The invention provides a low-emission low-rotational-flow
combustion chamber head structure for an airascraft engine. The low-emission low-rotational-flow
combustion chamber head structure comprises a pre-burning level and a main-burning level. The pre-burning level is designed with low
rotational flow, that is the gas flow is divided into two parts through an inner ring of a
cyclone, one part of the flow forms
jet flow with the extremely-low
rotational flow strength through a
current limiting plate of a center channel, and the other part of the flow forms rotational
jet flow with the large
rotational flow strength through an outer-side
cyclone. Pre-burning level fuel is ejected from a centrifugal
nozzle and then enters the
combustion chamber along with pre-burning level
jet flow. A pre-film type air atomizing
nozzle is adopted in the main-burning level for supplying oil, the fuel is sheared and atomized by rotational jet flow, ejected by a pre-burning level external
cyclone, of fuel and rotational gas flow, ejected by a main-burning level cyclone and then enters the
combustion chamber. Due to a low-rotational-flow flow field, the
staying time of
combustion products is reduced, generation of
heating power type
NOx is reduced, and the
combustion chamber can work stably in extremely-poor conditions. Working can be achieved by replacing the
combustion chamber head of the aircraft engine, the requirement for transforming the engine is extremely low, the
pollution emission level in the whole landing-taking off circulation can be reduced, and earnings are obvious.