The invention discloses a flame stabilizer which can be used for an aero-engine afterburner and the like, comprising a jet device installed in a mainstream channel, wherein the jet device is providedwith injection ports, and the shape of the injection port is in a slot shape; alternatively, the shape of the injection port is a circular hole shape, the plurality of circular hole-shaped injection ports are divided into at least two groups, each group of circular hole-shaped injection ports is distributed perpendicular to the direction of the main flow direction, and the adjacent two groups of circular hole-shaped injection ports are staggered. The flame stabilizer sprays continuous jet at a certain angle in the mainstream through the jet device, and the jet forms an aerodynamic barrier in the mainstream, and then forms a return zone after the aerodynamic barrier. The return zone can effectively stabilize the flame, so the flame stabilizer is also called a jet flame stabilizer. The flamestabilizer has the advantages of high temperature resistance and deformation resistance, high combustion efficiency, low pressure loss, weak infrared radiation, continuous, effective and stable aerodynamic barrier, large return zone, good flame stabilization effect and wide combustion stabilization boundary.