GB693616A - Improvements in or relating to internal combustion gas turbines - Google Patents

Improvements in or relating to internal combustion gas turbines

Info

Publication number
GB693616A
GB693616A GB3120549A GB3120549A GB693616A GB 693616 A GB693616 A GB 693616A GB 3120549 A GB3120549 A GB 3120549A GB 3120549 A GB3120549 A GB 3120549A GB 693616 A GB693616 A GB 693616A
Authority
GB
United Kingdom
Prior art keywords
heat
exchanger
air
fuel
combustion
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
GB3120549A
Inventor
Reginald George Voysey
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB3120549A priority Critical patent/GB693616A/en
Publication of GB693616A publication Critical patent/GB693616A/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
    • F02C3/22Gas-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 gaseous at standard temperature and pressure
    • 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
    • F02C7/00Features, 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
    • F02C7/08Heating air supply before combustion, e.g. by exhaust gases

Landscapes

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

Abstract

693,616. Thermal regenerators and recuperators. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. Feb. 1, 1951 [Dec. 5, 1949], No. 31205/49. Class 64 (i) [Also in Group XXVI] To enable a fuel of low calorific value, such as a gaseous mixture of coal dust dispersed in air or methane in mine ventilating air, or solid fuel, e.g. peat saturated with water or sewage sludge, to be used in a gas turbine plant, the combustible gas mixture or combustion air is heated in a regenerative type heat-exchanger before its entry into the combustion chamber by the combustion gases prior to their entry into the turbine. In the arrangement shown, the compressor 1 feeds air to a gas turbine 3 through a heat-exchanger 2 heated by the turbine exhaust gases and a further regenerative heat-exchanger 5. The heat-exchanger 5 is arranged to add sufficient heat to the air for combustion when using solid fuel and to the fuel-air mixture when using a gaseous fuel so that the combustion is self sustaining. This heat-exchanger comprises two parts 7 and 9 with a combustion chamber midway at 8 and changeover valve gear 6. The arrangement is such that, at one stage, the incoming air-fuel mixture passes through part 7, which has been previously heated, to the combustion chamber 8 where it is burnt and then passes through the part 9 to the turbine 3. When the temperature of the part 7 has fallen sufficiently, the valve gear 6 is operated so that the air-fuel mixture passes through in the reverse direction, i.e. through the part 9 to the combustion chamber 8 and from this chamber through the part 7 to the turbine 3. When the temperature of the part 9 falls sufficiently, the valve gear 6 is again operated and the cycle repeated. Auxiliary fuel may be supplied through conduit 5a and valve 5b for starting purposes. The plant may be used to bum a solid fuel such as peat. In this case, the peat is comminuted and shredded and fed to the combustion chamber 8 and only the combustion air is preheated in the heat-exchanger 5. To avoid blocking the outlet side of the hea-texchanger with ash, a cyclone separator may be arranged at the outlet of the combustion chamber. If there is no risk of the ash impairing the efficiency of the heat-exchanger, the cyclone separator may be arranged at the outlet of the heat-exchanger to avoid damage to the turbine blades. An auxiliary heater may be arranged between the heat exchanger 5 and the turbine inlet to correct any temperature fluctuations. The regenerative heat-exchanger described may be replaced by one of the rotary matrix type. The matrix of the regenerative heat-exchangers may be constructed at least partly of combustion-promoting catalysts. This enables the size of the heat-exchanger 5 to be reduced. A further auxiliary combustion chamber may be arranged between the conduits 12 and 15 to bum an auxiliary fuel which may be of higher calorific value. According to the Provisional Specification, a recuperative heat-exchanger may be used.
GB3120549A 1949-12-05 1949-12-05 Improvements in or relating to internal combustion gas turbines Expired GB693616A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3120549A GB693616A (en) 1949-12-05 1949-12-05 Improvements in or relating to internal combustion gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3120549A GB693616A (en) 1949-12-05 1949-12-05 Improvements in or relating to internal combustion gas turbines

Publications (1)

Publication Number Publication Date
GB693616A true GB693616A (en) 1953-07-01

Family

ID=10319583

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3120549A Expired GB693616A (en) 1949-12-05 1949-12-05 Improvements in or relating to internal combustion gas turbines

Country Status (1)

Country Link
GB (1) GB693616A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1549842A1 (en) * 2002-09-27 2005-07-06 Commonwealth Scientific And Industrial Research Organisation A system for catalytic combustion

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1549842A1 (en) * 2002-09-27 2005-07-06 Commonwealth Scientific And Industrial Research Organisation A system for catalytic combustion
EP1549842A4 (en) * 2002-09-27 2009-05-13 Commw Scient Ind Res Org A system for catalytic combustion

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