首页> 外国专利> Aircraft with combined aerofoils and control surfaces has annulus on each side of fuselage and formed by aerofoils and control surfaces together with side walls of fuselage, and annulus accommodates propeller

Aircraft with combined aerofoils and control surfaces has annulus on each side of fuselage and formed by aerofoils and control surfaces together with side walls of fuselage, and annulus accommodates propeller

机译:机翼和控制面组合在一起的飞机在机身的每一侧都有环空,由机翼和控制面以及机身的侧壁组成,并且环空容纳螺旋桨

摘要

The aerofoils(2,3) and control surfaces together with the fuselage side walls form an annulus on both sides of the fuselage(1). At least one propeller(9,10) is located in each annulus and positioned between the rear upper section of the aerofoil and forward lower section of the elevator surface(4). Each annulus has additional load bearing surfaces(7,8) for suspension of the propeller shaft and for guiding of the propulsion force transmission or engine suspension.
机译:机翼(2,3)和控制表面与机身侧壁一起在机身(1)的两侧形成环形空间。至少一个螺旋桨(9,10)位于每个环带中,并位于机翼的后上部和升降机表面(4)的下部之间。每个环具有额外的承载表面(7,8),用于悬挂螺旋桨轴并引导推进力传递或发动机悬挂。

著录项

  • 公开/公告号DE19919626A1

    专利类型

  • 公开/公告日2000-11-02

    原文格式PDF

  • 申请/专利权人 FURMANEK ANDREAS;

    申请/专利号DE19991019626

  • 发明设计人 FURMANEK ANDREAS;

    申请日1999-04-29

  • 分类号B64C39/10;B64C3/16;B64D27/26;

  • 国家 DE

  • 入库时间 2022-08-22 01:42:06

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