首页> 外国专利> AUXILIARY CONTROL DEVICE FOR FREELY FLYING WIND ENGAGEMENT ELEMENTS HAVING A WING AREA GREATER THAN 20 M2

AUXILIARY CONTROL DEVICE FOR FREELY FLYING WIND ENGAGEMENT ELEMENTS HAVING A WING AREA GREATER THAN 20 M2

机译:翼面积大于20 M 2 的自由飞行风接合元件的辅助控制装置

摘要

In commercial shipping, a new age began with the use of wind force to drive ships by means of controlled, kite-like wind engagement elements. As a result of the connection by means of a pulling rope, the wind engagement element operates at heights, at which conventional sails are unusable, at said heights greater wind speed and wind steadiness prevail. Said technology can also be used in wind power plants having a controllable kite. The present auxiliary control device is characterized by an improvement in regard to the operational reliability, service life, and energy yield of known systems by means of the skillful arrangement of proven components. The problem solutions shown are based on the principle of a central roller for reversing the direction of control lines having two movably fastened ends. Said function, in combination with the block-and-tackle principle, permits a more flexible design of gear reduction ratios. Differentiated control strokes of the wing segments can thereby be realized. The use of control strokes is thus technically independent of the actuating strokes acting on the rear edge of wing segments by means of a mechanical addition of said motions. Accordingly, several different advantages can be achieved, which nevertheless can be simply combined with each other: The reduction according to the invention of the load jumps between the wing segments, which are caused by the conventional gear reduction ratios resulting from the block and tackle, lowers the material load of the wing and reduces the susceptibility to tearing. The use of separate control lines for the rear wing edge enables both an asymmetrical adjustment of the angle of incidence of the segments in order to improve the flight dynamics and a symmetrical adjustment which realizes both the adaptation to the wind speed and a load limiting function. This reduces the risk of damage in the event of gusts of wind and expands the possibility of usage to higher wind strengths. The combination with the control device having a rope store applied for at the same time results in the option of a front profile adjustment in order to optimize the tensile force yields for broad-reach winds or close-to-the-wind courses. Thus, one and the same wing module can cover a large range of use.
机译:在商业运输中,新时代开始于使用风力通过可控的,像风筝一样的风接合元件来驱动船舶。由于借助于拉绳的连接,所述风接合元件在无法使用常规帆的高度处操作,在所述高度处存在较大的风速和风的稳定性。所述技术还可以用于具有可控风筝的风力发电厂中。本发明的辅助控制装置的特征在于,借助于成熟的部件的熟练布置,在已知系统的运行可靠性,使用寿命和能量产出方面有所改进。所示的问题解决方案基于中央滚子的原理,该中央滚子用于反转具有两个可移动固定端的控制线的方向。所述功能与联动装置原理相结合,可实现齿轮减速比的更灵活设计。由此可以实现机翼段的不同的控制行程。因此,控制行程的使用在技术上独立于通过所述运动的机械相加作用在机翼段的后边缘上的致动行程。相应地,可以获得几个不同的优点,但是这些优点可以简单地彼此组合:根据本发明,翼段之间的载荷跳跃的减小是由滑车和滑车产生的常规齿轮减速比引起的,降低机翼的材料负荷并降低易撕裂性。对于后翼边缘使用单独的控制线,既可以对翼片的入射角进行非对称调节以改善飞行动力学,也可以实现对风速的适应和负载限制功能的对称调节。这降低了阵风时损坏的风险,并扩大了使用更高风强度的可能性。与具有同时应用绳索存储装置的控制设备的组合,可以选择调整前轮廓,以便针对大范围风向或接近风向优化拉力屈服。因此,一个和相同的机翼模块可以覆盖很大的使用范围。

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