| 摘要 |
The present invention relates to a fuel nozzle for a combustor, which is arranged in a compressed air path formed between a body part of a gas turbine combustor and a housing. The fuel nozzle for the combustor comprises: a nozzle body which has a supply path to supply fuel, and coupled to the housing to be rotated; and a fuel supply rod which has an injection hole connected to the supply path, and extended to an outer side of the nozzle body to rotate the nozzle body to the housing using power to inject fuel through the injection hole. As such, the present invention promotes mixing of compressed air and fuel. |
