One way to significantly improve the efficiency of work combustion processes in stabilizer type burners is to use various means of intensifying of heat transfer and fuel burn. Such means include as follows: preheating the air, going to the combustion, air flow twisting, organization of developed surface ignition and combustion, increasing shading coefficient burner, use of additional elements of tubulisation etc. The existing papers devoted to the study of transport processes in the application of these ways of combustion intensification in stabilizer burners do not cover many aspects of this direction of research. Thus, the further development of research of flow characteristics, which largely determine the course of work processes in burners, deserves attention. Therefore our objective is to define patterns of flow in the system of angular turbulence stimulator-niche cavity modelling the main elements of the stabilizer type burner. Studies are conducted on the operation area at the following initial data: the height of the channel was operation area of 120 mm, width – 190 mm, length – 500 mm. Length niches downstream 75 mm, height – 35 mm. To measure the flow velocity of T-shaped pneumatic probe, using cement nozzle Witoszynskyj was used. First of all, comparison of velocity profiles in various vertical sections of niche cavities in the plane of symmetry of turbulence stimulator for the present and absent of availability of turbulence stimulator of flow indicates that without of turbulence stimulator reverse flows zone is significantly pressed to the niche bottom. That is if turbulence stimulators are installed behind niche cavity reverse flows zone is visible pressed against the bottom of the niche. Secondly, there is a tendency to the emergence of forward flow near the wall stabilizer in the area of the location of the turbulence stimulator. There is a direct-flow trend outside return flows zone of turbulence stimulator, accelerated down the stream as you approach to the section x = 120 mm, which corresponds to the maximum width of said zone. Further down the stream-flow this trend is slowed. The return flows zone behind the turbulence stimulator appears more clearly on some distance from the wall of the turbulence stimulator. This fact becomes evident due to effect of the emergence of forward flow in the wall area of the stabilizer. Thus, the analysis of experimental data on flow patterns in the system of corner vortex flow is niche cavity. Setting of angle vortex flow on a section of the back wall of the niche leads to inhibition of specific areas of backward flows in the niche cavity and pressed it to the bottom of the niche.