PL3980692T3 - Sposób wytwarzania rury płomieniowej do maszyny wirowej - Google Patents

Sposób wytwarzania rury płomieniowej do maszyny wirowej

Info

Publication number
PL3980692T3
PL3980692T3 PL20740371.8T PL20740371T PL3980692T3 PL 3980692 T3 PL3980692 T3 PL 3980692T3 PL 20740371 T PL20740371 T PL 20740371T PL 3980692 T3 PL3980692 T3 PL 3980692T3
Authority
PL
Poland
Prior art keywords
turbomachine
manufacturing
flame tube
flame
tube
Prior art date
Application number
PL20740371.8T
Other languages
English (en)
Inventor
Stéphane LAVIGNOTTE
Guillaume Thierry COTTIN
Jean-Paul Didier AUTRET
Mehdi DELIBA
Thomas Sebastien Alexandre GRESY
Nicolas Roland Guy SAVARY
Original Assignee
Safran Helicopter Engines
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
Priority claimed from FR1906074A external-priority patent/FR3097028B1/fr
Priority claimed from FR1906073A external-priority patent/FR3097029B1/fr
Application filed by Safran Helicopter Engines filed Critical Safran Helicopter Engines
Publication of PL3980692T3 publication Critical patent/PL3980692T3/pl

Links

Classifications

    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/44—Combustion chambers comprising a single tubular flame tube within a tubular casing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20—Direct sintering or melting
    • B22F10/28—Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/34—Laser welding for purposes other than joining
    • B23K26/342—Build-up welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y10/00—Processes of additive manufacturing
    • 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
    • F23R3/005—Combined with pressure or heat exchangers
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2301/00—Metallic composition of the powder or its coating
    • B22F2301/15—Nickel or cobalt
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/001—Turbines
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00018—Manufacturing combustion chamber liners or subparts
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03043—Convection cooled combustion chamber walls with means for guiding the cooling air flow
    • 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
    • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00—Technologies related to metal processing
    • Y02P10/25—Process efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Optics & Photonics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Powder Metallurgy (AREA)
PL20740371.8T 2019-06-07 2020-06-03 Sposób wytwarzania rury płomieniowej do maszyny wirowej PL3980692T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1906074A FR3097028B1 (fr) 2019-06-07 2019-06-07 Procédé de fabrication d’un tube à flamme pour une turbomachine
FR1906073A FR3097029B1 (fr) 2019-06-07 2019-06-07 Procédé de fabrication d’un tube à flamme pour une turbomachine
PCT/FR2020/050940 WO2020245537A1 (fr) 2019-06-07 2020-06-03 Procédé de fabrication d'un tube à flamme pour une turbomachine

Publications (1)

Publication Number Publication Date
PL3980692T3 true PL3980692T3 (pl) 2025-02-03

Family

ID=71614919

Family Applications (1)

Application Number Title Priority Date Filing Date
PL20740371.8T PL3980692T3 (pl) 2019-06-07 2020-06-03 Sposób wytwarzania rury płomieniowej do maszyny wirowej

Country Status (6)

Country Link
US (1) US12345418B2 (pl)
EP (1) EP3980692B1 (pl)
CN (1) CN113924444A (pl)
CA (1) CA3141179A1 (pl)
PL (1) PL3980692T3 (pl)
WO (1) WO2020245537A1 (pl)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3980692B1 (fr) * 2019-06-07 2024-10-23 Safran Helicopter Engines Procédé de fabrication d'un tube à flamme pour une turbomachine
CN119642221B (zh) * 2023-09-15 2025-11-25 中国航发商用航空发动机有限责任公司 燃烧室及燃烧室级间段

Family Cites Families (36)

