FR1130169A - Improvements to the combustion equipment of gas turbine engines - Google Patents

Improvements to the combustion equipment of gas turbine engines

Info

Publication number
FR1130169A
FR1130169A FR1130169DA FR1130169A FR 1130169 A FR1130169 A FR 1130169A FR 1130169D A FR1130169D A FR 1130169DA FR 1130169 A FR1130169 A FR 1130169A
Authority
FR
France
Prior art keywords
gas turbine
turbine engines
combustion equipment
combustion
equipment
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.)
Expired
Application number
Other languages
French (fr)
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
Application granted granted Critical
Publication of FR1130169A publication Critical patent/FR1130169A/en
Expired 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1130169D 1954-09-03 1955-08-22 Improvements to the combustion equipment of gas turbine engines Expired FR1130169A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1130169X 1954-09-03

Publications (1)

Publication Number Publication Date
FR1130169A true FR1130169A (en) 1957-01-31

Family

ID=10876269

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1130169D Expired FR1130169A (en) 1954-09-03 1955-08-22 Improvements to the combustion equipment of gas turbine engines

Country Status (1)

Country Link
FR (1) FR1130169A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2226470A3 (en) * 2009-03-05 2014-01-08 General Electric Company Methods and apparatus involving cooling fins
WO2017133819A1 (en) * 2016-02-01 2017-08-10 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustion chamber having a wall contour
EP3719401A1 (en) * 2019-04-04 2020-10-07 Raytheon Technologies Corporation Non-axisymmetric combustor for improved durability

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2226470A3 (en) * 2009-03-05 2014-01-08 General Electric Company Methods and apparatus involving cooling fins
WO2017133819A1 (en) * 2016-02-01 2017-08-10 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustion chamber having a wall contour
US10670270B2 (en) 2016-02-01 2020-06-02 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustion chamber with wall contouring
EP3719401A1 (en) * 2019-04-04 2020-10-07 Raytheon Technologies Corporation Non-axisymmetric combustor for improved durability

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