WO2021104012A1 - Antenna and aircraft - Google Patents

Antenna and aircraft Download PDF

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Publication number
WO2021104012A1
WO2021104012A1 PCT/CN2020/127932 CN2020127932W WO2021104012A1 WO 2021104012 A1 WO2021104012 A1 WO 2021104012A1 CN 2020127932 W CN2020127932 W CN 2020127932W WO 2021104012 A1 WO2021104012 A1 WO 2021104012A1
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WO
WIPO (PCT)
Prior art keywords
arm
circuit board
antenna
transmission line
away
Prior art date
Application number
PCT/CN2020/127932
Other languages
French (fr)
Chinese (zh)
Inventor
谭杰洪
Original Assignee
深圳市道通智能航空技术股份有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Priority claimed from CN201922078759.2U external-priority patent/CN211428332U/en
Priority claimed from CN201911185074.6A external-priority patent/CN111029719A/en
Application filed by 深圳市道通智能航空技术股份有限公司 filed Critical 深圳市道通智能航空技术股份有限公司
Publication of WO2021104012A1 publication Critical patent/WO2021104012A1/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/36Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/22Supports; Mounting means by structural association with other equipment or articles
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/27Adaptation for use in or on movable bodies
    • H01Q1/28Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/36Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith
    • H01Q1/38Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewith formed by a conductive layer on an insulating support
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/48Earthing means; Earth screens; Counterpoises
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/50Structural association of antennas with earthing switches, lead-in devices or lightning protectors

Definitions

  • the present invention relates to the field of communication, in particular to an antenna and an aircraft.
  • antennas are an important element in the field of wireless communication.
  • large-size antennas occupy a larger space and are inconvenient to install.
  • the antennas used by drones need to meet the characteristics of small size and uniform omnidirectional radiation.
  • the purpose of the present invention is to provide an antenna and an aircraft to reduce the size of the antenna and achieve uniform omnidirectional radiation.
  • the present invention provides an antenna including a substrate, a circuit board provided on the substrate, a first radiation portion provided on one side of the substrate, and a second radiation portion provided on the other side of the substrate.
  • the first radiating part is provided with a feeding point, the first radiating part is electrically connected to the circuit board through the feeding point;
  • the second radiating part is provided with a grounding point, the first The two radiating parts are electrically connected to the circuit board through the ground point.
  • the first radiating part includes a first transmission line, a first connecting arm connected to an end of the first transmission line away from the circuit board in the middle, and an end connected to the first connecting arm and facing the circuit board
  • a first vibrator arm extending on one side of the first connecting arm and a second vibrator arm extending toward one side of the circuit board connected to the other end of the first connecting arm, and the feeding point is provided on the first transmission line.
  • the first transmission line includes an extension part and a feeding part connected to the extension part, the feeding point is provided at an end of the feeding part away from the extension part, and the feeding part is far away One end of the extension part is pointed.
  • first vibrator arm and the second vibrator arm are symmetrically arranged with respect to the first transmission line.
  • the distance between the first dipole arm and the circuit board is 1/16 to 1 of the resonant wavelength of the antenna, and the distance between the second dipole arm and the circuit board is the 1/16 to 1 of the resonant wavelength of the antenna.
  • the second radiating portion includes a second transmission line, a second connecting arm at an end of the second transmission line away from the circuit board in the middle, and an end connected to the second connecting arm and facing away from the circuit.
  • a third vibrator arm extending from one side of the board and a fourth vibrator arm connected to the other end of the second connecting arm and extending toward the side away from the circuit board, the grounding point is set on the second transmission line on.
  • the second radiating portion further includes a fifth dipole arm connected to an end of the third dipole arm away from the second connecting arm and extending toward the side of the fourth dipole arm, and connected to The sixth vibrator arm extending from one end of the fourth vibrator arm away from the second connecting arm and toward the side of the third vibrator arm.
  • the third vibrator arm and the fourth vibrator arm are arranged symmetrically with respect to a line where the midpoint of the ground point and the midpoint of the second connecting arm are located.
  • the antenna further includes a first shielding plate arranged on one side of the circuit board and a second shielding plate arranged on the other side of the circuit board.
  • the present invention also provides an aircraft including a fuselage, a landing gear arranged below the fuselage, and the above-mentioned antenna, and the antenna is arranged in the landing gear.
  • the beneficial effect of the present invention is that by providing a circuit board on a substrate, a first radiation portion and a second radiation portion are respectively provided on both sides of the substrate, and the first radiation portion is electrically connected to the circuit board through the feeding point. Connected, the second radiating part is electrically connected to the circuit board through the grounding point, the circuit board and the antenna are integrated design, the antenna structure is simplified, the antenna volume is reduced, and the omnidirectional uniform radiation of the antenna can be realized.
  • FIG. 1 is a schematic diagram of the front structure of an antenna provided by an embodiment of the present invention.
  • FIG. 2 is a schematic diagram of the back structure of the antenna provided by the first embodiment of the present invention.
  • FIG. 3 is a schematic diagram of the rear structure of the antenna of the first embodiment of the second embodiment of the present invention.
  • FIG. 4 is a schematic diagram of the rear structure of the antenna of the second embodiment of the second embodiment of the present invention.
  • FIG. 5 is a schematic diagram of the back structure of the antenna of the third embodiment of the second embodiment of the present invention.
  • FIG. 6 is a diagram of S parameters of an antenna provided by an embodiment of the present invention.
  • FIG. 7 is a directional diagram of an antenna provided by an embodiment of the present invention.
  • Fig. 8 is a schematic diagram of an aircraft provided by an embodiment of the present invention.
  • the antenna 10 provided by the embodiment of the present invention includes a substrate 1, a circuit board 2 provided on the substrate 1, a first radiating portion 3 provided on one side of the substrate 1, and another The second radiating part 4 on the side; the first radiating part 3 is provided with a feeding point 31, and the first radiating part 3 is electrically connected to the circuit board 2 through the feeding point 31; the second radiating part 4 is provided with a grounding point 41, The second radiating part 4 is electrically connected to the circuit board 2 through the ground point 41.
  • the circuit board 2, the first radiating part 3, and the second radiating part 4 are integrated to design, simplify the structure of the antenna 10, reduce the size of the antenna 10, and realize the omnidirectional uniform radiation of the antenna.
  • the first radiating part 3 includes a first transmission line 32, a first connecting arm 33 connected to the first transmission line 32 at an end away from the circuit board 2 in the middle, and an end connected to the first connecting arm 33 and facing the circuit board 2.
  • a first vibrator arm 34 extending on one side of the first connecting arm 33 and a second vibrator arm 35 extending toward one side of the circuit board 2 connected to the other end of the first connecting arm 33, and the feeding point 31 is provided on the first transmission line 32.
  • the first transmission line 32 includes an extension portion 321 and a feeding portion 322 connected to the extension portion 321.
  • the feeding point 31 is provided at an end of the feeding portion 322 away from the extension portion 321, and the feeding portion 322 is away from the extension portion 321.
  • One end is pointed.
  • the feeding point 31 is provided at the tip of the feeding portion 322, and the tip of the feeding portion 322 is electrically connected to the circuit board 2 to realize feeding.
  • the first transmission line 32 is disposed at the center line of the substrate 1, and the first dipole arm 34 and the second dipole arm 35 are symmetrically disposed with respect to the first transmission line 32.
  • the size of the first dipole arm 34 and the second dipole arm 35 is 1/8 to 3/4 of the antenna resonance wavelength.
  • the distance between the first dipole arm 34 and the circuit board 2 is 1/16 to 1 of the resonant wavelength of the antenna, and the distance between the second dipole arm 35 and the circuit board 2 is 1/16 to 1 of the resonant wavelength of the antenna.
  • the second radiating part 4 includes a second transmission line 42, a second connecting arm 43 at an end far away from the circuit board 2 connected to the second transmission line 42 in the middle, and connected to the second connecting arm 43 one end and the third vibrator arm 44 extending toward the side away from the circuit board 2 and the fourth vibrator arm 45 connected to the other end of the second connecting arm 43 and extending toward the side away from the circuit board 2, the ground point 41 is set On the second transmission line 42. Specifically, the ground point 41 is provided at an end of the second transmission line 42 away from the second connecting arm 43, and the end of the second transmission line 42 is soldered to the circuit board 2.
  • the second connecting arm 43 and the first connecting arm 33 are respectively arranged on both sides of the substrate 1 and arranged symmetrically with respect to the substrate 1. In another embodiment, the width of the second connecting arm 43 and the first connecting arm 33 may also be different.
  • the second radiating part 4 further includes a fifth dipole arm 46 connected to the end of the third dipole arm 44 away from the second connecting arm 43 and extending toward the side of the fourth dipole arm 45, and a connection At the end of the fourth vibrator arm 45 away from the second connecting arm 43 and the sixth vibrator arm 47 extending toward the side of the third vibrator arm 44, the fifth vibrator arm 46 and the sixth vibrator arm 47 are centered about the ground point 41 The point is symmetrically arranged with the line where the midpoint of the second connecting arm 43 is located.
  • the third vibrator arm 44 and the fourth vibrator arm 45 are arranged symmetrically with respect to a line where the midpoint of the ground point 41 and the midpoint of the second connecting arm 43 are located.
  • the size of the third dipole arm 44 and the fourth dipole arm 45 is 1/8 to 3/4 of the resonant wavelength of the antenna.
  • the second radiating part 4 includes a second transmission line 42 and a radiating sheet 48 connected to an end of the second transmission line 42 away from the circuit board 2.
  • the shape of the radiation sheet 48 is rectangular.
  • the shape of the radiation sheet 48 is a trapezoid.
  • the shape of the radiation sheet 48 is an ellipse.
  • the antenna 10 further includes a first shielding plate 5 arranged on one side of the circuit board 2 and a second shielding plate 6 arranged on the other side of the circuit board 2 to effectively reduce signal interference between the antenna 10 and other circuit modules.
  • FIG. 6 it is the S parameter diagram of the antenna 10. It can be seen that the antenna can achieve omnidirectional coverage at 5.5 GHz, and the maximum antenna radiation direction is in the horizontal direction.
  • the aircraft provided by the embodiment of the present invention includes a fuselage 20, a landing gear 30 provided under the fuselage 20, and the aforementioned antenna 10, and the antenna 10 is provided in the landing gear 30.
  • the antenna 10 is placed perpendicular to the body 20.
  • the bottom view of the aircraft is taken as an example to schematically show the installation position of the antenna 10.
  • the installation position of the antenna 10 in this embodiment is not limited to the installation position shown in FIG.
  • the installation position of the antenna 10 for signal transmission and reception may also be used.
  • the antenna 10 provided in the landing gear 30 of the aircraft broadens the wave width of the antenna 10 on the elevation plane, and the signal remains stable when the antenna is tilted. This reduces the influence of the aircraft's flight posture on communication during the flight process, and guarantees the communication of the aircraft during the flight.
  • the circuit board 2 is provided on the substrate 1, and the first radiating part 3 and the second radiating part 4 are respectively provided on both sides of the substrate 1, and the first radiating part 3 passes through the feeding point.
  • 31 is electrically connected to the circuit board 2
  • the second radiating part 4 is electrically connected to the circuit board 2 through the grounding point 41.
  • the circuit board 2 and the antenna 10 are designed integrally, which simplifies the antenna structure, reduces the antenna volume, and can realize the full antenna To uniform radiation.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Mechanical Engineering (AREA)
  • Details Of Aerials (AREA)

Abstract

Disclosed are an antenna and an aircraft. The antenna comprises a substrate, a circuit board disposed on the substrate, a first radiation part disposed on one side of the substrate, and a second radiation part disposed on the other side of the substrate. The first radiation part is provided with a feed point, and the first radiation part is electrically connected to the circuit board by means of the feed point. The second radiation part is provided with a grounding point, and the second radiation part is electrically connected to the circuit board by means of the grounding point. In the present invention, the circuit board and the antenna are integrally designed, the structure of the antenna is simplified, and the volume of the antenna is reduced, which can achieve the omnidirectional uniform radiation of the antenna.

Description

一种天线及飞行器Antenna and aircraft
本申请要求于2019年11月27日提交中国专利局、申请号为201922078759.2、申请名称为“一种天线及飞行器”的中国专利申请的优先权,其全部内容通过引用结合在本申请中。This application claims the priority of a Chinese patent application filed with the Chinese Patent Office on November 27, 2019, with application number 201922078759.2 and application titled "An Antenna and Aircraft", the entire content of which is incorporated into this application by reference.
技术领域Technical field
本发明涉及通讯领域,尤其涉及一种天线及飞行器。The present invention relates to the field of communication, in particular to an antenna and an aircraft.
背景技术Background technique
目前,天线是无线通信领域的重要元件,随着无人机的发展,大尺寸的天线占用空间较大,安装不方便,无人机使用的天线需要满足体积小、全向均匀辐射的特点。At present, antennas are an important element in the field of wireless communication. With the development of drones, large-size antennas occupy a larger space and are inconvenient to install. The antennas used by drones need to meet the characteristics of small size and uniform omnidirectional radiation.
发明内容Summary of the invention
为了克服现有技术的天线尺寸较大的问题,本发明的目的在于提供一种天线及飞行器,以缩小天线体积,且实现全向均匀辐射。In order to overcome the problem of the large size of the antenna in the prior art, the purpose of the present invention is to provide an antenna and an aircraft to reduce the size of the antenna and achieve uniform omnidirectional radiation.
为了实现上述目的,本发明提供一种天线,包括基板、设于所述基板上的电路板、设于所述基板一侧的第一辐射部和设于所述基板另一侧的第二辐射部;所述第一辐射部上设有馈电点,所述第一辐射部通过所述馈电点与所述电路板电连接;所述第二辐射部上设有接地点,所述第二辐射部通过所述接地点与所述电路板电连接。In order to achieve the above objective, the present invention provides an antenna including a substrate, a circuit board provided on the substrate, a first radiation portion provided on one side of the substrate, and a second radiation portion provided on the other side of the substrate. Part; the first radiating part is provided with a feeding point, the first radiating part is electrically connected to the circuit board through the feeding point; the second radiating part is provided with a grounding point, the first The two radiating parts are electrically connected to the circuit board through the ground point.
进一步地,所述第一辐射部包括第一传输线、中部连接于所述第一传输线之远离所述电路板一端的第一连接臂、连接于所述第一连接臂一端且朝向所述电路板的一侧延伸的第一振子臂以及连接于所述第一连接臂另一端且朝向所述 电路板的一侧延伸的第二振子臂,所述馈电点设于所述第一传输线上。Further, the first radiating part includes a first transmission line, a first connecting arm connected to an end of the first transmission line away from the circuit board in the middle, and an end connected to the first connecting arm and facing the circuit board A first vibrator arm extending on one side of the first connecting arm and a second vibrator arm extending toward one side of the circuit board connected to the other end of the first connecting arm, and the feeding point is provided on the first transmission line.
进一步地,所述第一传输线包括延伸部和与所述延伸部连接的馈电部,所述馈电点设于所述馈电部远离所述延伸部的一端,且所述馈电部远离所述延伸部的一端呈尖端状。Further, the first transmission line includes an extension part and a feeding part connected to the extension part, the feeding point is provided at an end of the feeding part away from the extension part, and the feeding part is far away One end of the extension part is pointed.
进一步地,所述第一振子臂和所述第二振子臂关于所述第一传输线对称设置。Further, the first vibrator arm and the second vibrator arm are symmetrically arranged with respect to the first transmission line.
进一步地,所述第一振子臂与所述电路板之间的距离为所述天线的谐振波长的1/16~1,所述第二振子臂与所述电路板之间的距离为所述天线的谐振波长的1/16~1。Further, the distance between the first dipole arm and the circuit board is 1/16 to 1 of the resonant wavelength of the antenna, and the distance between the second dipole arm and the circuit board is the 1/16 to 1 of the resonant wavelength of the antenna.
进一步地,所述第二辐射部包括第二传输线、中部连接于所述第二传输线之远离所述电路板一端的第二连接臂、连接于所述第二连接臂一端且朝向背离所述电路板的一侧延伸的第三振子臂以及连接于所述第二连接臂另一端且朝向背离所述电路板的一侧延伸的第四振子臂,所述接地点设于所述第二传输线上。Further, the second radiating portion includes a second transmission line, a second connecting arm at an end of the second transmission line away from the circuit board in the middle, and an end connected to the second connecting arm and facing away from the circuit. A third vibrator arm extending from one side of the board and a fourth vibrator arm connected to the other end of the second connecting arm and extending toward the side away from the circuit board, the grounding point is set on the second transmission line on.
进一步地,所述第二辐射部还包括连接于所述第三振子臂之远离所述第二连接臂的一端且朝向所述第四振子臂一侧延伸的第五振子臂,以及连接于所述第四振子臂之远离所述第二连接臂的一端且朝向所述第三振子臂一侧延伸的第六振子臂。Further, the second radiating portion further includes a fifth dipole arm connected to an end of the third dipole arm away from the second connecting arm and extending toward the side of the fourth dipole arm, and connected to The sixth vibrator arm extending from one end of the fourth vibrator arm away from the second connecting arm and toward the side of the third vibrator arm.
进一步地,所述第三振子臂和所述第四振子臂关于所述接地点的中点与所述第二连接臂的中点所在的直线对称设置。Further, the third vibrator arm and the fourth vibrator arm are arranged symmetrically with respect to a line where the midpoint of the ground point and the midpoint of the second connecting arm are located.
进一步地,所述天线还包括设于所述电路板一侧的第一屏蔽板和设于所述电路板另一侧的第二屏蔽板。Further, the antenna further includes a first shielding plate arranged on one side of the circuit board and a second shielding plate arranged on the other side of the circuit board.
本发明还提供一种飞行器,所述飞行器包括机身、设于所述机身下方的起落架以及上述的天线,所述天线设置在所述起落架中。The present invention also provides an aircraft including a fuselage, a landing gear arranged below the fuselage, and the above-mentioned antenna, and the antenna is arranged in the landing gear.
相比现有技术,本发明的有益效果在于:通过在基板上设置电路板,在基板的两侧分别设置第一辐射部和第二辐射部,第一辐射部通过馈电点与电路板电连接,第二辐射部通过接地点与电路板电连接,将电路板和天线进行一体设计,简化天线结构,减小天线体积,且能实现天线的全向均匀辐射。Compared with the prior art, the beneficial effect of the present invention is that by providing a circuit board on a substrate, a first radiation portion and a second radiation portion are respectively provided on both sides of the substrate, and the first radiation portion is electrically connected to the circuit board through the feeding point. Connected, the second radiating part is electrically connected to the circuit board through the grounding point, the circuit board and the antenna are integrated design, the antenna structure is simplified, the antenna volume is reduced, and the omnidirectional uniform radiation of the antenna can be realized.
附图说明Description of the drawings
图1为本发明实施例提供的天线的正面结构示意图;FIG. 1 is a schematic diagram of the front structure of an antenna provided by an embodiment of the present invention;
图2为本发明第一实施例提供的天线的背面结构示意图;2 is a schematic diagram of the back structure of the antenna provided by the first embodiment of the present invention;
图3为本发明第二实施例的第一实施方式的天线的背面结构示意图;3 is a schematic diagram of the rear structure of the antenna of the first embodiment of the second embodiment of the present invention;
图4为本发明第二实施例的第二实施方式的天线的背面结构示意图;4 is a schematic diagram of the rear structure of the antenna of the second embodiment of the second embodiment of the present invention;
图5为本发明第二实施例的第三实施方式的天线的背面结构示意图;5 is a schematic diagram of the back structure of the antenna of the third embodiment of the second embodiment of the present invention;
图6为本发明实施例提供的天线的S参数图;FIG. 6 is a diagram of S parameters of an antenna provided by an embodiment of the present invention;
图7为本发明实施例提供的天线的方向图;FIG. 7 is a directional diagram of an antenna provided by an embodiment of the present invention;
图8为本发明实施例提供的飞行器的示意图。Fig. 8 is a schematic diagram of an aircraft provided by an embodiment of the present invention.
