WO2023155429A1 - 天线支撑件和天线 - Google Patents

天线支撑件和天线 Download PDF

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Publication number
WO2023155429A1
WO2023155429A1 PCT/CN2022/120195 CN2022120195W WO2023155429A1 WO 2023155429 A1 WO2023155429 A1 WO 2023155429A1 CN 2022120195 W CN2022120195 W CN 2022120195W WO 2023155429 A1 WO2023155429 A1 WO 2023155429A1
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Prior art keywords
support arm
support
antenna
base
support body
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PCT/CN2022/120195
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English (en)
French (fr)
Inventor
王健
方铁勇
徐宝亮
孙伟华
张赛
赵越
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中兴通讯股份有限公司
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Publication of WO2023155429A1 publication Critical patent/WO2023155429A1/zh

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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/42Housings not intimately mechanically associated with radiating elements, e.g. radome
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q15/00Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
    • H01Q15/14Reflecting surfaces; Equivalent structures

Definitions

  • Embodiments of the present disclosure relate to the technical field of antennas, and in particular, to an antenna support and an antenna assembly.
  • the base station antenna is an indispensable part in the 4G and 5G era.
  • the radiation unit on the reflector is one of the most important parts inside the antenna, its safe distance from the FRP radome will also be limited by space.
  • an antenna support is provided inside the radome to prevent the radiation unit from colliding with the radome.
  • the antenna support in the related art cannot effectively buffer the external impact force. Vibrator and other important parts are damaged.
  • the main purpose of the embodiments of the present disclosure is to provide an antenna support and an antenna assembly.
  • An embodiment of the present disclosure provides an antenna support, including a base, a middle support body and an elastic support body, the middle support body connects the base and the elastic support body, the middle support body is a rigid structure, and the elastic support body is a hollow structure.
  • An embodiment of the present disclosure also provides an antenna assembly, including a radome, a reflection plate accommodated in the radome, and a plurality of above-mentioned antenna supports arranged between the radome and the reflection plate.
  • FIG. 1 is a schematic diagram of a three-dimensional structure of an antenna support according to an embodiment of the present disclosure
  • Fig. 2 is a three-dimensional structural schematic diagram of an antenna assembly according to an embodiment of the present disclosure
  • FIG. 3 is a right side view of the antenna assembly shown in FIG. 2 in an embodiment of the present disclosure.
  • connection should be interpreted in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral Connection; can be direct or indirect through an intermediary.
  • connection should be interpreted in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral Connection; can be direct or indirect through an intermediary.
  • An embodiment of the present disclosure provides an antenna support 10, as shown in FIG. 1 , including a base 103, a middle support 102 and an elastic support 101. It is a rigid structure; the elastic support body 101 is a hollow structure.
  • the antenna support 10 proposed by the embodiment of the present disclosure includes a base 103, a middle support body 102 and an elastic support body 101.
  • the middle support body 102 connects the base 103 and the elastic support body 101 to play a role of supporting connection, and the middle support body 102 is a rigid structure.
  • the elastic support 101 above the middle support 102 is a hollow structure, and the elastic support 101 is prone to deformation when subjected to an external force. Therefore, when the antenna support 10 collides with the radome, the impact force will first act on the elastic support 101 of the antenna support 10, and the elastic support 101 is deformed under force, which acts as a buffer absorption. It can effectively buffer the external impact force, protect the internal vibrator and other important parts of the antenna from being damaged when the antenna is collided or impacted, and play a very good role in protecting the internal parts of the antenna.
  • the surface of the elastic support body 101 away from the base 103 is arc-shaped, and the arc-shaped upper surface of the elastic support body 101 can also play a buffer role. Therefore, when the elastic support body 101 is subjected to an external force, it first contacts The arc-shaped upper surface of the elastic support body 101 buffers a part of the impact force, and then the elastic support body 101 deforms under force to further play a role in buffering and absorbing energy.
  • middle support body 102 The specific structure of the middle support body 102 will be described below with reference to FIG. 1 .
