CN210108148U - Waterproof shockproof high temperature resistant unmanned aerial vehicle defense shield - Google Patents
Waterproof shockproof high temperature resistant unmanned aerial vehicle defense shield Download PDFInfo
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- CN210108148U CN210108148U CN201920508905.8U CN201920508905U CN210108148U CN 210108148 U CN210108148 U CN 210108148U CN 201920508905 U CN201920508905 U CN 201920508905U CN 210108148 U CN210108148 U CN 210108148U
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- 230000007123 defense Effects 0.000 title claims abstract description 22
- 238000004891 communication Methods 0.000 claims description 12
- 238000004804 winding Methods 0.000 claims description 4
- 239000012781 shape memory material Substances 0.000 claims description 3
- 229920001971 elastomer Polymers 0.000 description 2
- 239000000806 elastomer Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000001629 suppression Effects 0.000 description 1
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Abstract
The utility model discloses a waterproof high temperature resistant unmanned aerial vehicle defense shield that takes precautions against earthquakes, including waterproof high temperature resistant unmanned aerial vehicle defense shield that takes precautions against earthquakes include elasticity rope winder, strutting arrangement and accommodate device. One side of elasticity rope coiler towards accommodate device has the coiler trompil, elasticity rope coiler is used for first to fourth elasticity rope of coiling, the one end of first to fourth elasticity rope is drawn forth from the coiler trompil respectively. The supporting device comprises a first elastic body, a first elastic body first side wing and a first elastic body second side wing, wherein the first elastic body first side wing and the first elastic body second side wing are positioned on two sides of the first elastic body, and the first elastic body first side wing and the first elastic body second side wing are simultaneously integrally formed with the first elastic body. The utility model discloses a waterproof high temperature resistant unmanned aerial vehicle defense shield that takes precautions against earthquakes has better portability and higher integrated level, is fit for single carrying, receive and release and operate.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle defense, concretely relates to waterproof high temperature resistant unmanned aerial vehicle defense shield that takes precautions against earthquakes.
Background
The utility model discloses a utility model patent with publication number CN208366170U, subject name unmanned aerial vehicle comprehensive defense system, its technical scheme discloses "include that several survey tracking equipment and anti-unmanned aerial vehicle rejection equipment installed on the building in the no-fly zone are rejected, and respectively with survey tracking equipment and anti-unmanned aerial vehicle rejection equipment communication connection, be used for receiving the unmanned aerial vehicle information that this survey tracking equipment detected, and control the anti-unmanned aerial vehicle rejection equipment sends the unmanned aerial vehicle interference signal's surveillance center platform; any one of the detection tracking devices comprises a second supporting base (9) fixedly installed on a building in a no-fly area, a second rotating platform (10) arranged on the second supporting base (9), a right-angle support (11) fixed on the second rotating platform (10), a radar antenna (12) fixed on the right-angle support (11) and driven to rotate by the second rotating platform (10), a high-definition camera (4) fixed on the second rotating platform (10) and keeping the same rotation angular velocity with the radar antenna (12), a second communication interface (13) and a third communication interface (14) which are arranged on the second supporting base (9) and are connected with the high-definition camera (4) and the radar antenna (12) in a one-to-one correspondence manner, and a second power supply interface (15) arranged on the second supporting base (9); the second communication interface (13) and the third communication interface (14) are both connected with the monitoring center platform by communication cables and are used for transmitting the intercepted unmanned aerial vehicle information to the monitoring center platform; a second driving motor connected with a second power interface (15) is arranged in the second rotating platform (10); any anti-unmanned aerial vehicle rejection equipment comprises a first supporting base (1) fixedly installed on a building in a no-fly area, a first communication interface (8) and a first power interface (7) which are respectively arranged on the side edge of the first supporting base (1), a first rotating platform (2) which is arranged on the first supporting base (1) and has a rotation angle of 360 degrees along the horizontal direction, a control host (3) which is fixed on the first rotating platform (2), and a first antenna (5) and a second antenna (6) which are arranged on the control host (3) and are used for controlling the unmanned aerial vehicle in the no-fly area; the first communication interface (8) is connected with the monitoring center platform and used for receiving the unmanned aerial vehicle interference control signal sent by the monitoring center platform; a first driving motor connected with a first power interface (7) is arranged in the first rotating platform (2); the monitoring center platform comprises a DSP image processing module, a control host and a memory, wherein the DSP image processing module is connected with the second communication interface (13) and used for extracting the directional gradient histogram characteristics of the unmanned aerial vehicle in a video picture shot by the high-definition camera (4), the control host is connected with the DSP image processing module and used for acquiring the remote control frequency, the flight height and the distance of the unmanned aerial vehicle from the third communication interface and sending an unmanned aerial vehicle interference control signal to the first communication interface (8), and the memory is connected with the control host.
