首页> 外国专利> TAKEOFF-AND-LANDING COMPLEX FOR GROUND-EFFECT CRAFT AND METHOD OF PERFORMING TAKEOFF AND LANDING OF SUCH CRAFT

TAKEOFF-AND-LANDING COMPLEX FOR GROUND-EFFECT CRAFT AND METHOD OF PERFORMING TAKEOFF AND LANDING OF SUCH CRAFT

机译:地效工艺的起降复杂装置和执行这种工艺的起降方法

摘要

FIELD: building ground-effect craft and takeoff-and-landing complexes for such craft with the use of static air cushion.;SUBSTANCE: proposed complex includes pusher-type propeller for horizontal thrust which embraces tail section of fuselage. Screw propeller of ground-effect craft is embraced by ring-shaped fairwater and is provided with engine mounted in tail section of fuselage. Ground-effect craft is provided with hermetic center-wing section and hermetic longitudinal beams mounted on peripheral ends of center-wing section. Inflatable shock-absorbing balloons are mounted in lower portion of longitudinal beams. Complex is also provided with units for forming static air cushion under center-wing section. Method of takeoff and landing of ground-effect craft consists in maintenance of excessive pressure in shock-absorbing balloons under longitudinal beams on sides of center-wing section; front and rear retractable guides of air cushion are placed in working position; swivel door is shifted from air duct shutoff position to position at angle relative to upper surface of center-wing section corresponding to 10-15% of air offtake flow created by air propeller at takeoff and landing modes, thus forming air intake for this part of air flow; part of air flow is transported to space for forming air cushion under front part of center-wing section behind front flexible guard and creating excessive static pressure of air.;EFFECT: improved flight and technical characteristics of ground-effect craft.;8 cl, 9 dwg
机译:领域:用静态气垫建造地效飞行器以及该飞行器的起降综合体。物质:拟建的综合体包括水平推力的推进器式螺旋桨,其包围机身尾部。地面效应飞机的螺旋桨被环形的淡水包围,并在机身尾部装有发动机。地效飞行器具有密封的中央翼部分和安装在中央翼部分的外围端的密封纵梁。充气减震气球安装在纵梁的下部。综合大楼还设有在中央翼部分下方形成静态气垫的装置。地效飞行器的起降方法是在中翼部分侧面的纵梁下保持减震气球的过大压力。气垫的前后伸缩导轨位于工作位置;旋转门从风道关闭位置移至相对于中央机翼部分上表面成一定角度的位置,该角度对应于起飞和降落模式下空气螺旋桨产生的空气流量的10-15%,因此形成了该部分进气口空气流动;一部分气流被输送到空间,该空间在前柔性护板后面的中央翼部分的前部下方形成气垫,并产生过多的空气静压。效果:改进了地面效应飞行器的飞行和技术特性; 8厘升, 9天

著录项

  • 公开/公告号RU2254251C2

    专利类型

  • 公开/公告日2005-06-20

    原文格式PDF

  • 申请/专利权人

    申请/专利号RU20020119276

  • 发明设计人 MARTIROSOV R.G.;

    申请日2002-07-22

  • 分类号B60V1/08;

  • 国家 RU

  • 入库时间 2022-08-21 22:02:03

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