CN104061599B - 用于向燃烧器提供燃料的系统 - Google Patents

用于向燃烧器提供燃料的系统 Download PDF

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Publication number
CN104061599B
CN104061599B CN201410100637.8A CN201410100637A CN104061599B CN 104061599 B CN104061599 B CN 104061599B CN 201410100637 A CN201410100637 A CN 201410100637A CN 104061599 B CN104061599 B CN 104061599B
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China
Prior art keywords
fuel distribution
fuel
flow
flange
downstream
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English (en)
Chinese (zh)
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CN104061599A (zh
Inventor
R.M.迪钦蒂奥
P.B.梅尔顿
L.J.斯托亚
C.P.威利斯
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General Electric Company PLC
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General Electric Co
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    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/222—Fuel flow conduits, e.g. manifolds
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
CN201410100637.8A 2013-03-18 2014-03-18 用于向燃烧器提供燃料的系统 Active CN104061599B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/845365 2013-03-18
US13/845,365 US9316155B2 (en) 2013-03-18 2013-03-18 System for providing fuel to a combustor
US13/845,365 2013-03-18

Publications (2)

Publication Number Publication Date
CN104061599A CN104061599A (zh) 2014-09-24
CN104061599B true CN104061599B (zh) 2018-01-09

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CN201410100637.8A Active CN104061599B (zh) 2013-03-18 2014-03-18 用于向燃烧器提供燃料的系统

Country Status (5)

Country Link
US (1) US9316155B2 (enExample)
JP (1) JP6506503B2 (enExample)
CN (1) CN104061599B (enExample)
CH (1) CH707852A2 (enExample)
DE (1) DE102014103087A1 (enExample)

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Also Published As

Publication number Publication date
US20140260272A1 (en) 2014-09-18
US9316155B2 (en) 2016-04-19
JP2014181902A (ja) 2014-09-29
JP6506503B2 (ja) 2019-04-24
CN104061599A (zh) 2014-09-24
CH707852A2 (de) 2014-09-30
DE102014103087A1 (de) 2014-09-18

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