DE2114895A1 - Nachbrenner für Gasturbinen - Google Patents

Nachbrenner für Gasturbinen

Info

Publication number
DE2114895A1
DE2114895A1 DE19712114895 DE2114895A DE2114895A1 DE 2114895 A1 DE2114895 A1 DE 2114895A1 DE 19712114895 DE19712114895 DE 19712114895 DE 2114895 A DE2114895 A DE 2114895A DE 2114895 A1 DE2114895 A1 DE 2114895A1
Authority
DE
Germany
Prior art keywords
injectors
tubes
afterburner
ring
gas turbine
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
DE19712114895
Other languages
German (de)
English (en)
Inventor
John Kahley Palos Verdes Peninsula Calif. Arand (V.StA.)
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of DE2114895A1 publication Critical patent/DE2114895A1/de
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
    • F23R3/02—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)
  • Fuel-Injection Apparatus (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
DE19712114895 1970-06-29 1971-03-27 Nachbrenner für Gasturbinen Pending DE2114895A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US5041570A 1970-06-29 1970-06-29

Publications (1)

Publication Number Publication Date
DE2114895A1 true DE2114895A1 (de) 1972-01-05

Family

ID=21965128

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19712114895 Pending DE2114895A1 (de) 1970-06-29 1971-03-27 Nachbrenner für Gasturbinen

Country Status (6)

Country Link
US (1) US3670501A (enExample)
BE (1) BE764167A (enExample)
CA (1) CA936369A (enExample)
DE (1) DE2114895A1 (enExample)
FR (1) FR2096537B1 (enExample)
GB (1) GB1335750A (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4312185A (en) * 1980-02-19 1982-01-26 General Electric Company Low profile fuel injection system
US4901527A (en) * 1988-02-18 1990-02-20 General Electric Company Low turbulence flame holder mount
US5022805A (en) * 1989-02-16 1991-06-11 Rolls-Royce Incorporated Cantilever mounting system for structural members having dissimilar coefficients of thermal expansion
US7568346B2 (en) * 2006-10-31 2009-08-04 General Electric Company Method and apparatus for assembling a flameholder for an augmenter
US20100146980A1 (en) * 2007-05-22 2010-06-17 Volvo Aero Corporation masking arrangement for a gas turbine engine
US8776527B1 (en) * 2008-06-17 2014-07-15 Rolls-Royce North American Technologies, Inc. Techniques to reduce infrared detection of a gas turbine engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2714287A (en) * 1950-01-03 1955-08-02 Westinghouse Electric Corp Flameholder device for turbojet afterburner
US2975589A (en) * 1955-06-06 1961-03-21 Gen Electric Wide modulation range reheat fuel system
GB821286A (en) * 1956-06-05 1959-10-07 Rolls Royce Improvements in or relating to reheat combustion equipment of jet-propulsion engines
US2934891A (en) * 1956-08-31 1960-05-03 United Aircraft Corp Anti-screech inner body
US3056261A (en) * 1959-09-01 1962-10-02 Gen Electric Flameholder configuration
US3315468A (en) * 1965-10-01 1967-04-25 Gen Electric Cooled flameholder assembly

Also Published As

Publication number Publication date
BE764167A (fr) 1971-08-02
US3670501A (en) 1972-06-20
GB1335750A (en) 1973-10-31
FR2096537A1 (enExample) 1972-02-18
FR2096537B1 (enExample) 1974-03-01
CA936369A (en) 1973-11-06

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