FR3046951B1 - Procede de fabrication d'une piece d'une turbomachine et piece ainsi realisee - Google Patents

Procede de fabrication d'une piece d'une turbomachine et piece ainsi realisee Download PDF

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Publication number
FR3046951B1
FR3046951B1 FR1650492A FR1650492A FR3046951B1 FR 3046951 B1 FR3046951 B1 FR 3046951B1 FR 1650492 A FR1650492 A FR 1650492A FR 1650492 A FR1650492 A FR 1650492A FR 3046951 B1 FR3046951 B1 FR 3046951B1
Authority
FR
France
Prior art keywords
piece
turbomachine
manufacturing
produced
piece produced
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
FR1650492A
Other languages
English (en)
Other versions
FR3046951A1 (fr
Inventor
Nicolas Pommier
Mathieu BISSARDON
Mathieu DELALANDRE
Nicolas Piron Stephane
Olivier Renon
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
Safran Aircraft Engines SAS
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 Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1650492A priority Critical patent/FR3046951B1/fr
Priority to US15/409,852 priority patent/US11346250B2/en
Publication of FR3046951A1 publication Critical patent/FR3046951A1/fr
Application granted granted Critical
Publication of FR3046951B1 publication Critical patent/FR3046951B1/fr
Priority to US17/655,748 priority patent/US11692459B2/en
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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • F01D17/145—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path by means of valves, e.g. for steam turbines
    • 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
    • F01D25/30—Exhaust heads, chambers, or the like
    • 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
    • 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
    • F02K3/075—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 controlling flow ratio between flows
    • 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
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/10—Manufacture by removing material
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Exhaust Silencers (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
FR1650492A 2016-01-21 2016-01-21 Procede de fabrication d'une piece d'une turbomachine et piece ainsi realisee Active FR3046951B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1650492A FR3046951B1 (fr) 2016-01-21 2016-01-21 Procede de fabrication d'une piece d'une turbomachine et piece ainsi realisee
US15/409,852 US11346250B2 (en) 2016-01-21 2017-01-19 Method for manufacturing a turbine engine part and the thereby produced part
US17/655,748 US11692459B2 (en) 2016-01-21 2022-03-21 Method for manufacturing a turbine engine part and the thereby produced part

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1650492A FR3046951B1 (fr) 2016-01-21 2016-01-21 Procede de fabrication d'une piece d'une turbomachine et piece ainsi realisee
FR1650492 2016-01-21

Publications (2)

Publication Number Publication Date
FR3046951A1 FR3046951A1 (fr) 2017-07-28
FR3046951B1 true FR3046951B1 (fr) 2018-01-12

Family

ID=55486941

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1650492A Active FR3046951B1 (fr) 2016-01-21 2016-01-21 Procede de fabrication d'une piece d'une turbomachine et piece ainsi realisee

Country Status (2)

Country Link
US (2) US11346250B2 (fr)
FR (1) FR3046951B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3046951B1 (fr) 2016-01-21 2018-01-12 Safran Aircraft Engines Procede de fabrication d'une piece d'une turbomachine et piece ainsi realisee
FR3051840B1 (fr) * 2016-05-31 2020-01-10 Safran Aircraft Engines Carter intermediaire de turbomachine, equipee d'une piece d'etancheite a interface bras/virole
US11162425B2 (en) * 2019-06-11 2021-11-02 Rolls-Royce Corporation Assembly fixture
FR3110201B1 (fr) * 2020-05-15 2022-04-08 Safran Aircraft Engines Carter d’échappement de turbomachine

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2896906A (en) * 1956-03-26 1959-07-28 William J Durkin Turbine cooling air metering system
US3286461A (en) * 1965-07-22 1966-11-22 Gen Motors Corp Turbine starter and cooling
US5134844A (en) * 1990-07-30 1992-08-04 General Electric Company Aft entry cooling system and method for an aircraft engine
US5292227A (en) * 1992-12-10 1994-03-08 General Electric Company Turbine frame
FR2829193B1 (fr) * 2001-08-30 2005-04-08 Snecma Moteurs Systeme de prelevement d'air d'un compresseur
EP1780382A3 (fr) * 2003-07-29 2011-03-09 Pratt & Whitney Canada Corp. Enveloppe de réacteur à double flux et procédé de fabrication
US7370467B2 (en) * 2003-07-29 2008-05-13 Pratt & Whitney Canada Corp. Turbofan case and method of making
FR2897006B1 (fr) * 2006-02-09 2008-05-09 Snecma Sa Procede de decoupe par faisceau laser
US9194258B2 (en) * 2012-02-27 2015-11-24 Pratt & Whitney Canada Corp. Gas turbine engine case bosses
US8888427B2 (en) * 2012-07-26 2014-11-18 Cnh Industrial America Llc System for preventing rotation of fasteners
FR2994712B1 (fr) * 2012-08-27 2018-04-13 Safran Aircraft Engines Procede d'assemblage d'une tuyere et d'un carter d'echappement d'une turbomachine
US9376935B2 (en) * 2012-12-18 2016-06-28 Pratt & Whitney Canada Corp. Gas turbine engine mounting ring
US10240532B2 (en) 2012-12-29 2019-03-26 United Technologies Corporation Frame junction cooling holes
EP3114328B1 (fr) * 2014-02-19 2020-01-29 United Technologies Corporation Géométrie de bossage à contrainte réduite pour une carcasse d'un moteur à turbine à gaz
FR3018114B1 (fr) * 2014-03-03 2016-03-25 Turbomeca Dispositif pour le positionnement d'un outil d'inspection
US10202857B2 (en) * 2015-02-06 2019-02-12 United Technologies Corporation Vane stages
FR3039207B1 (fr) * 2015-07-21 2019-07-26 Safran Aircraft Engines Carter d'echappement d'une turbomachine a duree de vie augmentee
FR3046951B1 (fr) * 2016-01-21 2018-01-12 Safran Aircraft Engines Procede de fabrication d'une piece d'une turbomachine et piece ainsi realisee

Also Published As

Publication number Publication date
US11346250B2 (en) 2022-05-31
US20220213807A1 (en) 2022-07-07
FR3046951A1 (fr) 2017-07-28
US11692459B2 (en) 2023-07-04
US20170211420A1 (en) 2017-07-27

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