CH315324A - Method for reducing the adverse effects of combustion products of the combustion chamber in a gas turbine plant - Google Patents

Method for reducing the adverse effects of combustion products of the combustion chamber in a gas turbine plant

Info

Publication number
CH315324A
CH315324A CH315324DA CH315324A CH 315324 A CH315324 A CH 315324A CH 315324D A CH315324D A CH 315324DA CH 315324 A CH315324 A CH 315324A
Authority
CH
Switzerland
Prior art keywords
gas turbine
reducing
combustion chamber
adverse effects
combustion
Prior art date
Application number
Other languages
German (de)
Original Assignee
Sulzer 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 Sulzer Ag filed Critical Sulzer Ag
Publication of CH315324A publication Critical patent/CH315324A/en

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
    • 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
    • F02C7/30Preventing corrosion or unwanted deposits in gas-swept spaces

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Solid Fuels And Fuel-Associated Substances (AREA)

Description

  

  Verfahren zum Vermindern störender Wirkungen von Verbrennungsprodukten  der Brennkammer in einer     Gasturbinenanlage       Die Erfindung bezieht sich auf ein Ver  fahren zum Vermindern störender     MTirkungen     von     Verbrennllngsprodulrten    der     Brennkam-          mer    in einer     Gasturbinenanlage    mittels eines  Zusatzstoffes,     weleher        Aluminium    und Sili  zium enthält.  



  Zum Vermindern dieser störenden Wir  kungen, welche insbesondere durch erhöhte       Korrosion    und Ablagerungen entstehen, und  die z. B. auf     Vanadiumverbindungen    und  auch auf Alkali- und.     Erdalkalisulfat.e        zurück-          gefiihrt    werden können, hat man schon ver  schiedene Zusätze     zum        Brennstoff,    zur  Flamme oder     zu    den Verbrennungsprodukten       vorgesehla;

  gen,        darunter        auchZusatzstoffe,die,     wie     erwähnt,        Aluminium    und Silizium ent  halten.  



  Die Erfindung besteht darin, dass     als        Zu-          satzstoff    ein     soleber    gewählt wird,     weleher    ne  ben Kaolin     aueh        metallisches    Aluminium ent  <U>hält.</U>    Dieser erfindungsgemässe     Zusatzstoff    er  weist sich     als        wesentlich    wirksamer als andere  Aluminium und Silizium enthaltende Zusatz  stoffe.  



  Es empfiehlt sich, darauf zu achten, dass  das metallische     Ahuninium        oxydarm    ist, da       sehon    ein etwa 1      /o        ALOg        übersteigender          Oxydgehalt    die     Wirksamkeit    zu     vermindern     vermag.  



  Für das     Misehltngsverhältnis    zwischen  Kaolin und     metallischem        Ahiminiiun    (z. B.       Aluminiumpulver)    kann die Grössenordnung  von     7.0-1.00        Gewichtsteilen    zu einem gewählt  werden.



  Method for reducing disruptive effects of combustion products of the combustion chamber in a gas turbine system The invention relates to a method for reducing disruptive effects of combustion products in the combustion chamber in a gas turbine system by means of an additive which contains aluminum and silicon.



  To reduce these disruptive effects, which arise in particular from increased corrosion and deposits, and the z. B. on vanadium compounds and also on alkali and. Alkaline earth sulfate can be recycled, various additives to the fuel, to the flame or to the combustion products have already been provided;

  genes, including additives which, as mentioned, contain aluminum and silicon.



  The invention consists in that the additive selected is a liver which, in addition to kaolin, also contains metallic aluminum. This additive according to the invention is found to be significantly more effective than other additives containing aluminum and silicon.



  It is advisable to ensure that the metallic ammonium is low in oxide, since an oxide content exceeding about 1 / o ALOg can reduce the effectiveness.



  The order of magnitude of 7.0-1.00 parts by weight to one can be selected for the mixing ratio between kaolin and metallic Ahiminiiun (e.g. aluminum powder).

 

Claims (1)

PATENTANSPRUCH Verfahren zum Vermindern störender Wir kungen. von Verbrennungsprodukten der Brennkammer in einer Gasturbinenanlage mittels eines Zusatzstoffes, welcher Alumi nium und Silizium enthält, dadurch gekenn zeichnet, da.ss der Zusatzstoff neben Kaolin auch metallisches Aluminium enthält. PATENT CLAIM Method for reducing disruptive effects. of combustion products of the combustion chamber in a gas turbine system by means of an additive which contains aluminum and silicon, characterized in that the additive contains metallic aluminum in addition to kaolin.
CH315324D 1953-06-18 1953-06-18 Method for reducing the adverse effects of combustion products of the combustion chamber in a gas turbine plant CH315324A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH315324T 1953-06-18

Publications (1)

Publication Number Publication Date
CH315324A true CH315324A (en) 1956-08-15

Family

ID=4495944

Family Applications (1)

Application Number Title Priority Date Filing Date
CH315324D CH315324A (en) 1953-06-18 1953-06-18 Method for reducing the adverse effects of combustion products of the combustion chamber in a gas turbine plant

Country Status (1)

Country Link
CH (1) CH315324A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2993336A (en) * 1957-09-06 1961-07-25 British Petroleum Co Operation of gas turbine engines and fuel compositions for use in said engines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2993336A (en) * 1957-09-06 1961-07-25 British Petroleum Co Operation of gas turbine engines and fuel compositions for use in said engines
DE1157031B (en) * 1957-09-06 1963-11-07 British Petroleum Co Process for the production of a fuel mixture for gas turbines

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