SG126022A1 - fuel injector bearing plate assembly and swirler assembly - Google Patents
fuel injector bearing plate assembly and swirler assemblyInfo
- Publication number
- SG126022A1 SG126022A1 SG200600353A SG200600353A SG126022A1 SG 126022 A1 SG126022 A1 SG 126022A1 SG 200600353 A SG200600353 A SG 200600353A SG 200600353 A SG200600353 A SG 200600353A SG 126022 A1 SG126022 A1 SG 126022A1
- Authority
- SG
- Singapore
- Prior art keywords
- bearing plate
- fuel injector
- race
- assembly
- ball
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L27/00—Adjustable joints, Joints allowing movement
- F16L27/08—Adjustable joints, Joints allowing movement allowing adjustment or movement only about the axis of one pipe
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C5/00—Disposition of burners with respect to the combustion chamber or to one another; Mounting of burners in combustion apparatus
- F23C5/02—Structural details of mounting
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Rolling Contact Bearings (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Mounting Of Bearings Or Others (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Fuel-Injection Apparatus (AREA)
- Support Of The Bearing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/085,493 US7628019B2 (en) | 2005-03-21 | 2005-03-21 | Fuel injector bearing plate assembly and swirler assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
SG126022A1 true SG126022A1 (en) | 2006-10-30 |
Family
ID=36088452
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG200600353A SG126022A1 (en) | 2005-03-21 | 2006-01-18 | fuel injector bearing plate assembly and swirler assembly |
Country Status (9)
Country | Link |
---|---|
US (3) | US7628019B2 (zh) |
EP (2) | EP1710503B1 (zh) |
JP (1) | JP2006266669A (zh) |
CN (1) | CN1837591A (zh) |
AU (1) | AU2006200260A1 (zh) |
CA (1) | CA2533045A1 (zh) |
DE (1) | DE602006005805D1 (zh) |
IL (1) | IL173262A0 (zh) |
SG (1) | SG126022A1 (zh) |
Families Citing this family (50)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2907177B1 (fr) * | 2006-10-13 | 2009-12-04 | Snecma | Assemblage d'un dispositif rotulant sur une chape de renvoi d'angle, systeme de commande d'un redresseur a calage variable le comportant, et moteur d'aeronef en etant muni |
FR2910115B1 (fr) * | 2006-12-19 | 2012-11-16 | Snecma | Deflecteur pour fond de chambre de combustion, chambre de combustion en etant equipee et turboreacteur les comportant |
US7861530B2 (en) * | 2007-03-30 | 2011-01-04 | Pratt & Whitney Canada Corp. | Combustor floating collar with louver |
US7870737B2 (en) * | 2007-04-05 | 2011-01-18 | United Technologies Corporation | Hooded air/fuel swirler for a gas turbine engine |
US8276836B2 (en) * | 2007-07-27 | 2012-10-02 | General Electric Company | Fuel nozzle assemblies and methods |
FR2927367B1 (fr) * | 2008-02-11 | 2010-05-28 | Snecma | Dispositif de montage d'une bougie d'allumage dans une chambre de combustion de moteur a turbine a gaz |
JP4815513B2 (ja) * | 2009-07-06 | 2011-11-16 | 川崎重工業株式会社 | ガスタービン燃焼器 |
US8689563B2 (en) * | 2009-07-13 | 2014-04-08 | United Technologies Corporation | Fuel nozzle guide plate mistake proofing |
US8375548B2 (en) * | 2009-10-07 | 2013-02-19 | Pratt & Whitney Canada Corp. | Fuel nozzle and method of repair |
US10317081B2 (en) * | 2011-01-26 | 2019-06-11 | United Technologies Corporation | Fuel injector assembly |
DE102011014972A1 (de) * | 2011-03-24 | 2012-09-27 | Rolls-Royce Deutschland Ltd & Co Kg | Brennkammerkopf mit Halterungen für Dichtungen an Brennern in Gasturbinen |
US20130174562A1 (en) * | 2012-01-11 | 2013-07-11 | Marcus Timothy Holcomb | Gas turbine engine, combustor and dome panel |
