Caramra combustion Gas Turbine, comprising: unapared Side, to define a volume of a Main Nozzle, combustion;Tibera provided around the pilot; and Means for supplying Air Volume in a laminar combustion downstream of the main nozzle.

摘要

A Gas Turbine combustor includes a side wall to define a volume of combustion, taking Extreme up and down stream, a JET PILOT.Willing adjacent to the upstream end of the side wall, to download a Pilot Flame to form a fuel distribution in the combustion Volume.A Plurality of main Nozzle, Air Nozzle around the pilotTo download a fuel air mixture premixed Flames to form in the combustion Volume.Laminar Air is supplied into the combustion Volume downstream of the main Nozzle, along the Inner surface of the side wall.In order to reduce the Air FUEL RATIO in a region adjacent to the surface of the side wall.And restrict a Vibration driven by combustion in the combustion Volume.