GB201306124D0 - A combustion chamber - Google Patents

A combustion chamber

Info

Publication number
GB201306124D0
GB201306124D0 GB201306124A GB201306124A GB201306124D0 GB 201306124 D0 GB201306124 D0 GB 201306124D0 GB 201306124 A GB201306124 A GB 201306124A GB 201306124 A GB201306124 A GB 201306124A GB 201306124 D0 GB201306124 D0 GB 201306124D0
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
combustion
chamber
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Withdrawn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
GB201306124A
Other versions
GB2512642A (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.)
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 GB201306124A priority Critical patent/GB2512642A/en
Publication of GB201306124D0 publication Critical patent/GB201306124D0/en
Publication of GB2512642A publication Critical patent/GB2512642A/en
Withdrawn legal-status Critical Current

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
    • F23R3/02—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB201306124A 2013-04-05 2013-04-05 A combustion chamber Withdrawn GB2512642A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB201306124A GB2512642A (en) 2013-04-05 2013-04-05 A combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB201306124A GB2512642A (en) 2013-04-05 2013-04-05 A combustion chamber

Publications (2)

Publication Number Publication Date
GB201306124D0 true GB201306124D0 (en) 2013-05-22
GB2512642A GB2512642A (en) 2014-10-08

Family

ID=48483352

Family Applications (1)

Application Number Title Priority Date Filing Date
GB201306124A Withdrawn GB2512642A (en) 2013-04-05 2013-04-05 A combustion chamber

Country Status (1)

Country Link
GB (1) GB2512642A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11686473B2 (en) 2021-11-11 2023-06-27 General Electric Company Combustion liner
US11754284B2 (en) 2021-11-11 2023-09-12 General Electric Company Combustion liner
US11808454B2 (en) 2021-11-11 2023-11-07 General Electric Company Combustion liner
CN116221774A (en) 2021-12-06 2023-06-06 通用电气公司 Variable dilution hole design for combustor liner

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2890156A1 (en) * 2005-08-31 2007-03-02 Snecma Turbomachine e.g. aircraft turbojet, combustion chamber, has internal and external flanges with orifices of triangular shape, where successive triangular orifices are arranged in staggered and head-to-tail configuration

Also Published As

Publication number Publication date
GB2512642A (en) 2014-10-08

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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)