(19)
(11) EP 1 975 513 A3

(12) EUROPEAN PATENT APPLICATION

(88) Date of publication A3:
20.05.2015 Bulletin 2015/21

(43) Date of publication A2:
01.10.2008 Bulletin 2008/40

(21) Application number: 08152724.4

(22) Date of filing: 13.03.2008
(51) International Patent Classification (IPC): 
F23R 3/28(2006.01)
(84) Designated Contracting States:
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR
Designated Extension States:
AL BA MK RS

(30) Priority: 14.03.2007 IT TO20070193

(71) Applicant: Ansaldo Energia S.p.A.
Genova (IT)

(72) Inventors:
  • Mori, Giulio
    17100 Savona (IT)
  • Anisimov, Vyacheslav V.
    16161 Genova (IT)
  • De Oliveira Silva Parente, Joao Miguel
    2795-136 Linda-a-Velha, Oeiras (PT)

(74) Representative: Bergadano, Mirko et al
Studio Torta S.p.A. Via Viotti, 9
10121 Torino
10121 Torino (IT)

   


(54) A premix burner for a gas turbine, in particular a microturbine


(57) A gas turbine premix burner (1) is provided with a main annular duct (7) and a secondary annular duct (24), which are concentric with respect to a longitudinal axis (3) and have respective inlets (8, 25) for combustion air and respective axial outlets (9, 26), which give out, in use, into a combustion chamber (2); the main annular duct (7) has an initial portion (10) housing a blading (12) generating vortices and houses a plurality of pipes (39) for feeding combustible gas into the main annular duct (7); said pipes (39) are arranged about the longitudinal axis (3) and downstream of the blading (12) and each have at least one outlet hole (41), which has a radial component with respect to the axis (40) of the pipe (39).





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