MX2016011222A - Inyector de combustible para motor de turbina de gas con un protector termico interno. - Google Patents

Inyector de combustible para motor de turbina de gas con un protector termico interno.

Info

Publication number
MX2016011222A
MX2016011222A MX2016011222A MX2016011222A MX2016011222A MX 2016011222 A MX2016011222 A MX 2016011222A MX 2016011222 A MX2016011222 A MX 2016011222A MX 2016011222 A MX2016011222 A MX 2016011222A MX 2016011222 A MX2016011222 A MX 2016011222A
Authority
MX
Mexico
Prior art keywords
heat shield
tube
fuel injector
gas
turbine engine
Prior art date
Application number
MX2016011222A
Other languages
English (en)
Inventor
Venkat BANDARU Ramarao
Scott PIPER James
Michael Lindner Scott
Paul BATAKIS Anthony
Joseph GIELLA Peter
Original Assignee
Solar Turbines Inc
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 Solar Turbines Inc filed Critical Solar Turbines Inc
Publication of MX2016011222A publication Critical patent/MX2016011222A/es

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
    • 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
    • F23R3/36—Supply of different fuels
    • 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
    • F23R2900/00004—Preventing formation of deposits on surfaces of gas turbine components, e.g. coke deposits

Abstract

Se describe un inyector de combustible (310) para un quemador (300) de un motor de turbina de gas (100). El inyector (310) incluye un tubo exterior de gas (351), un tubo interior de gas (340), un tubo de líquido (370) y un protector térmico (390). El tubo exterior de gas (351) y el tubo interior de gas (340) forman un anillo de combustible gaseoso (335). El tubo interior de gas (340) y el tubo de líquido (370) forman un anillo de combustible líquido (336). El tubo de líquido (370) forma una cavidad de aire. El protector térmico (390) se extiende en el tubo de líquido (370) y forma un espacio aislante (339) entre el protector térmico (390) y el tubo de líquido (370).
MX2016011222A 2014-03-06 2015-02-23 Inyector de combustible para motor de turbina de gas con un protector termico interno. MX2016011222A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/199,419 US9618209B2 (en) 2014-03-06 2014-03-06 Gas turbine engine fuel injector with an inner heat shield
PCT/US2015/017054 WO2015134216A1 (en) 2014-03-06 2015-02-23 Gas turbine engine fuel injector with an inner heat shield

Publications (1)

Publication Number Publication Date
MX2016011222A true MX2016011222A (es) 2017-01-05

Family

ID=54016983

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2016011222A MX2016011222A (es) 2014-03-06 2015-02-23 Inyector de combustible para motor de turbina de gas con un protector termico interno.

Country Status (5)

Country Link
US (1) US9618209B2 (es)
CN (1) CN106068372B (es)
MX (1) MX2016011222A (es)
RU (1) RU2672205C2 (es)
WO (1) WO2015134216A1 (es)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11453484B2 (en) 2018-12-17 2022-09-27 Goodrich Corporation Heat shield retainer and method

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9957897B2 (en) * 2015-03-19 2018-05-01 United Technologies Corporation Gimbal tube systems for tangential onboard injectors
US10132500B2 (en) * 2015-10-16 2018-11-20 Delavan Inc. Airblast injectors
US10830446B2 (en) * 2017-12-15 2020-11-10 Delavan Inc. Fuel injector assemblies
US11060460B1 (en) 2019-04-01 2021-07-13 Marine Turbine Technologies, LLC Fuel distribution system for gas turbine engine
US11525403B2 (en) * 2021-05-05 2022-12-13 Pratt & Whitney Canada Corp. Fuel nozzle with integrated metering and flashback system

