FR3088412B1 - Chambre de combustion de turbomachine, turbomachine associee - Google Patents

Chambre de combustion de turbomachine, turbomachine associee Download PDF

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Publication number
FR3088412B1
FR3088412B1 FR1860411A FR1860411A FR3088412B1 FR 3088412 B1 FR3088412 B1 FR 3088412B1 FR 1860411 A FR1860411 A FR 1860411A FR 1860411 A FR1860411 A FR 1860411A FR 3088412 B1 FR3088412 B1 FR 3088412B1
Authority
FR
France
Prior art keywords
turbomachine
combustion chamber
turbomachine combustion
associated turbomachine
chamber
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
FR1860411A
Other languages
English (en)
Other versions
FR3088412A1 (fr
Inventor
Laurent Bernard Cameriano
Jean-Francois Cabre
Christophe Pieussergues
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
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 filed Critical Safran Aircraft Engines SAS
Priority to FR1860411A priority Critical patent/FR3088412B1/fr
Publication of FR3088412A1 publication Critical patent/FR3088412A1/fr
Application granted granted Critical
Publication of FR3088412B1 publication Critical patent/FR3088412B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F23R3/002—Wall structures
    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F02C7/266—Electric
    • 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
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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
    • F23R2900/00017—Assembling 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
    • F23R2900/00018—Manufacturing combustion chamber liners or subparts

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spark Plugs (AREA)
FR1860411A 2018-11-12 2018-11-12 Chambre de combustion de turbomachine, turbomachine associee Active FR3088412B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1860411A FR3088412B1 (fr) 2018-11-12 2018-11-12 Chambre de combustion de turbomachine, turbomachine associee

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1860411A FR3088412B1 (fr) 2018-11-12 2018-11-12 Chambre de combustion de turbomachine, turbomachine associee

Publications (2)

Publication Number Publication Date
FR3088412A1 FR3088412A1 (fr) 2020-05-15
FR3088412B1 true FR3088412B1 (fr) 2022-07-15

Family

ID=65685716

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1860411A Active FR3088412B1 (fr) 2018-11-12 2018-11-12 Chambre de combustion de turbomachine, turbomachine associee

Country Status (1)

Country Link
FR (1) FR3088412B1 (fr)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8726631B2 (en) * 2009-11-23 2014-05-20 Honeywell International Inc. Dual walled combustors with impingement cooled igniters
FR2953908A1 (fr) * 2009-12-16 2011-06-17 Snecma Guidage d'une bougie dans une chambre de combustion de turbomachine
FR2956187B1 (fr) 2010-02-11 2012-07-06 Snecma Etancheite d'un guide-bougie pour une chambre de combustion de turbomachine
US20120156020A1 (en) * 2010-12-20 2012-06-21 General Electric Company Method of repairing a transition piece of a gas turbine engine
DE102013222932A1 (de) * 2013-11-11 2015-05-28 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit Schindel zur Durchführung einer Zündkerze
FR3030741B1 (fr) * 2014-12-23 2017-07-21 Snecma Ensemble a guide-bougie pour banc d'essai
US20180030899A1 (en) * 2016-07-27 2018-02-01 Honda Motor Co., Ltd. Structure for supporting spark plug for gas turbine engine

Also Published As

Publication number Publication date
FR3088412A1 (fr) 2020-05-15

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