CN114941965A - Anti-unmanned aerial vehicle comprehensive defense system - Google Patents
Anti-unmanned aerial vehicle comprehensive defense system Download PDFInfo
- Publication number
- CN114941965A CN114941965A CN202210668768.0A CN202210668768A CN114941965A CN 114941965 A CN114941965 A CN 114941965A CN 202210668768 A CN202210668768 A CN 202210668768A CN 114941965 A CN114941965 A CN 114941965A
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- support
- hollow column
- rotating shaft
- screw rod
- 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.)
- Pending
Links
- 230000007123 defense Effects 0.000 title claims abstract description 26
- 230000002457 bidirectional effect Effects 0.000 description 6
- 230000003139 buffering effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to the technical field of defense equipment, in particular to an anti-unmanned aerial vehicle comprehensive defense system which comprises a base, a supporting frame, a hollow column, a rotating shaft, a supporting table, an interference device, a connecting disc, a first spring, a sleeve and a lock column, wherein the connecting disc is provided with a plurality of lock holes; during the use, fix the base at the roof, move down the sleeve pipe when the position of interference ware needs to be adjusted, first spring is compressed, the sleeve pipe moves down and drives the lock post and move down, make the lock post move out from the lockhole, remove the fixed to the connection pad, can rotate the countershaft this moment, with the position of adjusting the interference ware, after the interference ware position control is good, loosen the sleeve pipe, sleeve pipe and lock post move up under the promotion of first spring, make the lock post insert in the lockhole, with connection pad rigidity, thereby make the interference ware rigidity, and then can realize rotating the interference ware, the electromagnetic wave of adjusting the interference ware sends the angle.
Description
Technical Field
The invention relates to the technical field of defense equipment, in particular to an anti-unmanned aerial vehicle comprehensive defense system.
Background
Anti unmanned aerial vehicle defense system has extensive application in the field of air defense, and current anti unmanned aerial vehicle defense system of countering relies on the electromagnetic wave that the interference ware sent to interfere with unmanned aerial vehicle's flight, and the interference ware is placed on the roof usually, but the easy emergence of back is removed on the roof to the interference ware is placed.
Present prior art discloses an anti-unmanned aerial vehicle synthesizes defense system includes base and interference unit, and the interference unit is fixed on the base, is equipped with the screw on the base, through seting up the screw at the roof, utilizes the bolt to fix the base to make interference unit rigidity.
However, with the above method, the position of the jammer is fixed, the jammer cannot rotate, and the electromagnetic wave emission angle of the jammer cannot be adjusted.
Disclosure of Invention
The invention aims to provide an anti-unmanned aerial vehicle comprehensive defense system which can rotate an interference unit so as to adjust the electromagnetic wave emission angle of the interference unit.
In order to achieve the purpose, the invention provides an anti-unmanned aerial vehicle comprehensive defense system which comprises a base, a supporting frame, a hollow column, a rotating shaft, a supporting table, an interference device, a connecting disc, a first spring, a sleeve and a lock column, wherein the supporting frame is arranged on the base; the support frame is fixedly connected with the base and is positioned at the top of the base; the hollow column is fixedly connected with the support frame and is positioned on the side edge of the support frame; the rotating shaft is rotatably connected with the hollow column and is positioned at the top of the hollow column; the support table is fixedly connected with the rotating shaft and is positioned at the top of the rotating shaft; the interference device is arranged on the top of the support platform; the connecting disc is fixedly connected with the rotating shaft and is positioned on the side edge of the rotating shaft, the connecting disc is provided with a plurality of locking holes, and the locking holes are uniformly distributed on the side edge of the connecting disc; the first spring is fixedly connected with the hollow column and is positioned between the hollow column and the rotating shaft; the sleeve is fixedly connected with the first spring and is positioned at the top of the first spring; the lock column is fixedly connected with the sleeve and is positioned on the side edge of the sleeve.
The anti-unmanned aerial vehicle comprehensive defense system further comprises two fixing clamps; the two fixing clamps are respectively and fixedly connected with the hollow column and are respectively positioned on the side edges of the hollow column.
The fixing clamp comprises a support and a first screw rod; the support is fixedly connected with the hollow column and is positioned on the side edge of the hollow column; the first screw rod is in threaded connection with the support and penetrates through the support.
The fixing clamp further comprises a guide rod and a clamping jaw; the guide rod is connected with the support in a sliding manner and penetrates through the support; the clamping jaw is connected with the first screw rod in a rotating mode, fixedly connected with the guide rod and located on one side, close to the rotating shaft, of the first screw rod.
Wherein the fixing clip further comprises a knob; the knob is fixedly connected with the first screw rod and is positioned on one side, far away from the clamping jaw, of the first screw rod.
The support frame comprises a guide rail, a sliding block and a second screw rod; the guide rail is fixedly connected with the base and is positioned at the top of the base; the sliding block is connected with the guide rail in a sliding manner, is fixedly connected with the hollow column and is positioned on the side edge of the guide rail; the second screw rod is rotatably connected with the guide rail, is in threaded connection with the sliding block and is positioned on the side edge of the guide rail.
Wherein the support further comprises a motor; the motor and the guide rail are fixedly connected, the output end of the motor is fixedly connected with the second screw rod and is positioned at the top of the guide rail.
According to the anti-unmanned aerial vehicle comprehensive defense system, during installation, the base is fixed on the roof, the support frame, the hollow column and the support table are used for supporting the interference device, when the position of the interference device needs to be adjusted, the sleeve is moved downwards, the first spring is compressed, the sleeve moves downwards to drive the lock column to move downwards, the lock column is moved out of the lock hole, the fixing of the connecting disc is released, the rotating shaft can be rotated at the moment to adjust the position of the interference device, after the position of the interference device is adjusted, the sleeve is loosened, the sleeve and the lock column move upwards under the pushing of the first spring, the lock column is inserted into the lock hole, the position of the connecting disc is fixed, and the position of the interference device is fixed; through the mode, the interference unit can be rotated, so that the electromagnetic wave emission angle of the interference unit can be adjusted.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a schematic structural diagram of an anti-unmanned aerial vehicle comprehensive defense system of the invention.
Fig. 2 is a sectional view of an anti-drone comprehensive defense system of the present invention.
Fig. 3 is a schematic view of the structure of the support table of the present invention.
Figure 4 is a cross-sectional view of a support table of the present invention.
1-base, 2-support frame, 3-hollow column, 4-rotating shaft, 5-support table, 6-interference unit, 7-connecting disc, 8-first spring, 9-sleeve, 10-locking column, 11-fixing clamp, 21-guide rail, 22-slide block, 23-second screw, 24-motor, 51-table body, 52-bidirectional threaded screw rod, 53-moving block, 54-clamping element, 70-locking hole, 111-support, 112-first screw rod, 113-guide rod, 114-clamping jaw, 115-knob, 541-support rod, 542-second spring, 543-clamping plate.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the accompanying drawings are illustrative and intended to explain the present invention and should not be construed as limiting the present invention.
In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships illustrated in the drawings, and are used merely for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention. Further, in the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
Referring to fig. 1 to 4, the present invention provides an anti-drone comprehensive defense system: the device comprises a base 1, a support frame 2, a hollow column 3, a rotating shaft 4, a support table 5, an interference unit 6, a connecting disc 7, a first spring 8, a sleeve 9 and a lock column 10; the support frame 2 is fixedly connected with the base 1 and is positioned at the top of the base 1; the hollow column 3 is fixedly connected with the support frame 2 and is positioned on the side edge of the support frame 2; the rotating shaft 4 is rotatably connected with the hollow column 3 and is positioned at the top of the hollow column 3; the support table 5 is fixedly connected with the rotating shaft 4 and is positioned at the top of the rotating shaft 4; the interference unit 6 is arranged on the top of the support table 5; the connecting disc 7 is fixedly connected with the rotating shaft 4 and is positioned on the side edge of the rotating shaft 4, the connecting disc 7 is provided with a plurality of locking holes 70, and the locking holes 70 are uniformly distributed on the side edge of the connecting disc 7; the first spring 8 is fixedly connected with the hollow column 3 and is positioned between the hollow column 3 and the rotating shaft 4; the sleeve 9 is fixedly connected with the first spring 8 and is positioned at the top of the first spring 8; the lock cylinder 10 is fixedly connected with the sleeve 9 and is positioned on the side edge of the sleeve 9.
In this embodiment, when the base 1 is fixed to the roof and the interference unit 6 is supported by the support frame 2, the hollow column 3 and the support base 5, when it is desired to adjust the position of the interference means 6, the sleeve 9 is moved downwards, the first spring 8 is compressed, the sleeve 9 moves downwards to drive the lock column 10 to move downwards, so that the lock column 10 moves out of the lock hole 70, the fixing of the connecting disc 7 is released, the rotating shaft 4 can be rotated at the moment to adjust the position of the interference device 6, after the position of the interference device 6 is adjusted, the sleeve 9 is released, the sleeve 9 and the lock cylinder 10 move upwards under the pushing of the first spring 8, inserting the lock cylinder 10 into the lock hole 70 to fix the position of the connecting disc 7, so that the interference unit 6 is fixed; by the above manner, the jammer 6 can be rotated, so that the electromagnetic wave emission angle of the jammer 6 can be adjusted.
Further, the anti-unmanned aerial vehicle comprehensive defense system further comprises two fixing clamps 11; the two fixing clamps 11 are respectively and fixedly connected with the hollow column 3 and are respectively positioned on the side edges of the hollow column 3.
In this embodiment, the two fixing clips 11 can clamp the rotating shaft 4, so as to prevent the rotating shaft 4 from rotating.
Further, the fixing clip 11 includes a support 111 and a first screw 112; the support 111 is fixedly connected with the hollow column 3 and is positioned on the side edge of the hollow column 3; the first screw rod 112 is connected with the support 111 in a threaded manner and penetrates through the support 111. The fixing clamp 11 further comprises a guide rod 113 and a clamping jaw 114; the guide rod 113 is connected with the support 111 in a sliding manner and penetrates through the support 111; the clamping jaw 114 is rotatably connected with the first screw rod 112, is fixedly connected with the guide rod 113, and is located on one side of the first screw rod 112 close to the rotating shaft 4. The retaining clip 11 further comprises a knob 115; the knob 115 is fixedly connected with the first screw rod 112 and is located on one side of the first screw rod 112 away from the clamping jaw 114.
In this embodiment, the first screw 112 is rotated to move the first screw 112 along the support 111, the first screw 112 drives the clamping jaw 114 to approach the rotating shaft 4, and the two clamping jaws 114 can clamp and fix the rotating shaft 4, so as to prevent the rotating shaft 4 from rotating after the position of the disturber 6 is good and the disturber 6 from moving; the guide rod 113 can prevent the clamping jaw 114 from rotating; the knob 115 can be grasped by a user to facilitate rotation of the first threaded rod 112.
Further, the support frame 2 comprises a guide rail 21, a slide block 22 and a second screw rod 23; the guide rail 21 is fixedly connected with the base 1 and is positioned at the top of the base 1; the sliding block 22 is connected with the guide rail 21 in a sliding manner, is fixedly connected with the hollow column 3 and is positioned on the side edge of the guide rail 21; the second screw 23 is rotatably connected with the guide rail 21, is in threaded connection with the slider 22, and is located on the side of the guide rail 21. The support further comprises a motor 24; the motor 24 is fixedly connected with the guide rail 21, and the output end of the motor 24 is fixedly connected with the second screw 23 and is positioned at the top of the guide rail 21.
In this embodiment, the motor 24 drives the second screw 23 to rotate, and the guide rail 21 can limit the slide block 22 from rotating, so that when the second screw 23 rotates, the slide block 22 slides longitudinally along the guide rail 21, and the slide block 22 drives the hollow column 3 to slide longitudinally, so that the height position of the interference unit 6 can be adjusted.
Further, the supporting table 5 comprises a table body 51, a bidirectional threaded screw 52, two moving blocks 53 and two clamping pieces 54; the table body 51 is fixedly connected with the rotating shaft 4 and is positioned at the top of the rotating shaft 4; the bidirectional threaded screw rod 52 is in threaded connection with the table body 51 and penetrates through the table body 51; the two moving blocks 53 are respectively connected with the table body 51 in a sliding manner, respectively connected with the bidirectional threaded screw rod 52 in a threaded manner, and respectively positioned at the top of the table body 51; the two clamping members 54 are respectively fixedly connected with the two moving blocks 53 and are respectively positioned at the tops of the two moving blocks 53.
In this embodiment, a sliding groove adapted to the moving block 53 is formed in the table body 51, the moving block 53 can be limited from rotating, external threads with opposite thread directions are formed at two ends of the bidirectional threaded lead screw 52, the interference unit 6 is placed on the top of the table body 51, the interference unit 6 is located between the two clamping members 54, the bidirectional threaded lead screw 52 is rotated clockwise, the two moving blocks 53 are made to approach each other, and the two moving blocks 53 drive the two clamping members 54 to approach each other, so that the interference unit 6 is clamped and fixed; when the interference unit 6 is disassembled, the two clamping pieces 54 can be far away from the interference unit 6 by rotating the bidirectional threaded screw rod 52 anticlockwise, and the interference unit 6 can be conveniently assembled and disassembled in the above manner.
