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    • 6. 发明授权
    • Deployable helical antenna
    • 可部署螺旋天线
    • US5721558A
    • 1998-02-24
    • US642454
    • 1996-05-03
    • Walter Holemans
    • Walter Holemans
    • H01Q1/36H01Q11/08
    • H01Q1/362H01Q11/086Y10S343/02
    • The deployable helical antenna of the present invention and helical antenna deployment system includes a helical antenna having a plurality of helical filars and at least two guide plates positioned with respect to the helical filars. Each of the guide plates is provided with a plurality of guide elements operably attached to a corresponding helical filar. The novel helical antenna of the present invention can be collapsed into a stowed position such that each of the helical filars, and portions thereof, are tightly and efficiently layered one over another. Upon actuation of a retention mechanism, the stored energy in each of the collapsed helical filars initiates antenna deployment whereby the guide elements accurately and reliably control the movement and final position of a corresponding helical filar. The novel deployment system of the present invention controls the operational parameters of the antenna (such as diameter, height, and pitch angle), insures quick and reliable antenna deployment, and increases the lateral stiffness of the deployed antenna.
    • 本发明的可展开螺旋天线和螺旋天线展开系统包括具有多个螺旋丝状物的螺旋天线和相对于螺旋丝状物定位的至少两个引导板。 每个引导板设置有可操作地连接到相应的螺旋丝状体上的多个引导元件。 本发明的新型螺旋天线可以折叠成收起位置,使得每个螺旋丝及其部分彼此紧密有效地分层。 在启动保持机构时,每个收缩的螺旋丝状体中存储的能量启动天线展开,由此引导元件精确可靠地控制相应螺旋丝状丝的运动和最终位置。 本发明的新型部署系统控制天线的操作参数(如直径,高度和俯仰角),确保快速可靠的天线部署,并增加部署天线的横向刚度。
    • 9. 发明授权
    • Deployable quadrifilar helical antenna
    • US09742058B1
    • 2017-08-22
    • US15223672
    • 2016-07-29
    • Gregory A. O'Neill, Jr.
    • Gregory A. O'Neill, Jr.David M. Cross
    • H01Q1/28H01Q1/36H01Q1/08
    • H01Q1/288H01Q1/08H01Q1/362H01Q11/086
    • Systems, devices, and methods for providing deployable and collapsible Quadrifilar Helical Antennas (QHA) on small satellites to improve communications in low earth orbit satellites. Monopole antennas are very popular for use on small satellites, generally because they are relatively easy to attach. By using circularly polarized antennas for the spacecraft and the ground station, polarization losses are virtually eliminated. The QHA can be designed to have a wide range of circularly polarized antenna patterns. Low power transmitters are employed on the small satellite to be consistent with the available energy. The communication link budgets are dependent on good radiation pattern characteristics for the small satellite downlink where higher data rates are required. Quadrifilar Helical Antennas can be collapsed and stowed inside a module to mount inside typical cubes known as 1U through 27U size small satellites. After launch from the rocket, the QHA can be deployed to its stored memory shape. The QHA radiating filars can be made from Nitinol wires having an activation temperature above which the filars resume their stored memory shape acquired during heating treatments. QHA applies an electrical direct current onto the filars after launch of the small satellite independent of the radio frequency of the QHA.