| 主权项 |
1. A vertical takeoff and landing transport plane, comprising: a line passing through a front-back direction of an aircraft being a front-back direction line of an aircraft, a line being perpendicular to the front-back direction line of an aircraft and passing through a left-right direction of a main wing being a left-right direction line of an aircraft, and a line in a direction perpendicular to the front-back direction line of an aircraft and the left-right direction line of an aircraft being a top-bottom direction line of an aircraft, where the vertical takeoff and landing transport plane
has a door for entrance and exit near a rear part of a fuselage of an airframe of an aircraft, through which goods are loaded and unloaded and a passenger is allowed to board and descend, is structured to have a distance from a connection part between the door and the airframe to near a horizontal tail of an airframe, is capable of performing a forward movement while a propeller and an engine are faced obliquely upward relative to the airframe, performing an operation in a vertical takeoff and landing mode when the engine is faced upward, and flying in a fixed wing mode in which the propeller is faced forward when the engine is faced forward, wherein a rear structure of the vertical takeoff and landing transport plane is characterized by being configured by: in a region in an airframe rear part from an area near the door for entrance and exit of an airframe to an area near an elevator at a rear part of a horizontal tail, a through-hole structure of the airframe rear part, having a hole penetrating from an airframe bottom surface to an airframe top surface; a thrust generation device having a rotary moving blade for exhausting air in a direction from a lower side to an upper side of an airframe and having a size allowing a part or all of the device to be inserted in said through-hole structure of the airframe rear part; and an actuator mechanism: where the actuator mechanism has a size allowing a part or all of the actuator mechanism to be housed in said through-hole in the airframe rear part; where a rotation shaft mechanism having a rotation shaft in parallel or approximately parallel to the left-right direction line of an aircraft is configured both in an area near said through-hole structure of the airframe rear part and said thrust generation device; and where one end is linked to the rotation shaft mechanism in an area near said through-hole structure of the airframe rear part and the other end is linked to the rotation shaft mechanism of said thrust generation device. |