Further, the clamping member 54 includes a rod 541, a second spring 542, and a clamping plate 543; the supporting rod 541 is fixedly connected with the moving block 53 and is positioned at the top of the moving block 53; the second spring 542 is fixedly connected with the supporting rod 541 and is positioned at the side of the supporting rod 541; the clamp plate 543 is fixedly connected with the second spring 542 and is located at the side of the second spring 542.
In this embodiment, the two clamping plates 543 can clamp and fix the interference unit 6, and when the moving block 53 drives the clamping plates 543 through the supporting rods 541 to clamp the interference unit 6, the second springs 542 can provide a buffering effect to prevent an excessive pressing force from being applied to the interference unit 6.
While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes in form and detail may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.
Claims (7)
1. An anti-unmanned aerial vehicle comprehensive defense system is characterized in that,
the device comprises a base, a support frame, a hollow column, a rotating shaft, a support table, an interference unit, a connecting disc, a first spring, a sleeve and a lock column; the support frame is fixedly connected with the base and is positioned at the top of the base; the hollow column is fixedly connected with the support frame and is positioned on the side edge of the support frame; the rotating shaft is rotatably connected with the hollow column and is positioned at the top of the hollow column; the support table is fixedly connected with the rotating shaft and is positioned at the top of the rotating shaft; the interference device is arranged on the top of the support platform; the connecting disc is fixedly connected with the rotating shaft and is positioned on the side edge of the rotating shaft, the connecting disc is provided with a plurality of locking holes, and the locking holes are uniformly distributed on the side edge of the connecting disc; the first spring is fixedly connected with the hollow column and is positioned between the hollow column and the rotating shaft; the sleeve is fixedly connected with the first spring and is positioned at the top of the first spring; the lock column is fixedly connected with the sleeve and is positioned on the side edge of the sleeve.
2. The system of claim 1, wherein the unmanned aerial vehicle defense system,
the anti-unmanned aerial vehicle comprehensive defense system further comprises two fixing clamps; the two fixing clamps are respectively and fixedly connected with the hollow column and are respectively positioned on the side edges of the hollow column.
3. The system of claim 2, wherein the unmanned aerial vehicle defense system,
the fixing clamp comprises a support and a first screw rod; the support is fixedly connected with the hollow column and is positioned on the side edge of the hollow column; the first screw rod is in threaded connection with the support and penetrates through the support.
4. An anti-drone comprehensive defense system according to claim 3,
the fixing clamp further comprises a guide rod and a clamping jaw; the guide rod is connected with the support in a sliding manner and penetrates through the support; the clamping jaw is rotatably connected with the first screw rod, fixedly connected with the guide rod and positioned on one side of the first screw rod close to the rotating shaft.
5. An anti-UAV comprehensive defense system according to claim 4,
the fixing clamp further comprises a knob; the knob is fixedly connected with the first screw rod and is positioned on one side, far away from the clamping jaw, of the first screw rod.
6. The system of claim 1, wherein the unmanned aerial vehicle defense system,
the support frame comprises a guide rail, a sliding block and a second screw rod; the guide rail is fixedly connected with the base and is positioned at the top of the base; the sliding block is connected with the guide rail in a sliding manner, is fixedly connected with the hollow column and is positioned on the side edge of the guide rail; the second screw rod is rotatably connected with the guide rail, is in threaded connection with the sliding block and is positioned on the side edge of the guide rail.
7. The system of claim 6, wherein the unmanned aerial vehicle defense system,
the support further comprises a motor; the motor and the guide rail are fixedly connected, the output end of the motor is fixedly connected with the second screw rod and is positioned at the top of the guide rail.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210668768.0A CN114941965A (en) | 2022-06-14 | 2022-06-14 | Anti-unmanned aerial vehicle comprehensive defense system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210668768.0A CN114941965A (en) | 2022-06-14 | 2022-06-14 | Anti-unmanned aerial vehicle comprehensive defense system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114941965A true CN114941965A (en) | 2022-08-26 |
Family
ID=82909741
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210668768.0A Pending CN114941965A (en) | 2022-06-14 | 2022-06-14 | Anti-unmanned aerial vehicle comprehensive defense system |
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| Country | Link |
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| CN (1) | CN114941965A (en) |
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