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GB201516231D0 - Combustion system of a flow engine and method for determining a dimension of a resonator cavity - Google Patents

Combustion system of a flow engine and method for determining a dimension of a resonator cavity

Info

Publication number
GB201516231D0
GB201516231D0 GBGB1516231.6A GB201516231A GB201516231D0 GB 201516231 D0 GB201516231 D0 GB 201516231D0 GB 201516231 A GB201516231 A GB 201516231A GB 201516231 D0 GB201516231 D0 GB 201516231D0
Authority
GB
United Kingdom
Prior art keywords
dimension
determining
combustion system
resonator cavity
flow engine
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.)
Withdrawn
Application number
GBGB1516231.6A
Other versions
GB2527688A (en
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.)
Siemens AG
Siemens Corp
Original Assignee
Siemens AG
Siemens Corp
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
Priority claimed from EP13165158.0A external-priority patent/EP2851618A1/en
Application filed by Siemens AG, Siemens Corp filed Critical Siemens AG
Publication of GB201516231D0 publication Critical patent/GB201516231D0/en
Publication of GB2527688A publication Critical patent/GB2527688A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23K—FEEDING FUEL TO COMBUSTION APPARATUS
    • F23K5/00—Feeding or distributing other fuel to combustion apparatus
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M20/00—Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
    • F23M20/005—Noise absorbing means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23K—FEEDING FUEL TO COMBUSTION APPARATUS
    • F23K5/00—Feeding or distributing other fuel to combustion apparatus
    • F23K5/002—Gaseous fuel
    • F23K5/005—Gaseous fuel from a central source to a plurality of burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23K—FEEDING FUEL TO COMBUSTION APPARATUS
    • F23K5/00—Feeding or distributing other fuel to combustion apparatus
    • F23K5/02—Liquid fuel
    • F23K5/06—Liquid fuel from a central source to a plurality of burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M20/00—Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Measuring Volume Flow (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
GB1516231.6A 2013-04-23 2014-04-04 Combustion system of a flow engine and method for determining a dimension of a resonator cavity Withdrawn GB2527688A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP13164908 2013-04-23
EP13165158.0A EP2851618A1 (en) 2013-04-24 2013-04-24 Combustion system of a flow engine comprising a resonator
PCT/EP2014/056803 WO2014173660A1 (en) 2013-04-23 2014-04-04 Combustion system of a flow engine and method for determining a dimension of a resonator cavity

Publications (2)

Publication Number Publication Date
GB201516231D0 true GB201516231D0 (en) 2015-10-28
GB2527688A GB2527688A (en) 2015-12-30

Family

ID=50630759

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1516231.6A Withdrawn GB2527688A (en) 2013-04-23 2014-04-04 Combustion system of a flow engine and method for determining a dimension of a resonator cavity

Country Status (4)

Country Link
US (1) US20160076766A1 (en)
KR (1) KR20160003733A (en)
GB (1) GB2527688A (en)
WO (1) WO2014173660A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3034945B1 (en) * 2014-12-19 2018-05-30 Ansaldo Energia Switzerland AG Gas turbine fuel pipe comprising a damper
US10087845B2 (en) * 2015-11-30 2018-10-02 General Electric Company Pressure damping device for fuel manifold
US11092084B2 (en) * 2016-05-26 2021-08-17 General Electric Company Fuel delivery system for a gas turbine engine
US10386074B2 (en) 2016-12-09 2019-08-20 Solar Turbines Incorporated Injector head with a resonator for a gas turbine engine
US10663170B2 (en) * 2017-01-19 2020-05-26 Doosan Heavy Industries Construction Co., Ltd. Flow conditioner to reduce combustion dynamics in a combustion system
US10415480B2 (en) * 2017-04-13 2019-09-17 General Electric Company Gas turbine engine fuel manifold damper and method of dynamics attenuation
US10167780B2 (en) * 2017-05-25 2019-01-01 Pratt & Whitney Canada Corp. Tunable resonator
US10948188B2 (en) 2018-12-12 2021-03-16 Solar Turbines Incorporated Fuel injector with perforated plate
US11156164B2 (en) 2019-05-21 2021-10-26 General Electric Company System and method for high frequency accoustic dampers with caps
US11174792B2 (en) 2019-05-21 2021-11-16 General Electric Company System and method for high frequency acoustic dampers with baffles

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1590684A (en) 1968-09-12 1970-04-20
EP0611434A1 (en) 1991-11-15 1994-08-24 Siemens Aktiengesellschaft Arrangement for suppressing combustion-caused vibrations in the combustion chamber of a gas turbine system
DE19818874C2 (en) * 1998-04-28 2001-06-07 Man B & W Diesel As Kopenhagen Reciprocating machine
US6536457B2 (en) * 2000-12-29 2003-03-25 Pratt & Whitney Canada Corp. Fluid and fuel delivery systems reducing pressure fluctuations and engines including such systems
JP2005527761A (en) * 2001-09-07 2005-09-15 アルストム テクノロジー リミテッド Damping device for reducing combustion chamber pulsation of gas turbine device
US7464552B2 (en) * 2004-07-02 2008-12-16 Siemens Energy, Inc. Acoustically stiffened gas-turbine fuel nozzle
CN101868602B (en) * 2007-11-21 2013-09-04 三菱重工业株式会社 Damping device and gas turbine combustor
DE102009027539A1 (en) 2009-07-08 2011-01-20 Ford Global Technologies, LLC, Dearborn Internal combustion engine with intercooler

Also Published As

Publication number Publication date
US20160076766A1 (en) 2016-03-17
KR20160003733A (en) 2016-01-11
WO2014173660A1 (en) 2014-10-30
GB2527688A (en) 2015-12-30

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)