GB2499196B (en) * | 2012-02-07 | 2017-08-02 | Rolls Royce Plc | Combustor head arrangement |
FR2987428B1 (fr) * | 2012-02-23 | 2024-06-21 | Snecma | Liaison mecanique amelioree entre un nez d'injecteur et une bague de traversee d'un systeme d'injection pour chambre de combustion de turbomachine |
FR2988813B1 (fr) * | 2012-03-29 | 2017-09-01 | Snecma | Dispositif d'injection d'un melange d'air et de carburant dans une chambre de combustion de turbomachine |
US20130255263A1 (en) * | 2012-03-30 | 2013-10-03 | Solar Turbines Incorporated. | Air blocker ring assembly with radial retention |
US9388986B2 (en) | 2012-03-30 | 2016-07-12 | Solar Turbines Incorporated | Air blocker ring assembly with leading edge configuration |
US9341373B2 (en) * | 2012-03-30 | 2016-05-17 | Solar Turbines Incorporated | Air blocker ring assembly with blocker ring protrusions |
USD755864S1 (en) * | 2012-05-10 | 2016-05-10 | Oerlikon Metco (Us) Inc. | Injector ring |
US9447974B2 (en) * | 2012-09-13 | 2016-09-20 | United Technologies Corporation | Light weight swirler for gas turbine engine combustor and a method for lightening a swirler for a gas turbine engine |
WO2014163669A1 (en) * | 2013-03-13 | 2014-10-09 | Rolls-Royce Corporation | Combustor assembly for a gas turbine engine |
US10598381B2 (en) | 2013-07-15 | 2020-03-24 | United Technologies Corporation | Swirler mount interface for gas turbine engine combustor |
US10101031B2 (en) | 2013-08-30 | 2018-10-16 | United Technologies Corporation | Swirler mount interface for gas turbine engine combustor |
US10830441B2 (en) | 2013-10-04 | 2020-11-10 | Raytheon Technologies Corporation | Swirler for a turbine engine combustor |
EP3055536B1 (en) | 2013-10-07 | 2020-04-08 | United Technologies Corporation | Air cooled fuel injector for a turbine engine |
FR3015640B1 (fr) * | 2013-12-20 | 2015-12-25 | Snecma | Chambre annulaire de combustion dans une turbomachine |
FR3015639B1 (fr) * | 2013-12-20 | 2018-08-31 | Safran Aircraft Engines | Chambre de combustion dans une turbomachine |
FR3015641B1 (fr) * | 2013-12-20 | 2018-05-18 | Safran Aircraft Engines | Dispositif d'injection dans une turbomachine |
US10934890B2 (en) | 2014-05-09 | 2021-03-02 | Raytheon Technologies Corporation | Shrouded conduit for arranging a fluid flowpath |
FR3026827B1 (fr) * | 2014-10-01 | 2019-06-07 | Safran Aircraft Engines | Chambre de combustion de turbomachine |
EP3009746B1 (en) | 2014-10-17 | 2019-11-27 | United Technologies Corporation | Swirler assembly for a turbine engine |
EP3242834B1 (en) | 2015-01-07 | 2018-11-28 | LORD Corporation | Aircraft engine mount |
US9957897B2 (en) * | 2015-03-19 | 2018-05-01 | United Technologies Corporation | Gimbal tube systems for tangential onboard injectors |
GB201506017D0 (en) * | 2015-04-09 | 2015-05-27 | Rolls Royce Plc | Fuel injector system |
GB2543803B (en) * | 2015-10-29 | 2019-10-30 | Rolls Royce Plc | A combustion chamber assembly |
GB2548585B (en) * | 2016-03-22 | 2020-05-27 | Rolls Royce Plc | A combustion chamber assembly |
CN106705123A (zh) * | 2016-12-20 | 2017-05-24 | 成都航利航空科技有限责任公司 | 一种焊接结构式发动机燃油喷嘴 |
US10253976B2 (en) | 2017-04-24 | 2019-04-09 | United Technologies Corporation | Fuel swirler with anti-rotation features |
USD851237S1 (en) * | 2017-11-01 | 2019-06-11 | Systems Spray-Cooled, Inc | Watertight sidewall dustcover |
USD849227S1 (en) * | 2017-12-12 | 2019-05-21 | Systems Spray-Cooled, Inc. | Burner bump out |
USD851743S1 (en) * | 2017-12-19 | 2019-06-18 | Systems Spray-Cooled, Inc | Burner bump out |
USD849228S1 (en) * | 2017-12-19 | 2019-05-21 | Systems Spray-Cooled, Inc | Burner bump out |