* Cited by examiner, † Cited by third party
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US3360929A (en) * 1966-03-10 1968-01-02 Montrose K. Drewry Gas turbine combustors
US3719046A (en) * 1970-07-02 1973-03-06 Rocket Research Corp Rocket engine cooling system
US3735806A (en) * 1970-12-07 1973-05-29 Trw Inc Unidirectional thermal transfer means
GB1505499A (en) * 1975-06-23 1978-03-30 Lucas Industries Ltd Flame tube assembly for a gas turbine engine
FR2340453A1 (fr) * 1976-02-06 1977-09-02 Snecma Corps de chambre de combustion, notamment pour turboreacteurs
US4896510A (en) * 1987-02-06 1990-01-30 General Electric Company Combustor liner cooling arrangement
DE59208713D1 (de) * 1992-11-09 1997-08-21 Asea Brown Boveri Gasturbinen-Brennkammer
US5623827A (en) * 1995-01-26 1997-04-29 General Electric Company Regenerative cooled dome assembly for a gas turbine engine combustor
US6581386B2 (en) * 2001-09-29 2003-06-24 General Electric Company Threaded combustor baffle
US7043921B2 (en) * 2003-08-26 2006-05-16 Honeywell International, Inc. Tube cooled combustor
GB2455021B (en) * 2006-09-14 2011-03-23 Solar Turbines Inc Splash plate dome assembly for a turbine engine
US9377198B2 (en) * 2012-01-31 2016-06-28 United Technologies Corporation Heat shield for a combustor
FR2996289B1 (fr) 2012-10-01 2018-10-12 Turbomeca Chambre de combustion comprenant un tube a flamme fixe au moyen de trois elements de centrage.
EP2846096A1 (de) * 2013-09-09 2015-03-11 Siemens Aktiengesellschaft Rohrbrennkammer mit einem Flammrohr-Endbereich und Gasturbine
EP2927596A1 (de) * 2014-03-31 2015-10-07 Siemens Aktiengesellschaft Silobrennkammer für eine Gasturbine
US9810148B2 (en) * 2014-07-24 2017-11-07 United Technologies Corporation Self-cooled orifice structure
US9470421B2 (en) * 2014-08-19 2016-10-18 General Electric Company Combustor cap assembly
FR3030323B1 (fr) 2014-12-23 2019-08-09 Safran Aircraft Engines Plateau de fabrication pour la fabrication de pieces par fusion selective ou frittage selectif sur lit de poudre, outillage et procede de fabrication mettant en oeuvre un tel plateau
US10480787B2 (en) 2015-03-26 2019-11-19 United Technologies Corporation Combustor wall cooling channel formed by additive manufacturing
FR3038699B1 (fr) * 2015-07-08 2022-06-24 Snecma Chambre de combustion coudee d'une turbomachine
EP3144485A1 (en) * 2015-09-16 2017-03-22 Siemens Aktiengesellschaft Turbomachine component with cooling features and a method for manufacturing such a turbomachine component
US9989260B2 (en) * 2015-12-22 2018-06-05 General Electric Company Staged fuel and air injection in combustion systems of gas turbines
DE102016219424A1 (de) * 2016-10-06 2018-04-12 Rolls-Royce Deutschland Ltd & Co Kg Brennkammeranordnung einer Gasturbine sowie Fluggasturbine
DE102016224632A1 (de) 2016-12-09 2018-06-14 Rolls-Royce Deutschland Ltd & Co Kg Plattenförmiges Bauteil einer Gasturbine sowie Verfahren zu dessen Herstellung
WO2018144008A1 (en) * 2017-02-03 2018-08-09 Siemens Aktiengesellschaft Combustor with three-dimensional lattice premixer
US11073282B2 (en) 2017-08-25 2021-07-27 Delavan Inc. Gas turbine combustion liner comprising heat transfer cell heat pipes
US10982851B2 (en) * 2017-09-18 2021-04-20 General Electric Company Additively manufactured wall and floating ferrule having a frangible member between the floating ferrule and a build support arm
DE102017216595A1 (de) 2017-09-19 2019-03-21 Rolls-Royce Deutschland Ltd & Co Kg Triebwerksbauteil mit mindestens einem Kühlloch
US10928067B2 (en) * 2017-10-31 2021-02-23 Pratt & Whitney Canada Corp. Double skin combustor
US11187412B2 (en) * 2018-08-22 2021-11-30 General Electric Company Flow control wall assembly for heat engine
US11280492B2 (en) * 2018-08-23 2022-03-22 General Electric Company Combustor assembly for a turbo machine
US10982852B2 (en) * 2018-11-05 2021-04-20 Rolls-Royce Corporation Cowl integration to combustor wall
FR3097029B1 (fr) * 2019-06-07 2021-05-21 Safran Helicopter Engines Procédé de fabrication d’un tube à flamme pour une turbomachine
FR3097028B1 (fr) * 2019-06-07 2021-05-14 Safran Helicopter Engines Procédé de fabrication d’un tube à flamme pour une turbomachine
EP3980692B1 (fr) * 2019-06-07 2024-10-23 Safran Helicopter Engines Procédé de fabrication d'un tube à flamme pour une turbomachine
CN113175688B (zh) * 2021-04-15 2022-07-01 中国航发湖南动力机械研究所 双层壁大弯管

Also Published As

Publication number Publication date
CA3141179A1 (fr) 2020-12-10
US20220252268A1 (en) 2022-08-11
US12345418B2 (en) 2025-07-01
CN113924444A (zh) 2022-01-11
EP3980692B1 (fr) 2024-10-23
EP3980692A1 (fr) 2022-04-13
WO2020245537A1 (fr) 2020-12-10

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