GB743633A - Improvements in or relating to gas turbine engines - Google Patents

Improvements in or relating to gas turbine engines

Info

Publication number
GB743633A
GB743633A GB34510/53A GB3451053A GB743633A GB 743633 A GB743633 A GB 743633A GB 34510/53 A GB34510/53 A GB 34510/53A GB 3451053 A GB3451053 A GB 3451053A GB 743633 A GB743633 A GB 743633A
Authority
GB
United Kingdom
Prior art keywords
air
ignited
gas
gas turbine
dec
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
GB34510/53A
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation 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 Motors Liquidation Co filed Critical Motors Liquidation Co
Publication of GB743633A publication Critical patent/GB743633A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • 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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)

Abstract

743,633. Gas burners. GENERAL MOTORS CORPORATION. Dec. 11, 1953 [Dec. 31, 1952], No. 34510/53. Classes 75(1) and 75(3). [Also in Groups XII and XXVI] A gas turbine is supplied with working fluid by a number of combustion chambers 60 enclosed in an air casing 32. Two of the combustion chambers are ignited by igniters 118 bolted to the air casing 32. The remaining chambers are ignited through crossover tubes. Each igniter 118 comprises a gas supply conduit 126 which delivers gas through an adjustable nozzle 128 to a mixing venturi where it is mixed with air from the air casing supplied through the passage 136. The mixture is ignited in the chamber 132 by a spark plug 134 and passes to the flame tube and burner 114 through a conduit 122. Axial adjustment of the nozzle 128 varies the air to fuel ratio.
GB34510/53A 1952-12-31 1953-12-11 Improvements in or relating to gas turbine engines Expired GB743633A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US318027XA 1952-12-31 1952-12-31

Publications (1)

Publication Number Publication Date
GB743633A true GB743633A (en) 1956-01-18

Family

ID=21861469

Family Applications (1)

Application Number Title Priority Date Filing Date
GB34510/53A Expired GB743633A (en) 1952-12-31 1953-12-11 Improvements in or relating to gas turbine engines

Country Status (3)

Country Link
CH (1) CH318027A (en)
FR (1) FR1090334A (en)
GB (1) GB743633A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1985001987A1 (en) * 1983-10-25 1985-05-09 Alan Edward Coppin Transportable power unit
US5353586A (en) * 1991-04-17 1994-10-11 Rolls-Royce Plc Combustion chamber assembly with hollow support strut for carrying cooling air

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1080820B (en) * 1957-08-20 1960-04-28 Wagner Fa Ferd Combustion device, especially for rocket engines
GB1080747A (en) * 1964-09-29 1967-08-23 English Electric Co Ltd Improvements in or relating to turbines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1985001987A1 (en) * 1983-10-25 1985-05-09 Alan Edward Coppin Transportable power unit
US5353586A (en) * 1991-04-17 1994-10-11 Rolls-Royce Plc Combustion chamber assembly with hollow support strut for carrying cooling air

Also Published As

Publication number Publication date
FR1090334A (en) 1955-03-29
CH318027A (en) 1956-12-15

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