GB682141A - Improvements in combined steam turbine and gas turbine plants - Google Patents

Improvements in combined steam turbine and gas turbine plants

Info

Publication number
GB682141A
GB682141A GB7856/51A GB785651A GB682141A GB 682141 A GB682141 A GB 682141A GB 7856/51 A GB7856/51 A GB 7856/51A GB 785651 A GB785651 A GB 785651A GB 682141 A GB682141 A GB 682141A
Authority
GB
United Kingdom
Prior art keywords
turbine
low pressure
plant
gases
steam
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
GB7856/51A
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.)
Rheinmetall Air Defence AG
Maschinenfabrik Oerlikon AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Maschinenfabrik Oerlikon AG
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 Werkzeugmaschinenfabrik Oerlikon Buhrle AG, Maschinenfabrik Oerlikon AG filed Critical Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Publication of GB682141A publication Critical patent/GB682141A/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
    • F01K23/10Plants 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 with exhaust fluid of one cycle heating the fluid in another cycle
    • F01K23/103Plants 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 with exhaust fluid of one cycle heating the fluid in another cycle with afterburner in exhaust boiler

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

682,141. Gas turbine plant. MASCHINENFABRIK OERLIKON. April 4, 1951 [April.24, 1950], No. 7856/51. Class 110(iii) In a combined multi-stage steam turbine and multi-staged gas turbine plant, at least a part of the gases from the high pressure stage of the gas turbine are used to effect a superheating of the, steam between the stages of the steam turbine plant and at least a part of the exhaust gases of the gas turbine plant gives up heat to the combustion air for the boiler of the steam turbine plant. In the plant shown, steam from a boiler plant I is used in a multi-stage steam turbine plant 11 comprising high, intermediate and low pressure stages 6, 8, 8<SP>1</SP>, interstage superheaters 7, 7<SP>1</SP>, a condenser 9 and an electric generator 10. The compressed air from a compressor 11 of a gas turbine plant III is heated in a heat exchanger 15, further heated in a heat exchanger 4<SP>1</SP> located in the path of the combustion gases leaving the boiler, and then used in a high pressure air turbine 12". The exhaust gases from the turbine 12<SP>11</SP> is used to heat the interstage superheaters 7, 7<SP>1</SP> and the heat exchanger 15 before passing to a combustion chamber 13<SP>1</SP> the gases from which are used to drive a low pressure gas turbine 12<SP>1</SP>. The exhaust gases from the turbine 12<SP>1</SP> are used in part as combustion air in the grate 1 of the boiler and in part to heat the feed water heater 16. In a modification, the air from the compressor 11 is heated in a combustion chamber, which supplies gas to a high pressure turbine the exhaust of which is used in part in an interstage superheater and in part in a feed water heater. After passing through the superheater and feed water heater, the gases are re-united and then pass to another combustion chamber which supplies a low pressure turbine. It is stated that part of exhaust gases of the high or low pressure turbines may be used to heat the compressed air leaving the compressor. When multiple interstage superheating is employed the temperature of the superheated steam in the various superheaters may be different from one another. The compressor may be arranged in two stages driven by the high pressure and low pressure turbines respectively or the compressor may be driven by the low pressure turbine at variable speed independently of the high pressure turbine. The combustion chamber before the low pressure turbine may be dispensed with.
GB7856/51A 1950-04-24 1951-04-04 Improvements in combined steam turbine and gas turbine plants Expired GB682141A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH682141X 1950-04-24

Publications (1)

Publication Number Publication Date
GB682141A true GB682141A (en) 1952-11-05

Family

ID=4528552

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7856/51A Expired GB682141A (en) 1950-04-24 1951-04-04 Improvements in combined steam turbine and gas turbine plants

Country Status (1)

Country Link
GB (1) GB682141A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2006069948A2 (en) * 2004-12-23 2006-07-06 Alstom Technology Ltd Power plant
EP2011972A2 (en) 2007-07-03 2009-01-07 clm technologie ag Method and device for generating an overheated medium

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2006069948A2 (en) * 2004-12-23 2006-07-06 Alstom Technology Ltd Power plant
WO2006069948A3 (en) * 2004-12-23 2006-09-08 Alstom Technology Ltd Power plant
US7661268B2 (en) 2004-12-23 2010-02-16 Alstom Technology Ltd Power plant
EP2011972A2 (en) 2007-07-03 2009-01-07 clm technologie ag Method and device for generating an overheated medium
EP2011972A3 (en) * 2007-07-03 2009-08-05 clm technologie ag Method and device for generating an overheated medium

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