图中:10、天线;1、基板;2、电路板;3、第一辐射部;31、馈电点;32、第一传输线;321、延伸部;322、馈电部;33、第一连接臂;34、第一振子臂;35、第二振子臂;4、第二辐射部;41、接地点;42、第二传输线;43、第二连接臂;44、第三振子臂;45、第四振子臂;46、第五振子臂;47、第六振子臂;48、辐射片;5、第一屏蔽板;6、第二屏蔽板;20、机身;30、起落架。In the figure: 10. Antenna; 1. Substrate; 2. Circuit board; 3. First radiating part; 31. Feeding point; 32. First transmission line; 321. Extension; 322. Feeding part; 33. First 34, the first vibrator arm; 35, the second vibrator arm; 4. the second radiating part; 41, the ground point; 42, the second transmission line; 43, the second connecting arm; 44, the third vibrator arm; 45. The fourth oscillator arm; 46. The fifth oscillator arm; 47. The sixth oscillator arm; 48. Radiation sheet; 5. The first shielding plate; 6. The second shielding plate; 20. The fuselage; 30. Landing gear.
具体实施方式Detailed ways
为了便于理解本发明,下面结合附图和具体实施例,对本发明进行更详细的说明。需要说明的是,当元件被表述“固定于”另一个元件,它可以直接在另一个元件上、或者其间可以存在一个或多个居中的元件。当一个元件被表述“连 接”另一个元件,它可以是直接连接到另一个元件、或者其间可以存在一个或多个居中的元件。本说明书所使用的术语“垂直的”、“水平的”、“左”、“右”以及类似的表述只是为了说明的目的。In order to facilitate the understanding of the present invention, the present invention will be described in more detail below with reference to the accompanying drawings and specific embodiments. It should be noted that when an element is expressed as being "fixed to" another element, it can be directly on the other element, or there may be one or more elements in between. When an element is said to be "connected" to another element, it can be directly connected to the other element, or there may be one or more intervening elements in between. The terms "vertical", "horizontal", "left", "right" and similar expressions used in this specification are for illustrative purposes only.
除非另有定义,本说明书所使用的所有的技术和科学术语与属于本发明的技术领域的技术人员通常理解的含义相同。本说明书中在本发明的说明书中所使用的术语只是为了描述具体的实施例的目的,不是用于限制本发明。本说明书所使用的术语“和/或”包括一个或多个相关的所列项目的任意的和所有的组合。Unless otherwise defined, all technical and scientific terms used in this specification have the same meaning as commonly understood by those skilled in the technical field of the present invention. The terms used in the specification of the present invention in this specification are only for the purpose of describing specific embodiments, and are not used to limit the present invention. The term "and/or" used in this specification includes any and all combinations of one or more related listed items.
下面,结合附图以及具体实施方式,对本发明做进一步描述,需要说明的是,在不相冲突的前提下,以下描述的各实施例之间或各技术特征之间可以任意组合形成新的实施例。In the following, the present invention will be further described with reference to the drawings and specific implementations. It should be noted that, provided that there is no conflict, the following embodiments or technical features can be combined to form new embodiments. .
如图1-2所示,本发明实施例提供的天线10,包括基板1、设于基板1上的电路板2、设于基板1一侧的第一辐射部3和设于基板1另一侧的第二辐射部4;第一辐射部3上设有馈电点31,第一辐射部3通过馈电点31与电路板2电连接;第二辐射部4上设有接地点41,第二辐射部4通过接地点41与电路板2电连接。将电路板2、第一辐射部3、第二辐射部4一体设计,简化天线10的结构,减小天线10的尺寸,且能实现天线的全向均匀辐射。As shown in Figures 1-2, the antenna 10 provided by the embodiment of the present invention includes a substrate 1, a circuit board 2 provided on the substrate 1, a first radiating portion 3 provided on one side of the substrate 1, and another The second radiating part 4 on the side; the first radiating part 3 is provided with a feeding point 31, and the first radiating part 3 is electrically connected to the circuit board 2 through the feeding point 31; the second radiating part 4 is provided with a grounding point 41, The second radiating part 4 is electrically connected to the circuit board 2 through the ground point 41. The circuit board 2, the first radiating part 3, and the second radiating part 4 are integrated to design, simplify the structure of the antenna 10, reduce the size of the antenna 10, and realize the omnidirectional uniform radiation of the antenna.
