CN213517531U - Unmanned aerial vehicle control monitoring radar - Google Patents
Unmanned aerial vehicle control monitoring radar Download PDFInfo
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- CN213517531U CN213517531U CN202022648549.5U CN202022648549U CN213517531U CN 213517531 U CN213517531 U CN 213517531U CN 202022648549 U CN202022648549 U CN 202022648549U CN 213517531 U CN213517531 U CN 213517531U
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle control monitoring radar, which comprises a monitoring head, a mounting seat and a rotary table, wherein the mounting seat is arranged on the top surface of the rotary table, the monitoring head is arranged on the mounting seat by utilizing a rotating shaft, the monitoring head also comprises a support rod and a hoop, the hoop is sleeved on the support rod, the outer wall of the hoop is articulated with three stable support legs which are distributed in an annular shape at equal intervals, the bottom ends of the stable support legs are articulated with ground cones, and three groups of locking components which are distributed in an annular shape at equal intervals are; an adjusting component for adjusting the height of the supporting rod is arranged in the supporting rod; the utility model discloses an unmanned aerial vehicle control monitoring radar, the equipment monitoring head highly can carry out the pertinence and adjust, has improved the application scope of equipment to the height-adjustable of cuff to change the inclination of stabilizing the supporting leg, when heightening the monitoring head, reduce the cuff and with the great supporting area of activity, guarantee the stability of supporting monitoring head, guarantee the reliable use of equipment.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to unmanned aerial vehicle control monitoring radar.
Background
Unmanned aircraft is called unmanned aerial vehicle for short, and is called UAV in short in English, and is an unmanned aircraft operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, compared with the unmanned aircraft, the unmanned aircraft is more suitable for tasks too 'fool, dirty or dangerous', the unmanned aircraft can be divided into military and civil according to the application field, and the unmanned aircraft can be divided into reconnaissance aircraft and target aircraft in the military, and the unmanned aircraft can be applied to the industry in the civil field, and is really just needed by the unmanned aircraft; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the use of the unmanned aerial vehicle is greatly expanded, the developed countries actively expand the industrial application and develop the unmanned aerial vehicle technology, a monitoring radar is important equipment for monitoring the position and other information of the unmanned aerial vehicle, and a monitoring head can automatically adjust the pitch angle and the horizontal turning angle.
Original unmanned aerial vehicle control monitoring radar utilizes the support to fix on ground when using usually to can need highly adjusting the monitoring head to the in-service use, but, when the monitoring head was increaseed, its focus can become high, leads to the stability step-down of monitoring head, influences the reliable use of monitoring head.
SUMMERY OF THE UTILITY MODEL
For solving the above-mentioned problem that exists among the prior art, the utility model provides an unmanned aerial vehicle control monitoring radar has convenient to use, easily adjusts and fixed stable characteristics.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle control monitoring radar comprises a monitoring head, a mounting seat and a rotary table, wherein the mounting seat is mounted on the top surface of the rotary table, the monitoring head is mounted on the mounting seat through a rotating shaft, the unmanned aerial vehicle control monitoring radar also comprises a supporting rod and a hoop, the hoop is sleeved on the supporting rod, three stable supporting legs which are distributed in an annular shape at equal intervals are hinged to the outer wall of the hoop, a ground cone is hinged to the bottom end of each stable supporting leg, and three groups of locking assemblies which are distributed in an annular shape at equal intervals are mounted on the hoop; an adjusting component for adjusting the height of the supporting rod is arranged in the supporting rod.
As a preferred technical solution of the present invention, the adjusting assembly includes an adjusting screw and a connecting post, a chassis is fixed at the bottom end of the connecting post, an adjusting cavity capable of accommodating the connecting post is formed in the supporting rod, the adjusting screw is supported and installed in the adjusting cavity through a bearing, and a thread deep groove matched with the adjusting screw is formed in the connecting post; the transverse sections of the support rods and the connecting columns are both rectangular structures.
As a preferred technical scheme of the utility model, adjusting part still includes hand wheel, initiative umbelliform gear and driven umbelliform gear, the hand wheel passes through the bearing support frame to be established on the bracing piece, the initiative umbelliform gear is fixed the center pin of hand wheel is last and is in adjust the intracavity, driven umbelliform gear is fixed adjusting screw is last and with initiative umbelliform gear engagement links to each other.