However, taking the above utility model patent as an example, current unmanned aerial vehicle defense device needs to arrange "survey and survey tracking equipment", "anti-unmanned aerial vehicle huge system equipment" etc. at the multiple spot, and cooperativity requirement is higher in practical application, and the operation is comparatively complicated, probably is applicable to in the airspace on a large scale disturb and defend unmanned aerial vehicle, thereby is difficult to simplify by a wide margin and realize taking one person to carry and operate, needs to give further improvement.
SUMMERY OF THE UTILITY MODEL
The utility model discloses to prior art's situation, overcome above-mentioned defect, provide a waterproof high temperature resistant unmanned aerial vehicle defense shield that takes precautions against earthquakes.
The utility model discloses a following technical scheme, waterproof shockproof high temperature resistant unmanned aerial vehicle defense shield includes that waterproof shockproof high temperature resistant unmanned aerial vehicle defense shield includes elasticity rope winder, strutting arrangement and accommodate device, wherein
One side of the elastic rope winder, which faces the accommodating device, is provided with a winder opening, the elastic rope winder is used for winding first to fourth elastic ropes, and the tail ends of one ends of the first to fourth elastic ropes are led out from the winder opening respectively;
the supporting device comprises a first elastic body, a first elastic body first side wing and a first elastic body second side wing, wherein the first elastic body first side wing and the first elastic body second side wing are positioned on two sides of the first elastic body and are simultaneously integrally formed with the first elastic body;
the supporting device further comprises a second elastic body, and a first elastic body side wing and a second elastic body side wing which are positioned on two sides of the second elastic body, the first elastic body side wing and the second elastic body side wing are simultaneously integrally formed with the second elastic body, the tail end of the other end of the third elastic rope is fixedly connected with the first elastic body side wing, and the tail end of the other end of the fourth elastic rope is fixedly connected with the second elastic body side wing;
the accommodating device comprises a signal transmitting cover and an accommodating main body integrally formed with the signal transmitting cover, the signal transmitting cover is positioned on one side of the supporting device, away from the elastic rope winder, and the accommodating main body is positioned on one side of the supporting device, close to the elastic rope winder.
According to the above aspect, as a further preferable aspect of the above aspect, the accommodating body grip portion is formed by integrally extending one end of the accommodating body.
According to the above technical means, as a further preferable technical means of the above technical means, one end of the accommodating main body is integrally extended to form an accommodating main body first extending portion.
According to the above aspect, as a further preferable aspect of the above aspect, a shape of a longitudinal section of the first extension portion of the accommodating main body is a half circumference.
According to the above aspect, as a further preferable aspect of the above aspect, one end of the accommodating main body integrally extends to form an accommodating main body second extending portion, and the accommodating main body second extending portion communicates with the accommodating main body first extending portion.
According to the above aspect, as a further preferable aspect of the above aspect, a shape of a longitudinal section of the second extension portion of the accommodating main body is an equilateral triangle.
According to the above aspect, as a more preferable aspect of the above aspect, the housing body has a plate shape.
According to the above technical means, as a further preferable technical means of the above technical means, the signal transmitting cover is tapered.
According to the above technical solution, as a further preferable technical solution of the above technical solution, the supporting device is made of a shape memory material.
According to the above technical means, as a further preferable technical means of the above technical means, the support means is horizontally symmetrical.
The utility model discloses a waterproof shockproof high temperature resistant unmanned aerial vehicle defense shield, its beneficial effect lies in, has better portability and higher integrated level, is fit for single carrying, receive and release and operate.
Drawings
Fig. 1 is a schematic view of the overall structure of an angle of the present invention.
Fig. 2 is a schematic view of the overall structure of another aspect of the present invention.
The reference numerals include: 10-elastic rope winder; 11-opening a hole of a winder; 12-an elastic cord; 20-a support device; 21-a first elastomer; 22-a first elastomeric first side flap; 23-a first elastomeric second side flap; 24-a second elastomer; 25-a second elastomeric first side flap; 26-a second elastomeric second side flap; 30-a containment device; 31-a signal emitting cap; 32-a containment body; 33-accommodating body grip; 34-a containment body first extension; 35-accommodating the body second extension.
Detailed Description
The utility model discloses a waterproof shockproof high temperature resistant unmanned aerial vehicle defense shield, below combine preferred embodiment, right the utility model discloses a detailed embodiment further describes.
Referring to fig. 1 to 2 of the drawings, fig. 1 shows a front-view-direction visual structure of the waterproof, shockproof and high-temperature-resistant unmanned aerial vehicle defense shield, and fig. 2 shows a rear-view-direction visual structure of the waterproof, shockproof and high-temperature-resistant unmanned aerial vehicle defense shield.
Preferred embodiments.
Preferably, the waterproof, shockproof and high temperature resistant unmanned aerial vehicle defense shield comprises an elastic rope winder 10, a supporting device 20 for signal transceiver devices such as embedded (flexible) signal antennas (not shown in the figure), and a containing device 30 for containing built-in components such as signal pressing circuit boards (not shown in the figure), wherein the supporting device 20 is used for containing built-in components such as signal receiving and transmitting devices such as signal antennas (not shown in the figure), and the containing device 30 is used for
The elastic rope winder 10 has an inner cavity (not shown in the drawings) for receiving an elastic rope 12, a winder opening 11 is formed in one side of the elastic rope winder 10 facing the accommodating device 30, the elastic rope winder 10 is used for winding (in other words, winding and unwinding) first to fourth elastic ropes 12, and one end ends of the first to fourth elastic ropes 12 are led out from (the inside of the elastic rope winder 10 and) the winder opening 11 respectively;
the supporting device 20 comprises a first elastic body 21, and a first elastic body first side wing 22 and a first elastic body second side wing 23 which are positioned at two sides of (specifically, above and below) the first elastic body 21, wherein the first elastic body first side wing 22 and the first elastic body second side wing 23 are simultaneously and integrally formed with the first elastic body 21, the tail end of the other end of the first elastic rope 12 is fixedly connected with the first elastic body first side wing 22, and the tail end of the other end of the second elastic rope 12 is fixedly connected with the first elastic body second side wing 23;
the supporting device 20 further includes a second elastic body 24, and a second elastic body first side wing 25 and a second elastic body second side wing 26 located at two sides of (specifically, above and below) the second elastic body 24, the second elastic body first side wing 25 and the second elastic body second side wing 26 are simultaneously integrally formed with the second elastic body 24, the other end of the third elastic cord 12 is fixedly connected to the second elastic body first side wing 25, and the other end of the fourth elastic cord 12 is fixedly connected to the second elastic body second side wing 26;
the accommodating device 30 comprises a signal transmitting cover 31 and an accommodating main body 32 integrally formed with the signal transmitting cover 31, the signal transmitting cover 31 is positioned on one side of the supporting device 20 far away from the elastic rope winder 10, and the accommodating main body 32 is positioned on one side of the supporting device 20 close to the elastic rope winder 10.
Further, the one end (specifically the end of keeping away from signal emission cover 31) of holding main part 32 further integrative extension forms the main part of holding 33 that holds that supplies the user to grip for the user holds main part 32 when strutting arrangement 20 with this waterproof shockproof high temperature resistant unmanned aerial vehicle defense shield struts, and the other hand holds and holds main part of holding 33, thereby keeps defense shield relatively stable, avoids the excessive shake of defense shield.
Further, an end of the accommodating main body 32 (specifically, an end near the signal transmitting cover 31) further integrally extends to form an accommodating main body first extending portion 34 for accommodating built-in components such as a signal pressing circuit board, a signal collecting circuit board and the like.
Wherein the longitudinal section of the first extension 34 of the receiving body is preferably shaped as a half circumference.
Further, an end portion of the accommodating main body 32 (specifically, a portion close to the accommodating main body first extension portion 34) further integrally extends to form an accommodating main body second extension portion 35 for accommodating built-in components such as the processor and its peripheral circuits, and the accommodating main body second extension portion 35 is communicated with the accommodating main body first extension portion 34.
The longitudinal section of the second extension 34 of the containing body is preferably in the shape of an equilateral triangle.
Further, the accommodating main body 32 (where the accommodating main body first extension portion 34 and the accommodating main body second extension portion 35 are not provided) has a plate shape (in other words, a sheet shape), so that the occupied space of the accommodating device 30 is reduced as required, and the integration degree is improved.
Further, the signal transmitting cover 31 is preferably tapered.
Further, the support means 20 is preferably made of a shape memory material (in a default state the support means 20 is under tension and in a distracted state).
Further, the supporting device 20 is preferably horizontally symmetrical.
Further, the elastic cord winder 10 and the accommodating device 30 are preferably integrally formed by using a light material such as a waterproof, shockproof and high-temperature-resistant aluminum alloy.
It should be mentioned that the technical features such as the signal suppression circuit board, the signal acquisition circuit board, the flexible signal antenna that the utility model discloses a patent application relates to should be regarded as prior art, and the concrete structure of these technical features, theory of operation and the control mode that may involve, spatial arrangement mode adopt in the field conventional selection can, should not be regarded as the utility model discloses a point of the invention is located, the utility model discloses a do not further expand the detailed description specifically, can refer to fig. 1, the publication number is CN208366170U that is the CN205508116U fig. 2 etc..
