首页> 外国专利> LAUNCH AND RETRIEVAL ARRANGEMENT FOR AN AERODYNAMIC PROFILE ELEMENT AND AN AERODYNAMIC PROFILE ELEMENT

LAUNCH AND RETRIEVAL ARRANGEMENT FOR AN AERODYNAMIC PROFILE ELEMENT AND AN AERODYNAMIC PROFILE ELEMENT

机译:气动外形元件和气动外形元件的发射和回收布置

摘要

The invention concerns an aerodynamic profile element for energy production by means of traction force, in particular for driving watercraft, including an upper flexible layer which extends in a transverse direction and a longitudinal direction, a lower flexible layer which extends parallel to the upper layer and which is connected to the upper layer by means of a plurality of webs extending in the depthwise direction of the profile element, an air-filled internal space between the upper and lower layers, at least one air intake opening for supplying air to the internal space, said opening being arranged between two mutually parallel leading edges of the upper and lower layers, a plurality of pulling lines which are fixed with a first end to spaced locations on the profile element and which are connected with a second end to a pulling cable for connecting the profile element to a watercraft, and a plurality of reefing lines which are fixed at a first end to the layers and/or webs and which are adapted to reduce or increase the size of the profile element by reefing or unreefing the upper and lower layers, which is developed by a bar element extending in the longitudinal direction of the profile element to stabilise the aerodynamic profile, wherein the bar element is fixed to the upper and/or lower layer and/or to a web and at the bar element at least one of the reefing lines experiences a change in direction from a reefing line portion which extends in the transverse direction of the profile element of the upper or lower layer respectively from the fixing point at the first end, into a reefing line portion which extends in the longitudinal direction.
机译:用于通过牵引力产生能量的空气动力学轮廓元件,特别是用于驱动船只的空气动力学轮廓元件,其包括在横向和纵向方向上延伸的上柔性层,平行于上层延伸的下柔性层和通过在轮廓元件的深度方向上延伸的多个腹板连接到上层,在上层和下层之间充有空气的内部空间,至少一个用于向内部空间供应空气的进气口所述开口布置在上层和下层的两个相互平行的前边缘之间,多条拉线以第一端固定在型材上的间隔位置,并以第二端连接到拉索,用于将轮廓元件连接至船只,以及多条收帆线,所述收帆线的第一端固定至层和/或腹板s和适于通过对上层和下层进行加料或脱料来减小或增加型材元件的尺寸,其由在型材元件的纵向方向上延伸以稳定空气动力学型材的条形元件形成,其中元件被固定到上层和/或下层和/或纤维网上,并且在条形元件上,至少一条收帆线经历了从收帆线部分的方向改变,该收帆线部分沿型材的横向方向延伸。上层或下层分别从第一端的固定点进入沿纵向延伸的收帆线部分。

著录项

  • 公开/公告号IN2009CN01430A

    专利类型

  • 公开/公告日2016-08-31

    原文格式PDF

  • 申请/专利权人

    申请/专利号IN1430/CHENP/2009

  • 发明设计人 WRAGE STEPHAN;BRABECK STEPHAN;

    申请日2009-03-12

  • 分类号B63H9/06;B63B15/00;B63B35/79;B64C31/06;B63B15/02;B63H9/04;

  • 国家 IN

  • 入库时间 2022-08-21 14:25:55

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