As a preferred technical scheme of the utility model, the locking Assembly includes locking screw, just locking screw closes soon through the screw thread and fixes on the cuff the embedding of locking screw is served and is utilized the bearing to install the ejector pad the outside end of locking screw is fixed with the knob.
As a preferred technical scheme of the utility model, the surface bonding of push jack is fixed with anti-skidding rubber gasket.
As a preferred technical scheme of the utility model, the utility model also comprises a linkage component, the linkage component comprises a sleeve, three connecting rods and a lantern ring, the three connecting rods are annularly and equidistantly fixed on the outer wall of the sleeve, and the lantern ring is hinged at the end part of the connecting rod; the support rod may extend through the sleeve and the stabilizing support leg may extend through the collar.
Compared with the prior art, the beneficial effects of the utility model are that: the utility model discloses an unmanned aerial vehicle control monitoring radar, the equipment monitoring head highly can carry out the pertinence and adjust, has improved the application scope of equipment to the height-adjustable of cuff to change the inclination of stabilizing the supporting leg, when heightening the monitoring head, reduce the cuff and with the great supporting area of activity, guarantee the stability of supporting monitoring head, guarantee the reliable use of equipment.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
fig. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic top view of the ferrule of the present invention;
fig. 3 is a schematic front sectional view of the support rod of the present invention;
fig. 4 is a schematic top view of the linkage assembly of the present invention;
in the figure: 1. a monitoring head; 2. a mounting seat; 3. a turntable; 4. a support bar; 5. a ferrule; 6. stabilizing the support leg; 7. a ground cone; 8. a chassis; 9. an adjustment assembly; 10. a linkage assembly; 11. a knob; 12. locking the screw rod; 13. pushing the sheet; 14. an anti-slip rubber gasket; 15. an adjustment chamber; 16. adjusting the screw rod; 17. connecting columns; 18. deep groove of screw thread; 19. a hand wheel; 20. a drive bevel gear; 21. a driven bevel gear; 22. a sleeve; 23. a connecting rod; 24. a collar.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Example 1
Referring to fig. 1-3, the present invention provides the following technical solutions: an unmanned aerial vehicle control monitoring radar comprises a monitoring head 1, a mounting seat 2 and a rotary table 3, wherein the mounting seat 2 is mounted on the top surface of the rotary table 3, the monitoring head 1 is mounted on the mounting seat 2 by utilizing a rotating shaft, the unmanned aerial vehicle control monitoring radar also comprises a supporting rod 4 and a hoop 5, the hoop 5 is sleeved on the supporting rod 4, three stable supporting legs 6 which are distributed in an annular shape at equal intervals are hinged to the outer wall of the hoop 5, a ground cone 7 is hinged to the bottom end of each stable supporting leg 6, and three groups of locking assemblies which are distributed in an annular shape at equal intervals are mounted; be equipped with the adjusting part 9 of adjusting support pole 4 height in bracing piece 4, when using, place the device in suitable position department, it launches certain angle to stabilize supporting leg 6, and insert ground awl 7 and stabilize equipment, utilize monitoring head 1 to monitor unmanned aerial vehicle, need to the in-service use, usable adjusting part 9 adjusts the bracing piece 4 height, with the height of adjusting monitoring head 1, furthermore, when heightening monitoring head 1, after the altitude mixture control of monitoring head 1 is good, remove the locking subassembly, extract ground awl 7 earlier, adjust cuff 5 downwards along bracing piece 4, at this moment, if need insert ground awl 7 again ground, need stabilize supporting leg 6 to the outside upset, enlarge the holding area, improve the stability to equipment support.
Specifically, according to fig. 1 and fig. 3, in this embodiment, the adjusting assembly 9 includes an adjusting screw 16 and a connecting column 17, a base plate 8 is fixed at the bottom end of the connecting column 17, an adjusting cavity 15 capable of accommodating the connecting column 17 is formed in the supporting rod 4, the adjusting screw 16 is supported and installed in the adjusting cavity 15 through a bearing, and a threaded deep groove 18 matched with the adjusting screw 16 is formed in the connecting column 17; the horizontal tangent plane of bracing piece 4 and spliced pole 17 is equilateral triangle structure, when adjusting monitoring head 1's height, rotates adjusting screw 16, and under the screw thread closes the effect soon, spliced pole 17 can remove along adjusting chamber 15, and chassis 8 ground connection, therefore the height of bracing piece 4 can change, monitoring head 1's high change.
