.A gas turbine combustor control is possible by using a dual fuel tube containing the sensor and Burner control method using a pressure sensor.

摘要

The present invention relates to a gas turbine capable of controlling the operation of a combustor by using a double fuel tube equipped with a pressure sensor, and more particularly, to a gas turbine capable of controlling combustion of gas The present invention relates to a gas turbine including a double fuel tube equipped with a pressure sensor capable of directly detecting a gas leak and preventing danger, in addition to a leak detection sensor. A gas turbine capable of controlling a combustor using a dual fuel pipe equipped with a pressure sensor according to the present invention can be applied to a gas turbine combustor as a double pipe to directly measure a leakage gas pressure due to pipe breakage or the like , The fuel leakage is directly detected and the combustor of the gas turbine is protected. There is thus the effect of using a conventional gas detector to more accurately and sensitively control the combustor in response to the leaking gas or outflow gas than is the method of detecting leakage gas.