Atomizing dual fuel nozzle for a combustion turbine

Details Atomizing dual fuel nozzle for a combustion turbine Atomizing dual fuel nozzle for a combustion turbine

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/36 (2006.01) F23D 11/10 (2006.01) F23D 17/00 (2006.01)

Patent

CA 2278481

The dual fuel nozzle assembly (70) comprises a swirl cap (82) that is adapted to securely mount with an independent atomizing cylinder (74). A nozzle tip (78) that is adapted to removably mount with a liquid fuel pipe (76) is provided. The independent liquid fuel pipe and nozzle tip are removably positioned within the receptacle of the independent atomizing air cylinder. An atomizing airflow passage (84) is defined between the air cylinder wall and the outer surface (106) of the liquid fuel pipe such that the airflow passage is in fluid communication with the atomizing air supply channel (86) defined by the liquid fuel pipe flange portion (108).

L'ensemble ajutage (70) bicombustible comprend une coupelle (82) de turbulences pouvant être montée solidement sur un cylindre de pulvérisation indépendant (74). On a prévu une pointe (78) de buse adaptée pour être montée amovible sur un conduit (76) de combustible liquide. Le conduit de combustible liquide et la pointe de l'ajutage indépendant sont positionnés de manière amovible à l'intérieur de l'espace d'un cylindre à air de pulvérisation indépendant. Un passage (84) d'écoulement d'air de pulvérisation est défini entre la paroi du cylindre à air et la surface extérieure (106) du conduit de combustible liquide, de manière que le passage d'écoulement d'air soit en communication fluide avec le canal (86) d'alimentation en air de pulvérisation défini par la partie (108) de bord du conduit de combustible liquide.

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