发明名称 AIRFRAME STABILIZATION MECHANISM FOR VERTICAL TAKEOFF AND LANDING TRANSPORT PLANE
摘要 <p>[Problem] When parts such as an elevator located at the back of a horizontal tail and a flaperon located on a main wing which provide lift to an airframe cannot easily generate lift during a low-speed flight, conventional vertical takeoff and landing transport planes are in danger of crashing if the center of gravity of the airframe shifts forward by the vertical takeoff and landing transport planes catching a tailwind or the like, the falling direction of the airframe and the direction of traveling using a propeller become a direction toward the ground, and the distance from the ground becomes such a short distance that the airframe cannot be put back in place. [Solution] This vertical takeoff and landing transport plane is characterized in that a structure formed in the top-bottom direction of an airframe penetrates a rear structure of the vertical takeoff and landing transport plane in order to let a tailwind escape, and characterized by comprising, in the rear structure of the vertical takeoff and landing transport plane, a device for generating thrust rearward behind the rear on the top side of the airframe from the bottom of the airframe.</p>
申请公布号 WO2014010634(A1) 申请公布日期 2014.01.16
申请号 WO2013JP68893 申请日期 2013.07.10
申请人 FUJIMOTO HIROMICHI 发明人 FUJIMOTO HIROMICHI
分类号 B64C27/28 主分类号 B64C27/28
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