FR3116567B1 - METHOD FOR ASSEMBLING TURBOMACHINE INJECTORS AND ASSOCIATED KEYING DEVICE - Google Patents

METHOD FOR ASSEMBLING TURBOMACHINE INJECTORS AND ASSOCIATED KEYING DEVICE Download PDF

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Publication number
FR3116567B1
FR3116567B1 FR2011945A FR2011945A FR3116567B1 FR 3116567 B1 FR3116567 B1 FR 3116567B1 FR 2011945 A FR2011945 A FR 2011945A FR 2011945 A FR2011945 A FR 2011945A FR 3116567 B1 FR3116567 B1 FR 3116567B1
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FR
France
Prior art keywords
turbomachine
joint
injectors
injector
gripping
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
FR2011945A
Other languages
French (fr)
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FR3116567A1 (en
Inventor
Christophe Xavier Herault
Alexandre Jourdain-Derros
Steve Richard
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 FR2011945A priority Critical patent/FR3116567B1/en
Publication of FR3116567A1 publication Critical patent/FR3116567A1/en
Application granted granted Critical
Publication of FR3116567B1 publication Critical patent/FR3116567B1/en
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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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • F23R2900/00012—Details of sealing devices
    • 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

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)
  • Automatic Assembly (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

L'invention concerne un procédé de montage de plusieurs injecteurs (24) de turbomachine (10) sur un carter (14) externe d'une chambre (12) à combustion de la turbomachine (10), un joint (46a, 46b) annulaire étant intercalé entre une bride (34) de fixation de chaque injecteur (24) et le carter (14) externe, la turbomachine (10) comportant des joints (46a, 46b) d'au moins deux modèles différents, le procédé comportant pour chaque injecteur (24) une étape (E1) de préhension d'un joint (46a, 46b) du modèle correspondant, caractérisé en ce qu'il comporte une étape (E2) de détrompage suivant chronologiquement l'étape (E1) de préhension qui consiste à vérifier que le joint (46a, 46b) saisi lors de l'étape (E1) de préhension est conforme au modèle de joint requis pour le montage dudit injecteur (24). Figure pour l'abrégé : Figure 8The invention relates to a method for mounting several injectors (24) of a turbomachine (10) on an outer casing (14) of a combustion chamber (12) of the turbomachine (10), an annular joint (46a, 46b) being interposed between a flange (34) for fixing each injector (24) and the external casing (14), the turbomachine (10) comprising seals (46a, 46b) of at least two different models, the method comprising for each injector (24) a step (E1) of gripping a joint (46a, 46b) of the corresponding model, characterized in that it includes a step (E2) of keying chronologically following the step (E1) of gripping which consists verifying that the joint (46a, 46b) entered during step (E1) of gripping conforms to the model of joint required for mounting said injector (24). Figure for abstract: Figure 8

FR2011945A 2020-11-20 2020-11-20 METHOD FOR ASSEMBLING TURBOMACHINE INJECTORS AND ASSOCIATED KEYING DEVICE Active FR3116567B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2011945A FR3116567B1 (en) 2020-11-20 2020-11-20 METHOD FOR ASSEMBLING TURBOMACHINE INJECTORS AND ASSOCIATED KEYING DEVICE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2011945 2020-11-20
FR2011945A FR3116567B1 (en) 2020-11-20 2020-11-20 METHOD FOR ASSEMBLING TURBOMACHINE INJECTORS AND ASSOCIATED KEYING DEVICE

Publications (2)

Publication Number Publication Date
FR3116567A1 FR3116567A1 (en) 2022-05-27
FR3116567B1 true FR3116567B1 (en) 2023-06-16

Family

ID=74045940

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2011945A Active FR3116567B1 (en) 2020-11-20 2020-11-20 METHOD FOR ASSEMBLING TURBOMACHINE INJECTORS AND ASSOCIATED KEYING DEVICE

Country Status (1)

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FR (1) FR3116567B1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422214A (en) * 1944-08-17 1947-06-17 Westinghouse Electric Corp Fuel injector mounting for combustion chambers
FR2616889B1 (en) * 1987-06-18 1992-07-31 Snecma TURBOJET COMBUSTION CHAMBER HOUSING HAVING AIR TAKE-OFFS
FR2939171B1 (en) * 2008-11-28 2010-12-31 Snecma TURBOMACHINE WITH SEPARATE FUEL INJECTION SYSTEMS USING IDENTICAL SEALING JOINTS.
EP2971685B1 (en) * 2013-03-15 2021-06-23 Raytheon Technologies Corporation Combustor section for a gas turbine engine

Also Published As

Publication number Publication date
FR3116567A1 (en) 2022-05-27

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