CN210665888U - Composite test system - Google Patents

Composite test system Download PDF

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Publication number
CN210665888U
CN210665888U CN201921515875.XU CN201921515875U CN210665888U CN 210665888 U CN210665888 U CN 210665888U CN 201921515875 U CN201921515875 U CN 201921515875U CN 210665888 U CN210665888 U CN 210665888U
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testing device
test system
composite test
test
testing
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CN201921515875.XU
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夏冬雪
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Shenzhen Rongsheng Technology Co Ltd
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Shenzhen Rongsheng Technology Co Ltd
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Abstract

The utility model relates to a compound test system, include: the device comprises a first testing device, a second testing device and a rotary table; the tested piece is arranged on the rotary table; the first testing device is used for measuring the radiation performance of the tested piece; the second testing device is a radar target simulation testing device; the second testing device is arranged in a region which can not be reached by the transmitting signal and the reflected signal of the first testing device. The utility model discloses the test environment with radiation performance test and radar target simulation test unites two into one, when avoiding the two all need test, is surveyed the repeated installation of piece in two test environment, improves efficiency of software testing, saves test space.

Description

Composite test system
Technical Field
The utility model relates to a technical field is measured to the microwave anechoic chamber, especially relates to a compound test system.
Background
At present, the test of the radiation performance of a tested piece and the simulation test of a radar target are realized by different test systems.
When the radiation performance test is carried out, the tested piece needs to be placed in a special test environment. When the radar target simulation is carried out, the tested piece needs to be transferred to another testing environment, or the current measuring environment is changed into the environment capable of measuring the radar target, so that the radar target measuring environment is simulated. Therefore, when the two performance indexes are detected on the same detected piece, time and labor are wasted, and efficiency is not high.
SUMMERY OF THE UTILITY MODEL
For overcoming the above-mentioned problem among the prior art to at least a certain extent, the utility model provides a compound test system.
The utility model provides a compound test system, include: the device comprises a first testing device, a second testing device and a rotary table;
the tested piece is arranged on the rotary table;
the first testing device is used for measuring the radiation performance of the tested piece;
the second testing device is a radar target simulation testing device;
the second testing device is arranged in a region which can not be reached by the transmitting signal and the reflected signal of the first testing device.
Furthermore, in the composite test system, the first test device, the turntable and the second test device are distributed in an L shape;
the rotary table is arranged at the corner of the L-shaped distribution;
the first testing device and the second testing device are respectively positioned at the free ends of the L-shaped distribution.
Further, in the composite test system, a wave absorbing structure is arranged between the first test device and the second test device.
Further, in the composite test system, the first test device is a test probe.
Further, in the above composite test system, the first test apparatus is a compact range test apparatus, including:
a feed source and a reflecting surface;
the feed source is arranged at the focus of the paraboloid curved surface of the reflecting surface.
Further, in the above composite test system, the second test apparatus includes at least one radar simulator.
Further, in the composite test system, the position of the radio frequency front end of at least one radar simulator in the at least one radar simulator is fixed; and the radio frequency front ends of the rest radar simulators can move along the arc-shaped sliding rail.
Further, in the composite test system, the radio frequency front end of the radar simulator can move along the arc-shaped slide rail.
Further, in the composite test system, the radio frequency front end of the radar simulator is a horn antenna.
Further, in the above-described composite test system, the first test apparatus, the second test apparatus, and the turntable are disposed in a darkroom; the darkroom is an L-shaped darkroom.
The utility model discloses among the combined test system, the revolving stage of piece is surveyed in first testing arrangement and the sharing of second testing arrangement, that is to say, the piece is surveyed on radiation performance testing arrangement and the revolving stage of radar target simulation testing arrangement sharing, unites two into one the test environment of radiation performance testing and radar target simulation testing, when avoiding the two all need test, is surveyed the repeated installation of piece in two test environment, improves efficiency of software testing, saves test space.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention as claimed.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the invention and together with the description, serve to explain the principles of the invention.
FIG. 1 is a schematic structural diagram of an embodiment of the composite test system of the present invention;
3 FIG. 32 3 is 3 a 3 view 3 in 3 the 3 direction 3 of 3 A 3- 3 A 3 of 3 the 3 embodiment 3 of 3 the 3 composite 3 test 3 system 3 shown 3 in 3 FIG. 31 3, 3 showing 3 a 3 front 3 view 3 of 3 a 3 first 3 test 3 device 3; 3
FIG. 3 is a top view of a first testing device in an embodiment of the composite testing system of the present invention;
FIG. 4 is a view of an embodiment of the composite test system shown in FIG. 1, taken in the direction B-B, and shown in front view in a second test setup;
fig. 5 is a top view of a second testing device in an embodiment of the composite testing system of the present invention.
Wherein:
1 rotating platform
2 arc slide rail
31 first radar simulator radio frequency front end
32 second radar simulator radio frequency front end
4 holding pole
5 feed source
6 reflective surface
7 darkroom
Detailed Description
It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
Referring to fig. 1-5, a preferred embodiment of the composite test system of the present invention is shown.
Referring to fig. 1, the composite test system of the present embodiment includes: a first testing device, a second testing device and a turntable 1. The measured piece is arranged on the rotary table 1. The first testing device is used for measuring the radiation performance of the tested piece; the second testing device is a radar target simulation testing device. The second testing device is arranged in an area which can not be reached by the transmission signal and the reflection signal of the first testing device.
Referring to fig. 2 and 3, in the present embodiment, the first testing device is a compact range testing device, and includes a feed source 5 and a reflecting surface 6; the feed antenna of the feed 5 is disposed at the focus of the parabolic curved surface of the reflecting surface 6. The paraboloid curved surface of the reflecting surface receives spherical waves sent by the feed source, and the spherical waves are converted into plane waves after being reflected and sent to a quiet area in a compact range.
Of course, the first testing device is not limited to the compact field testing device, and may be a direct field testing device, that is, an antenna probe is used for testing. The utility model discloses do not limit to this.
Referring to fig. 4 and 5, in the present embodiment, the second testing device includes a first radar simulator and a second radar simulator, a first radio frequency front end 31 of the first radar simulator is fixedly connected to the holding pole 4, and a second radio frequency front end 32 of the second radar simulator is also fixedly connected to the other holding pole 4. The holding pole 4 where the second radio frequency front end 32 is located can move along the arc-shaped slide rail 2.
When the second testing device is used, the arc-shaped slide rail 2 enables the second radio frequency front end 32 of the second radar simulator to move with a track as an arc by taking the tested piece as a circle center. By means of the arc-shaped slide rail 2, the specific angle of the second radio frequency front end 32 can be always ensured to be aligned with the tested piece. Therefore, when the input power of the second rf front end 32 is stable, the gain is also stable; the space loss of the electromagnetic wave at a fixed distance is fixed under the same environment, and finally the power received by the tested piece is also stable.
In addition, the second rf front-end 31 and the second rf front-end 32 are in signal connection with a radar simulator located outside the darkroom 7. The radar simulator is connected with a PC as an upper computer. The control of each radar simulator, the rotary table and the like is realized by means of a good graphical user interface of the PC.
Referring to fig. 1 again, in the present embodiment, the first testing device, the turntable and the second testing device are distributed in an L shape. The turntable 1 is arranged at the corners of the L-shaped distribution. The first testing device and the second testing device are respectively positioned at the free ends of the L-shaped distribution. As can be seen from fig. 1, the first rf front end 31 of the first radar simulator, the second rf front end 32 of the second radar simulator, the holding pole 4, and the slide rail 2 are all located at one free end of the L-shaped distribution, and the reflective surface 6 and the feed source 5 of the second testing device are located at the other free end of the L-shaped distribution
In order to arrange the second testing device in the area where neither the transmission signal nor the reflection signal of the first testing device can reach, a wave-absorbing structure is preferably arranged between the first testing device and the second testing device.
It should be noted that the second testing apparatus in the present embodiment includes two radar simulators, but the present invention is not limited thereto. It is also possible to include only one radar simulator, or a plurality of radar simulators. If a plurality of radar simulators are included, the position of the radio-frequency front end of at least one radar simulator is fixed, and the radio-frequency front ends of the rest radar simulators can move along the arc-shaped sliding rail; and the radio frequency front ends of all the radar simulators can move along the arc-shaped slide rail. In one embodiment, the radio frequency front end of the radar simulator is a horn antenna, and the sliding type of the rest of the holding poles fixedly connected with the horn antenna is realized by sliding the holding poles on the arc-shaped sliding rail.
The utility model discloses a first testing arrangement, second testing arrangement and revolving stage in the embodiment set up in the darkroom, and the darkroom also can be designed into L type darkroom, and the wall of darkroom is provided with absorbing structure.
The utility model discloses among the combined test system, the revolving stage of piece is surveyed in first testing arrangement and the sharing of second testing arrangement, that is to say, the piece is surveyed on radiation performance testing arrangement and the revolving stage of radar target simulation testing arrangement sharing, unites two into one the test environment of radiation performance testing and radar target simulation testing, when avoiding the two all need test, is surveyed the repeated installation of piece in two test environment, improves efficiency of software testing, saves test space.
In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
Although embodiments of the present invention have been shown and described, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and that variations, modifications, substitutions and alterations can be made to the above embodiments by those of ordinary skill in the art without departing from the scope of the present invention.

