DE602005001289D1 - Strahlturbinengehäuse und Fluidleitung mit Vorrichtung zum Befestigen der Fluidleitung im Strahlturbinengehäuse - Google Patents

Strahlturbinengehäuse und Fluidleitung mit Vorrichtung zum Befestigen der Fluidleitung im Strahlturbinengehäuse

Info

Publication number
DE602005001289D1
DE602005001289D1 DE602005001289T DE602005001289T DE602005001289D1 DE 602005001289 D1 DE602005001289 D1 DE 602005001289D1 DE 602005001289 T DE602005001289 T DE 602005001289T DE 602005001289 T DE602005001289 T DE 602005001289T DE 602005001289 D1 DE602005001289 D1 DE 602005001289D1
Authority
DE
Germany
Prior art keywords
fluid line
turbine housing
jet turbine
securing
jet
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.)
Expired - Fee Related
Application number
DE602005001289T
Other languages
English (en)
Other versions
DE602005001289T2 (de
Inventor
Jacques Bunel
Jacques Roche
Frederic Ruellan
Philippe Henry
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
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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE602005001289D1 publication Critical patent/DE602005001289D1/de
Application granted granted Critical
Publication of DE602005001289T2 publication Critical patent/DE602005001289T2/de
Expired - Fee Related 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
    • F23R3/28—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
    • 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
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105—Heating the by-pass flow
    • F02K3/11—Heating the by-pass flow by means of burners or combustion chambers
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means

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)
  • Fuel-Injection Apparatus (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Clamps And Clips (AREA)
  • Processes For Solid Components From Exhaust (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
DE602005001289T 2004-05-05 2005-04-19 Strahlturbinengehäuse und Fluidleitung mit Vorrichtung zum Befestigen der Fluidleitung im Strahlturbinengehäuse Expired - Fee Related DE602005001289T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0404796A FR2869875B1 (fr) 2004-05-05 2004-05-05 Dispositif de fixation d'un conduit de fluide sur un carter d'un turboreacteur
FR0404796 2004-05-05

Publications (2)

Publication Number Publication Date
DE602005001289D1 true DE602005001289D1 (de) 2007-07-19
DE602005001289T2 DE602005001289T2 (de) 2008-02-07

Family

ID=34942166

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005001289T Expired - Fee Related DE602005001289T2 (de) 2004-05-05 2005-04-19 Strahlturbinengehäuse und Fluidleitung mit Vorrichtung zum Befestigen der Fluidleitung im Strahlturbinengehäuse

Country Status (8)

Country Link
US (1) US7370477B2 (de)
EP (1) EP1593912B1 (de)
JP (1) JP2006009786A (de)
CA (1) CA2506208C (de)
DE (1) DE602005001289T2 (de)
ES (1) ES2286771T3 (de)
FR (1) FR2869875B1 (de)
RU (1) RU2362896C2 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7540157B2 (en) 2005-06-14 2009-06-02 Pratt & Whitney Canada Corp. Internally mounted fuel manifold with support pins
US7506514B2 (en) * 2005-06-30 2009-03-24 United Technologies Corporation Augmentor fuel conduit bushing
FR2891170B1 (fr) * 2005-09-29 2009-02-13 Snecma Sa Procede facilitant l'usinage d'une piece en particulier de turbomachine
US7854120B2 (en) * 2006-03-03 2010-12-21 Pratt & Whitney Canada Corp. Fuel manifold with reduced losses
GB0605432D0 (en) * 2006-03-17 2006-04-26 Rolls Royce Plc Component for fuel supply
FR2899316B1 (fr) * 2006-03-30 2008-05-16 Snecma Sa Bras accroche-flammes d'une chambre de post-combustion
FR2899280B1 (fr) * 2006-03-30 2012-08-31 Snecma Dispositif de montage d'une paroi de separation de flux dans une chambre de post-combustion d'un turboreacteur
FR2902150B1 (fr) * 2006-06-09 2011-10-14 Snecma Dispositif injecteur de carburant, systeme de post-combustion et turboreacteur a double flux
FR2913725B1 (fr) * 2007-03-16 2011-10-28 Snecma Drain de carter d'echappement de turbomachine
US7856825B2 (en) * 2007-05-16 2010-12-28 Pratt & Whitney Canada Corp. Redundant mounting system for an internal fuel manifold
GB0918089D0 (en) 2009-10-16 2009-12-02 Rolls Royce Plc Fuel injector mounting system
GB0918099D0 (en) * 2009-10-16 2009-12-02 Rolls Royce Plc Fuel injector mounting system
US8776835B2 (en) 2012-12-05 2014-07-15 Hamilton Sundstrand Corporation Fluid duct with improved connecting bead
US9797313B2 (en) 2014-01-16 2017-10-24 Pratt & Whitney Canada Corp. Internal manifold with fuel inlet
GB202006964D0 (en) * 2020-05-12 2020-06-24 Rolls Royce Plc Afterburner strut with integrated fueld feed lines
GB2615335B (en) * 2022-02-04 2024-05-08 Rolls Royce Plc A reheat assembly

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US689630A (en) * 1901-04-10 1901-12-24 George Lewis Autenrieth Boiler-flue coupling.
US1086964A (en) * 1913-04-10 1914-02-10 William H White Sand-trap.
US3879940A (en) * 1973-07-30 1975-04-29 Gen Electric Gas turbine engine fuel delivery tube assembly
US6354085B1 (en) * 2000-01-13 2002-03-12 General Electric Company Fuel injector with a fuel filter arrangement for a gas turbine engine

Also Published As

Publication number Publication date
EP1593912B1 (de) 2007-06-06
CA2506208A1 (fr) 2005-11-05
ES2286771T3 (es) 2007-12-01
US7370477B2 (en) 2008-05-13
RU2362896C2 (ru) 2009-07-27
EP1593912A1 (de) 2005-11-09
CA2506208C (fr) 2012-12-11
DE602005001289T2 (de) 2008-02-07
FR2869875A1 (fr) 2005-11-11
FR2869875B1 (fr) 2006-06-16
JP2006009786A (ja) 2006-01-12
US20060016194A1 (en) 2006-01-26
RU2005113682A (ru) 2006-11-20

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee