CN114678691A - Low profile broadband conformal antenna elements and arrays - Google Patents
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- H—ELECTRICITY
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- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q9/00—Electrically-short antennas having dimensions not more than twice the operating wavelength and consisting of conductive active radiating elements
- H01Q9/04—Resonant antennas
- H01Q9/0407—Substantially flat resonant element parallel to ground plane, e.g. patch antenna
- H01Q9/045—Substantially flat resonant element parallel to ground plane, e.g. patch antenna with particular feeding means
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- H—ELECTRICITY
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- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
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- H—ELECTRICITY
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- H—ELECTRICITY
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- H01Q21/00—Antenna arrays or systems
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Abstract
Description
技术领域technical field
本发明属于雷达与宽带无线通信技术领域,涉及一种低剖面宽带共形天线单元及阵列,可应用于宽带射频信号的收发。The invention belongs to the technical field of radar and broadband wireless communication, and relates to a low-profile broadband conformal antenna unit and an array, which can be applied to the transceiver of broadband radio frequency signals.
背景技术Background technique
L型馈电天线具有小型化、剖面低、成本低、重量轻等微带天线的常见优点,同时还克服了常见微带天线带宽较窄的问题。目前L型馈电天线通常由水平探针和垂直探针以及一个位于探针上方的辐射贴片组成。L型探针垂直部分及水平部分可以和辐射贴片之间耦合馈电,且它们之间产生的感抗和容抗两者相互作用产生谐振,这可以使天线频带得到拓宽。因为以上的优点L型探针馈电天线在通信系统中得到了广泛的应用。然而,传统的L型馈电天线为平面结构且工作带宽受限,难以满足飞行器平台异形面安装约束下的宽角域波束覆盖要求。The L-shaped feed antenna has the common advantages of microstrip antennas such as miniaturization, low profile, low cost, and light weight, and also overcomes the problem of narrow bandwidth of common microstrip antennas. Current L-shaped feed antennas usually consist of horizontal and vertical probes and a radiating patch above the probes. The vertical part and the horizontal part of the L-shaped probe can be coupled with the radiating patch for feeding, and the inductive and capacitive reactances generated between them interact to generate resonance, which can widen the antenna frequency band. Because of the above advantages, L-type probe feed antennas have been widely used in communication systems. However, the traditional L-shaped feed antenna has a planar structure and limited operating bandwidth, which makes it difficult to meet the wide-angle beam coverage requirements under the installation constraints of the special-shaped surface of the aircraft platform.
发明内容SUMMARY OF THE INVENTION
本发明旨在至少解决现有技术中存在的技术问题之一。The present invention aims to solve at least one of the technical problems existing in the prior art.
为此,本发明提供了一种低剖面宽带共形天线单元及阵列。To this end, the present invention provides a low-profile broadband conformal antenna unit and array.
本发明的技术解决方案如下:The technical solution of the present invention is as follows:
根据一方面,提供一种低剖面宽带共形天线单元,该低剖面宽带共形天线单元包括:According to one aspect, a low-profile broadband conformal antenna unit is provided, the low-profile broadband conformal antenna unit comprising:
载体,所述载体上具有开口的腔体;a carrier having an open cavity on the carrier;
单元结构,所述单元结构包括:Unit structure, the unit structure includes:
矩形地,所述矩形地设置在所述腔体的内侧表面上;Rectangularly, the rectangle is disposed on the inner side surface of the cavity;
L型馈电单元,所述馈电单元设置在所述腔体内,包括互相垂直设置的渐变型馈电贴片和渐变型馈电探针,其中,所述渐变型馈电探针垂直于所述腔体的底面;L-shaped feeding unit, the feeding unit is disposed in the cavity, and includes a gradient feeding patch and a gradient feeding probe arranged perpendicular to each other, wherein the gradient feeding probe is perpendicular to the the bottom surface of the cavity;
馈电结构,所述馈电结构设置在所述腔体内,所述馈电结构分别与所述矩形地和渐变型馈电探针相连接;a feeding structure, the feeding structure is arranged in the cavity, and the feeding structure is respectively connected with the rectangular ground and the gradient feeding probe;
天线罩,所述天线罩设置在所述腔体的开口处以覆盖所述开口,所述天线罩与所述载体共形;a radome, the radome is disposed at the opening of the cavity to cover the opening, and the radome is conformal to the carrier;
共形辐射单元和寄生辐射单元,所述共形辐射单元和寄生辐射单元间隔设置且均贴合设置在所述天线罩的朝向腔体的一面,所述共形辐射单元和寄生辐射单元均与所述天线罩共形,共同用于高频电磁信号的辐射。The conformal radiating element and the parasitic radiating element, the conformal radiating element and the parasitic radiating element are arranged at intervals and are attached to the side of the radome facing the cavity, and the conformal radiating element and the parasitic radiating element are both arranged with the radome. The radomes are conformal and are commonly used for radiation of high-frequency electromagnetic signals.
进一步地,所述渐变型馈电探针为圆台结构,圆台结构的轴线垂直于所述腔体的底面,所述圆台结构的顶面与馈电结构连接,所述圆台结构的底面与渐变型馈电贴片连接,其中,顶面靠近腔体的底面设置,顶面面积小于底面面积。Further, the tapered feeding probe is a circular truncated structure, the axis of the circular truncated structure is perpendicular to the bottom surface of the cavity, the top surface of the circular truncated structure is connected to the feeding structure, and the bottom surface of the circular truncated structure is connected to the gradient type. The feeding patch is connected, wherein the top surface is arranged close to the bottom surface of the cavity, and the area of the top surface is smaller than that of the bottom surface.
进一步地,所述渐变型馈电贴片为等腰梯形结构,等腰梯形结构的下底所在的一侧与所述圆台结构的底面相连接,所述下底在底面的投影与底面的直径完全重合。Further, the gradient feeding patch is an isosceles trapezoid structure, the side where the lower bottom of the isosceles trapezoid structure is located is connected to the bottom surface of the circular truncated structure, and the projection of the lower bottom on the bottom surface is the diameter of the bottom surface. completely coincident.
进一步地,所述变型馈电贴片和渐变型馈电探针为一体化成型。Further, the modified feeding patch and the gradient feeding probe are integrally formed.
进一步地,所述天线罩采用透波材料制成。Further, the radome is made of wave-transmitting material.
进一步地,所述馈电结构为同轴线馈电结构,包括同轴设置的内导体和外导体,其中,所述内导体与渐变型馈电探针连接,外导体与矩形地连接。Further, the feeding structure is a coaxial feeding structure, comprising an inner conductor and an outer conductor arranged coaxially, wherein the inner conductor is connected with the tapered feeding probe, and the outer conductor is connected with the rectangular ground.
进一步地,所述腔体为矩形金属腔体,和/或,所述共形辐射单元和寄生辐射单元在腔体底面的投影均为矩形。Further, the cavity is a rectangular metal cavity, and/or the projections of the conformal radiation unit and the parasitic radiation unit on the bottom surface of the cavity are both rectangular.
根据另一方面,提供一种低剖面宽带共形天线阵列,该低剖面宽带共形天线阵列包括多个上述的低剖面宽带共形天线单元。According to another aspect, a low-profile broadband conformal antenna array is provided, the low-profile broadband conformal antenna array comprising a plurality of the above-described low-profile broadband conformal antenna elements.
进一步地,所述天线阵列中,多个低剖面宽带共形天线单元的载体构成一体结构。Further, in the antenna array, the carriers of the plurality of low-profile broadband conformal antenna units form an integral structure.
进一步地,所述天线阵列包括的多个单元结构划分为第一组和第二组,其中,第一组包括多个单元结构,第二组也包括多个单元结构,第一组的多个单元结构和第二组的多个单元结构均沿一体结构的第一方向间隔设置,第一组的多个单元结构和第二组的多个单元结构还相对设置在一体结构的两侧并一一对应设置。Further, the plurality of unit structures included in the antenna array are divided into a first group and a second group, wherein the first group includes a plurality of unit structures, the second group also includes a plurality of unit structures, and the first group includes a plurality of unit structures. The unit structure and the plurality of unit structures of the second group are all arranged at intervals along the first direction of the integrated structure, and the plurality of unit structures of the first group and the plurality of unit structures of the second group are also arranged opposite to the two sides of the integrated structure and meet one another. A corresponding setting.
上述技术方案通过设计L型馈电单元包括渐变结构的馈电探针和馈电贴片,由此能够改善阻抗匹配从而拓展带宽。同时,由于天线单元放置于金属腔体内部,使得增益增加但是驻波情况恶化,通过设计单元包括共形辐射单元和寄生辐射单元,且在两辐射贴片上设计天线罩也即介质匹配层,并令介质匹配层与载体表面共形,由此可以改善天线的驻波情况,同时提升天线在要求角度范围的增益,也即使天线的辐射方向图整体朝方位角向下的方向偏移,拓宽了天线的增益带宽。In the above technical solution, by designing the L-shaped feeding unit to include feeding probes and feeding patches with a gradient structure, impedance matching can be improved and bandwidth can be expanded. At the same time, since the antenna unit is placed inside the metal cavity, the gain is increased but the standing wave situation is deteriorated. By designing the unit to include a conformal radiation unit and a parasitic radiation unit, and designing the radome, that is, the dielectric matching layer, on the two radiation patches, And make the dielectric matching layer conformal to the surface of the carrier, which can improve the standing wave of the antenna, and at the same time increase the gain of the antenna in the required angle range, even if the radiation pattern of the antenna as a whole shifts in the downward direction of the azimuth, widening the gain bandwidth of the antenna.
本发明提供的天线单元为宽角域、高增益、小型化,且与载体表面共形的天线单元,其在所要求的频段内在特定侧向角度范围内满足低驻波和高增益、宽带宽的需求,本发明还进一步基于该天线单元构造了天线阵列,为高精度的测向奠定基础。The antenna unit provided by the present invention is a wide-angle, high-gain, miniaturized, and conformal antenna unit with the surface of the carrier, which satisfies low standing waves, high gain, and wide bandwidth within a specific lateral angle range within the required frequency band. The present invention further constructs an antenna array based on the antenna unit, which lays a foundation for high-precision direction finding.
附图说明Description of drawings
所包括的附图用来提供对本发明实施例的进一步的理解,其构成了说明书的一部分,用于例示本发明的实施例,并与文字描述一起来阐释本发明的原理。显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。The accompanying drawings, which are included to provide a further understanding of the embodiments of the invention, constitute a part of the specification, are used to illustrate the embodiments of the invention, and together with the description, serve to explain the principles of the invention. Obviously, the drawings in the following description are only some embodiments of the present invention, and for those of ordinary skill in the art, other drawings can also be obtained from these drawings without creative effort.
图1为本发明低剖面宽带共形天线阵列的俯视图;1 is a top view of a low-profile broadband conformal antenna array of the present invention;
图2为图1的正视图;Fig. 2 is the front view of Fig. 1;
图3为本发明低剖面宽带共形天线单元的分解图。Figure 3 is an exploded view of the low profile broadband conformal antenna element of the present invention.
图4为本发明L型渐变探针馈电共形天线驻波图;4 is a standing wave diagram of an L-shaped gradient probe fed conformal antenna according to the present invention;
图5为本发明天线单元在低频f1时当方位角在45°-135°范围内,俯仰角选择75°、95°、105°三个角度时增益曲线。5 is the gain curve of the antenna unit of the present invention when the azimuth angle is in the range of 45°-135° at the low frequency f1, and the pitch angle is selected from three angles of 75°, 95°, and 105°.
图6为本发明天线单元在中频f2时当方位角在45°-135°范围内,俯仰角选择75°、95°、105°三个角度时增益曲线。6 is the gain curve of the antenna unit of the present invention when the azimuth angle is in the range of 45°-135° and the pitch angle is selected at three angles of 75°, 95° and 105° at the intermediate frequency f2.
