GB2073399B - Dual premix tube fuel nozzle - Google Patents

Dual premix tube fuel nozzle

Info

Publication number
GB2073399B
GB2073399B GB8110151A GB8110151A GB2073399B GB 2073399 B GB2073399 B GB 2073399B GB 8110151 A GB8110151 A GB 8110151A GB 8110151 A GB8110151 A GB 8110151A GB 2073399 B GB2073399 B GB 2073399B
Authority
GB
United Kingdom
Prior art keywords
dual
fuel nozzle
tube fuel
premix tube
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
GB8110151A
Other versions
GB2073399A (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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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 Technologies Corp filed Critical United Technologies Corp
Publication of GB2073399A publication Critical patent/GB2073399A/en
Application granted granted Critical
Publication of GB2073399B publication Critical patent/GB2073399B/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
    • F23R3/26—Controlling the air flow
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
GB8110151A 1980-04-02 1981-04-01 Dual premix tube fuel nozzle Expired GB2073399B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13664780A 1980-04-02 1980-04-02

Publications (2)

Publication Number Publication Date
GB2073399A GB2073399A (en) 1981-10-14
GB2073399B true GB2073399B (en) 1983-11-02

Family

ID=22473753

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8110151A Expired GB2073399B (en) 1980-04-02 1981-04-01 Dual premix tube fuel nozzle

Country Status (2)

Country Link
JP (1) JPS56168018A (en)
GB (1) GB2073399B (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3241162A1 (en) * 1982-11-08 1984-05-10 Kraftwerk Union AG, 4330 Mülheim PRE-MIXING BURNER WITH INTEGRATED DIFFUSION BURNER
JPH0663646B2 (en) * 1985-10-11 1994-08-22 株式会社日立製作所 Combustor for gas turbine
JPH0735823B2 (en) * 1987-03-25 1995-04-19 エヌエスケー・ワーナー株式会社 Roller synchronous one-way clutch
FR2665729B1 (en) * 1990-08-08 1994-09-23 Snecma FUEL INJECTION DEVICE FOR A TURBOMACHINE COMBUSTION CHAMBER.
US5435139A (en) * 1991-03-22 1995-07-25 Rolls-Royce Plc Removable combustor liner for gas turbine engine combustor
US5307634A (en) * 1992-02-26 1994-05-03 United Technologies Corporation Premix gas nozzle
IT1255613B (en) * 1992-09-24 1995-11-09 Eniricerche Spa LOW EMISSION COMBUSTION SYSTEM FOR GAS TURBINES
EP0747635B1 (en) * 1995-06-05 2003-01-15 Rolls-Royce Corporation Dry low oxides of nitrogen lean premix module for industrial gas turbine engines
US9366432B2 (en) 2012-05-17 2016-06-14 Capstone Turbine Corporation Multistaged lean prevaporizing premixing fuel injector
US10184664B2 (en) 2014-08-01 2019-01-22 Capstone Turbine Corporation Fuel injector for high flame speed fuel combustion

Also Published As

Publication number Publication date
JPS56168018A (en) 1981-12-24
GB2073399A (en) 1981-10-14

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee