CN205050984U - Spiral array antenna - Google Patents

Spiral array antenna Download PDF

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Publication number
CN205050984U
CN205050984U CN201520554475.5U CN201520554475U CN205050984U CN 205050984 U CN205050984 U CN 205050984U CN 201520554475 U CN201520554475 U CN 201520554475U CN 205050984 U CN205050984 U CN 205050984U
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CN
China
Prior art keywords
antenna element
antenna
utility
model
array
Prior art date
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Expired - Fee Related
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CN201520554475.5U
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Chinese (zh)
Inventor
冯赵
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Shaanxi Yongnuo Information Science & Technology Co Ltd
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Shaanxi Yongnuo Information Science & Technology Co Ltd
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Priority to CN201520554475.5U priority Critical patent/CN205050984U/en
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Publication of CN205050984U publication Critical patent/CN205050984U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a spiral array antenna, including the reflecting plate, install antenna element A, antenna element B, antenna element C and antenna element D on the reflecting plate, antenna element A, antenna element B, antenna element C and antenna element D are array and arrange, antenna element A, antenna element B, antenna element C and antenna element D are copper wire wound helical structure, respective the presenting of antenna element A, antenna element B, antenna element C and antenna element D a little utilizes 4 merits minute ware or 4 way couplers to combine together. The utility model discloses simple structure, reasonable in design utilizes array geometry to combine 4 group's antenna elements, has improved buff, has compensatied the shortcoming of the low gain of simple helical antenna. The utility model discloses low in cost, production simple process is fit for using on a large scale.

Description

A kind of helical array antenna
Technical field
The utility model relates to technical field of satellite navigation, specifically a kind of helical array antenna.
Background technology
Beidou satellite navigation system is global positioning satellite and the communication system of China's independent research.With GPS of America, Russian Ge Luonasi, European Union's Galileo system be called global four large satellite navigation system.At present, these 4 systems are confirmed as GPS (Global Position System) core supplier by the United Nations together.It changes the situation that China lacks high accuracy, in real time positioning means for a long time, break the U.S. and the Russia monopoly position in this field, can be China land, ocean, all kinds of military and civilians that are aerial and space provide multiple business guarantee, especially the modernization of raising China's national defense is had great significance.
China's Beidou satellite navigation system is the GPS (Global Position System) of China's independent research, autonomous operation, can be widely used in the every field of economic society, is the important space information infrastructure that country is building.This system is applied at numerous areas such as mapping, fishery, communications and transportation, telecommunications, water conservancy, forest fire protection, the mitigation disaster relief and national security, creates significant economic benefit and social benefit.
Since dipper system is towards since civilian, there is the hand-hold type Big Dipper terminal of the multiple frequency range of multiple compatibility; And the Big Dipper terminal that a compatible Big Dipper generation is received and dispatched, Beidou II receive frequency comprises such five frequencies of GPS frequency, because compatible frequency causes antenna size larger more, or the difficulty that minification increases making the spacing of cracking of antenna element less in production technology, hinders the broader applications of multifrequency dipper system.Current helical antenna gain is low, is unfavorable for that antenna carries out high accuracy use.
Utility model content
The purpose of this utility model is to provide a kind of helical array antenna, to solve the problem proposed in above-mentioned background technology.
For achieving the above object, the utility model provides following technical scheme:
A kind of helical array antenna, comprises reflecting plate; Described reflecting plate is provided with antenna element A, antenna element B, antenna element C and antenna element D, antenna element A, antenna element B, antenna element C and antenna element D are array arrangement.
As further program of the utility model: described antenna element A, antenna element B, antenna element C and antenna element D are the helical structure that copper wire is coiled into.
As the utility model further scheme: described antenna element A, antenna element B, antenna element C and antenna element D feedback point separately utilizes 4 power splitters or No. 4 couplers to combine.
Compared with prior art, the beneficial effects of the utility model are: the utility model structure is simple, reasonable in design, utilizes array format to combine 4 groups of antenna elements, improves gain effect, compensate for the shortcoming of simple helical antenna low gain.The utility model is cheap, and production technology is simple, is applicable to using on a large scale.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is vertical view of the present utility model.
In figure: 1-antenna element A, 2-antenna element B, 3-antenna element C, 4-antenna element D, 5-reflecting plate.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Refer to Fig. 1 ~ 2, a kind of helical array antenna, comprise reflecting plate 5; Described reflecting plate 5 is provided with antenna element A1, antenna element B2, antenna element C3 and antenna element D4, antenna element A1, antenna element B2, antenna element C3 and antenna element D4 are array arrangement.
Further, antenna element A1 described in the utility model, antenna element B2, antenna element C3 and antenna element D4 are the helical structure that copper wire is coiled into, and the parameters such as copper wire radius, the radius of spin and spacing regulate according to design frequency and determine.
Further, antenna element A1 described in the utility model, antenna element B2, antenna element C3 and antenna element D4 feedback point separately utilizes 4 power splitters or No. 4 couplers to combine.
The utility model coordinates and loads low noise amplifier and use, can the high-quality signal of stable output; Wider band designs demand can be met, comprise and be not limited only to GPS, the Big Dipper, Glonass and galileo satellite navigation system.
To those skilled in the art, obvious the utility model is not limited to the details of above-mentioned one exemplary embodiment, and when not deviating from spirit of the present utility model or essential characteristic, can realize the utility model in other specific forms.Therefore, no matter from which point, all should embodiment be regarded as exemplary, and be nonrestrictive, scope of the present utility model is limited by claims instead of above-mentioned explanation, and all changes be therefore intended in the implication of the equivalency by dropping on claim and scope are included in the utility model.Any Reference numeral in claim should be considered as the claim involved by limiting.
In addition, be to be understood that, although this specification is described according to execution mode, but not each execution mode only comprises an independently technical scheme, this narrating mode of specification is only for clarity sake, those skilled in the art should by specification integrally, and the technical scheme in each embodiment also through appropriately combined, can form other execution modes that it will be appreciated by those skilled in the art that.