图7为本发明天线单元在高频f3时当方位角在45°-135°范围内,俯仰角选择75°、95°、105°三个角度时增益曲线。7 is the gain curve of the antenna unit of the present invention when the azimuth angle is in the range of 45°-135° and the elevation angle is selected at three angles of 75°, 95° and 105° at high frequency f3.
附图标记:Reference number:
1-天线罩;2-寄生辐射单元;3-共形辐射单元;4-渐变型馈电贴片;5-一体结构;5a-载体;6-渐变型馈电探针;7-矩形地;8-外导体;9-内导体;10-腔体;11-单元结构。1-radome; 2-parasitic radiation element; 3-conformal radiation element; 4-graded feed patch; 5-integrated structure; 5a-carrier; 6-graded feed probe; 7-rectangular ground; 8-outer conductor; 9-inner conductor; 10-cavity; 11-unit structure.
具体实施方式Detailed ways
需要说明的是,在不冲突的情况下,本申请中的实施例及实施例中的特征可以相互组合。下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。以下对至少一个示例性实施例的描述实际上仅仅是说明性的,决不作为对本发明及其应用或使用的任何限制。基于本发明中的实施例,本领域普通技术人员在没有作出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。It should be noted that the embodiments in the present application and the features of the embodiments may be combined with each other in the case of no conflict. The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. The following description of at least one exemplary embodiment is merely illustrative in nature and is in no way intended to limit the invention, its application, or uses. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
需要注意的是,这里所使用的术语仅是为了描述具体实施方式,而非意图限制根据本申请的示例性实施方式。如在这里所使用的,除非上下文另外明确指出,否则单数形式也意图包括复数形式,此外,还应当理解的是,当在本说明书中使用术语“包含”和/或“包括”时,其指明存在特征、步骤、操作、器件、组件和/或它们的组合。It should be noted that the terminology used herein is for the purpose of describing specific embodiments only, and is not intended to limit the exemplary embodiments according to the present application. As used herein, unless the context clearly dictates otherwise, the singular is intended to include the plural as well, furthermore, it is to be understood that when the terms "comprising" and/or "including" are used in this specification, it indicates that There are features, steps, operations, devices, components and/or combinations thereof.
除非另外具体说明,否则在这些实施例中阐述的部件和步骤的相对布置、数字表达式和数值不限制本发明的范围。同时,应当明白,为了便于描述,附图中所示出的各个部分的尺寸并不是按照实际的比例关系绘制的。对于相关领域普通技术人员已知的技术、方法和设备可能不作详细讨论,但在适当情况下,所述技术、方法和设备应当被视为授权说明书的一部分。在这里示出和讨论的所有示例中,任何具体值应被解释为仅仅是示例性的,而不是作为限制。因此,示例性实施例的其它示例可以具有不同的值。应注意到:相似的标号和字母在下面的附图中表示类似项,因此,一旦某一项在一个附图中被定义,则在随后的附图中不需要对其进行进一步讨论。The relative arrangement of the components and steps, the numerical expressions and numerical values set forth in these embodiments do not limit the scope of the invention unless specifically stated otherwise. Meanwhile, it should be understood that, for the convenience of description, the dimensions of various parts shown in the accompanying drawings are not drawn in an actual proportional relationship. Techniques, methods, and devices known to those of ordinary skill in the relevant art may not be discussed in detail, but where appropriate, such techniques, methods, and devices should be considered part of the authorized description. In all examples shown and discussed herein, any specific value should be construed as illustrative only and not as limiting. Accordingly, other examples of exemplary embodiments may have different values. It should be noted that like numerals and letters refer to like items in the following figures, so once an item is defined in one figure, it does not require further discussion in subsequent figures.
如图1-7所示,在本发明的一个实施例中,提供一种低剖面宽带共形天线单元,该低剖面宽带共形天线单元包括载体5a和单元结构11,所述载体5a上具有开口的腔体10;所述单元结构11包括矩形地7、L型馈电单元、馈电结构、天线罩1、共形辐射单元3和寄生辐射单元2,所述矩形地7设置在所述腔体10的内侧表面上;所述馈电单元设置在所述腔体10内,包括互相垂直设置的渐变型馈电贴片4和渐变型馈电探针6,其中,所述渐变型馈电探针6垂直于所述腔体10的底面;所述馈电结构设置在所述腔体10内,分别与所述矩形地7和渐变型馈电探针6相连接;所述天线罩1设置在所述腔体10的开口处以覆盖所述开口,所述天线罩1与所述载体5a共形;所述共形辐射单元3和寄生辐射单元2间隔设置且均贴合设置在所述天线罩1的朝向腔体10的一面,所述共形辐射单元3和寄生辐射单元2均与所述天线罩1共形,共同用于高频电磁信号的辐射。As shown in FIGS. 1-7 , in one embodiment of the present invention, a low-profile broadband conformal antenna unit is provided. The low-profile broadband conformal antenna unit includes a
举例来说,所述腔体10可以为矩形金属腔体10,腔体10深度可以为67.03mm,平面尺寸可以为150mm*150mm,作为单元结构11的安装环境。For example, the
举例来说,所述渐变型馈电贴片4和渐变型馈电探针6、所述共形辐射单元3和寄生辐射单元2均为贴片,也均为理想导体。其中,渐变型馈电探针6由馈电结构进行馈电激励,馈电贴片对上方的共形辐射单元3进行耦合馈电。For example, the gradient feeding patch 4 and the gradient feeding probe 6, the
可见,上述技术方案通过设计L型馈电单元包括渐变结构的馈电探针和馈电贴片,由此能够改善阻抗匹配从而拓展带宽。同时,由于天线单元放置于金属腔体内部,使得增益增加但是驻波情况恶化,通过设计单元包括共形辐射单元和寄生辐射单元,且在两辐射贴片上设计天线罩也即介质匹配层,并令介质匹配层与载体表面共形,由此可以改善天线的驻波情况,同时提升天线在要求角度范围的增益,也即使天线的辐射方向图整体朝方位角向下的方向偏移,拓宽了天线的增益带宽。It can be seen that the above technical solution can improve the impedance matching and expand the bandwidth by designing the L-shaped feeding unit to include the feeding probe and the feeding patch of the gradient structure. At the same time, since the antenna unit is placed inside the metal cavity, the gain is increased but the standing wave situation is deteriorated. By designing the unit to include a conformal radiation unit and a parasitic radiation unit, and designing the radome, that is, the dielectric matching layer, on the two radiation patches, And make the dielectric matching layer conformal to the surface of the carrier, which can improve the standing wave of the antenna, and at the same time increase the gain of the antenna in the required angle range, even if the radiation pattern of the antenna as a whole shifts in the downward direction of the azimuth, widening the gain bandwidth of the antenna.
也即,本发明实施例通过应用金属腔体、渐变形状的馈电单元以及天线罩和辐射单元的设计,使得天线单元在辐射单元共形的情况下保持小尺寸、宽频段、宽角域高增益波束覆盖的特点。That is, in the embodiment of the present invention, by applying the design of a metal cavity, a feed unit with a gradient shape, and a radome and a radiating element, the antenna element maintains a small size, a wide frequency band, and a wide angular domain height when the radiating element is conformal. Gain beam coverage characteristics.
根据本发明一种实施例,为了实现侧向辐射的L频段天线方案,设计所述腔体10位于载体5a的侧面,也即,在载体5a的侧面上开设一个金属腔体10,并将馈电单元和辐射单元设置于腔体10内部形成L型探针馈电天线,满足在载体5a侧面的金属腔体10内实现侧向辐射的L频段天线方案。According to an embodiment of the present invention, in order to realize the L-band antenna scheme of lateral radiation, the
在上述实施例中,为了更好改善阻抗匹配从而更好地拓展带宽:In the above embodiment, in order to better improve impedance matching and thus better expand the bandwidth:
所述渐变型馈电探针6为圆台结构,圆台结构的轴线垂直于所述腔体10的底面,所述圆台结构的顶面与馈电结构连接,所述圆台结构的底面与渐变型馈电贴片4连接,其中,顶面靠近腔体10的底面设置,顶面面积小于底面面积。The tapered feeding probe 6 has a circular truncated structure, the axis of the circular truncated structure is perpendicular to the bottom surface of the
所述渐变型馈电贴片4为等腰梯形结构,等腰梯形结构的下底所在的一侧与所述圆台结构的底面相连接,所述下底在底面的投影与底面的直径完全重合。The gradient feeding patch 4 is an isosceles trapezoid structure, the side where the lower bottom of the isosceles trapezoid structure is located is connected to the bottom surface of the circular truncated structure, and the projection of the lower bottom on the bottom surface completely coincides with the diameter of the bottom surface. .
也即,沿远离所述腔体10底面的方向,渐变型馈电探针6半径随高度增加而递增,呈现倒圆台形结构。渐变型馈电探针6上端部接有一渐变型馈电贴片4,宽度随着长度增加而减小,呈现等腰梯形形状。也即,本发明实施例基于L型探针馈电天线基本宽带原理,通过设计渐变型馈电探针6和渐变型馈电贴片4的具体渐变形状为位置关系,从而能够更好改善阻抗匹配从而更好地拓展带宽。That is, along the direction away from the bottom surface of the
较佳地,所述变型馈电贴片和渐变型馈电探针6为一体化成型。Preferably, the modified feeding patch and the gradient feeding probe 6 are integrally formed.
在上述实施例中,为了更好地改善金属腔体反射对驻波造成的影响,所述天线罩1采用透波材料制成。In the above embodiment, in order to better improve the influence of the reflection of the metal cavity on the standing wave, the
也即,当L型探针馈电天线周围为理想电边界时,由于导体边界带来的强反射效应,其在中低频的性能将大幅恶化,针对这一问题,本发明实施例通过在两辐射贴片上方添加一层透波材料,令其与载体5a表面共形,从而改善金属腔体10反射对驻波造成的影响,最终实现了天线在中低频段驻波性能的改善,同时在不改变辐射单元形状的前提下改善天线的性能,实现共形效果。That is, when the L-shaped probe feed antenna is surrounded by an ideal electrical boundary, its performance at medium and low frequencies will be greatly deteriorated due to the strong reflection effect brought by the conductor boundary. A layer of wave-transmitting material is added above the radiation patch to make it conformal to the surface of the
根据本发明一种实施例,所述馈电结构为同轴线馈电结构,包括同轴设置的内导体9和外导体8,其中,所述内导体9与渐变型馈电探针6连接,外导体8与矩形地7连接。According to an embodiment of the present invention, the feed structure is a coaxial feed structure, including an
也即,渐变型馈电探针6下端连接内导体9进行馈电激励,渐变型馈电贴片4对上方的共形辐射单元3进行耦合馈电。同轴线馈电结构的外导体8连接矩形地7。That is, the lower end of the tapered feeding probe 6 is connected to the
本发明实施例中,同轴线馈电结构包括内导体9、外导体8和激励端口,外导体8依托于矩形地7部分,在矩形地7特定位置开孔,孔直径为9.2mm,同轴线外导体8与矩形地7相连接。内导体9上端与渐变型馈电探针6下端相连接,内导体9直径为4mm,长度为6mm,为预留给激励端口的长度,该长度不影响天线性能。同轴线馈电结构特性阻抗为50Ω。In the embodiment of the present invention, the coaxial feed structure includes an
较佳地,渐变型馈电探针6下端直径与内导体9直径同为4mm,渐变型馈电探针6的上端直径为12mm,高度为27.105mm。渐变型馈电贴片4连接渐变型馈电探针6端的宽度为12mm,远端宽度为3mm,长度为19mm。Preferably, the diameter of the lower end of the tapered feeding probe 6 and the diameter of the
较佳地,所述共形辐射单元3和寄生辐射单元2在腔体10底面的投影均为矩形。Preferably, the projections of the
在本实施例中,共形辐射单元3为理想导体,下方由渐变型馈电贴片4进行耦合馈电激励。共形辐射单元3与天线罩1共形,即共形辐射单元3的形状为矩形弧面,在沿金属腔体10方向上的投影面为矩形,其伸展后尺寸为55mm*35mm。In this embodiment, the
在本实施例中,寄生辐射单元2为理想导体,其水平高度与共形辐射贴片相同,二者中心距离为89.5mm。寄生辐射单元2与天线罩1共形,为矩形弧面,其伸展后尺寸为60mm*39mm。In this embodiment, the parasitic radiation element 2 is an ideal conductor, and its level is the same as that of the conformal radiation patch, and the center distance between the two is 89.5 mm. The parasitic radiating element 2 is conformal to the
此外,上述实施例中的矩形地7尺寸可以为150mm*150mm,可作为天线的参考地。In addition, the size of the rectangular ground 7 in the above embodiment can be 150mm*150mm, which can be used as the reference ground of the antenna.
