Procedure for assembling a fuel injector for a turbine...

F - Mech Eng,Light,Heat,Weapons – 23 – R

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F23R 3/28 (2006.01) F23D 11/36 (2006.01)

Patent

CA 2363305

Assembly process in which first occurs the filling with additive metal of radial wells (159, 175) drilled in an annular injection part (152) comprising first injection orifices (188) for discharging a primary fuel and in a cylindrical end piece (158) covering the annular injection part and comprising second injection orifices (190) for discharging a secondary fuel; then the annular injection part is assembled in the cylindrical end piece and these parts are in turn assembled on a first tube (170) for feeding primary fuel and a second tube (176) for feeding secondary fuel, covering the first tube, and on an external wall of the injector (160); and last, the terminal part of the injector (14, 16) thus assembled is placed in a closed space where it will be heated to allow the additive metal to fuse with these parts.

Procédé d'assemblage dans lequel tout d'abord il est procédé à un remplissage par un métal d'apport de puits radiaux (159, 175) percés dans une pièce annulaire d'injection (152) comportant des premiers orifices d'injection (188) pour décharger un combustible primaire et dans un embout cylindrique (158) entourant la pièce annulaire d'injection et comportant des seconds orifices d'injection (190) pour décharger un combustible secondaire; puis la pièce annulaire d'injection est montée dans l'embout cylindrique et ces pièces sont à leur tour montées sur un premier tube (170) d'alimentation en combustible primaire et un second tube (176) d'alimentation en combustible secondaire, entourant le premier tube, et sur une paroi externe de l'injecteur (160); et enfin la partie terminale de l'injecteur (14, 16) ainsi assemblée est placée dans une enceinte où elle sera chauffée pour permettre une fusion du métal d'apport avec ces pièces.

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