  • the central support body 102 includes a base 1021 and a reinforcing rib 1022 fixedly connected to the surface of the base 1021 .
  • the reinforcing ribs 1022 are fixed on the surface of the base 1021 to strengthen the structural strength of the base 1021 and improve the rigid supporting force of the middle supporting body 102 .
  • the base 1021 and the reinforcing rib 1022 are integrally formed to further improve the overall structural strength of the middle support body 102 .
  • the base 1021 is a rectangular parallelepiped.
  • the shape of the base 1021 is not limited to a rectangular parallelepiped, and may be other shapes, such as a cube, a cylinder, an elliptical cylinder, and the like.
  • the reinforcing rib 1022 includes a longitudinal reinforcing rib 1022 and a transverse reinforcing rib 1022, and the longitudinal reinforcing rib 1022 and the transverse reinforcing rib 1022 are fixedly connected.
  • fixedly connected longitudinal reinforcing ribs 1022 and transverse reinforcing ribs 1022 are arranged on the surface of the base 1021 to further strengthen the structural strength of the base 1021 and increase the rigid support force of the middle supporting body 102 .
  • the structural pattern of the reinforcing rib 1022 in this embodiment is not limited to that shown in FIG. 1 , as long as it can strengthen the structural strength of the base 1021 and can effectively receive and disperse the impact force transmitted by the elastic support body 101 .
  • the elastic support body 101 includes: an arc support arm 1011, a first support arm 1012 and a second support arm 1013 connecting the arc support arm 1011 and the middle support body 102, the first support arm 1012 and the second support arm 1013 is cross-fixed; the arc-shaped support arm 1011 is arc-shaped and protrudes away from the surface of the base 103 .
  • the arc-shaped support arm 1011, the first support arm 1012 and the second support arm 1013 are integrally formed, thereby further improving the overall structural strength of the elastic support body 101, and avoiding that the elastic support body 101 has not yet Deformation causes damage.
  • the first support arm 1012 and the second support arm 1013 are used to connect the arc support arm 1011 and the middle support body 102, and both the first support arm 1012 and the second support arm 1013 are cross-fixed. There is a large buffer gap between the supporting arm 1012 , the second supporting arm 1013 and the arc-shaped supporting arm 1011 , so that the elastic supporting body 101 has a hollow structure. When subjected to a relatively large impact force, the elastic support body 101 will elastically deform to play the role of buffering and absorbing energy.
  • the arc-shaped support arm 1011 is arc-shaped and protrudes away from the surface of the base 103.
  • the arc-shaped support arm 1011 can also play a buffering role, so when the elastic support body 101 is subjected to external force, it first contacts the arc-shaped support arm 1011 to buffer a part Impact force, after that, the elastic support body 101 deforms under the force to further play the role of buffering and absorbing energy.
  • the arc-shaped support arm 1011 is the part that mainly receives the impact force, and is also the part that first receives the impact force. Its structural form is not limited to the arc-shaped structure, for example, it may be a flat plate structure.
  • the intersection point of the first support arm 1012 and the second support arm 1013 is located on the same longitudinal straight line as the midpoint of the arc-shaped support arm 1011, and the first support arm 1012 and the second support arm 1013 are aligned with respect to the longitudinal straight line. Axisymmetric distribution. In this way, the first support arm 1012 and the second support arm 1013 form a cross-symmetric structure, and when the arc-shaped support arm 1011 is deformed by pressure, the cross-symmetry structure formed by the first support arm 1012 and the second support arm 1013 can be evenly eliminated The transmitted impact force. When the impact force is too large, the degree of deformation exceeds the buffer gap, and the middle support body 102 will play a role of rigid support.
  • the arc-shaped support arm 1011 includes opposite first ends and second ends, and the first support arm 1012 can be connected to a position adjacent to the first end of the arc-shaped support arm 1011; the second support arm 1013 can be connected to At a position adjacent to the second end of the arc-shaped support arm 1011 .
  • the first support arm 1012 and the second support arm 1013 are fixedly connected to the middle position of the elastic support body 101;
  • the elastic support body 101 also includes: a third support arm 1014 and a fourth support arm 1015;
  • One end of the support arm 1014 is fixedly connected to the connection position between the middle support body 102 and the first support arm 1012, the other end of the third support arm 1014 is fixed to one end of the arc support arm 1011;
  • one end of the fourth support arm 1015 is fixedly connected At the connection position between the middle support body 102 and the second support arm 1013 , the other end of the fourth support arm 1015 is fixedly connected to the other end of the arc-shaped support arm 1011 .
  • the elastic support body 101 Form four buffer gaps.
  • the first support arm 1012 and the second support arm 1013 are fixedly connected to the middle position of the elastic support body 101
  • the third support arm 1014 is fixedly connected to an end (such as the first end) of the arc support arm 1011
  • the fourth support arm 1015 Fixedly connected to the other end (for example, the second end) of the arc-shaped support arm 1011, so that the four support arms support the elastic support body 101 at four positions, improve the impact resistance of the elastic support body 101, and avoid excessive impact force As a result, the degree of deformation of the elastic support body 101 exceeds the buffer gap.
  • the arc-shaped support arm 1011, the first support arm 1012, the second support arm 1013, the third support arm 1014 and the fourth support arm 1015 are integrally formed, thereby further improving the overall structural strength of the elastic support body 101, This prevents the elastic support body 101 from being damaged without being deformed when subjected to an impact force.
  • the specific structure of the base 103 will be described below with reference to FIG. 1 .
  • the base 103 includes a bottom plate 1031 , and a positioning portion 1032 and a limiting portion 1033 fixedly connected under the bottom plate 1031 ; the middle support body 102 is fixed above the bottom plate 1031 .
  • the limiting part 1033 is used to fix the base 103 on the reflector of the antenna structure, and the positioning part 1032 is used to position the base 103 on the reflector of the antenna structure to avoid displacement or rotation of the base 103 .
  • the limiting part 1033 is detachably fixed on the reflector, for example: the limiting part 1033 can be a buckle, and a corresponding card slot is provided on the reflecting plate 20, and the limiting part 1033 can be embedded in the card groove to realize the connection between the limiting part 1033 and the reflecting plate. card connection.
  • the base 103 can be fixed on the reflector by sliding and clamping.
  • the clamping method is not limited to sliding and clamping. on the reflector.
  • the limiting portion 1033 can also be non-detachably fixed to the reflection plate, for example: welding, bolting and the like.
  • the fixing method of the limiting portion 1033 and the reflecting plate is not limited to buckle, welding, bolt fixing, etc., and may be detachable or non-detachable. It only needs to ensure that the antenna supporting member 10 can be firmly fixed on the reflector.
  • the positioning part 1032 can be a raised structure, and the reflector is provided with a groove or a through hole corresponding to the raised structure. When the antenna support 10 is fixed on the reflector, the positioning part 1032 is embedded in the corresponding groove or through hole on the reflector. In order to realize the positioning of the base 103 on the reflector and prevent the base 103 from being displaced or rotated.
  • the base 103 , the middle supporting body 102 and the elastic supporting body 101 are integrally formed, so as to improve the overall structural strength of the entire antenna support 10 , and further improve the impact resistance of the antenna support 10 .
  • the application scenarios of the antenna support 10 in the embodiments of the present disclosure are not limited to reflectors, and may also be other installation scenarios.
  • the antenna support 10 when the antenna support 10 is installed and used, the antenna support 10 is first fixed on the reflector through the limiting part 1033 of the bottom base 103, and the positioning part 1032 is used to realize the positioning of the antenna support 10 on the reflector. position.
  • the impact force When the antenna support 10 collides with the radome, the impact force will first act on the elastic support body 101, and the elastic support body 101 will be deformed under the force, which will play a role in buffering and absorbing energy, and protect important parts such as the vibrator inside the antenna. Avoid damage in the event of a collision or impact.
  • the middle support body 102 plays the role of supporting and connecting the base 103 and the elastic support body 101.
  • the middle support body 102 is a rigid structure.
  • the middle support body 102 When the deformation degree of the elastic support body 101 exceeds the buffer gap, the middle support body 102 will play a role of rigid support.
  • the antenna supporting member 10 has a simple structure and is easy to install, and its elastic supporting body 101 can effectively buffer external impact force and play a good role in protecting the inside of the antenna.
  • An embodiment of the present disclosure also provides an antenna assembly, as shown in FIG. 2 and FIG. A plurality of antenna supports 10 as in the above-mentioned embodiments.

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  • Electromagnetism (AREA)
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Abstract

本公开实施例涉及天线技术领域,公开了一种天线支撑件,包括底座、中部支撑体和弹性支撑体,所述中部支撑体连接所述底座和所述弹性支撑体,所述中部支撑体为刚性结构;所述弹性支撑体为镂空结构。本公开实施例还公开了天线组件,包括天线罩、收容于所述天线罩的反射板、以及排布于天线罩与反射板之间的多个上述天线支撑件。

Description

天线支撑件和天线
相关申请的交叉引用
本公开要求享有2022年02月21日提交的名称为“天线支撑件和天线”的中国专利申请CN202220351980.X的优先权,其全部内容通过引用并入本公开中。
技术领域
本公开实施例涉及天线技术领域,特别涉及一种天线支撑件和天线组件。
背景技术
基站天线在4G、5G时代中是不可或缺的一环,天线内部零件众多,且发展趋势越来越趋向于小型化,轻量化,所以留给天线内部的空间会越来越小。而反射板上的辐射单元作为天线内部最重要的零件之一,其离玻璃钢天线罩的安全距离也会受到空间限制。在天线运输中存在大风等外作用力的情况下,反射板上的辐射单元很可能会与变形的天线罩发生碰撞,轻则影响天线性能,重则导致天线无法正常工作。因此,在天线罩内会设置天线支撑件以防止辐射单元与天线罩发生碰撞,但相关技术中的天线支撑件无法有效缓冲外部冲击力,若天线罩受到较大的冲击力则容易导致天线内振子等重要零件损坏。
发明内容
本公开实施例的主要目的在于提出一种天线支撑件和天线组件。
本公开实施例提供了一种天线支撑件,包括底座、中部支撑体和弹性支撑体,中部支撑体连接底座和弹性支撑体,中部支撑体为刚性结构;弹性支撑体为镂空结构。
本公开实施例还提供了一种天线组件,包括天线罩、收容于天线罩的反射板、以及排布于天线罩与反射板之间的多个上述天线支撑件。
附图说明
一个或多个实施例通过与之对应的附图中的图片进行示例性说明,这些示例性说明并不构成对实施例的限定。
图1是本公开实施例天线支撑件的立体结构示意图;
图2是本公开实施例天线组件的立体结构示意图;
图3是本公开实施例中图2所示天线组件的右视图。
具体实施方式
为使本公开实施例的目的、技术方案和优点更加清楚,下面将结合附图对本公开的各实施例进行详细的阐述。然而,本领域的普通技术人员可以理解,在本公开各实施例中,为了使读者更好地理解本公开而提出了许多技术细节。但是,即使没有这些技术细节和基于以下各实施例的种种变化和修改,也可以实现本公开所要求保护的技术方案。以下各个实施例的划分是为了描述方便,不应对本公开的具体实现方式构成任何限定,各个实施例在不矛盾的前提下可以相互结合相互引用。