Claims (3)

1. a helical array antenna, comprises reflecting plate (5); It is characterized in that: described reflecting plate (5) is provided with antenna element A (1), antenna element B (2), antenna element C (3) and antenna element D (4), antenna element A (1), antenna element B (2), antenna element C (3) and antenna element D (4) and arranges in array.
2. helical array antenna according to claim 1, is characterized in that: described antenna element A (1), antenna element B (2), antenna element C (3) and antenna element D (4) are the helical structure that copper wire is coiled into.
3. helical array antenna according to claim 1, is characterized in that: the respective feedback point of described antenna element A (1), antenna element B (2), antenna element C (3) and antenna element D (4) utilizes 4 power splitters or No. 4 couplers to combine.
CN201520554475.5U 2015-07-28 2015-07-28 Spiral array antenna Expired - Fee Related CN205050984U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520554475.5U CN205050984U (en) 2015-07-28 2015-07-28 Spiral array antenna

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520554475.5U CN205050984U (en) 2015-07-28 2015-07-28 Spiral array antenna

Publications (1)

Publication Number Publication Date
CN205050984U true CN205050984U (en) 2016-02-24

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520554475.5U Expired - Fee Related CN205050984U (en) 2015-07-28 2015-07-28 Spiral array antenna

Country Status (1)

Country Link
CN (1) CN205050984U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017161959A1 (en) * 2016-03-23 2017-09-28 上海航天测控通信研究所 Fixed multibeam stereoscopic helical antenna array and helical antenna flexible support device thereof
CN114389040A (en) * 2022-01-21 2022-04-22 河源广工大协同创新研究院 High-gain omnidirectional circularly polarized array antenna based on array element coupling

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017161959A1 (en) * 2016-03-23 2017-09-28 上海航天测控通信研究所 Fixed multibeam stereoscopic helical antenna array and helical antenna flexible support device thereof
CN114389040A (en) * 2022-01-21 2022-04-22 河源广工大协同创新研究院 High-gain omnidirectional circularly polarized array antenna based on array element coupling
CN114389040B (en) * 2022-01-21 2024-10-15 河源广工大协同创新研究院 High-gain omnidirectional circularly polarized array antenna based on array element coupling

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160224

Termination date: 20200728