公开(公告)号：US20160167780A1

公开(公告)日：2016-06-16

申请号：US14908850

申请日：2014-08-07

Applicant: UNIT 1SRL

Inventor： Pietro GIOVENGA

IPC: B64C29/00 ,  B64C39/02 ,  B64C3/54

CPC classification number: B64C29/0033 ,  B64C3/385 ,  B64C3/54 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/162 ,  B64D27/08 ,  Y02T50/14

Abstract: A convertiplane has the ability to take off like a helicopter and then fly horizontally like a conventional aircraft. The aircraft includes a variable incidence front wing of variable span located below the fuselage and mounted on a structure in the form of a venturi tube, a rear wing having two propellers for controlling the stability of the vehicle in pitch and roll installed therein, two counter-rotating, pivotally mounted ducted propellers equipped with four flaps orthogonal to each other provided on the sides of the cockpit, engines placed behind the cockpit close to the center of gravity, a static balancing system for controlling the center of gravity of the aircraft consisting of a weight placed in the lower part of the fuselage, self-propelled on the track rack longitudinally to the fuselage, and a digital flight control system.

Abstract translation: 转换飞机具有像直升机一样起飞的能力，然后像常规飞机一样水平飞行。 飞机包括位于机身下方的可变跨度的可变入射前翼，并安装在文丘里管形式的结构上，后翼具有两个螺旋桨，用于控制安装在其中的俯仰和滚动中的车辆的稳定性，两个计数器 旋转的，枢转安装的管道螺旋桨，其配备有四个彼此正交的翼片，设置在驾驶舱的两侧，放置在靠近重心的驾驶舱后面的发动机，用于控制飞行器重心的静态平衡系统， 放置在机身下部的重量，纵向自动推进到机身，以及数字飞行控制系统。