FUEL ATOMISER Russian patent published in 2014 - IPC F23D14/58 F23D14/22 

Abstract RU 2506497 C2

FIELD: heating.

SUBSTANCE: invention relates to a fuel atomiser. Fuel atomiser is intended mainly for coaxial fuel spray into air flow (8), which annularly envelopes the fuel atomiser; it includes pipe (2) with outlet opening (10); besides, pipe (2) is connected to fuel supply main line for fuel supply to pipe (2). Fuel is sprayed from outlet opening (10) to air flow (8), and the first section (4) of the pipe, which reaches its outlet opening (10), is made in the form of petals (6); core (14) of petals, which is closed and has a conical shape, is located in outlet opening (10). Core (14) of petals is pointed in the stream direction. Core (14) of petals is made in the form of a double cone. Core (14) of petals includes notches (16) that are straight in the stream direction and/or curved. The first pipe section (4) converges in the stream direction. Core (14) of petals is connected to supply pipe (30) of high-calorific fuel, which passes coaxially to atomiser pipe (2), and has at least one tangential (16) and/or axial (17) inlet opening. At least one tangential inlet opening (16) is located on connection strap (19) of petals between two petals (18) of outlet opening (10).

EFFECT: invention allows reducing formation of nitrogen oxides.

10 cl, 8 dwg

Similar patents RU2506497C2

Title Year Author Number
COMBUSTION CHAMBER UNITS FOR, IN PARTICULARLY, GAS TURBINE 2013
  • Paskualotto Ehnnio
  • Shissel' Pirmin
  • Khellat Jaan
RU2573090C2
MULTICON-TYPE PREMIXING BURNER FOR GAS TURBINE 2013
  • Paskualotto Ehnnio
  • Knepfel' Khanspeter
RU2551706C2
BURNER 2013
  • Bernero Stefano
  • Paskualotto Ehnnio
  • Frajtag Ehval'D
RU2560087C2
BURNER OF MULTI-CONE TYPE FOR PRE-MIXING FOR GAS TURBINE 2013
  • Paskualotto Ehnnio
  • Zhenehn Franklin Mari
  • Khellat Jaan
RU2561767C2
ASSEMBLY OF BURNERS WITH ULTRALOW NOx EMISSION 2007
  • Tsao Tszin'
  • Dzhoshi Makhendra Ladkharam
  • Slavezhkov Aleksandar Dzhordzhi
RU2426030C2
SYSTEM OF FUEL SPRAY TO COMBUSTION CHAMBER OF GAS TURBINE ENGINE; COMBUSTION CHAMBER EQUIPPED WITH SUCH SYSTEM, AND GAS TURBINE ENGINE 2008
  • Sandeli Deni
  • Dezol'Ti Mishel'
  • Boduehn Kristof
RU2468297C2
NO LOW-EJECTION BURNER WITH PERFORATED PLATE-TYPE FLAME HEAD 2019
  • Lee, Jong-Tae
  • Park, Jae-Un
RU2743686C1
POWER PLANT GAS TURBINE COMBUSTION CHAMBER 1995
  • Andrjukov N.A.
  • Baranov V.A.
  • Kirievskij Ju.E.
  • Maksin V.I.
  • Serov A.V.
  • Khajrullin M.F.
RU2098719C1
GAS TURBINE ENGINE COMBUSTION CHAMBER ASSEMBLY WITH A STRUCTURAL ELEMENT THAT PROVIDES A CAPTURED VORTEX 2018
  • Bulat, Ghenadie
RU2748110C1
PRE-MIXED FUEL INJECTOR (ALTERNATIVES) AND FUEL COMBUSTION PROCESS (ALTERNATIVES) 1998
  • Snajder Timoti S.
  • Sova Uil'Jam A.
  • Morford Stefen A.
  • Van Dajk Kevin Dzh.
RU2215243C2

RU 2 506 497 C2

Authors

Kol'Men'Ja Dzhakomo

Verts Ul'Rikh

Van Kampen Jap

Dates

2014-02-10Published

2009-09-25Filed