GB706352A - Improvements in and relating to combustion chambers of the pulsatory column type andthermal power plants - Google Patents

Improvements in and relating to combustion chambers of the pulsatory column type andthermal power plants

Info

Publication number
GB706352A
GB706352A GB1793951A GB1793951A GB706352A GB 706352 A GB706352 A GB 706352A GB 1793951 A GB1793951 A GB 1793951A GB 1793951 A GB1793951 A GB 1793951A GB 706352 A GB706352 A GB 706352A
Authority
GB
United Kingdom
Prior art keywords
air
fuel
chamber
admission
vanes
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
GB1793951A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB1793951A priority Critical patent/GB706352A/en
Publication of GB706352A publication Critical patent/GB706352A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01KSTEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K23/00Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
    • F01K23/02Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
    • F01K23/06Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Air-Conditioning For Vehicles (AREA)

Abstract

706,352. Gas and steam turbines. HALLOWELL, E. July 14, 1952 [July 28, 1951], No. 17939/51. Class 110 (3). [Also in Group XII] A power plant comprises a pulse-jet combustion chamber 10 with pre-heated fuel mixtures, an air turbine 17, a steam generator 22 and steam turbine 23 and a number of heat-exchangers 30, 27, 19, 21. The exhaust gases from the chamber 10 contain surplus air which is mixed with fuel and air supplied by a fan 31, to heat the generator 22. The turbine 23 exhausts to a condenser 25 and feed water is passed by a pump 26 through pre-heaters 27, economizer 28 to the steamgenerator. Air is supplied to the chamber 10 by a fan 29 through a pre-heater 30 and heatexchanger 19, an annular space 11, a high-temperature heat-exchanger 21 (or bye-pass 20) to the hot-air turbine 17 which drives an electrical generator or the like 18. The turbine 17 exhausts at below atmospheric pressure to the exchanger 19, losing some heat to the air from the fan 29, and is fed to an inlet 13 of the chamber 10. The duct 10 has one or more sparking plugs 32, for starting purposes, and is supplied with fuel mixture through a port 14 by a fan 15. A rotor has vanes 38, 39 on a spindle 37 which is driven by an electric motor. The rotor ends have ported discs 44, containing fuel-admission ports 45, 46, rotating with fine clearances relative to the casing ends which contain co-acting ports ; the ends may be angularly adjustable. The interior of the spindle 37 and the vanes may be cooled. In between the full-open position of the vanes 38, 39, as shown, and the fully-closed position one or other of the admission ports 45, 46 in the end discs comes into alignment with the fuel admission port to allow admission of the fuel into the air stream entering the inlet 13. As the rotor rotates successive charges of air and air fuel mixture enter the duct 35 and during the intervals when the vanes cut off the supplies of air and fuel, a succession of explosions occurs near the admission end of the duct due to the plug 32. High-velocity gas columns travel outwardly thus inducing fresh charges of air and air-fuel mixture during the periods when the vanes are open, and when a gas column reaches an intermediate point it rebounds to compress an incoming charge of air followed by an airfuel mixture. The intermediate " cushion " of air prevents pre-ignition of the fuel charge by hot exhaust products. When the chamber 10 is warmed up it operates on compression-ignition and the sparking plug is cut out. A reduction in the aspiration pressure at the inlet 13 causes increasing frequency of rebound compression of the gas columns in the chamber 10, the duct of which may be very long. A valve 33 regulates the amount of air passing through the heat exchanger 21. Figs. 4 and 5 show other designs of the rotor. In the former two combustion chambers 50, 51 are arranged back to back, the air inlets being shown at 57 and 58. Fuel admission points 60 ... 63 are provided in rotary end discs 59 and co-act with ports 65, 66 in the casing ends. The quantity of excess air admitted to a chamber 10 may vary between 20 per cent and 200 per cent. Firebricks or the like may be used in the high temperature heat exchanger 21. Heat exchanger 19 may be omitted.
GB1793951A 1951-07-28 1951-07-28 Improvements in and relating to combustion chambers of the pulsatory column type andthermal power plants Expired GB706352A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1793951A GB706352A (en) 1951-07-28 1951-07-28 Improvements in and relating to combustion chambers of the pulsatory column type andthermal power plants

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1793951A GB706352A (en) 1951-07-28 1951-07-28 Improvements in and relating to combustion chambers of the pulsatory column type andthermal power plants

Publications (1)

Publication Number Publication Date
GB706352A true GB706352A (en) 1954-03-31

Family

ID=10103888

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1793951A Expired GB706352A (en) 1951-07-28 1951-07-28 Improvements in and relating to combustion chambers of the pulsatory column type andthermal power plants

Country Status (1)

Country Link
GB (1) GB706352A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1253851B (en) * 1955-12-16 1967-11-09 Gustavsbergs Fabriker Ab Installation on a boiler with a combustion chamber working with pulsating combustion

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1253851B (en) * 1955-12-16 1967-11-09 Gustavsbergs Fabriker Ab Installation on a boiler with a combustion chamber working with pulsating combustion

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