GB690804A - Improvements in process of generating power involving catalytic oxidation - Google Patents

Improvements in process of generating power involving catalytic oxidation

Info

Publication number
GB690804A
GB690804A GB7336/49A GB733649A GB690804A GB 690804 A GB690804 A GB 690804A GB 7336/49 A GB7336/49 A GB 7336/49A GB 733649 A GB733649 A GB 733649A GB 690804 A GB690804 A GB 690804A
Authority
GB
United Kingdom
Prior art keywords
turbine
chamber
pipe
fuel
compressor
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
GB7336/49A
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 GB7336/49A priority Critical patent/GB690804A/en
Publication of GB690804A publication Critical patent/GB690804A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B51/00Other methods of operating engines involving pretreating of, or adding substances to, combustion air, fuel, or fuel-air mixture of the engines
    • F02B51/02Other methods of operating engines involving pretreating of, or adding substances to, combustion air, fuel, or fuel-air mixture of the engines involving catalysts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G3/00Combustion-product positive-displacement engine plants
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

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

Abstract

690,804. Generating combustion products under pressure. HOUDRY, E. J. March 17, 1949, No. 7336/49. Class 51(i) [Also in Group XXVI] Compressed air, fresh fuel, and previously oxidized fuel are admitted to the combustion chamber of a gas turbine or other power plant in such proportion that the mixture is too weak to ignite under the operating conditions. Oxidization of the fuel is secured by the presence of a reducing oxidizing catalyst. An example of the catalysts mentioned is copper manganese finely divided over an activated alumina support. The gas turbine plant shown in Fig. 2 is of the partly closed circuit type. Turbines n, p in series drive compressors t, u. Part of the exhaust from turbine p is returned to the circuit at 17 and the rest goes to a turbine r which drives a make-up compressor s. An interstage cooler o between the compressor stages t, u acts as a reheater for the working fluid, giving up heat first to the fluid in pipe 12 connecting turbine stages n, p and then to fluid in pipe 14 connecting turbine p with turbine r. The air from compressor u passes to the combustion chamber and fuel is supplied thereto by a pump P. In another plant there are three turbines in place of turbine n with catalytic re-heat chambers between them. Air from the delivery of pump s is further compressed and passed to the re-heat chambers. In the plant shown in Fig. 4, there are four combustion chambers 50, 60, 70, 80 with inlet and outlet pipes controlled by valves 56. With the valves as shown, chamber 50 receives compressed gas from pipe 61 and fuel from pipe 59 and discharges working fluid to turbine 51. The inlets of chamber 60 are closed and the contents of the chamber expand and pass through a reducing valve 55 to the low-pressure turbine 52. The chamber 70 receives scavenging air from a pipe 71 and discharges it to atmosphere by pipe 62. The upper inlets of chamber 80 are closed and the chamber is filled with compressed gas from compressor 53 through a restricted orifice 58. The valves are manipulated so that these four operations take place in turn in each chamber. Specifications 494,098 and 690,805 are referred to.
GB7336/49A 1949-03-17 1949-03-17 Improvements in process of generating power involving catalytic oxidation Expired GB690804A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7336/49A GB690804A (en) 1949-03-17 1949-03-17 Improvements in process of generating power involving catalytic oxidation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7336/49A GB690804A (en) 1949-03-17 1949-03-17 Improvements in process of generating power involving catalytic oxidation

Publications (1)

Publication Number Publication Date
GB690804A true GB690804A (en) 1953-04-29

Family

ID=9831154

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7336/49A Expired GB690804A (en) 1949-03-17 1949-03-17 Improvements in process of generating power involving catalytic oxidation

Country Status (1)

Country Link
GB (1) GB690804A (en)

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