基于气液双相燃料的火焰稳定器和燃烧室
By using a flame stabilizer with gas-liquid dual-phase fuel, an aerodynamic barrier is formed by the gas and liquid phase fuels, which solves the performance impact problem caused by high-pressure air extraction in the prior art and achieves high-efficiency combustion and low-loss combustion chamber performance.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- TSINGHUA UNIVERSITY
- Filing Date
- 2024-06-20
- Publication Date
- 2026-07-17
AI Technical Summary
Existing jet flame stabilizers require drawing high-pressure air from behind the engine compressor to form an aerodynamic barrier, which reduces the amount of air entering the combustion chamber for heating and turbine work, affecting the overall performance of the engine in afterburner mode.
The flame stabilizer uses gas-liquid dual-phase fuel. Gas and liquid phase fuels are sprayed out through gas jet nozzles and liquid jet nozzles. The liquid phase fuel is atomized under the kinetic energy of the high-speed gas phase fuel and forms an arched aerodynamic barrier, which stabilizes the flame and entrains high-temperature combustion gas, avoiding the introduction of high-pressure air to form a barrier.
It improves combustion efficiency, reduces flow losses in the combustion chamber, ensures the performance of the engine under afterburner conditions, and eliminates the need for large-area blunt body structures, thus reducing mechanical structure and weight.
Smart Images
Figure CN118669822B_ABST