It will be apparent to those skilled in the art that modifications and variations can be made in the above-described embodiments, or some features of the invention may be substituted or omitted, and any modification, substitution, or improvement made within the spirit and principle of the present invention shall fall within the protection scope of the present invention.
Claims (10)
1. A waterproof shockproof high temperature resistant unmanned aerial vehicle defense shield is characterized by comprising an elastic rope winder, a supporting device and a containing device, wherein
One side of the elastic rope winder, which faces the accommodating device, is provided with a winder opening, the elastic rope winder is used for winding first to fourth elastic ropes, and the tail ends of one ends of the first to fourth elastic ropes are led out from the winder opening respectively;
the supporting device comprises a first elastic body, a first elastic body first side wing and a first elastic body second side wing, wherein the first elastic body first side wing and the first elastic body second side wing are positioned on two sides of the first elastic body and are simultaneously integrally formed with the first elastic body;
the supporting device further comprises a second elastic body, and a first elastic body side wing and a second elastic body side wing which are positioned on two sides of the second elastic body, the first elastic body side wing and the second elastic body side wing are simultaneously integrally formed with the second elastic body, the tail end of the other end of the third elastic rope is fixedly connected with the first elastic body side wing, and the tail end of the other end of the fourth elastic rope is fixedly connected with the second elastic body side wing;
the accommodating device comprises a signal transmitting cover and an accommodating main body integrally formed with the signal transmitting cover, the signal transmitting cover is positioned on one side of the supporting device, away from the elastic rope winder, and the accommodating main body is positioned on one side of the supporting device, close to the elastic rope winder.
2. The unmanned aerial vehicle defense shield of claim 1, wherein one end of the accommodating body integrally extends to form an accommodating body holding portion.
3. The waterproof, shockproof and high temperature resistant unmanned aerial vehicle defensive shield of claim 1, wherein one end of the receiving body integrally extends to form a receiving body first extension.
4. The waterproof, shockproof and high temperature resistant unmanned aerial vehicle defensive shield of claim 3, wherein a longitudinal section of the first extension of the containment body is shaped as one-half of a circumference.
5. The waterproof, shockproof and high temperature resistant unmanned aerial vehicle defensive shield of claim 3, wherein one end of the receiving body integrally extends to form a receiving body second extension portion, the receiving body second extension portion being in communication with the receiving body first extension portion.
6. The waterproof, shockproof and high temperature resistant unmanned aerial vehicle defensive shield of claim 5, wherein the shape of the longitudinal section of the second extension of the containment body is an equilateral triangle.
7. The waterproof, shockproof and high temperature resistant unmanned aerial vehicle defensive shield of claim 1, wherein the containment body is plate shaped.
8. The waterproof, shockproof and high temperature resistant unmanned aerial vehicle defensive shield of claim 1, wherein the signal transmitting cover is cone-shaped.
9. The waterproof, shockproof and high temperature resistant unmanned aerial vehicle defensive shield of claim 1, wherein the support device is made of a shape memory material.
10. The waterproof, shockproof and high temperature resistant unmanned aerial vehicle defensive shield of claim 1, wherein the support device is horizontally symmetrical.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920508905.8U CN210108148U (en) | 2019-04-15 | 2019-04-15 | Waterproof shockproof high temperature resistant unmanned aerial vehicle defense shield |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920508905.8U CN210108148U (en) | 2019-04-15 | 2019-04-15 | Waterproof shockproof high temperature resistant unmanned aerial vehicle defense shield |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210108148U true CN210108148U (en) | 2020-02-21 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920508905.8U Active CN210108148U (en) | 2019-04-15 | 2019-04-15 | Waterproof shockproof high temperature resistant unmanned aerial vehicle defense shield |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210108148U (en) |
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2019
- 2019-04-15 CN CN201920508905.8U patent/CN210108148U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Waterproof, shockproof and high temperature resistant UAV defense shield Effective date of registration: 20220602 Granted publication date: 20200221 Pledgee: Bank of Jiaxing science and technology branch of Limited by Share Ltd. Pledgor: ZHEJIANG RUITONG ELECTRONIC TECHNOLOGY Co.,Ltd. Registration number: Y2022980006965 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20231213 Granted publication date: 20200221 Pledgee: Bank of Jiaxing science and technology branch of Limited by Share Ltd. Pledgor: ZHEJIANG RUITONG ELECTRONIC TECHNOLOGY Co.,Ltd. Registration number: Y2022980006965 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right |