The invention relates to an exhaust
resonance tube of a two-
stroke horizontally-opposed four-cylinder
piston engine, which belongs to the field of two-
stroke engines and comprises an
exhaust manifold, a connecting component, an
exhaust manifold and a tension spring component. One end of the
exhaust manifold is provided with four
branch air channels, and the other end of the exhaust manifold is a main
air channel where the
branch air channels converge. The four
branch air passages are correspondingly connected with four exhaust ports of an engine respectively, and an air outlet of the exhaust manifold main air passage is in elastic airtight connection with an air inlet of the exhaust manifold through a connecting
assembly. The exhaust manifold is a return reducing
pipe, sequentially comprises a thin
pipe section, a first diverging
pipe section, a second diverging pipe section, an expansion pipe section, a rear taper pipe section and an exhaust
tail pipe section and is used for adjusting contraction and expansion of exhaust
waves in the exhaust manifold, and the phenomenon of
back pressure is avoided. The tension spring
assembly is used for vibration decoupling between the exhaust
resonance tube and the engine. The two-
stroke horizontally-opposed four-cylinder
piston engine solves the problems that an existing two-stroke horizontally-opposed four-cylinder
piston engine for the unmanned aerial vehicle has short-circuit loss, and the power is obviously reduced within a certain rotating speed range.