 2017-02-28 2018-08-29 Safran Transmission Systems Sable de moulage comprenant des nanoparticules de graphite et moule fabriqué à partir d'un tel sable de moulage

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3965673A (en) * 1973-05-19 1976-06-29 Vereinigte Flugtechnische Werke-Fokker Gesellschaft Mit Beschrankter Haftung Apparatus for starting aircraft engines and for operating auxiliary on-board power generating equipment
GB2076897B (en) * 1980-06-02 1983-06-29 Rockwell International Corp Integrated auxiliary and environmental control unit
US5184458A (en) * 1989-11-21 1993-02-09 Lampe Steven W Power unit fuel pressurization system
US5125597A (en) * 1990-06-01 1992-06-30 General Electric Company Gas turbine engine powered aircraft environmental control system and boundary layer bleed with energy recovery system
US5402631A (en) * 1991-05-10 1995-04-04 Praxair Technology, Inc. Integration of combustor-turbine units and integral-gear pressure processors
US7805947B2 (en) * 2005-05-19 2010-10-05 Djamal Moulebhar Aircraft with disengageable engine and auxiliary power unit components
GB0714924D0 (en) * 2007-08-01 2007-09-12 Rolls Royce Plc An engine arrangement

Also Published As

Publication number Publication date
FR2976975A1 (fr) 2012-12-28
GB2506543B (en) 2016-01-13
US9599023B2 (en) 2017-03-21
WO2012175883A1 (fr) 2012-12-27
GB2506543A (en) 2014-04-02
GB201322868D0 (en) 2014-02-12
US20140116064A1 (en) 2014-05-01

Similar Documents

Publication Publication Date Title
EP2809909A4 (fr) Système tampon pour moteur à turbine à gaz assurant une ventilation par zones
EP2837789A4 (fr) Moteur à essence à deux temps
SG11201403706WA (en) Low noise turbine for geared turbofan engine
FR2987079B1 (fr) Cone d'echappement avec systeme d'attenuation acoustique
EP2528674A4 (fr) Coalesceur rotatif à flux de l'intérieur vers l'extérieur pour la ventilation de carter de moteur
BR112013014429A2 (pt) composições de cultura iniciadora
EP2673492A4 (fr) Ensemble filtre à air pour un moteur
EP2821613A4 (fr) Structure de ventilation d'un compartiment moteur
EP2534030A4 (fr) Capot de moteur
BR112013030537A2 (pt) condicionador de ar.
PL2582923T3 (pl) Konfiguracja niesmarowanej maszyny wirowej
BR112013010654A2 (pt) nacela de motor turbojato compreendendo uma estrutura fixa
EP2865866A4 (fr) Carter de ventilateur destiné à un moteur d'avion
EP2650529A4 (fr) Démarreur de moteur
EP2580465A4 (fr) Démarreur de moteur
EP2698510A4 (fr) Dispositif de ventilation de carter
IT1398957B1 (it) Apparato di pulizia di gas prodotto da gassificatori.
BRPI1008068A2 (pt) nacela de motor turbojato
EP2754864A4 (fr) Appareil de ventilation de moteur
EP2924254A4 (fr) Structure de montage de système de récupération des gaz du carter moteur
DK2638132T3 (da) Ildstarter
MX2011011059A (es) Uso de propineb como repelente de aves.
EP2921399A4 (fr) Structure d'admission d'air pour moteur hors-bord
EP2789645A4 (fr) Capot moteur
FR2969412B1 (fr) Support moteur a decouplage ameliore pour systeme de ventilation

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170719

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13