如图1-2所示,根据本发明另一实施例,提供一种低剖面宽带共形天线阵列,该低剖面宽带共形天线阵列包括多个上述的低剖面宽带共形天线单元。As shown in FIGS. 1-2 , according to another embodiment of the present invention, a low-profile broadband conformal antenna array is provided, and the low-profile broadband conformal antenna array includes a plurality of the above-mentioned low-profile broadband conformal antenna units.
也即,本发明实施例还进一步基于该天线单元构造了天线阵列,为高精度的测向奠定基础。That is, the embodiment of the present invention further constructs an antenna array based on the antenna unit, which lays a foundation for high-precision direction finding.
较佳地,所述天线阵列中,多个低剖面宽带共形天线单元的载体5a为一体结构5。Preferably, in the antenna array, the
也即,多个低剖面宽带共形天线单元的多个载体5a均属于所述一体结构5的一部分,多个载体5a共同构成一体结构5,该一体结构5作为整个阵列的载体,如图1-2所示的,类圆柱的一体结构5,类圆柱的半径大致为300mm。That is, the
在上述实施例中,为了实现侧向天线阵,所述天线阵列包括的多个单元结构11划分为第一组和第二组,其中,第一组包括多个单元结构11,第二组也包括多个单元结构11,第一组的多个单元结构11和第二组的多个单元结构11均沿一体结构5的第一方向间隔设置,第一组的多个单元结构11和第二组的多个单元结构11还相对设置在一体结构5的两侧并一一对应设置。In the above embodiment, in order to realize a lateral antenna array, the plurality of
也即,该天线阵列包括了一体结构5,该一体结构5上具有两组腔体10,每一组腔体10均包括多个沿一体结构5的第一方向间隔设置的多个腔体10,两组腔体10对称设置在一体结构5的两侧,其中一组腔体10的多个腔体10作为第一组的多个单元结构11的安装环境,另一组腔体10的多个腔体10作为第二组的多个单元结构11的安装环境,连接关系与上述天线单元保持一致。That is, the antenna array includes an
举例来说,所述第一方向可以为一体结构5的轴线方向。For example, the first direction may be the axial direction of the
如图4所示,本发明L型渐变探针馈电共形天线单元在大于25%的相对带宽内驻波均小于3.0。As shown in FIG. 4 , the standing wave of the L-shaped gradient probe-fed conformal antenna unit of the present invention is less than 3.0 in the relative bandwidth greater than 25%.
