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GB889271A - Improvements in combustion apparatus - Google Patents

Improvements in combustion apparatus

Info

Publication number
GB889271A
GB889271A GB40997/60A GB4099760A GB889271A GB 889271 A GB889271 A GB 889271A GB 40997/60 A GB40997/60 A GB 40997/60A GB 4099760 A GB4099760 A GB 4099760A GB 889271 A GB889271 A GB 889271A
Authority
GB
United Kingdom
Prior art keywords
fuel
burner
tubular member
cross
gas stream
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
GB40997/60A
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 GB889271A publication Critical patent/GB889271A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)

Abstract

889,271. Generating combustion products under pressure. GENERAL ELECTRIC CO. Nov. 29, 1960 [Dec. 14, 1959], No. 40997/60. Class 51 (1). [Also in Group XI] A pilot burner 18 for the after-burner of a gas turbine engine comprises a fuel supply pipe 21 extending transversely into the hot combustion gas stream in the after-burner and an open-ended tubular member 24 of cardioidal cross-section disposed at the discharge end of the fuel supply pipe 21 and arranged with its longitudinal axis parallel to the hot combustion gas stream. The fuel pipe 21 directs the fuel towards the cusp of the cardiodal cross-section. The flow of combustible gas through the tubular member forms with the fuel a pair of spiralling vortices which are directed into a liner 16 in the after burner casing 13. The main supply of fuel is provided by spray bars 17. An annular flame holder 32 comprising four scoop sections is provided.
GB40997/60A 1959-12-14 1960-11-29 Improvements in combustion apparatus Expired GB889271A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US889271XA 1959-12-14 1959-12-14

Publications (1)

Publication Number Publication Date
GB889271A true GB889271A (en) 1962-02-14

Family

ID=22214322

Family Applications (1)

Application Number Title Priority Date Filing Date
GB40997/60A Expired GB889271A (en) 1959-12-14 1960-11-29 Improvements in combustion apparatus

Country Status (1)

Country Link
GB (1) GB889271A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2316162A (en) * 1996-08-07 1998-02-18 Europ Gas Turbines Ltd Device for imparting swirl to a fluid flow

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2316162A (en) * 1996-08-07 1998-02-18 Europ Gas Turbines Ltd Device for imparting swirl to a fluid flow
GB2316162B (en) * 1996-08-07 1999-12-08 Europ Gas Turbines Ltd Devices for imparting swirl to fluid flow

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