在本公开的描述中,除非另有说明,“多个”的含义是两个以上;术语“上”、“下”、“左”、“右”、“内”、“外”等指示的方位或位置关系仅是为了便于描述本公开和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本公开的限制。此外,术语“第一”、“第二”、“第三”等仅用于描述目的,而不能理解为指示或暗示相对重要性。“垂直”并不是严格意义上的垂直,而是在误差允许范围之内。“平行”并不是严格意义上的平行,而是在误差允许范围之内。
下述描述中出现的方位词均为图中示出的方向,并不是对本公开的具体结构进行限定。在本公开的描述中,除非另有明确的规定和限定,术语“安装”、“相连”、“连接”应做广义理解,例如,可以是固定连接,也可以是可拆卸连接,或一体地连接;可以是直接相连,也可以通过中间媒介间接相连。对于本领域的普通技术人员而言,可视具体情况理解上述术语在本公开中的具体含义。
本公开实施例提供了一种天线支撑件10,如图1所示,包括底座103、中部支撑体102和弹性支撑体101,中部支撑体102连接底座103和弹性支撑体101,中部支撑体102为刚性结构;弹性支撑体101为镂空结构。
本公开实施例提出的天线支撑件10包括底座103、中部支撑体102和弹性支撑体101,中部支撑体102连接底座103和弹性支撑体101,起到支撑连接作用,中部支撑体102为刚性结构以避免天线支撑件10整体变形而导致天线罩与反射板上的辐射单元发生碰撞;中部支撑体102上方的弹性支撑体101为镂空结构,弹性支撑体101在受到外力作用时易发生形变,起到缓冲吸能作用,因此,当天线支撑件10和天线罩发生碰撞时,冲击力会首先作用在天线支撑件10的弹性支撑体101上,弹性支撑体101受力而变形,起到缓冲吸能作用,有效的缓冲外部冲击力,保护天线内振子等重要零件在天线受到碰撞或者冲击时,避免遭受破坏,对天线内部零件起到很好的保护作用。
在一实施方式中,弹性支撑体101远离底座103的表面呈弧形凸起,弹性支撑体101的弧形上表面也能起到缓冲作用,因此弹性支撑体101在受到外力作用时,先接触到弹性支撑体101的弧形上表面,缓冲一部分冲击力,之后,弹性支撑体101受力变形进一步起到缓冲吸能作用。
下面结合图1对中部支撑体102的具体结构进行说明。
本公开实施例中部支撑体102包括基座1021、固定连接于基座1021表面的加强筋1022。加强筋1022固定于基座1021表面用于加强基座1021的结构强度,提高中部支撑体102的刚性支撑力。在一实施方式中,基座1021和加强筋1022一体成型从而进一步提高中部支撑体102的整体结构强度。在一实施方式中,基座1021呈长方体,当然,基座1021的形状不限于长方体形状,也可以是其他形状,例如:正方体形状、圆柱体形状、椭圆柱体形状等。在一实施方式中,加强筋1022包括纵向加强筋1022和横向加强筋1022,且纵向加强筋1022和横向加强筋1022固定连接。本实施例中,在基座1021表面设置固定连接的纵向加强筋1022和横向加强筋1022,进一步加强基座1021的结构强度,提高中部支撑体102的刚性支撑力。本实施例中加强筋1022的结构样式不限于图1所示,只要可以加强基座1021的结构强度,且能有效承接并分散弹性支撑体101传递过来的冲击力即可。
下面结合图1对弹性支撑体101的具体结构进行说明。
本实施例中弹性支撑体101包括:弧形支撑臂1011,连接弧形支撑臂1011和中部支撑体102的第一支撑臂1012和第二支撑臂1013,第一支撑臂1012和第二支撑臂1013交叉固定;弧形支撑臂1011呈弧形,且远离底座103的表面凸起。在一实施方式中,弧形支撑臂1011、第一支撑臂1012和第二支撑臂1013一体成型,从而进一步提高弹性支撑体101的整体结构强度,避免在受到冲击力时弹性支撑体101还未发生形变便损坏。
