CA994117A - Premix combustor assembly for gas turbine engines - Google Patents

Premix combustor assembly for gas turbine engines

Info

Publication number
CA994117A
CA994117A CA192,857A CA192857A CA994117A CA 994117 A CA994117 A CA 994117A CA 192857 A CA192857 A CA 192857A CA 994117 A CA994117 A CA 994117A
Authority
CA
Canada
Prior art keywords
gas turbine
turbine engines
combustor assembly
premix combustor
premix
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
CA192,857A
Inventor
Kenneth A. Cashman
Richard L. Marshall
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft 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
Application filed by United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of CA994117A publication Critical patent/CA994117A/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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • 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
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
CA192,857A 1973-02-28 1974-02-15 Premix combustor assembly for gas turbine engines Expired CA994117A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US33657773A 1973-02-28 1973-02-28

Publications (1)

Publication Number Publication Date
CA994117A true CA994117A (en) 1976-08-03

Family

ID=23316720

Family Applications (1)

Application Number Title Priority Date Filing Date
CA192,857A Expired CA994117A (en) 1973-02-28 1974-02-15 Premix combustor assembly for gas turbine engines

Country Status (5)

Country Link
JP (1) JPS5024618A (en)
CA (1) CA994117A (en)
DE (1) DE2403657A1 (en)
FR (1) FR2219310B1 (en)
GB (1) GB1450649A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3973390A (en) * 1974-12-18 1976-08-10 United Technologies Corporation Combustor employing serially staged pilot combustion, fuel vaporization, and primary combustion zones
US4194358A (en) * 1977-12-15 1980-03-25 General Electric Company Double annular combustor configuration
GB9201542D0 (en) * 1992-01-24 1992-03-11 Bmw Rolls Royce Gmbh Combustion apparatus for use in a gas turbine
FR2694624B1 (en) * 1992-08-05 1994-09-23 Snecma Combustion chamber with several fuel injectors.
WO2013028163A1 (en) * 2011-08-22 2013-02-28 Majed Toqan Tangential and flameless annular combustor for use on gas turbine engines

Also Published As

Publication number Publication date
DE2403657A1 (en) 1974-09-12
FR2219310B1 (en) 1980-05-23
FR2219310A1 (en) 1974-09-20
JPS5024618A (en) 1975-03-15
GB1450649A (en) 1976-09-22

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