IT963987B - Impianto di post combostione per motore a turbina a gas - Google Patents

Impianto di post combostione per motore a turbina a gas

Info

Publication number
IT963987B
IT963987B IT28185/72A IT2818572A IT963987B IT 963987 B IT963987 B IT 963987B IT 28185/72 A IT28185/72 A IT 28185/72A IT 2818572 A IT2818572 A IT 2818572A IT 963987 B IT963987 B IT 963987B
Authority
IT
Italy
Prior art keywords
combostion
post
gas turbine
turbine engine
engine
Prior art date
Application number
IT28185/72A
Other languages
English (en)
Original Assignee
Rolls Royce 1971 Ltd
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 1971 Ltd filed Critical Rolls Royce 1971 Ltd
Application granted granted Critical
Publication of IT963987B publication Critical patent/IT963987B/it

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
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Gas Burners (AREA)
IT28185/72A 1971-08-21 1972-08-12 Impianto di post combostione per motore a turbina a gas IT963987B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3933271A GB1390031A (en) 1971-08-21 1971-08-21 Reheat system for a gas turbine engine

Publications (1)

Publication Number Publication Date
IT963987B true IT963987B (it) 1974-01-21

Family

ID=10408995

Family Applications (1)

Application Number Title Priority Date Filing Date
IT28185/72A IT963987B (it) 1971-08-21 1972-08-12 Impianto di post combostione per motore a turbina a gas

Country Status (6)

Country Link
US (1) US3786632A (it)
JP (1) JPS4829919A (it)
DE (1) DE2239275C3 (it)
FR (1) FR2150403B1 (it)
GB (1) GB1390031A (it)
IT (1) IT963987B (it)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2188060B1 (it) * 1972-06-01 1976-06-11 Snecma
US9121608B2 (en) 2011-12-29 2015-09-01 General Electric Company Gas turbine engine including secondary combustion chamber integrated with the stator vanes in the turbine/expansion section of the engine and a method of operating the same
CN103277815B (zh) * 2013-05-10 2015-07-08 南京航空航天大学 贫油部分预混预蒸发均质供油装置
CN118328419B (zh) * 2024-06-04 2025-02-07 江苏科技大学 一种涡控式稳定器

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1082130A (en) * 1910-11-10 1913-12-23 George W Mccallen Oil-burner.
GB670247A (en) * 1948-02-19 1952-04-16 Power Jets Res & Dev Ltd Improvements in or relating to combustion apparatus
GB938553A (en) * 1961-05-09 1963-10-02 Rolls Royce Reheat combustion apparatus for a gas turbine engine
US3483649A (en) * 1968-10-29 1969-12-16 Us Interior Electrical trawl net system
US3652016A (en) * 1970-05-12 1972-03-28 Lucas Industries Ltd Liquid atomizing devices

Also Published As

Publication number Publication date
US3786632A (en) 1974-01-22
GB1390031A (en) 1975-04-09
FR2150403B1 (it) 1976-05-21
DE2239275A1 (de) 1973-03-08
FR2150403A1 (it) 1973-04-06
DE2239275C3 (de) 1975-11-06
DE2239275B2 (de) 1975-03-20
JPS4829919A (it) 1973-04-20

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