Support of fuel nozzle of gas turbine

The utility model relates to the technical field of gas turbine overhaul, and discloses a gas turbine fuel nozzle support which is characterized by comprising a main body rectangular frame which comprises two parallel transverse frame plates and two parallel longitudinal frame plates. The two ends of the transverse frame plate are perpendicularly and fixedly connected with one ends of the two longitudinal frame plates correspondingly, and a plurality of supporting foot rods are arranged at the bottom of the main body rectangular frame. A plurality of support partition plates are evenly and fixedly connected between the two transverse frame plates, main nozzle supporting spaces are formed between every two adjacent support partition plates and between the adjacent support partition plates and the longitudinal frame plates, and bolt holes are formed in the positions, corresponding to the middles of the main nozzle supporting spaces, of the transverse frame plates in a penetrating mode. Corresponding detachable