GB781428A - Improvements in or relating to gas-turbine engines - Google Patents

Improvements in or relating to gas-turbine engines

Info

Publication number
GB781428A
GB781428A GB1188454A GB1188454A GB781428A GB 781428 A GB781428 A GB 781428A GB 1188454 A GB1188454 A GB 1188454A GB 1188454 A GB1188454 A GB 1188454A GB 781428 A GB781428 A GB 781428A
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
column
conduit
peat
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.)
Expired
Application number
GB1188454A
Inventor
James Douglas Thorn
Meyer Julian Kemper
Anthony Victor George Jackman
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.)
Ruston and Hornsby Ltd
Original Assignee
Ruston and Hornsby 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 Ruston and Hornsby Ltd filed Critical Ruston and Hornsby Ltd
Priority to GB1188454A priority Critical patent/GB781428A/en
Publication of GB781428A publication Critical patent/GB781428A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/205Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products in a fluidised-bed combustor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/26Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being solid or pulverulent, e.g. in slurry or suspension

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

781,428. Gas turbine plant. RUSTON & HORNSBY, Ltd. April 25, 1955 [April 24, 1954], No. 11884/54. Class 110 (3). A two-stage arrangement for the supply of fluidized fuel to the combustion chamber of a gas turbine engine comprising two fluidizing columns in series, the first working at atmospheric pressure and the second at a pressure appropriate to the feeding of the fluidized fuel into the combustion chamber has the fluidized fuel supply from the pressurized column to the combustion chamber controlled in accordance with some engine variable such as speed or load. From the column 22, the fuel is pumped by means of a peat pump 23 and a high-pressure air supply 24 through a conduit 25 to a small cyclone 26, arranged on top of a pressurized fluidizing column 27, which separates the high pressure air from the peat. From the column 27 the peat is delivered from a valve 28 and conduit 29 to the combustion chamber 30 of the gas turbine plant. The high-pressure air from the cyclone 26 is led through the conduit 32 to the combustion chamber. The fluidizing air for the column 27 is taken from the gas turbine compressor through a booster fan and conduit 36. Air from the same source is used to convey fluidized peat from the control valve 28 into the combustion chamber 30. The control valve 28 is controlled by an engine speed responsive governor 38 through an oil pressure line 39. Specifications 781,427, 781,429, 781,430 and 781,431 are referred to.
GB1188454A 1954-04-24 1954-04-24 Improvements in or relating to gas-turbine engines Expired GB781428A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1188454A GB781428A (en) 1954-04-24 1954-04-24 Improvements in or relating to gas-turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1188454A GB781428A (en) 1954-04-24 1954-04-24 Improvements in or relating to gas-turbine engines

Publications (1)

Publication Number Publication Date
GB781428A true GB781428A (en) 1957-08-21

Family

ID=9994447

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1188454A Expired GB781428A (en) 1954-04-24 1954-04-24 Improvements in or relating to gas-turbine engines

Country Status (1)

Country Link
GB (1) GB781428A (en)

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