FR3082284B1 (fr) * | 2018-06-07 | 2020-12-11 | Safran Aircraft Engines | Chambre de combustion pour une turbomachine |
US11136953B2 (en) * | 2018-11-20 | 2021-10-05 | Delphi Technologies Ip Limited | Fuel injector with a locating pin, internal combustion engine using the same, and method |
US11346557B2 (en) * | 2019-08-12 | 2022-05-31 | Raytheon Technologies Corporation | Aerodynamic guide plate collar for swirler assembly |
US11280495B2 (en) * | 2020-03-04 | 2022-03-22 | General Electric Company | Gas turbine combustor fuel injector flow device including vanes |
FR3108162B1 (fr) * | 2020-03-10 | 2023-01-13 | Safran Aircraft Engines | Système d’injection pour une chambre annulaire de combustion de turbomachine |
US11486581B2 (en) * | 2020-09-29 | 2022-11-01 | Pratt & Whitney Canada Corp. | Fuel nozzle and associated method of assembly |
US11428411B1 (en) | 2021-05-18 | 2022-08-30 | General Electric Company | Swirler with rifled venturi for dynamics mitigation |
US20240288169A1 (en) * | 2023-02-27 | 2024-08-29 | Raytheon Technologies Corporation | Fuel injector air swirler structure with canted flow guide surface |
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GB1127637A (en) * | 1966-08-18 | 1968-09-18 | Lucas Industries Ltd | Supports for fuel burners |
US3677474A (en) * | 1970-05-06 | 1972-07-18 | Anzen Prod | Adjustable liquid discharge jet |
US3879940A (en) * | 1973-07-30 | 1975-04-29 | Gen Electric | Gas turbine engine fuel delivery tube assembly |
CA969218A (en) * | 1973-08-03 | 1975-06-10 | Emco Limited | Adjustable shower head |
US3995889A (en) * | 1975-05-22 | 1976-12-07 | Hydro-Dredge Accessory Co. | Dredge floating pontoon pipe-line joint |
GB1505499A (en) | 1975-06-23 | 1978-03-30 | Lucas Industries Ltd | Flame tube assembly for a gas turbine engine |
US4275843A (en) * | 1979-11-14 | 1981-06-30 | Stanadyne, Inc. | Automatically adjustable shower head |
US4322945A (en) * | 1980-04-02 | 1982-04-06 | United Technologies Corporation | Fuel nozzle guide heat shield for a gas turbine engine |
US4365470A (en) * | 1980-04-02 | 1982-12-28 | United Technologies Corporation | Fuel nozzle guide and seal for a gas turbine engine |
US4618173A (en) * | 1980-10-14 | 1986-10-21 | Big-Inch Marine Systems, Inc. | Swivel coupling element |
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US4717078A (en) * | 1984-08-20 | 1988-01-05 | Arp George F | Eyeball fitting for increasing flow of return water to swimming pool |
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US4840410A (en) * | 1988-05-05 | 1989-06-20 | Welkey Joseph J | Apparatus for making a swiveled flow line connection |
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DE4110507C2 (de) * | 1991-03-30 | 1994-04-07 | Mtu Muenchen Gmbh | Brenner für Gasturbinentriebwerke mit mindestens einer für die Zufuhr von Verbrennungsluft lastabhängig regulierbaren Dralleinrichtung |
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DE19515537A1 (de) * | 1995-04-27 | 1996-10-31 | Bmw Rolls Royce Gmbh | Kopfteil einer Gasturbinen-Ringbrennkammer |
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FR2753779B1 (fr) * | 1996-09-26 | 1998-10-16 | Systeme d'injection aerodynamique d'un melange air carburant | |
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US6158781A (en) * | 1998-05-18 | 2000-12-12 | Taper-Lok | Pipeline swivel coupling |
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US6502400B1 (en) * | 2000-05-20 | 2003-01-07 | General Electric Company | Combustor dome assembly and method of assembling the same |
