Abstract: Disclosed is a fuel mixed injection method for a gas turbine. The method includes the following steps: arranging a secondary fuel injection nozzle and a secondary air injection nozzle on a secondary combustion section, wherein the secondary fuel injection nozzles is closer to a main combustion section than the secondary air injection nozzle; and injecting secondary fuel and secondary primary air in sequence through the secondary fuel injection nozzle and the secondary air injection nozzle, respectively, thus enabling the secondary fuel to spontaneously combust in a mainstream high-temperature flue gas atmosphere to form a transverse jet flame and increase the flame lift-off height.

Abstract: A synchronous measurement system for a velocity and a temperature of an engine plume flow field is provided. The system includes multiple mid infrared lasers, a signal generator, two optical fiber amplifiers, two groups of optical fiber couplers, a photoelectric detector, a data acquisition device, and a host. The four mid infrared lasers are divided into two groups, one group is configured to emit two beams of first mid infrared lasers, and the other group to emit two beams of second mid infrared lasers. Each group of optical fiber couplers is arranged at an outlet of an engine through a mounting frame which are perpendicular to each other. The data acquisition device acquires photoelectric signals and processes them into corresponding spectral data. The host processes the spectral data to obtain the velocity and the temperature of the engine plume flow field.

Abstract: Disclosed is a fuel mixed injection method for a gas turbine. The method includes the following steps: arranging a secondary fuel injection nozzle and a secondary air injection nozzle on a secondary combustion section, wherein the secondary fuel injection nozzles is closer to a main combustion section than the secondary air injection nozzle; and injecting secondary fuel and secondary primary air in sequence through the secondary fuel injection nozzle and the secondary air injection nozzle, respectively, thus enabling the secondary fuel to spontaneously combust in a mainstream high-temperature flue gas atmosphere to form a transverse jet flame and increase the flame lift-off height.