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CELESTIAL TRACKING APPARATUS AND METHOD OF CONTROLLING WIND STOW THEREFOR

机译:尾迹跟踪装置和控制风积的方法

摘要

A celestial tracking apparatus (20) has a support (26), a tracking assembly (28) coupled to the support (26) by an azimuth pivot (36), a collector assembly (30) coupled to the tracking assembly (28) by an elevation pivot (38), a wind-speed sensor (172), and a controller (150) coupled to the azimuth and elevation pivots (36,38) and configured to cause the collector assembly (30) to assume a wind-stow position (66) when the sensor (172) detects a wind having a speed greater than a predetermined speed, upon failure of a component of the apparatus (20), or upon receipt of a wind-stow command. The collector assembly (30) has a solar collector (22) with a substantially flat surface (24), a center of gravity (52), and a target axis (54) substantially perpendicular to the substantially flat surface (24) and passing through the center of gravity (52). The elevation pivot (38) is displaced from the target axis (54) and the center of gravity (52) so that the collector assembly (30) is predisposed to pivot to the wind-stow position.
机译:天体跟踪设备(20)具有一个支架(26),一个通过方位角枢轴(36)耦合到支架(26)的跟踪组件(28),通过一个耦合到跟踪组件(28)的收集器组件(30)。仰角枢轴(38),风速传感器(172)和控制器(150),其耦合到方位角和仰角枢轴(36,38),并配置为使收集器组件(30)处于风积当传感器(172)检测到风速大于预定速度时,在设备(20)的组件发生故障时或在接收到风积命令时,将其置于位置(66)。收集器组件(30)具有太阳能收集器(22),该太阳能收集器(22)具有基本平坦的表面(24),重心(52)和基本垂直于基本平坦的表面(24)并穿过的目标轴线(54)。重心(52)。抬升枢轴(38)偏离目标轴(54)和重心(52),因此,收集器组件(30)倾向于枢转至风收藏位置。

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