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Aircraft has wings which can vary in their angle and so all height maneuvers can be carried out without direct involvement of fuselage which is kept passive or horizontal

机译:飞机的机翼可以改变角度,因此可以在不直接参与保持被动或水平的机身的情况下执行所有高度操作

摘要

The aircraft has wings which can vary in their angle and so all height maneuvers can be carried out without the direct involvement of the fuselage, which is kept passive or horizontal. The aircraft comprises wings (1,2), fuselage (3), rudders (4,5), ramps (6,7), tilt rods (8,9) and tilt mechanisms (10,11). The direct involvement of the wings exists in the movement for the angle modification in relation to the longitudinal axis (A). By this modification the lift force can be greater than, equal to, or less than the gravity force.
机译:飞机的机翼可以改变角度,因此可以在不直接参与机身的情况下进行所有高度机动,机身保持被动或水平。该飞机包括机翼(1,2,3),机身(3),方向舵(4,5),坡道(6,7),倾斜杆(8,9)和倾斜机构(10,11)。机翼直接参与了相对于纵轴(A)进行角度修改的运动。通过这种修改,提升力可以大于,等于或小于重力。

著录项

  • 公开/公告号DE102006017135A1

    专利类型

  • 公开/公告日2007-10-25

    原文格式PDF

  • 申请/专利权人 SZANTO STEFAN;

    申请/专利号DE20061017135

  • 发明设计人 SZANTO STEFAN;

    申请日2006-04-12

  • 分类号B64C3/38;

  • 国家 DE

  • 入库时间 2022-08-21 20:29:17

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