GB781431A - Improvements in or relating to gas turbine engines - Google Patents

Improvements in or relating to gas turbine engines

Info

Publication number
GB781431A
GB781431A GB1188754A GB1188754A GB781431A GB 781431 A GB781431 A GB 781431A GB 1188754 A GB1188754 A GB 1188754A GB 1188754 A GB1188754 A GB 1188754A GB 781431 A GB781431 A GB 781431A
Authority
GB
United Kingdom
Prior art keywords
conduit
column
gas turbine
fluidizing
air
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
GB1188754A
Inventor
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 GB1188754A priority Critical patent/GB781431A/en
Publication of GB781431A publication Critical patent/GB781431A/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
    • F02C3/26Gas-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R5/00Continuous combustion chambers using solid or pulverulent fuel

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Separation By Absorption (AREA)

Abstract

781,431. Gas turbine plant. RUSTON & HORNSBY, Ltd. April 25, 1955 [April 24, 1954], No. 11887/54. 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 fluidizing air supplied to the pressurized column taken from the duct between the compressor and combustion chamber of the engine. Peat from a de-watering press (not shown) is fed to a disintegrator 11, Fig. 1, and then passed to a rotary louvre drier 12 where it is dried by the gas turbine engine exhaust fed through a conduit 13. The peat leaving the drier 12 falls on to a rotary table 15 where it is divided into two parts, one part being led to the mix back conveyer 16 and returned to the de-watering press and the other to the conduit 17 leading to the air-swept grinding machine 19. The relative sizes of the two parts is controlled by the position of the adjustable blades 18. On leaving the grinding machine the pulverized fuel is separated from the carrying air in a cyclone 21 arranged on top of an atmospheric fluidizing column 22 which acts as a storage vessel. 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 34 through a booster fan 35 and conduit 36. The control valve 28 is controlled by an engine speed responsive governor 38 through an oil pressure line 38. To avoid velocity variations in the supply of fluidizing air to the pressurized column 27 a self-regulating throttle valve 62 is arranged in the conduit 61<SP>1</SP> upstream of a venturi 63. The pressures at the throat and downstream of the venturi actuate a diaphragm 66 controlling through a valve 67 the throttle valve 62. Specifications 781,427, 781,428, 781,429 and 781,430 are referred to.
GB1188754A 1954-04-24 1954-04-24 Improvements in or relating to gas turbine engines Expired GB781431A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1188754A GB781431A (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
GB1188754A GB781431A (en) 1954-04-24 1954-04-24 Improvements in or relating to gas turbine engines

Publications (1)

Publication Number Publication Date
GB781431A true GB781431A (en) 1957-08-21

Family

ID=9994491

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1188754A Expired GB781431A (en) 1954-04-24 1954-04-24 Improvements in or relating to gas turbine engines

Country Status (1)

Country Link
GB (1) GB781431A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114811658A (en) * 2022-05-11 2022-07-29 中南大学 Fuel supply device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114811658A (en) * 2022-05-11 2022-07-29 中南大学 Fuel supply device
CN114811658B (en) * 2022-05-11 2023-03-31 中南大学 Fuel supply device

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