CN213278388U - S, C wave band dual-frequency radar jammer antenna - Google Patents

S, C wave band dual-frequency radar jammer antenna Download PDF

Info

Publication number
CN213278388U
CN213278388U CN202022401140.3U CN202022401140U CN213278388U CN 213278388 U CN213278388 U CN 213278388U CN 202022401140 U CN202022401140 U CN 202022401140U CN 213278388 U CN213278388 U CN 213278388U
Authority
CN
China
Prior art keywords
feed source
focus
antenna
band
feed
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
CN202022401140.3U
Other languages
Chinese (zh)
Inventor
杨树涛
张雯
朱战飞
徐海峰
苏沛伦
李显龙
周敏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Pla 63896
Original Assignee
Pla 63896
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.)
Filing date
Publication date
Application filed by Pla 63896 filed Critical Pla 63896
Priority to CN202022401140.3U priority Critical patent/CN213278388U/en
Application granted granted Critical
Publication of CN213278388U publication Critical patent/CN213278388U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

An S, C waveband double-frequency radar jammer antenna comprises a main reflecting surface, an auxiliary reflecting surface and a first feed source, wherein the distance between the focus of the first feed source and the second focus is 40 mm; the distance between the focus of the second feed source and the second focus is 10 mm; and the focal points of the first feed source and the second feed source are distributed on two sides of the second focal point, and the focal points of the first feed source and the second feed source are collinear with the second focal point. Adopt two independent double feed source designs, and the double feed source is the offset feed setting, not only can solve the isolation problem of combination feed source, cooperation ring focal antenna simultaneously, can guarantee that antenna gain and beam broadband homoenergetic satisfy the index requirement, through outer guide data, control servo revolving stage drive antenna and rotate, guarantee that the antenna can stably shine under narrow beam width by the interference target object, realize the promotion to current equipment effective radiation power, satisfy experimental and training task demand.

Description

S, C wave band dual-frequency radar jammer antenna
The technical field is as follows:
the utility model belongs to the technical field of the radar, what mainly related to is an S, C wave band dual-frenquency radar jammer antenna.
Background art:
in a test training task, an S-band or C-band radar interference device generally adopts a medium-low power transmitter to improve the mobility, and adopts a wide beam to meet the requirement of regional coverage interference. In practical application, the radar interference device has wide wave beams and limited radiation distance, is difficult to simulate a high-power radar interference source released at a long distance, and has limited capability of simulating S, C wave band complex electromagnetic environment.
The utility model has the following contents:
in order to overcome foretell not enough, the utility model provides an S, C wave band dual-frenquency radar jammer antenna is applied to S, C wave band radar jamming equipment effective radiation power's promotion, satisfies the remote demand that founds the complicated electromagnetic signal environment of S, C frequency channels in the experimental training.
The utility model provides a technical scheme that its technical problem adopted:
an S, C waveband dual-frequency radar jammer antenna comprises
The main reflecting surface is provided with a central axis AN and is formed by rotating AN arc BP around the central axis AN for a circle;
the auxiliary reflecting surface is formed by rotating AN elliptic arc TM around a central axis AN for a circle, one focus of AN ellipse where the elliptic arc TM is located is superposed with the focus of AN arc BP to form a first focus, and the other focus of the ellipse where the elliptic arc TM is located is a second focus;
the distance between the focus of the first feed source and the second focus is 40 mm;
the distance between the focus of the second feed source and the second focus is 10 mm;
and the focal points of the first feed source and the second feed source are distributed on two sides of the second focal point, and the focal points of the first feed source and the second feed source are collinear with the second focal point.
The first feed source and the second feed source are ridged horn antennas.
The first feed source is a low-frequency band S feed source, and the frequency band of the low-frequency band S feed source is 2GHz-4 GHz.
The second feed source is a high-frequency band C feed source, and the frequency band of the high-frequency band C feed source is 4GHz-8 GHz.
The tail parts of the first feed source and the second feed source are provided with feed source polarization joints, so that the polarization mode of the antenna is switched among horizontal polarization, vertical polarization and oblique polarization.
And the base of the main reflecting surface is provided with an azimuth and elevation servo joint.
Due to the adoption of the technical scheme, the utility model discloses have following superiority:
the utility model provides a pair of S, C wave band dual-frenquency radar jammer antenna, adopt two independent dual feed designs, and the dual feed is the offset feed setting, not only can solve the isolation problem of combination feed, cooperate the ring focal antenna simultaneously, can guarantee that antenna gain and beam broadband homoenergetic satisfy the index requirement, through outer guide data, control servo revolving stage drive antenna rotates, guarantee that the antenna can stably shine under narrow beam width by the interference target object, realize the promotion to current equipment effective radiation power, satisfy experimental and training task demand.
Description of the drawings:
fig. 1 is a cross-sectional view of the present invention;
fig. 2 is an antenna pattern when the S feed is 2GHz, the C feed is 8GHz, and phi =0 °;
fig. 3 is an antenna pattern for an S feed of 2GHz, a C feed of 8GHz, and phi =90 °;
in the figure: 1. a main reflective surface; 2. a first feed source; 3. a second feed source; 4. a sub-reflecting surface; 5. a first focal point; 6. a second focal point.
The specific implementation mode is as follows:
the present invention will be explained in more detail by the following examples, which are intended to protect all the changes and improvements within the scope of the present invention, and are not limited to the following examples;
the S, C waveband dual-band radar jammer antenna described in the attached drawings comprises a main reflecting surface 1, wherein the main reflecting surface 1 is provided with a central axis AN, and the main reflecting surface 1 is formed by rotating AN arc BP around the central axis AN for a circle; the auxiliary reflecting surface 4 is formed by rotating AN elliptic arc TM around a central axis AN for a circle, one focus of AN ellipse where the elliptic arc TM is located is superposed with a focus of AN arc BP to form a first focus 5, and the other focus of the ellipse where the elliptic arc TM is located is a second focus 6; in fact, the main reflecting surface 1 and the sub reflecting surface 4 form a ring focal antenna, and fig. 1 shows only a cross section, so that only one first focal point 5 is shown, and if the first focal point 5 is rotated by one circle according to the central axis AN, the track of the first focal point 5 encloses a circular ring;
the first feed source 2 is a low-frequency band S feed source, the frequency band of the low-frequency band S feed source is 2GHz-4GHz, and the distance between the focus O1 of the first feed source 2 and the second focus 6 is 40 mm;
the second feed source 3 is a high-frequency band C feed source, the frequency band of the high-frequency band C feed source is 4GHz-8GHz, and the distance between the focus O2 of the second feed source 3 and the second focus 6 is 10 mm;
wherein the focal point O1 of the first feed 3 and the focal point O2 of the second feed 4 are distributed on two sides of the second focal point 6, and the focal point O1 of the first feed 2 and the focal point O2 of the second feed 3 are collinear with the second focal point 6.
The first feed source 2 and the second feed source 3 are ridged horn antennas, and high gain of the antennas can be guaranteed.
The system adopts an offset feed design, takes a 4.5-meter caliber parabolic antenna as an example, a low-frequency S feed source sets 2GHz radiation frequency, and a high-frequency C feed source sets 8GHz radiation frequency for simulation.
According to fig. 2 and 3, the utility model adopts independent low-frequency S feed source and high-frequency C feed source, the dual-frequency combined feed source solves the problem of port isolation, and two paths of feed sources are designed according to the design mode, namely the distance between the focus O1 of the low-frequency S feed source and the second focus 6 is 40 mm; the distance between the focus O2 of the high-frequency band C feed source and the second focus 6 is 10mm, the gain of the low-frequency antenna is 36.26dB, the gain of the high-frequency antenna is 48.08dB, and the two are both greater than the minimum requirement of the antenna gain of 36 dB, so that the design requirement of the antenna can be met.
The tail parts of the first feed source 2 and the second feed source 3 are provided with feed source polarization joints, so that the polarization mode of the antenna is switched among horizontal polarization, vertical polarization and oblique polarization.
The base of the main reflecting surface 1 is provided with an azimuth and elevation servo joint.
And acquiring radar external guide data sent by the network switch, and controlling the rotation of the azimuth joint and the pitching joint of the pitching servo joint according to the information such as the position, the azimuth angle, the antenna posture and the like sent by the GPS of the antenna and the shaft angle encoder, so that the antenna accurately points to the target position and tracks in real time. According to task requirements; and the feed source polarization joint is controlled, so that the polarization mode of the antenna can be switched among horizontal polarization, vertical polarization and oblique polarization at will.
The details of the above are not described in detail since they are prior art.