如图1所示,第一辐射部3包括第一传输线32、中部连接于第一传输线32之远离电路板2一端的第一连接臂33、连接于第一连接臂33一端且朝向电路板2的一侧延伸的第一振子臂34以及连接于第一连接臂33另一端且朝向电路板2的一侧延伸的第二振子臂35,馈电点31设于第一传输线32上。优选的,第一传输线32包括延伸部321和与延伸部321连接的馈电部322,馈电点31设于馈电部322远离延伸部321的一端,且馈电部322远离延伸部321的一端呈尖端 状。具体的,馈电点31设于馈电部322的尖端处,馈电部322的尖端与电路板2电连接以实现馈电。As shown in FIG. 1, the first radiating part 3 includes a first transmission line 32, a first connecting arm 33 connected to the first transmission line 32 at an end away from the circuit board 2 in the middle, and an end connected to the first connecting arm 33 and facing the circuit board 2. A first vibrator arm 34 extending on one side of the first connecting arm 33 and a second vibrator arm 35 extending toward one side of the circuit board 2 connected to the other end of the first connecting arm 33, and the feeding point 31 is provided on the first transmission line 32. Preferably, the first transmission line 32 includes an extension portion 321 and a feeding portion 322 connected to the extension portion 321. The feeding point 31 is provided at an end of the feeding portion 322 away from the extension portion 321, and the feeding portion 322 is away from the extension portion 321. One end is pointed. Specifically, the feeding point 31 is provided at the tip of the feeding portion 322, and the tip of the feeding portion 322 is electrically connected to the circuit board 2 to realize feeding.
在一种实施方式中,第一传输线32设于基板1的中线位置,第一振子臂34和第二振子臂35关于第一传输线32对称设置。第一振子臂34和第二振子臂35的尺寸为天线谐振波长的1/8~3/4。第一振子臂34与电路板2之间的距离为天线的谐振波长的1/16~1,第二振子臂35与电路板2之间的距离为天线的谐振波长的1/16~1。In one embodiment, the first transmission line 32 is disposed at the center line of the substrate 1, and the first dipole arm 34 and the second dipole arm 35 are symmetrically disposed with respect to the first transmission line 32. The size of the first dipole arm 34 and the second dipole arm 35 is 1/8 to 3/4 of the antenna resonance wavelength. The distance between the first dipole arm 34 and the circuit board 2 is 1/16 to 1 of the resonant wavelength of the antenna, and the distance between the second dipole arm 35 and the circuit board 2 is 1/16 to 1 of the resonant wavelength of the antenna.
如图2所示,在第一实施例中,第二辐射部4包括第二传输线42、中部连接于第二传输线42之远离电路板2一端的第二连接臂43、连接于第二连接臂43一端且朝向背离电路板2的一侧延伸的第三振子臂44以及连接于第二连接臂43另一端且朝向背离电路板2的一侧延伸的第四振子臂45,接地点41设于第二传输线42上。具体的,接地点41设于第二传输线42远离第二连接臂43的一端,第二传输线42的端部焊接于电路板2上。在一种实施方式中,第二连接臂43和第一连接臂33分别设于基板1的两侧且关于基板1对称设置。在另一实施方式中,第二连接臂43和第一连接臂33的宽度也可以不同。As shown in FIG. 2, in the first embodiment, the second radiating part 4 includes a second transmission line 42, a second connecting arm 43 at an end far away from the circuit board 2 connected to the second transmission line 42 in the middle, and connected to the second connecting arm 43 one end and the third vibrator arm 44 extending toward the side away from the circuit board 2 and the fourth vibrator arm 45 connected to the other end of the second connecting arm 43 and extending toward the side away from the circuit board 2, the ground point 41 is set On the second transmission line 42. Specifically, the ground point 41 is provided at an end of the second transmission line 42 away from the second connecting arm 43, and the end of the second transmission line 42 is soldered to the circuit board 2. In one embodiment, the second connecting arm 43 and the first connecting arm 33 are respectively arranged on both sides of the substrate 1 and arranged symmetrically with respect to the substrate 1. In another embodiment, the width of the second connecting arm 43 and the first connecting arm 33 may also be different.
在一种实施方式中,第二辐射部4还包括连接于第三振子臂44之远离第二连接臂43的一端且朝向第四振子臂45一侧延伸的第五振子臂46,以及连接于第四振子臂45之远离第二连接臂43的一端且朝向第三振子臂44一侧延伸的第六振子臂47,第五振子臂46和第六振子臂47关于接地点41的中点与第二连接臂43的中点所在的直线对称设置。In one embodiment, the second radiating part 4 further includes a fifth dipole arm 46 connected to the end of the third dipole arm 44 away from the second connecting arm 43 and extending toward the side of the fourth dipole arm 45, and a connection At the end of the fourth vibrator arm 45 away from the second connecting arm 43 and the sixth vibrator arm 47 extending toward the side of the third vibrator arm 44, the fifth vibrator arm 46 and the sixth vibrator arm 47 are centered about the ground point 41 The point is symmetrically arranged with the line where the midpoint of the second connecting arm 43 is located.
在一种实施方式中,第三振子臂44和第四振子臂45关于接地点41的中点与第二连接臂43的中点所在的直线对称设置。第三振子臂44和第四振子臂45的尺寸为天线的谐振波长的1/8~3/4。In an embodiment, the third vibrator arm 44 and the fourth vibrator arm 45 are arranged symmetrically with respect to a line where the midpoint of the ground point 41 and the midpoint of the second connecting arm 43 are located. The size of the third dipole arm 44 and the fourth dipole arm 45 is 1/8 to 3/4 of the resonant wavelength of the antenna.