第一支撑臂1012和第二支撑臂1013用于连接弧形支撑臂1011和中部支撑体102,且第一支撑臂1012和第二支撑臂1013两者交叉固定,在不受力时,第一支撑臂1012、第二支撑臂1013以及弧形支撑臂1011之间留有较大的缓冲间隙,以使弹性支撑体101呈镂空结构。在受到较大冲击力时,弹性支撑体101会发生弹性变形,起到缓冲吸能的作用。弧形支撑臂1011呈弧形,且远离底座103的表面凸起,弧形支撑臂1011也能起到缓冲作用,因此弹性支撑体101在受到外力作用时先接触到弧形支撑臂1011缓冲一部分冲击力,之后,弹性支撑体101受力变形进一步起到缓冲吸能作用。弧形支撑臂1011作为主要承接冲击力的部分,也是首先承接冲击力的部分,其结构形式不限于弧形结构,例如,可以为平板结构。
在一实施方式中,第一支撑臂1012和第二支撑臂1013的交点与弧形支撑臂1011的中点 位于同一纵向直线上,且第一支撑臂1012和第二支撑臂1013关于纵向直线呈轴对称分布。如此,第一支撑臂1012和第二支撑臂1013形成交叉对称结构,当弧形支撑臂1011受压力变形时,第一支撑臂1012和第二支撑臂1013所形成的交叉对称结构能均衡地消除传导过来的冲击力。当冲击力过大时,变形程度超出缓冲间隙,中部支撑体102会起到刚性支撑作用。
在一实施方式中,弧形支撑臂1011包括相对的第一端和第二端,第一支撑臂1012可连接于邻近弧形支撑臂1011第一端的位置处;第二支撑臂1013可连接于邻近弧形支撑臂1011第二端的位置处。
在一实施方式中,第一支撑臂1012和第二支撑臂1013固定连接于弹性支撑体101的中间位置处;弹性支撑体101还包括:第三支撑臂1014和第四支撑臂1015;第三支撑臂1014的一端固定连接于中部支撑体102与第一支撑臂1012的连接位置处,第三支撑臂1014的另一端固定于弧形支撑臂1011的一端;第四支撑臂1015的一端固定连接于中部支撑体102与第二支撑臂1013的连接位置处,第四支撑臂1015的另一端固定连接于弧形支撑臂1011的另一端。
本实施例中不仅设置第一支撑臂1012和第二支撑臂1013连接弧形支撑臂1011和中部支撑体102,还设置第三支撑臂1014和第四支撑臂1015,此时,弹性支撑体101形成四处缓冲间隙。第一支撑臂1012和第二支撑臂1013固定连接于弹性支撑体101的中间位置处,第三支撑臂1014固定连接于弧形支撑臂1011的一端(例如第一端),第四支撑臂1015固定连接于弧形支撑臂1011的另一端(例如第二端),如此,四个支撑臂在4个位置处支撑弹性支撑体101,提高弹性支撑体101的抗冲击能力,避免冲击力过大而导致弹性支撑体101的变形程度超出缓冲间隙。在一实施方式中,弧形支撑臂1011、第一支撑臂1012、第二支撑臂1013、第三支撑臂1014和第四支撑臂1015一体成型,从而进一步提高弹性支撑体101的整体结构强度,避免在受到冲击力时弹性支撑体101还未发生形变便损坏。
下面结合图1对底座103的具体结构进行说明。
底座103包括底板1031、以及固定连接于底板1031下方的定位部1032和限位部1033;中部支撑体102固定于底板1031上方。限位部1033用于将底座103固定于天线结构的反射板上,而定位部1032则用于将底座103定位在天线结构的反射板上避免底座103发生位移或旋转。
限位部1033可拆卸地固定于反射板,例如:限位部1033可为卡扣,反射板20上设置对应的卡槽,限位部1033可嵌入卡槽内实现限位部1033与反射板的卡接。在一实施方式中,底座103可通过滑入卡接的方式固定在反射板上,当然卡接方式不限于滑入卡接,也可以是 旋转卡接等,只要能保证底座103能顺利固定在反射板上即可。
限位部1033也可不可拆卸地固定于反射板,例如:焊接、螺栓固定等。本公开实施例中限位部1033与反射板的固定方式不限于卡扣、焊接、螺栓固定等,既可以是可拆卸方式也可以是不可拆卸方式。只要能保证天线支撑件10能牢固固定在反射板上即可。
