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GB0425901D0 - Combuster - Google Patents

Combuster

Info

Publication number
GB0425901D0
GB0425901D0 GBGB0425901.6A GB0425901A GB0425901D0 GB 0425901 D0 GB0425901 D0 GB 0425901D0 GB 0425901 A GB0425901 A GB 0425901A GB 0425901 D0 GB0425901 D0 GB 0425901D0
Authority
GB
United Kingdom
Prior art keywords
combuster
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.)
Ceased
Application number
GBGB0425901.6A
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GBGB0425901.6A priority Critical patent/GB0425901D0/en
Publication of GB0425901D0 publication Critical patent/GB0425901D0/en
Priority to GB0520278A priority patent/GB2420615B/en
Priority to US11/262,930 priority patent/US7637096B2/en
Priority to US12/500,887 priority patent/US20090286189A1/en
Ceased legal-status Critical Current

Links

Classifications

    • 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 
    • F23C15/00—Apparatus in which combustion takes place in pulses influenced by acoustic resonance in a gas mass
    • 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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/10—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect
    • F02C5/11—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect using valveless combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
    • F02K7/04—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet with resonant combustion chambers
    • 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 
    • F23C2205/00—Pulsating combustion
    • F23C2205/10—Pulsating combustion with pulsating fuel supply

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
GBGB0425901.6A 2004-11-25 2004-11-25 Combuster Ceased GB0425901D0 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GBGB0425901.6A GB0425901D0 (en) 2004-11-25 2004-11-25 Combuster
GB0520278A GB2420615B (en) 2004-11-25 2005-10-06 Pressure rise combustor
US11/262,930 US7637096B2 (en) 2004-11-25 2005-11-01 Pulse jet engine having pressure sensor means for controlling fuel delivery into a combustion chamber
US12/500,887 US20090286189A1 (en) 2004-11-25 2009-07-10 Combustor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0425901.6A GB0425901D0 (en) 2004-11-25 2004-11-25 Combuster

Publications (1)

Publication Number Publication Date
GB0425901D0 true GB0425901D0 (en) 2004-12-29

Family

ID=33561333

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB0425901.6A Ceased GB0425901D0 (en) 2004-11-25 2004-11-25 Combuster
GB0520278A Expired - Fee Related GB2420615B (en) 2004-11-25 2005-10-06 Pressure rise combustor

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB0520278A Expired - Fee Related GB2420615B (en) 2004-11-25 2005-10-06 Pressure rise combustor

Country Status (1)

Country Link
GB (2) GB0425901D0 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8499874B2 (en) 2009-05-12 2013-08-06 Icr Turbine Engine Corporation Gas turbine energy storage and conversion system
US8866334B2 (en) 2010-03-02 2014-10-21 Icr Turbine Engine Corporation Dispatchable power from a renewable energy facility
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
AU2011295668A1 (en) 2010-09-03 2013-05-02 Icr Turbine Engine Corporation Gas turbine engine configurations
CN101985904B (en) * 2010-10-28 2013-06-05 西北工业大学 Control method of detonation pipe for high-frequency pulse detonation engine
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
CA2980285C (en) 2015-03-19 2024-06-18 University Of Maryland, College Park Systems and methods for anti-phase operation of pulse combustors
EP3271654B1 (en) 2015-03-19 2019-09-25 North American Wave Engine Corporation System and method for improving operation of pulse combustors
WO2017106689A1 (en) 2015-12-18 2017-06-22 North American Wave Engine Corporation Systems and methods for air-breathing wave engines for thrust production
FI128276B (en) 2016-09-19 2020-02-28 Finno Energy Oy A method for operating a gas turbine
ES2938732T3 (en) 2018-04-17 2023-04-14 North American Wave Engine Corp Method and apparatus for starting and controlling pulse combustors using selective injector operation

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5361710A (en) * 1993-10-07 1994-11-08 The United States Of America As Represented By The Secretary Of The Navy Method and apparatus for the active control of a compact waste incinerator
JPH08226338A (en) * 1995-02-22 1996-09-03 Toshiba Corp Combustion vibration control device for combustor

Also Published As

Publication number Publication date
GB0520278D0 (en) 2005-11-16
GB2420615B (en) 2007-06-13
GB2420615A (en) 2006-05-31

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Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)