如图3所示,在第二实施例中,第二辐射部4包括第二传输线42和连接于第二传输线42远离电路板2一端的辐射片48。如图3所示,在第一实施方式中,辐射片48的形状为矩形。如图4所示,在第二实施方式中,辐射片48的形状为梯形。如图5所示,在第三实施方式中,辐射片48的形状为椭圆形。As shown in FIG. 3, in the second embodiment, the second radiating part 4 includes a second transmission line 42 and a radiating sheet 48 connected to an end of the second transmission line 42 away from the circuit board 2. As shown in FIG. 3, in the first embodiment, the shape of the radiation sheet 48 is rectangular. As shown in FIG. 4, in the second embodiment, the shape of the radiation sheet 48 is a trapezoid. As shown in FIG. 5, in the third embodiment, the shape of the radiation sheet 48 is an ellipse.
优选的,天线10还包括设于电路板2一侧的第一屏蔽板5和设于电路板2另一侧的第二屏蔽板6,有效降低天线10与其他电路模块之间的信号干扰。Preferably, the antenna 10 further includes a first shielding plate 5 arranged on one side of the circuit board 2 and a second shielding plate 6 arranged on the other side of the circuit board 2 to effectively reduce signal interference between the antenna 10 and other circuit modules.
如图6所示,为天线10的S参数图,可以看出天线在5.5GHz均可实现全方向覆盖,并且天线辐射方向最大值在水平方向。As shown in FIG. 6, it is the S parameter diagram of the antenna 10. It can be seen that the antenna can achieve omnidirectional coverage at 5.5 GHz, and the maximum antenna radiation direction is in the horizontal direction.
如图7所示,为天线在5.5GHz的方向图,可以看出天线在5.5GHz实现全方向覆盖。As shown in Figure 7, it is the antenna pattern at 5.5GHz, and it can be seen that the antenna achieves omnidirectional coverage at 5.5GHz.
如图8所示,本发明实施例提供的飞行器,飞行器包括机身20、设于机身20下方的起落架30以及上述的天线10,天线10设置在起落架30中。其中,天线10垂直于机身20放置。As shown in FIG. 8, the aircraft provided by the embodiment of the present invention includes a fuselage 20, a landing gear 30 provided under the fuselage 20, and the aforementioned antenna 10, and the antenna 10 is provided in the landing gear 30. Wherein, the antenna 10 is placed perpendicular to the body 20.
本实施例中,以飞行器的仰视图为例示意性的示出了天线10的安装位置,本实施例中天线10的安装位置并不仅限于图8示出的安装位置,其他能够较好的满足信号收发的天线10的安装位置亦可。In this embodiment, the bottom view of the aircraft is taken as an example to schematically show the installation position of the antenna 10. The installation position of the antenna 10 in this embodiment is not limited to the installation position shown in FIG. The installation position of the antenna 10 for signal transmission and reception may also be used.
在飞行器的起落架30中设置的天线10,拓宽了天线10在俯仰面的波宽,在天线倾斜时信号保持稳定。从而使飞行器在飞行过程,减小飞行器的飞行姿势对通信的影响,保障飞行器在飞行过程中的通信。The antenna 10 provided in the landing gear 30 of the aircraft broadens the wave width of the antenna 10 on the elevation plane, and the signal remains stable when the antenna is tilted. This reduces the influence of the aircraft's flight posture on communication during the flight process, and guarantees the communication of the aircraft during the flight.
本发明实施例提供的天线10及飞行器,通过在基板1上设置电路板2,在基板1的两侧分别设置第一辐射部3和第二辐射部4,第一辐射部3通过馈电点31与电路板2电连接,第二辐射部4通过接地点41与电路板2电连接,将电路板2和天线10进行一体设计,简化天线结构,减小天线体积,且能实现天线的 全向均匀辐射。In the antenna 10 and the aircraft provided by the embodiment of the present invention, the circuit board 2 is provided on the substrate 1, and the first radiating part 3 and the second radiating part 4 are respectively provided on both sides of the substrate 1, and the first radiating part 3 passes through the feeding point. 31 is electrically connected to the circuit board 2, and the second radiating part 4 is electrically connected to the circuit board 2 through the grounding point 41. The circuit board 2 and the antenna 10 are designed integrally, which simplifies the antenna structure, reduces the antenna volume, and can realize the full antenna To uniform radiation.
上述实施方式仅为本发明的优选实施方式,不能以此来限定本发明保护的范围,本领域的技术人员在本发明的基础上所做的任何非实质性的变化及替换均属于本发明所要求保护的范围。The foregoing embodiments are only preferred embodiments of the present invention, and cannot be used to limit the scope of protection of the present invention. Any insubstantial changes and substitutions made by those skilled in the art on the basis of the present invention belong to the present invention. The scope of protection required.

Claims (10)

  1. 一种天线,其特征在于,包括基板、设于所述基板上的电路板、设于所述基板一侧的第一辐射部和设于所述基板另一侧的第二辐射部;所述第一辐射部上设有馈电点,所述第一辐射部通过所述馈电点与所述电路板电连接;所述第二辐射部上设有接地点,所述第二辐射部通过所述接地点与所述电路板电连接。An antenna, characterized by comprising a substrate, a circuit board provided on the substrate, a first radiation portion provided on one side of the substrate, and a second radiation portion provided on the other side of the substrate; A feeding point is provided on the first radiating part, and the first radiating part is electrically connected to the circuit board through the feeding point; a grounding point is provided on the second radiating part, and the second radiating part passes through The ground point is electrically connected to the circuit board.