定位部1032可为凸起结构,反射板设有对应该凸起结构的凹槽或通孔,天线支撑件10固定在反射板上时,定位部1032嵌入反射板上对应的凹槽或通孔内,从而实现底座103在反射板上的定位,避免底座103发生位移或旋转。
底座103、中部支撑体102和弹性支撑体101一体成型,从而提高整个天线支撑件10的整体结构强度、进而提高天线支撑件10的抗冲击能力。
本公开实施例中天线支撑件10的应用场景不限于反射板、也可以是其他安装场景。
本公开实施例中天线支撑件10的在安装使用时,首先通过底部底座103的限位部1033将天线支撑件10固定在反射板上,通过定位部1032实现天线支撑件10在反射板上的定位。天线支撑件10和天线罩发生碰撞时,冲击力会首先作用在弹性支撑体101上,弹性支撑体101受力而变形,起到缓冲吸能作用,保护天线内振子等重要零件,在天线受到碰撞或者冲击时,避免遭受破坏。中部支撑体102起到支撑连接底座103和弹性支撑体101的作用,中部支撑体102为刚性结构,在弹性支撑体101的变形程度超出缓冲间隙时,中部支撑体102会起到刚性支撑作用。本公开实施例中天线支撑件10结构简单、安装方便,且其弹性支撑体101能有效的缓冲外部冲击力,对天线内部起到很好的保护作用。
本公开实施例还提供了一种天线组件,如图2和图3所示,包括天线罩30、收容于天线罩30的反射板20、以及排布于天线罩30与反射板20之间的多个如上述实施例的天线支撑件10。
本领域的普通技术人员可以理解,上述各实施例是实现本公开的具体实施例,而在实际应用中,可以在形式上和细节上对其作各种改变,而不偏离本公开的精神和范围。

Claims (10)

  1. 一种天线支撑件,其中,包括底座、中部支撑体和弹性支撑体,所述中部支撑体连接所述底座和所述弹性支撑体,所述中部支撑体为刚性结构;所述弹性支撑体为镂空结构。
  2. 根据权利要求1所述的天线支撑件,其中,所述中部支撑体包括基座、固定连接于所述基座表面的加强筋。
  3. 根据权利要求2所述的天线支撑件,其中,所述加强筋包括纵向加强筋和横向加强筋,且所述纵向加强筋和所述横向加强筋固定连接。
  4. 根据权利要求2或3所述的天线支撑件,其中,所述基座呈长方体。
  5. 根据权利要求1中所述的天线支撑件,其中,所述弹性支撑体包括:弧形支撑臂,连接所述弧形支撑臂和所述中部支撑体的第一支撑臂和第二支撑臂,所述第一支撑臂和所述第二支撑臂交叉固定;
    所述弧形支撑臂呈弧形,且远离所述底座的表面凸起。
  6. 根据权利要求5所述的天线支撑件,其中,所述第一支撑臂和所述第二支撑臂的交点与所述弧形支撑臂的中点位于同一纵向直线上,且所述第一支撑臂和所述第二支撑臂关于所述纵向直线呈轴对称分布。
  7. 根据权利要求5或6所述的天线支撑件,其中,所述第一支撑臂和所述第二支撑臂固定连接于所述弹性支撑体的中间位置处;
    所述弹性支撑体还包括:第三支撑臂和第四支撑臂;
    所述第三支撑臂的一端固定连接于所述中部支撑体与所述第一支撑臂的连接位置处,所述第三支撑臂的另一端固定于所述弧形支撑臂的一端;
    所述第四支撑臂的一端固定连接于所述中部支撑体与所述第二支撑臂的连接位置处,所述第四支撑臂的另一端固定连接于所述弧形支撑臂的另一端。
  8. 根据权利要求1所述的天线支撑件,其中,所述底座包括底板、以及固定连接于所述 底板下方的定位部和限位部;所述中部支撑体固定于所述底板上方。
  9. 根据权利要求1所述的天线支撑件,其中,所述底座、所述中部支撑体和所述弹性支撑体一体成型。
  10. 一种天线组件,其中,包括天线罩、收容于所述天线罩的反射板、以及排布于天线罩与反射板之间的多个如权利要求1至9任一项所述的天线支撑件。
PCT/CN2022/120195 2022-02-21 2022-09-21 天线支撑件和天线 WO2023155429A1 (zh)

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