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RESCUE TRIMARAN-TYPE GROUND-EFFECT CRAFT

机译:救援TRIMARAN型地效工艺品

摘要

FIELD: shipbuilding; designing rescue trimaran-type ground-effect craft.;SUBSTANCE: proposed ground-effect craft includes three fuselages-hulls which are interconnected by means of rectangular wings. Fuselage-hull located in axis of symmetry of ground-effect craft is extended forward. Ground-effect craft has keel and swept stabilizer. Fuselages-hulls are stepped in construction and are provided with several tiers; they are divided lengthwise into compartments. Length of side fuselages-hulls exceeds length of center fuselage-hull by at least twice. One of rectangular wings has passage inside it for connection with side fuselages-hulls. Swept wings at negative dihedral angle (v) are provided on external side of two fuselages-hulls in accordance with position of rectangular wings. End of each wing is secured to mooring rod protected on the outside with streamlined elastic belt. Lower part of said rod performs function of stall fence during flight. Bottoms of each fuselage-hull have recesses where extensible hydrofoils are mounted; area of hydrofoils is variable which is effected by means of remote control system. At the top each fuselage-hull is provided with evacuation and inspection openings covered with acrylic plastic and located at distance relative to one another. Mounted on front upper part of fuselage-hull lying in axis of symmetry of ground-effect craft is aerial rudder; tail parts of two side fuselages-hulls are provided with extensible coaxial propellers and hydrodynamic control surfaces. Mounted on last rear rectangular wing between side fuselages-hulls on streamlined brackets are ramjet engines located at equal distances. Turbo-jet engines are mounted on similar brackets at the same level with ramjet engines.;EFFECT: improved service characteristics of ground-effect craft.;4 cl, 9 dwg
机译:领域:造船;实质:拟议的地效飞行器包括三个机身船体,它们通过矩形机翼相互连接。位于地效飞行器对称轴上的机身外壳向前延伸。地效飞行器具有龙骨和后掠稳定器。机身船体是逐步建造的,并设有多层。它们在长度上分为多个部分。侧面机身的长度超过中央机身的长度至少两倍。矩形机翼之一在其内部具有通道,用于与侧机身壳连接。根据矩形机翼的位置,在两个机身外壳的外侧提供了具有负二面角(v)的后掠机翼。每个机翼的末端都固定在系泊杆上,系泊杆由流线型弹性带保护在外侧。所述杆的下部在飞行期间执行失速防护栏的功能。每个机身的底部都有凹槽,可延伸的水翼安装在凹槽中。水翼的面积是可变的,这是通过远程控制系统来实现的。在每个机身船体的顶部都设有疏散和检查孔,这些孔用丙烯酸塑料覆盖并且彼此隔开一定距离。在地效飞行器对称轴上安装的机身前部上部是空中舵。两侧机身机身的尾部设有可扩展的同轴螺旋桨和流体动力控制面。冲压喷气发动机安装在流线型支架上的侧机身壳之间的最后一个后方矩形机翼上,它们之间的距离相等。涡轮喷气发动机与冲压喷气发动机安装在同一高度的相似支架上;效果:改进了地面效应飞行器的服务特性; 4 cl,9 dwg

著录项

  • 公开/公告号RU2250845C2

    专利类型

  • 公开/公告日2005-04-27

    原文格式PDF

  • 申请/专利权人

    申请/专利号RU20010106850

  • 发明设计人 JANSUFIN N.R.;

    申请日2001-03-13

  • 分类号B60V1/08;

  • 国家 RU

  • 入库时间 2022-08-21 22:02:06

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