  2. 根据权利要求1所述的天线,其特征在于,所述第一辐射部包括第一传输线、中部连接于所述第一传输线之远离所述电路板一端的第一连接臂、连接于所述第一连接臂一端且朝向所述电路板的一侧延伸的第一振子臂以及连接于所述第一连接臂另一端且朝向所述电路板的一侧延伸的第二振子臂,所述馈电点设于所述第一传输线上。The antenna according to claim 1, wherein the first radiating part comprises a first transmission line, a first connecting arm at an end far away from the circuit board that is connected to the first transmission line in the middle, and is connected to the first transmission line. A first vibrator arm extending toward one side of the circuit board at one end of the connecting arm, and a second vibrator arm extending toward the side of the circuit board connected to the other end of the first connecting arm, the feeder The point is set on the first transmission line.
  3. 根据权利要求2所述的天线,其特征在于,所述第一传输线包括延伸部和与所述延伸部连接的馈电部,所述馈电点设于所述馈电部远离所述延伸部的一端,且所述馈电部远离所述延伸部的一端呈尖端状。The antenna according to claim 2, wherein the first transmission line includes an extension part and a feeding part connected to the extension part, and the feeding point is provided at the feeding part away from the extension part One end of the power feeding part, and one end of the power feeding part away from the extension part is pointed.
  4. 根据权利要求2所述的天线,其特征在于,所述第一振子臂和所述第二振子臂关于所述第一传输线对称设置。The antenna according to claim 2, wherein the first dipole arm and the second dipole arm are symmetrically arranged with respect to the first transmission line.
  5. 根据权利要求2所述的天线,其特征在于,所述第一振子臂与所述电路板之间的距离为所述天线的谐振波长的1/16~1,所述第二振子臂与所述电路板之间的距离为所述天线的谐振波长的1/16~1。The antenna according to claim 2, wherein the distance between the first dipole arm and the circuit board is 1/16 to 1 of the resonant wavelength of the antenna, and the second dipole arm is connected to the circuit board. The distance between the circuit boards is 1/16 to 1 of the resonant wavelength of the antenna.
  6. 根据权利要求1所述的天线,其特征在于,所述第二辐射部包括第二传输线、中部连接于所述第二传输线之远离所述电路板一端的第二连接臂、连接于所述第二连接臂一端且朝向背离所述电路板的一侧延伸的第三振子臂以及连接于所述第二连接臂另一端且朝向背离所述电路板的一侧延伸的第四振子臂, 所述接地点设于所述第二传输线上。The antenna according to claim 1, wherein the second radiating part comprises a second transmission line, a second connecting arm at an end away from the circuit board in the middle connected to the second transmission line, and connected to the first transmission line. A third vibrator arm extending toward the side away from the circuit board at one end of the second connecting arm, and a fourth vibrator arm extending toward the side away from the circuit board connected to the other end of the second connecting arm, so The ground point is set on the second transmission line.
  7. 根据权利要求6所述的天线,其特征在于,所述第二辐射部还包括连接于所述第三振子臂之远离所述第二连接臂的一端且朝向所述第四振子臂一侧延伸的第五振子臂,以及连接于所述第四振子臂之远离所述第二连接臂的一端且朝向所述第三振子臂一侧延伸的第六振子臂。The antenna according to claim 6, wherein the second radiating portion further comprises an end connected to the third dipole arm away from the second connecting arm and facing the fourth dipole arm An extended fifth vibrator arm, and a sixth vibrator arm connected to an end of the fourth vibrator arm away from the second connecting arm and extending toward the third vibrator arm.
  8. 根据权利要求6所述的天线,其特征在于,所述第三振子臂和所述第四振子臂关于所述接地点的中点与所述第二连接臂的中点所在的直线对称设置。The antenna according to claim 6, wherein the third dipole arm and the fourth dipole arm are symmetrically arranged with respect to a line between the midpoint of the ground point and the midpoint of the second connecting arm. .
  9. 根据权利要求1-8任一项所述的天线,其特征在于,所述天线还包括设于所述电路板一侧的第一屏蔽板和设于所述电路板另一侧的第二屏蔽板。The antenna according to any one of claims 1-8, wherein the antenna further comprises a first shield plate arranged on one side of the circuit board and a second shield plate arranged on the other side of the circuit board board.
  10. 一种飞行器,其特征在于,所述飞行器包括机身、设于所述机身下方的起落架以及如权利要求1-9任一项所述的天线,所述天线设置在所述起落架中。An aircraft, characterized in that it comprises a fuselage, a landing gear arranged below the fuselage, and the antenna according to any one of claims 1-9, the antenna being arranged in the landing gear .
PCT/CN2020/127932 2019-11-27 2020-11-11 Antenna and aircraft WO2021104012A1 (en)

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