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US6546732B1 (en) * | 2001-04-27 | 2003-04-15 | General Electric Company | Methods and apparatus for cooling gas turbine engine combustors |
US6497105B1 (en) * | 2001-06-04 | 2002-12-24 | Pratt & Whitney Canada Corp. | Low cost combustor burner collar |
FR2827367B1 (fr) * | 2001-07-16 | 2003-10-17 | Snecma Moteurs | Systeme d'injection aeromecanique a vrille primaire anti-retour |
DE50306252D1 (de) * | 2002-02-15 | 2007-02-22 | Brueninghaus Hydromatik Gmbh | Kolbenmaschine oder drehgleitlagerung |
US7104066B2 (en) * | 2003-08-19 | 2006-09-12 | General Electric Company | Combuster swirler assembly |
FR2859272B1 (fr) * | 2003-09-02 | 2005-10-14 | Snecma Moteurs | Systeme d'injection air/carburant, dans une chambre de combustion de turbomachine, ayant des moyens de generation de plasmas froids |
US7134286B2 (en) * | 2004-08-24 | 2006-11-14 | Pratt & Whitney Canada Corp. | Gas turbine floating collar arrangement |
GB2418462B (en) * | 2004-09-22 | 2006-11-01 | Minebea Co Ltd | Spherical bearing arrangement |
US7246494B2 (en) * | 2004-09-29 | 2007-07-24 | General Electric Company | Methods and apparatus for fabricating gas turbine engine combustors |
US7131273B2 (en) * | 2004-12-17 | 2006-11-07 | General Electric Company | Gas turbine engine carburetor with flat retainer connecting primary and secondary swirlers |
US7673460B2 (en) * | 2005-06-07 | 2010-03-09 | Snecma | System of attaching an injection system to a turbojet combustion chamber base |
FR2886714B1 (fr) * | 2005-06-07 | 2007-09-07 | Snecma Moteurs Sa | Systeme d'injection anti-rotatif pour turbo-reacteur |
FR2903171B1 (fr) * | 2006-06-29 | 2008-10-17 | Snecma Sa | Agencement a liaison par crabot pour chambre de combustion de turbomachine |
FR2903173B1 (fr) * | 2006-06-29 | 2008-08-29 | Snecma Sa | Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif |
FR2903172B1 (fr) * | 2006-06-29 | 2008-10-17 | Snecma Sa | Agencement pour chambre de combustion de turbomachine ayant un defecteur a collerette |
US7926280B2 (en) * | 2007-05-16 | 2011-04-19 | Pratt & Whitney Canada Corp. | Interface between a combustor and fuel nozzle |
US7857240B2 (en) * | 2009-02-20 | 2010-12-28 | So Mel Huang | Rotary shower head |
-
2005
- 2005-03-21 US US11/085,493 patent/US7628019B2/en active Active
-
2006
- 2006-01-17 CA CA002533045A patent/CA2533045A1/en not_active Abandoned
- 2006-01-18 SG SG200600353A patent/SG126022A1/en unknown
- 2006-01-19 JP JP2006010660A patent/JP2006266669A/ja active Pending
- 2006-01-19 EP EP06250272A patent/EP1710503B1/en not_active Not-in-force
- 2006-01-19 DE DE602006005805T patent/DE602006005805D1/de active Active
- 2006-01-19 IL IL173262A patent/IL173262A0/en unknown
- 2006-01-19 EP EP07021235A patent/EP1878973B1/en active Active
- 2006-01-20 AU AU2006200260A patent/AU2006200260A1/en not_active Abandoned
- 2006-01-21 CN CN200610008936.4A patent/CN1837591A/zh active Pending
-
2009
- 2009-06-11 US US12/482,513 patent/US8726667B2/en active Active
- 2009-06-11 US US12/482,516 patent/US8291706B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US8291706B2 (en) | 2012-10-23 |
CN1837591A (zh) | 2006-09-27 |
DE602006005805D1 (de) | 2009-04-30 |
EP1878973B1 (en) | 2009-03-18 |
IL173262A0 (en) | 2006-06-11 |
AU2006200260A1 (en) | 2006-10-05 |
US7628019B2 (en) | 2009-12-08 |
US20130341912A1 (en) | 2013-12-26 |
EP1878973A1 (en) | 2008-01-16 |
US8726667B2 (en) | 2014-05-20 |
US20120198653A1 (en) | 2012-08-09 |
JP2006266669A (ja) | 2006-10-05 |
EP1710503B1 (en) | 2012-07-11 |
US20060207258A1 (en) | 2006-09-21 |
EP1710503A1 (en) | 2006-10-11 |
CA2533045A1 (en) | 2006-09-21 |
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