MX2017014326A - Arandela de quemador con fuga controlada. - Google Patents

Arandela de quemador con fuga controlada.

Info

Publication number
MX2017014326A
MX2017014326A MX2017014326A MX2017014326A MX2017014326A MX 2017014326 A MX2017014326 A MX 2017014326A MX 2017014326 A MX2017014326 A MX 2017014326A MX 2017014326 A MX2017014326 A MX 2017014326A MX 2017014326 A MX2017014326 A MX 2017014326A
Authority
MX
Mexico
Prior art keywords
grommet
lower platform
slots
combustor
leak
Prior art date
Application number
MX2017014326A
Other languages
English (en)
Inventor
H Johnson Crosby
Weon Kim Yong
E Groocock Ted
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 MX2017014326A publication Critical patent/MX2017014326A/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
    • F23R3/002—Wall structures
    • 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
    • F23R3/045—Air inlet arrangements using pipes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • 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
    • F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators

Abstract

Se describe una arandela (341) para una cámara de combustión (320) de un motor de turbina de gas (100). La arandela (341) incluye una plataforma inferior (352) y un cuello (351). La plataforma inferior (352) incluye una pluralidad de ranuras superiores (347) ubicadas en la superficie superior (353) y una pluralidad de ranuras inferiores (348) ubicadas en la superficie inferior (354). Cada ranura superior (347) y ranura inferior (348) se extienden radialmente a lo largo de la plataforma inferior (352). La pluralidad de ranuras superiores (347) se pueden distanciar en forma equidistante entre sí a lo largo de la circunferencia de la plataforma inferior (352). La pluralidad de ranuras inferiores (348) se puede distanciar en forma equidistante entre sí a lo largo de la circunferencia de la plataforma inferior (352).
MX2017014326A 2015-05-13 2016-05-03 Arandela de quemador con fuga controlada. MX2017014326A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/711,628 US9803863B2 (en) 2015-05-13 2015-05-13 Controlled-leak combustor grommet
PCT/US2016/030501 WO2016182785A1 (en) 2015-05-13 2016-05-03 Controlled-leak combustor grommet

Publications (1)

Publication Number Publication Date
MX2017014326A true MX2017014326A (es) 2018-03-23

Family

ID=57248105

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2017014326A MX2017014326A (es) 2015-05-13 2016-05-03 Arandela de quemador con fuga controlada.

Country Status (5)

Country Link
US (1) US9803863B2 (es)
CN (1) CN107592904B (es)
MX (1) MX2017014326A (es)
RU (1) RU2707355C2 (es)
WO (1) WO2016182785A1 (es)

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US9989254B2 (en) * 2013-06-03 2018-06-05 General Electric Company Combustor leakage control system
US10612781B2 (en) * 2014-11-07 2020-04-07 United Technologies Corporation Combustor wall aperture body with cooling circuit
US10132498B2 (en) * 2015-01-20 2018-11-20 United Technologies Corporation Thermal barrier coating of a combustor dilution hole
US20170176004A1 (en) * 2015-12-18 2017-06-22 Pratt & Whitney Canada Corp. Combustor floating collar assembly
US10221769B2 (en) * 2016-12-02 2019-03-05 General Electric Company System and apparatus for gas turbine combustor inner cap and extended resonating tubes
BR112020009468B1 (pt) * 2017-11-16 2023-12-05 Wobben Properties Gmbh Pá de rotor, pá de rotor montada, rotor para uma turbina eólica, turbina eólica, e, métodos para produzir uma pá de rotor, para conectar uma pá de rotor a um cubo de rotor e para reparar um rotor de uma turbina eólica
US11149684B2 (en) * 2018-09-28 2021-10-19 Raytheon Technologies Corporation Method for fabricating dilution holes in ceramic matrix composite combustor panels
FR3090747B1 (fr) * 2018-12-21 2021-01-22 Turbotech Chambre de combustion d'une turbomachine
US11079111B2 (en) * 2019-04-29 2021-08-03 Solar Turbines Incorporated Air tube
DE102020213836A1 (de) 2020-11-04 2022-05-05 Siemens Energy Global GmbH & Co. KG Resonatorring, Verfahren und Brennkorb

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6715279B2 (en) * 2002-03-04 2004-04-06 General Electric Company Apparatus for positioning an igniter within a liner port of a gas turbine engine
GB0227842D0 (en) * 2002-11-29 2003-01-08 Rolls Royce Plc Sealing Arrangement
US6971242B2 (en) 2004-03-02 2005-12-06 Caterpillar Inc. Burner for a gas turbine engine
US7966832B1 (en) 2004-12-29 2011-06-28 Solar Turbines Inc Combustor
RU70936U1 (ru) * 2006-03-20 2008-02-20 Открытое акционерное общество "Климов" Система охлаждения турбины газотурбинного двигателя
US8479490B2 (en) * 2007-03-30 2013-07-09 Honeywell International Inc. Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters
US8257015B2 (en) * 2008-02-14 2012-09-04 General Electric Company Apparatus for cooling rotary components within a steam turbine
US20100212324A1 (en) * 2009-02-26 2010-08-26 Honeywell International Inc. Dual walled combustors with impingement cooled igniters
FR2952703B1 (fr) * 2009-11-19 2011-10-28 Snecma Guide d'une bougie d'allumage dans une chambre de combustion d'une turbomachine
US8973365B2 (en) * 2010-10-29 2015-03-10 Solar Turbines Incorporated Gas turbine combustor with mounting for Helmholtz resonators
US8978385B2 (en) 2011-07-29 2015-03-17 United Technologies Corporation Distributed cooling for gas turbine engine combustor
US9360215B2 (en) 2012-04-02 2016-06-07 United Technologies Corporation Combustor having a beveled grommet
US9249978B2 (en) * 2012-07-03 2016-02-02 Alstom Technology Ltd Retaining collar for a gas turbine combustion liner
US9625151B2 (en) 2012-09-25 2017-04-18 United Technologies Corporation Cooled combustor liner grommet
US10088162B2 (en) 2012-10-01 2018-10-02 United Technologies Corporation Combustor with grommet having projecting lip
US9587831B2 (en) * 2012-11-27 2017-03-07 United Technologies Corporation Cooled combustor seal
EP2946145B1 (en) 2013-01-16 2020-07-15 United Technologies Corporation Combustor cooled quench zone array
EP3047128B1 (en) 2013-09-16 2018-10-31 United Technologies Corporation Controlled variation of pressure drop through effusion cooling in a double walled combustor of a gas turbine engine
US10041675B2 (en) * 2014-06-04 2018-08-07 Pratt & Whitney Canada Corp. Multiple ventilated rails for sealing of combustor heat shields

Also Published As

Publication number Publication date
CN107592904A (zh) 2018-01-16
WO2016182785A1 (en) 2016-11-17
US9803863B2 (en) 2017-10-31
RU2707355C2 (ru) 2019-11-26
US20160334102A1 (en) 2016-11-17
CN107592904B (zh) 2020-06-12
RU2017141057A3 (es) 2019-10-22
RU2017141057A (ru) 2019-05-27

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