GB533394A - Heat power plant - Google Patents

Heat power plant

Info

Publication number
GB533394A
GB533394A GB29162/39A GB2916239A GB533394A GB 533394 A GB533394 A GB 533394A GB 29162/39 A GB29162/39 A GB 29162/39A GB 2916239 A GB2916239 A GB 2916239A GB 533394 A GB533394 A GB 533394A
Authority
GB
United Kingdom
Prior art keywords
gases
gas
heated
turbine
heating
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
GB29162/39A
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 GB533394A publication Critical patent/GB533394A/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
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

533,394. Gas turbines. MASCHINENFABRIK OERLIKON. Nov. 1, 1939, No. 29162. Convention date, Nov. 7, 1938. Drawings to Specification. [Class 110 (iii)] In a gas turbine installation, in which gases are heated at constant volume, the heating is arranged to produce a temperature stratification of the gases in the containing chambers and the cooler gases are expanded in the turbine. The residual gases in the chambers, being the gases which were initially at the highest temperatures, are subsequently expelled by a pipe byepassing the turbine The temperature stratification may be secured by differential heating of the gases and the last gas to enter the chamber may be heated most. If the gases are uniformly heated, the temperature of the gas the first to be heated is raised by adiabatic compression of gas due to the heating of the following gas. In this case, the last gas to enter the chamber is the coolest and the discharge to the turbine is in contrary direction to the entry of the heated gases. The operation of the process is described, inter alia, in connection with a plant similar in arrangement to that described in Specification 530,336.
GB29162/39A 1938-11-07 1939-11-01 Heat power plant Expired GB533394A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH533394X 1938-11-07

Publications (1)

Publication Number Publication Date
GB533394A true GB533394A (en) 1941-02-12

Family

ID=4518610

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29162/39A Expired GB533394A (en) 1938-11-07 1939-11-01 Heat power plant

Country Status (1)

Country Link
GB (1) GB533394A (en)

Similar Documents

Publication Publication Date Title
ES313130A1 (en) Thermal power installations utilizing liquefied natural gas
GB539069A (en) Improvements in and relating to pipes, containers, casings or the like for gases of high temperature
GB554112A (en) Method and device for cooling combustion chambers, particularly for gas turbines or the like
US2621481A (en) Closed cycle air turbine power plant having direct and indirect heat exchangers
GB765731A (en) Improvements relating to pressure exchangers
GB533394A (en) Heat power plant
GB544719A (en) Improvements in plants for producing a mixture of hot air and combustion products under pressure
US2641904A (en) Apparatus for cooling combustion chambers of movable power plants with an oxidizing agent
SU120087A1 (en) Semi-closed gas turbine installation
GB578686A (en) Improvements in regenerative gas turbine plant
US2399152A (en) Gas turbine plant
GB546275A (en) Heat power plant for gaseous working media
SU143815A1 (en) The method of operation of thermal power plants on low-boiling substances
US1894766A (en) Inert gas production
GB532443A (en) Thermal power plant, in which a gaseous working medium, preferably air, continuously describes a closed cycle under a pressure greater than atmospheric pressure
GB660090A (en) Method of operating a steam-power plant comprising a gas turbine or other heat engine producing exhaust gases, a steam producer and a steam turbine with associated condenser
GB621954A (en) Improvements in or relating to thermal power plant
GB568087A (en) A process for the generation of power using turbines
GB650934A (en) Improvements relating to a method of producing power in heat engines through cyclic changes of a gaseous working fluid
SU151157A1 (en) Gas turbine unit with regenerator
GB524694A (en) Improvements in and relating to the operation of metal air heaters and similar heat exchangers
US1888698A (en) Process and apparatus for operating turbines
GB562251A (en) Improvements in or relating to gas turbine plants
GB596305A (en) Improvements in or relating to plant for providing hot compressed air
GB581400A (en) Improvements relating to the continuous production of power from successive explosions