Turbojet engine and aircraft

The invention relates to a turbojet engine and an aircraft. The turbojet engine includes an engine, a fan casing and a nacelle (102) including a fixed structure (206) and a thrust-reversing system having a mobile assembly (207) with a mobile cowl (207a) and a frame (207b), in which the mobile assembly (207) is translationally mobile on the fixed structure (206) between an advanced position and a retracted position to define a window between the secondary jet (208) and the outside of the nacelle (102), inner doors (104) and outer doors (105), a runner (214) translationally mobile between a first position and a second position, in which each door is mounted articulated by a rear edge on the runner (214) between a stowed position and a deployed position, an actuator for ensuring the translational displacement of the runner (214) from the first position to the second position and an actuator for ensuring the displacement of the frame from the advanced position to the retracted position. 本发明涉及一种涡轮喷气发动机及飞行器，该涡轮喷气发动