GB202405688D0 - Burner for gas turbine engine and method for inhibiting effects of flashback on the burner - Google Patents

Burner for gas turbine engine and method for inhibiting effects of flashback on the burner

Info

Publication number
GB202405688D0
GB202405688D0 GBGB2405688.9A GB202405688A GB202405688D0 GB 202405688 D0 GB202405688 D0 GB 202405688D0 GB 202405688 A GB202405688 A GB 202405688A GB 202405688 D0 GB202405688 D0 GB 202405688D0
Authority
GB
United Kingdom
Prior art keywords
burner
flashback
gas turbine
turbine engine
inhibiting effects
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.)
Pending
Application number
GBGB2405688.9A
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.)
Siemens Energy Global GmbH and Co KG
Original Assignee
Siemens Energy Global GmbH and Co KG
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 Siemens Energy Global GmbH and Co KG filed Critical Siemens Energy Global GmbH and Co KG
Priority to GBGB2405688.9A priority Critical patent/GB202405688D0/en
Publication of GB202405688D0 publication Critical patent/GB202405688D0/en
Pending 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
GBGB2405688.9A 2024-04-23 2024-04-23 Burner for gas turbine engine and method for inhibiting effects of flashback on the burner Pending GB202405688D0 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GBGB2405688.9A GB202405688D0 (en) 2024-04-23 2024-04-23 Burner for gas turbine engine and method for inhibiting effects of flashback on the burner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB2405688.9A GB202405688D0 (en) 2024-04-23 2024-04-23 Burner for gas turbine engine and method for inhibiting effects of flashback on the burner

Publications (1)

Publication Number Publication Date
GB202405688D0 true GB202405688D0 (en) 2024-06-05

Family

ID=91248747

Family Applications (1)

Application Number Title Priority Date Filing Date
GBGB2405688.9A Pending GB202405688D0 (en) 2024-04-23 2024-04-23 Burner for gas turbine engine and method for inhibiting effects of flashback on the burner

Country Status (1)

Country Link
GB (1) GB202405688D0 (en)

Similar Documents

Publication Publication Date Title
EP4019838B8 (en) Torch ignitor system for a combustor of a gas turbine engine and method of operating the same
ATE373206T1 (en) OPERATING METHOD FOR A FIREPLACE SYSTEM
WO2009121781A8 (en) Pilot combustor in a burner
WO2009038652A3 (en) Apparatus and method for controlling the secondary injection of fuel
GB202016002D0 (en) An improved turbofan gas turbine engine
MX2020012111A (en) System and method of improving combustion stability in a gas turbine.
GB202405688D0 (en) Burner for gas turbine engine and method for inhibiting effects of flashback on the burner
WO2005028960A3 (en) Pilot combustor for stabilizing combustion in gas turbine engines
GB202210142D0 (en) Gas turbine engine
GB202201315D0 (en) Gas turbine engine
GB2612091B (en) Method of combustion and fuel injection system for hydrogen gas
GB202306310D0 (en) Fuel lance for burner of gas turbine engine
GB202306308D0 (en) Burner for gas turbine engine
GB202306306D0 (en) Burner for gas turbine engine
GB202403770D0 (en) Gas turbine engine with relative clocking of bifurcations
GB202408237D0 (en) Gas turbine emissions
GB202408231D0 (en) Gas turbine emissions
GB202102149D0 (en) Gas turbine engine nacelle and method of designing same
GB202018438D0 (en) Gas turbine engine nacelle and method of designing same
GB202403522D0 (en) Gas turbine engine
GB202319128D0 (en) Gas turbine fuel temperature
GB202204218D0 (en) System and method for use with gas turbine engine
GB202210496D0 (en) Liner for groove of gas turbine engine and method of manufacturing thereof
GB2614839B (en) Gas turbine fuel treatment circuit and method for starting up a gas turbine
GB202009568D0 (en) Burner of a reheat gas turbine engine