Claims (10)

1. A composite test system, comprising:
the device comprises a first testing device, a second testing device and a rotary table;
the tested piece is arranged on the rotary table;
the first testing device is used for measuring the radiation performance of the tested piece;
the second testing device is a radar target simulation testing device;
the second testing device is arranged in a region which can not be reached by the transmitting signal and the reflected signal of the first testing device.
2. The composite test system of claim 1,
the first testing device, the rotary table and the second testing device are distributed in an L shape;
the rotary table is arranged at the corner of the L-shaped distribution;
the first testing device and the second testing device are respectively positioned at the free ends of the L-shaped distribution.
3. The composite test system of claim 2,
and a wave absorbing structure is arranged between the first testing device and the second testing device.
4. The composite test system of claim 3,
the first testing device is a testing probe.
5. The composite test system of claim 3,
the first testing device is a compact range testing device comprising:
a feed source and a reflecting surface;
the feed source is arranged at the focus of the paraboloid curved surface of the reflecting surface.
6. Composite test system according to claim 4 or 5,
the second testing device comprises at least one radar simulator.
7. The composite test system of claim 6,
in the at least one radar simulator, the position of the radio frequency front end of the at least one radar simulator is fixed; and the radio frequency front ends of the rest radar simulators can move along the arc-shaped sliding rail.
8. The composite test system of claim 6,
the radio frequency front end of the radar simulator can move along the arc-shaped sliding rail.
9. The composite test system of claim 6,
the radio frequency front end of the radar simulator is a horn antenna.
10. The composite test system of claim 2,
the first testing device, the second testing device and the rotary table are arranged in a darkroom;
the darkroom is an L-shaped darkroom.
CN201921515875.XU 2019-09-12 2019-09-12 Composite test system Active CN210665888U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201921515875.XU CN210665888U (en) 2019-09-12 2019-09-12 Composite test system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201921515875.XU CN210665888U (en) 2019-09-12 2019-09-12 Composite test system

Publications (1)

Publication Number Publication Date
CN210665888U true CN210665888U (en) 2020-06-02

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CN201921515875.XU Active CN210665888U (en) 2019-09-12 2019-09-12 Composite test system

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113156224A (en) * 2021-03-31 2021-07-23 国家无线电监测中心检测中心 OTA test darkroom
CN113219244A (en) * 2021-05-07 2021-08-06 北京航空航天大学 Ultra-wide band plane wave generating system

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113156224A (en) * 2021-03-31 2021-07-23 国家无线电监测中心检测中心 OTA test darkroom
CN113156224B (en) * 2021-03-31 2023-01-10 国家无线电监测中心检测中心 OTA test darkroom
CN113219244A (en) * 2021-05-07 2021-08-06 北京航空航天大学 Ultra-wide band plane wave generating system

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