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4311277A (en) * 1979-06-20 1982-01-19 Lucas Industries Limited Fuel injector
US4600151A (en) * 1982-11-23 1986-07-15 Ex-Cell-O Corporation Fuel injector assembly with water or auxiliary fuel capability
US5761907A (en) 1995-12-11 1998-06-09 Parker-Hannifin Corporation Thermal gradient dispersing heatshield assembly
EP0886744B1 (en) 1996-03-13 2001-05-23 Parker Hannifin Corporation Internally heatshielded nozzle
US6688534B2 (en) 2001-03-07 2004-02-10 Delavan Inc Air assist fuel nozzle
US6622488B2 (en) * 2001-03-21 2003-09-23 Parker-Hannifin Corporation Pure airblast nozzle
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
US7779636B2 (en) 2005-05-04 2010-08-24 Delavan Inc Lean direct injection atomizer for gas turbine engines
US20070074518A1 (en) * 2005-09-30 2007-04-05 Solar Turbines Incorporated Turbine engine having acoustically tuned fuel nozzle
US8240151B2 (en) * 2006-01-20 2012-08-14 Parker-Hannifin Corporation Fuel injector nozzles for gas turbine engines
US7658074B2 (en) 2006-08-31 2010-02-09 United Technologies Corporation Mid-mount centerbody heat shield for turbine engine fuel nozzle
US7874164B2 (en) 2006-11-03 2011-01-25 Pratt & Whitney Canada Corp. Fuel nozzle flange with reduced heat transfer
US8015815B2 (en) * 2007-04-18 2011-09-13 Parker-Hannifin Corporation Fuel injector nozzles, with labyrinth grooves, for gas turbine engines
US8196845B2 (en) * 2007-09-17 2012-06-12 Delavan Inc Flexure seal for fuel injection nozzle
US7926744B2 (en) * 2008-02-21 2011-04-19 Delavan Inc Radially outward flowing air-blast fuel injector for gas turbine engine
US7926282B2 (en) * 2008-03-04 2011-04-19 Delavan Inc Pure air blast fuel injector
US8096135B2 (en) * 2008-05-06 2012-01-17 Dela Van Inc Pure air blast fuel injector
US8015816B2 (en) 2008-06-16 2011-09-13 Delavan Inc Apparatus for discouraging fuel from entering the heat shield air cavity of a fuel injector
US8484978B2 (en) * 2009-11-12 2013-07-16 General Electric Company Fuel nozzle assembly that exhibits a frequency different from a natural operating frequency of a gas turbine engine and method of assembling the same
US20110173983A1 (en) 2010-01-15 2011-07-21 General Electric Company Premix fuel nozzle internal flow path enhancement
US8555648B2 (en) * 2010-02-12 2013-10-15 General Electric Company Fuel injector nozzle
US9151227B2 (en) * 2010-11-10 2015-10-06 Solar Turbines Incorporated End-fed liquid fuel gallery for a gas turbine fuel injector
US9400104B2 (en) * 2012-09-28 2016-07-26 United Technologies Corporation Flow modifier for combustor fuel nozzle tip
US20140291418A1 (en) * 2013-03-26 2014-10-02 Parker-Hannifin Corporation Multi-circuit airblast fuel nozzle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11453484B2 (en) 2018-12-17 2022-09-27 Goodrich Corporation Heat shield retainer and method

Also Published As

Publication number Publication date
CN106068372B (zh) 2018-02-09
RU2016137841A3 (es) 2018-10-09
CN106068372A (zh) 2016-11-02
RU2672205C2 (ru) 2018-11-12
WO2015134216A1 (en) 2015-09-11
RU2016137841A (ru) 2018-03-23
US20150253009A1 (en) 2015-09-10
US9618209B2 (en) 2017-04-11

Similar Documents

Publication Publication Date Title
MX2016011222A (es) Inyector de combustible para motor de turbina de gas con un protector termico interno.
GB2573853B (en) Fuel injector assembly for gas turbine engine
WO2015050592A3 (en) Gas turbine engine combustor liner panel
WO2014200588A3 (en) Additive manufactured gas turbine engine combustor liner panel
CL2015001067A1 (es) Sistemas de energía y sistemas calefactores suplementarios mediante turbina a gas y métodos de fabricación y uso de los mismos.
MY195858A (en) System And Method For Generating Flame Effect
WO2014189556A3 (en) Gas turbine engine combustor liner assembly with convergent hyperbolic profile
WO2015147929A3 (en) Cooling an aperture body of a combustor wall
GB2562668B (en) Combustor panel, combustor, combustion device, gas turbine, and method of cooling combustor panel
EP3077728B8 (en) Gas turbine engine combustor having co-swirl orientation of combustor effusion passages, and method
WO2015076883A3 (en) Dual fuel nozzle with swirling axial gas injection for a gas turbine engine
WO2015069354A3 (en) Dual fuel nozzle with liquid filming atomization for a gas turbine engine
WO2015002686A3 (en) Gas turbine engine combustor liner panel
WO2014171994A3 (en) Borescope plug assembly for gas turbine engine
WO2014197070A3 (en) Gas turbine engine combustor
MX370552B (es) Ensamble de recepción de boquilla de combustible.
GB2490348B (en) A head part of an annular combustion chamber
EP2778533A3 (en) Combustor for gas turbine engine
MX2016001313A (es) Protector termico con separadores.
EP2951405A4 (en) A JOINT CONNECTION FOR A COMBUSTION CHAMBER, DIFFUSER AND TANGENTIAL INJECTOR OF A GAS TURBINE ENGINE
WO2014197072A3 (en) Fuel nozzle for a gas turbine engine
MX2015014400A (es) Montaje de generador de vortices removible para una camisa de la camara de combustion.
TW201614901A (en) Hermetic high temperature dielectric conduit assemblies
PL3443266T3 (pl) Ulepszone wtryskiwacze do komory spalania turbiny gazowej
SE546012C2 (en) Combustion chamber of a gas turbine, gas turbine and method for operating the same

Legal Events

Date Code Title Description
FG Grant or registration