AIRCRAFT WITH REAR MOUNTED ENGINES

• Main Author: MARTINEZ MUNOZ JOSE LUIS
• Format: Patent
• Language: Chinese; English
• Published: 21.08.2018
• Subjects: AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; COSMONAUTICS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING

Aircraft (1, 1 ') with rear mounted engines (2, 2'), comprises a vertical tail plane (3) and a horizontal tail plane (4), in which the engines (2, 2') are mounted on top of the horizontal tail plane (4), such that the horizontal tail plane (4) comprises an inner fixed part (5) attached to the fuselage (8) of the aircraft (1, 1 '), the inner fixed part (5) comprising an elevator (7), and two outermovable parts (6), each one of the outer movable parts (6) being located at each side end of the horizontal tail plane (4) which is furthest away from the fuselage (8) of the aircraft (1, 1 '), such that both the inner fixed part (5) and the outer movable parts (6) are at least partially subjected to the flow coming from the engines (2, 2') when they are in use. 种具有后置发动机(2，2')的飞行器(1，1')，飞行器(1，1')包括竖向尾翼平面(3)和水平尾翼平面(4)，其中，发动机(2，2')安装在水平尾翼平面(4)的顶部上，使得水平尾翼平面(4)包括内部固定部件(5)和两个外部可动部件(6)，内部固定部件(5)附接至飞行器(1，1')的机身(8)，内部固定部件(5)包括升降舵(7)，外部可动部件(6)中的每个外部可动部件位于水平尾翼平面(4)的距离飞行器(1，1')的机身(8)最远的每个侧端部处，使得内部固定部件(5)和外部可动部件(6)在它们使用时均至少部分地经受来