The utility model relates to the technical field of engine
crankshaft power transmission, in particular to a transmission
assembly of an in-line
piston engine, an engine and an aircraft thereof, which comprise a
crankshaft body, the
crankshaft body comprises a plurality of
crank pins, a plurality of cranks and a plurality of journals which are sequentially arranged in a staggered manner from the front end to the
tail end, a driving gear is arranged at the front end of the crankshaft body and integrally formed with the
crank, the center of the driving gear and a shaft neck of the crankshaft body are arranged on the same central axis, a transmission mechanism is arranged outside the driving gear in an engaged mode, and the transmission mechanism comprises a damping gear
assembly, a transmission gear, an idle gear and an output gear which are sequentially engaged. The integral
layout is optimized, the structure is compact, the simple idle gear is additionally arranged, an original idle gear shaft transmission mechanism is replaced, the basic function of
speed reduction of an engine is achieved, and meanwhile the purposes of
miniaturization, light weight, stability and aircraft carrying performance of the engine are achieved.