FR2907166B1 - Agencement de prelevement de gaz sur un carter de turbomachine, carter le comportant, et moteur d'aeronef en etant muni - Google Patents

Agencement de prelevement de gaz sur un carter de turbomachine, carter le comportant, et moteur d'aeronef en etant muni

Info

Publication number
FR2907166B1
FR2907166B1 FR0654241A FR0654241A FR2907166B1 FR 2907166 B1 FR2907166 B1 FR 2907166B1 FR 0654241 A FR0654241 A FR 0654241A FR 0654241 A FR0654241 A FR 0654241A FR 2907166 B1 FR2907166 B1 FR 2907166B1
Authority
FR
France
Prior art keywords
munied
casting
arrangement
component
aircraft engine
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
FR0654241A
Other languages
English (en)
Other versions
FR2907166A1 (fr
Inventor
Laurent Pierre Elysee Gaston Marnas
Gilles Charles Fernand Richard
Pierre Pascal Sablayrolles
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 FR0654241A priority Critical patent/FR2907166B1/fr
Publication of FR2907166A1 publication Critical patent/FR2907166A1/fr
Application granted granted Critical
Publication of FR2907166B1 publication Critical patent/FR2907166B1/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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002—Wall structures
    • 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
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • 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
    • F05D2250/00—Geometry
    • F05D2250/50—Inlet or outlet
    • F05D2250/51—Inlet

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)
FR0654241A 2006-10-12 2006-10-12 Agencement de prelevement de gaz sur un carter de turbomachine, carter le comportant, et moteur d'aeronef en etant muni Active FR2907166B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0654241A FR2907166B1 (fr) 2006-10-12 2006-10-12 Agencement de prelevement de gaz sur un carter de turbomachine, carter le comportant, et moteur d'aeronef en etant muni

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0654241A FR2907166B1 (fr) 2006-10-12 2006-10-12 Agencement de prelevement de gaz sur un carter de turbomachine, carter le comportant, et moteur d'aeronef en etant muni

Publications (2)

Publication Number Publication Date
FR2907166A1 FR2907166A1 (fr) 2008-04-18
FR2907166B1 true FR2907166B1 (fr) 2013-03-29

Family

ID=37949652

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0654241A Active FR2907166B1 (fr) 2006-10-12 2006-10-12 Agencement de prelevement de gaz sur un carter de turbomachine, carter le comportant, et moteur d'aeronef en etant muni

Country Status (1)

Country Link
FR (1) FR2907166B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2410138B8 (fr) * 2010-07-22 2017-07-19 Ansaldo Energia IP UK Limited Agencement de flasques du moteur de turbine à gaz et son procédé de reéquipement
US9200565B2 (en) * 2011-12-05 2015-12-01 Siemens Energy, Inc. Full hoop casing for midframe of industrial gas turbine engine
FR2992019B1 (fr) * 2012-06-18 2016-12-09 Snecma Carter en materiau composite pour chambre de combustion de moteur a turbine a gaz

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2702665A (en) * 1951-03-07 1955-02-22 United Aircraft Corp Stator construction for axial flow compressors
US3777489A (en) * 1972-06-01 1973-12-11 Gen Electric Combustor casing and concentric air bleed structure
FR2616889B1 (fr) * 1987-06-18 1992-07-31 Snecma Carter de chambre de combustion de turboreacteur comportant des orifices de prelevement d'air
FR2829193B1 (fr) * 2001-08-30 2005-04-08 Snecma Moteurs Systeme de prelevement d'air d'un compresseur

Also Published As

Publication number Publication date
FR2907166A1 (fr) 2008-04-18

Similar Documents

Publication Publication Date Title
FR2905983B1 (fr) Dispositif d'insonorisation d'un moteur d'helicoptere a turbine a gaz, et moteur ainsi obtenu
FR2855497B1 (fr) Nacelle pour moteur a turbine a gaz
EP1924762A4 (fr) Systemes de combustion pour turbine a gaz
FR2885167B1 (fr) Module de turbine pour moteur a turbine a gaz
GB0610271D0 (en) A gas turbine engine casing
GB2431435B (en) Gas turbine engine assembly
EP2092163A4 (fr) Ensemble d'aubes configurées pour faire tourner un écoulement dans un moteur de turbine à gaz, un composant de stator comprenant l'ensemble d'aubes, une turbine à gaz et un moteur à réaction d'avion
GB2414046B (en) Rotor assembly bypass system for gas turbine engines
EP2142761A4 (fr) Composant de moteur à turbine à gaz, moteur à turboréacteur muni de celui-ci, et avion muni de celui-ci
EP1998012A3 (fr) Porte d'accès dans le carter d'une turbine à gaz
GB2411437B (en) Aircraft gas turbine engines
GB2441342B (en) Wall elements with apertures for gas turbine engine components
GB2426289B (en) Cooling system for a gas turbine engine
GB0206139D0 (en) A variable position intake for an aircraft mounted gas turbine engine
GB2428087B (en) A gas turbine engine incorporating an engine monitoring arrangement for monitoring gas constituents in an exhaust flow
GB0403941D0 (en) A gas turbine engine blade containment assembly
FR2875535B1 (fr) Module de turbine pour moteur a turbine a gaz
GB2415749B (en) A gas turbine engine including an exhaust duct comprising a diffuser for diffusing the exhaust gas produced by the engine
FR2907166B1 (fr) Agencement de prelevement de gaz sur un carter de turbomachine, carter le comportant, et moteur d'aeronef en etant muni
EP2155555A4 (fr) Element de montage pour moteur de turbine a gaz et structure et aeronef comportant un tel element de montage
FR2895020B1 (fr) Agencement de prelevement de gaz sur un carter de turbomachine, carter le comportant, et moteur d'aeronef en etant muni
GB2405451B (en) Vane apparatus for a gas turbine engine
GB2444947B (en) Wall elements for gas turbine engine components
GB0617925D0 (en) Components for a gas turbine engine
FR2900979B1 (fr) Ensemble moteur pour aeronef comprenant un cone d'ejection des gaz monte sur un carter moteur a l'aide d'une bride de jonction externe

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170717

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 15

PLFP Fee payment

Year of fee payment: 16

PLFP Fee payment

Year of fee payment: 17

PLFP Fee payment

Year of fee payment: 18