如图5所示,本发明L型渐变探针馈电共形天线单元在低频f1处俯仰角范围-15°-15°范围,方位角45-135°范围内,最小增益为0.78dBi。(三条曲线自上而下分别为俯15度、仰5度、仰15度)As shown in FIG. 5 , the L-shaped gradient probe-fed conformal antenna unit of the present invention has a minimum gain of 0.78dBi in the pitch angle range of -15°-15° and the azimuth angle of 45°-135° at the low frequency f1. (The three curves from top to bottom are 15 degrees in pitch, 5 degrees in elevation, and 15 degrees in elevation)
如图6所示,本发明L型渐变探针馈电共形天线单元在中频f2处俯仰角范围-15°-15°范围,方位角45-135°范围内,最小增益为1.82dBi。(三条曲线自上而下分别为俯15度、仰5度、仰15度)As shown in FIG. 6 , the L-shaped gradient probe-fed conformal antenna unit of the present invention has a minimum gain of 1.82dBi in the pitch angle range of -15°-15° and the azimuth angle of 45°-135° at the intermediate frequency f2. (The three curves from top to bottom are 15 degrees in pitch, 5 degrees in elevation, and 15 degrees in elevation)
如图7所示,本发明L型渐变探针馈电共形天线单元在高频f3处俯仰角范围-15°-15°范围,方位角45-135°范围内,最小增益为0.76dBi。(三条曲线自上而下分别为俯15度、仰5度、仰15度)As shown in FIG. 7 , the L-shaped gradient probe-fed conformal antenna unit of the present invention has a minimum gain of 0.76dBi in the pitch angle range of -15°-15° and the azimuth angle of 45°-135° at high frequency f3. (The three curves from top to bottom are 15 degrees in pitch, 5 degrees in elevation, and 15 degrees in elevation)
综上,本发明的目的是提供了一种侧向单元宽角域、高增益、小型化,且与载体表面共形的侧向天线,在所要求的频段内在特定侧向角度范围内满足低驻波和高增益、宽带宽的需求,进一步基于该天线构造了天线阵,为高精度的测向奠定基础。To sum up, the purpose of the present invention is to provide a lateral unit with wide-angle range, high gain, miniaturization, and a lateral antenna conformal to the surface of the carrier, which satisfies the requirement of low frequency within a specific lateral angle range within the required frequency band. The requirements of standing wave, high gain and wide bandwidth further construct an antenna array based on this antenna, which lays the foundation for high-precision direction finding.
为了便于描述,在这里可以使用空间相对术语,如“在……之上”、“在……上方”、“在……上表面”、“上面的”等,用来描述如在图中所示的一个器件或特征与其他器件或特征的空间位置关系。应当理解的是,空间相对术语旨在包含除了器件在图中所描述的方位之外的在使用或操作中的不同方位。例如,如果附图中的器件被倒置,则描述为“在其他器件或构造上方”或“在其他器件或构造之上”的器件之后将被定位为“在其他器件或构造下方”或“在其他器件或构造之下”。因而,示例性术语“在……上方”可以包括“在……上方”和“在……下方”两种方位。该器件也可以其他不同方式定位(旋转90度或处于其他方位),并且对这里所使用的空间相对描述作出相应解释。For ease of description, spatially relative terms, such as "on", "over", "on the surface", "above", etc., may be used herein to describe what is shown in the figures. The spatial positional relationship of one device or feature shown to other devices or features. It should be understood that spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as "above" or "over" other devices or features would then be oriented "below" or "over" the other devices or features under other devices or constructions". Thus, the exemplary term "above" can encompass both an orientation of "above" and "below." The device may also be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptions used herein interpreted accordingly.
此外,需要说明的是,使用“第一”、“第二”等词语来限定零部件,仅仅是为了便于对相应零部件进行区别,如没有另行声明,上述词语并没有特殊含义,因此不能理解为对本发明保护范围的限制。In addition, it should be noted that the use of words such as "first" and "second" to define components is only for the convenience of distinguishing corresponding components. Unless otherwise stated, the above words have no special meaning and therefore cannot be understood to limit the scope of protection of the present invention.
以上所述仅为本发明的优选实施例而已,并不用于限制本发明,对于本领域的技术人员来说,本发明可以有各种更改和变化。凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included within the protection scope of the present invention.
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CN116093634A (en) * | 2022-12-08 | 2023-05-09 | 西北工业大学 | Antenna array for simultaneous transmission and reception of aircraft |
CN118281552A (en) * | 2024-04-09 | 2024-07-02 | 北京昊测科技有限公司 | L-band full-airspace coverage wing conformal antenna |
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