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FR3015579B1 - INJECTOR NOSE COMPRISING A MAITIEN SOLE SOAP IN A FIXED PART OF AN INJECTION SYSTEM - Google Patents

INJECTOR NOSE COMPRISING A MAITIEN SOLE SOAP IN A FIXED PART OF AN INJECTION SYSTEM Download PDF

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Publication number
FR3015579B1
FR3015579B1 FR1363377A FR1363377A FR3015579B1 FR 3015579 B1 FR3015579 B1 FR 3015579B1 FR 1363377 A FR1363377 A FR 1363377A FR 1363377 A FR1363377 A FR 1363377A FR 3015579 B1 FR3015579 B1 FR 3015579B1
Authority
FR
France
Prior art keywords
injector
injection system
fixed part
nose
injector nose
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
FR1363377A
Other languages
French (fr)
Other versions
FR3015579A1 (en
Inventor
Olivier BIDART
Bernard Cameriano Laurent
Galadriel DANCIE
Julien LEPAROUX
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 FR1363377A priority Critical patent/FR3015579B1/en
Publication of FR3015579A1 publication Critical patent/FR3015579A1/en
Application granted granted Critical
Publication of FR3015579B1 publication Critical patent/FR3015579B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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
    • 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
    • F23R3/60—Support structures; Attaching or mounting means
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

L'invention concerne un système d'injection (18) d'un mélange air-carburant pour chambre de combustion de turbomachine, et un injecteur de carburant (80) comprenant un nez d'injecteur (82) au moins partiellement annulaire autour d'un axe de nez d'injecteur (82). Selon l'invention, le nez d'injecteur (82) comprend une semelle de maintien (101) qui est en saillie du nez d'injecteur (82) radialement vers l'extérieur du nez d'injecteur (82). La semelle de maintien (101) est configurée pour être insérée dans un espace de logement (29) d'une partie fixe (25) de système d'injection (18), de sorte à former un moyen de centrage et de retenue axiale de l'injecteur (80) relativement à la partie fixe (25) de système d'injection (18).The invention relates to an injection system (18) for an air-fuel mixture for a turbomachine combustion chamber, and a fuel injector (80) comprising an at least partially annular injector nozzle (82) around an injector nose pin (82). According to the invention, the injector nose (82) comprises a holding flange (101) which projects from the injector nose (82) radially outwardly of the injector nose (82). The holding flange (101) is configured to be inserted into a housing space (29) of a fixed part (25) of the injection system (18), so as to form an axial centering and retaining means of the injector (80) relative to the fixed part (25) of the injection system (18).

FR1363377A 2013-12-23 2013-12-23 INJECTOR NOSE COMPRISING A MAITIEN SOLE SOAP IN A FIXED PART OF AN INJECTION SYSTEM Active FR3015579B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1363377A FR3015579B1 (en) 2013-12-23 2013-12-23 INJECTOR NOSE COMPRISING A MAITIEN SOLE SOAP IN A FIXED PART OF AN INJECTION SYSTEM

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1363377A FR3015579B1 (en) 2013-12-23 2013-12-23 INJECTOR NOSE COMPRISING A MAITIEN SOLE SOAP IN A FIXED PART OF AN INJECTION SYSTEM
FR1363377 2013-12-23

Publications (2)

Publication Number Publication Date
FR3015579A1 FR3015579A1 (en) 2015-06-26
FR3015579B1 true FR3015579B1 (en) 2019-04-26

Family

ID=50290036

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1363377A Active FR3015579B1 (en) 2013-12-23 2013-12-23 INJECTOR NOSE COMPRISING A MAITIEN SOLE SOAP IN A FIXED PART OF AN INJECTION SYSTEM

Country Status (1)

Country Link
FR (1) FR3015579B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114896717B (en) * 2022-04-15 2024-10-29 西安航天动力研究所 Design method of injection groove type of pintle injector
CN116398326A (en) * 2023-04-11 2023-07-07 西安航天动力研究所 Gas generator

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3532271A (en) * 1967-02-23 1970-10-06 Frederick F Polnauer Spray nozzles with spiral flow fluid
US4735044A (en) * 1980-11-25 1988-04-05 General Electric Company Dual fuel path stem for a gas turbine engine
US5167116A (en) * 1989-07-07 1992-12-01 Fuel Systems Textron Inc. Small airblast fuel nozzle with high efficiency inner air swirler
US5117637A (en) * 1990-08-02 1992-06-02 General Electric Company Combustor dome assembly
FR2886714B1 (en) * 2005-06-07 2007-09-07 Snecma Moteurs Sa ANTI-ROTARY INJECTION SYSTEM FOR TURBO-REACTOR
US7748221B2 (en) * 2006-11-17 2010-07-06 Pratt & Whitney Canada Corp. Combustor heat shield with variable cooling
GB2470742B (en) * 2009-06-03 2011-04-20 Rolls Royce Plc Fuel injector for a gas turbine engine

Also Published As

Publication number Publication date
FR3015579A1 (en) 2015-06-26

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