The invention discloses a
traction system used for traction of an aircraft. The
traction system comprises a rod body, a traction ring, a
hydraulic control system, a traveling mechanism, a front connecting rod I, a front connecting rod II, a
rocker arm I, a rear connecting rod I, a
rocker arm II, a rear connecting rod II, a
pulley and steel
wire rope assembly, an auxiliary wheel I and an auxiliary wheel II, wherein the traction ring is arranged at the front end of the rod body and used for being connected with a traction car; the
hydraulic control system is used for controlling the rod body to ascend and descend; the traveling mechanism is located in the middle of the rod body and arranged under the rod body; the front connecting rod I and the front connecting rod II are located on the two sides of the rod body correspondingly; the
rocker arm I and the rear connecting rod I are matched with the front connecting rod I; the rocker arm II and the rear connecting rod II are matched with the front connecting rod II; the
pulley and steel
wire rope assembly is arranged on the rear middle portion of the rod body; the auxiliary wheel I is arranged on the front connecting rod I; and the auxiliary wheel II is arranged on the front connecting rod II. The function that the aircraft can control steering in the traction process is achieved through the
traction system, and meanwhile the traction
system is simple in structure, low in manufacturing cost, good in buffer performance, convenient to
mount, dismount and convey and capable of being widely applied and popularized.