Claims (6)

1. An S, C waveband double-frequency radar jammer antenna, characterized by: comprises that
The main reflecting surface is provided with a central axis AN and is formed by rotating AN arc BP around the central axis AN for a circle;
the auxiliary reflecting surface is formed by rotating AN elliptic arc TM around a central axis AN for a circle, one focus of AN ellipse where the elliptic arc TM is located is superposed with the focus of AN arc BP to form a first focus, and the other focus of the ellipse where the elliptic arc TM is located is a second focus;
the distance between the focus of the first feed source and the second focus is 40 mm;
the distance between the focus of the second feed source and the second focus is 10 mm;
and the focal points of the first feed source and the second feed source are distributed on two sides of the second focal point, and the focal points of the first feed source and the second feed source are collinear with the second focal point.
2. The S, C-band dual-band radar jammer antenna of claim 1, wherein: the first feed source and the second feed source are ridged horn antennas.
3. The S, C-band dual-band radar jammer antenna of claim 2, wherein: the first feed source is a low-frequency band S feed source, and the frequency band of the low-frequency band S feed source is 2GHz-4 GHz.
4. The S, C-band dual-band radar jammer antenna of claim 1, wherein: the second feed source is a high-frequency band C feed source, and the frequency band of the high-frequency band C feed source is 4GHz-8 GHz.
5. The S, C-band dual-band radar jammer antenna of claim 1 or 2, wherein: the tail parts of the first feed source and the second feed source are provided with feed source polarization joints, so that the polarization mode of the antenna is switched among horizontal polarization, vertical polarization and oblique polarization.
6. The S, C-band dual-band radar jammer antenna of claim 1, wherein: and the base of the main reflecting surface is provided with an azimuth and elevation servo joint.
CN202022401140.3U 2020-10-26 2020-10-26 S, C wave band dual-frequency radar jammer antenna Expired - Fee Related CN213278388U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202022401140.3U CN213278388U (en) 2020-10-26 2020-10-26 S, C wave band dual-frequency radar jammer antenna

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202022401140.3U CN213278388U (en) 2020-10-26 2020-10-26 S, C wave band dual-frequency radar jammer antenna

Publications (1)

Publication Number Publication Date
CN213278388U true CN213278388U (en) 2021-05-25

Family

ID=75951601

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202022401140.3U Expired - Fee Related CN213278388U (en) 2020-10-26 2020-10-26 S, C wave band dual-frequency radar jammer antenna

Country Status (1)

Country Link
CN (1) CN213278388U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113258284A (en) * 2021-06-10 2021-08-13 中国人民解放军海军工程大学 High-power microwave ring-focus dual-reflector antenna
WO2024031929A1 (en) * 2022-08-10 2024-02-15 胡关平 Bifocal combined parabolic antenna

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113258284A (en) * 2021-06-10 2021-08-13 中国人民解放军海军工程大学 High-power microwave ring-focus dual-reflector antenna
CN113258284B (en) * 2021-06-10 2021-11-23 中国人民解放军海军工程大学 High-power microwave ring-focus dual-reflector antenna
WO2024031929A1 (en) * 2022-08-10 2024-02-15 胡关平 Bifocal combined parabolic antenna

Similar Documents

Publication Publication Date Title
CN213278388U (en) S, C wave band dual-frequency radar jammer antenna
JP5450106B2 (en) In-vehicle antenna and method for transmitting and receiving signals
CA2572561C (en) Low profile antenna system and associated methods
CN108539418A (en) A kind of Phased Array Radar Antenna control system and method
JP5786244B2 (en) In-vehicle directional flat antenna, vehicle including such antenna, and satellite communication system including such vehicle
CN108701905A (en) A kind of electromagnetic horn
CN101587188A (en) Monopulse radar system based on time modulation antenna array
KR20070057615A (en) Mobile tri-band antenna system with low profile
KR101390168B1 (en) Electrically scanned tacan antenna
JP2022174706A (en) Spherical dual-polarization phased array weather radar
CN103904430A (en) Terahertz beam two-dimensional mechanical scanning antenna feed system
CN105390822A (en) Cylindrical integrated active phased-array antenna
CN104868255A (en) Ground multibeam electric controlled scanning measuring and controlling antenna for unmanned aerial vehicle
CN103022699A (en) Satellite-borne sparse phased-array multi-beam antenna with reflector
CN110444851A (en) Multi-beam off-set feed reflector antenna
US6677908B2 (en) Multimedia aircraft antenna
WO2021169926A1 (en) Antenna and radar system
CN205176270U (en) Holographic safety inspection appearance system of active microwave
CN202285045U (en) Angle tracking system
CN203617425U (en) Dual-linear-polarization satellite data transmission antenna device
CN112615682B (en) External calibration network for cylindrical two-dimensional active phased array
CN111541011B (en) Lens miniaturization antenna
CN210074129U (en) Multi-beam offset feed source reflector antenna
Pivit et al. Compact 60-GHz lens antenna with self-alignment feature for small cell backhaul
CN107706541B (en) A kind of supersonic speed missile-borne combined type omnidirectional telemetering antenna

Legal Events

Date Code Title Description
GR01 Patent grant
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: 20210525

Termination date: 20211026