Combustion chamber based on plane jet flow flame stabilizer

The invention relates to a combustion chamber based on a plane jet flow flame stabilizer. The combustion chamber comprises a combustion chamber inlet, a plurality of plane jet flow flame stabilizers and an oil gas input device connected with the plane jet flow flame stabilizers. Under the condition that the combustion chamber works, the oil gas input device obtains air and/or fuel and transmits the air and/or fuel to the corresponding plane jet flow flame stabilizer; the plane jet flow flame stabilizer sprays out air and/or fuel to form plane jet flow, the plane jet flow is used for forming a pneumatic barrier under the action of high-speed incoming flow in an inlet of the combustion chamber and forming a backflow area behind the pneumatic barrier, and the total pressure loss of the combustion chamber is reduced. 本申请涉及一种基于平面射流火焰稳定器的燃烧室。该燃烧室包括燃烧室入口、多个平面射流火焰稳定器、与各平面射流火焰稳定器连接的油气输入装置；油气输入装置在燃烧室工作的情况下，获取空气和/或燃料，并将空气和/或燃料传递至对应的平面射流火焰稳定器；平面射流火焰稳定器将空气和/或燃料喷出以形成平面射流，平面射流用于在燃烧室入口中的高速来流的作用下，形成气动屏障以及在气动屏障后方形成回流区，减小了燃烧室的总