Specifically, according to fig. 1 and fig. 3, in this embodiment, the adjusting assembly 9 further includes a hand wheel 19, a driving bevel gear 20 and a driven bevel gear 21, the hand wheel 19 is disposed on the support rod 4 through a bearing support frame, the driving bevel gear 20 is fixed on a central shaft of the hand wheel 19 and is located in the adjusting cavity 15, the driven bevel gear 21 is fixed on the adjusting screw 16 and is engaged with the driving bevel gear 20, when the height of the monitoring head 1 is adjusted, the hand wheel 19 is rotated, the driving bevel gear 20 is rotated by the hand wheel 19, and the adjusting screw 16 is driven to rotate by the driven bevel gear 21 under the engagement relationship, under the screwing action of the threads, the connecting column 17 moves along the adjusting cavity 15, the chassis 8 is grounded, so that the height of the support rod 4 is changed, and the height of the monitoring head 1 is changed.
Specifically, according to fig. 1 and fig. 2, in the present embodiment, the locking assembly includes a locking screw 12, the locking screw 12 is screwed and fixed on the ferrule 5 through threads, a pushing piece 13 is mounted on an insertion end of the locking screw 12 by using a bearing, a knob 11 is fixed at an outer end of the locking screw 12, when the height of the ferrule 5 needs to be adjusted, the locking screw 12 is firstly unscrewed, and after the height of the ferrule 5 is adjusted, the locking screw 12 is screwed, so that the pushing piece 13 is tightly attached to the outer wall of the support rod 4.
Specifically, according to fig. 1 and 2, in the present embodiment, the anti-slip rubber pad 14 is adhered and fixed on the surface of the pushing piece 13, so as to increase the friction force, thereby further improving the stability of the height-adjusted ferrule 5.
Example 2
Referring to fig. 1-4, the present invention provides the following technical solutions: an unmanned aerial vehicle control monitoring radar comprises a monitoring head 1, a mounting seat 2 and a rotary table 3, wherein the mounting seat 2 is mounted on the top surface of the rotary table 3, the monitoring head 1 is mounted on the mounting seat 2 by utilizing a rotating shaft, the unmanned aerial vehicle control monitoring radar also comprises a supporting rod 4 and a hoop 5, the hoop 5 is sleeved on the supporting rod 4, three stable supporting legs 6 which are distributed in an annular shape at equal intervals are hinged to the outer wall of the hoop 5, a ground cone 7 is hinged to the bottom end of each stable supporting leg 6, and three groups of locking assemblies which are distributed in an annular shape at equal intervals are mounted; be equipped with the adjusting part 9 of adjusting support pole 4 height in bracing piece 4, when using, place the device in suitable position department, it launches certain angle to stabilize supporting leg 6, and insert ground awl 7 and stabilize equipment, utilize monitoring head 1 to monitor unmanned aerial vehicle, need to the in-service use, usable adjusting part 9 adjusts the bracing piece 4 height, with the height of adjusting monitoring head 1, furthermore, when heightening monitoring head 1, after the altitude mixture control of monitoring head 1 is good, remove the locking subassembly, extract ground awl 7 earlier, adjust cuff 5 downwards along bracing piece 4, at this moment, if need insert ground awl 7 again ground, need stabilize supporting leg 6 to the outside upset, enlarge the holding area, improve the stability to equipment support.
Specifically, according to fig. 1 and fig. 3, in this embodiment, the adjusting assembly 9 includes an adjusting screw 16 and a connecting column 17, a base plate 8 is fixed at the bottom end of the connecting column 17, an adjusting cavity 15 capable of accommodating the connecting column 17 is formed in the supporting rod 4, the adjusting screw 16 is supported and installed in the adjusting cavity 15 through a bearing, and a threaded deep groove 18 matched with the adjusting screw 16 is formed in the connecting column 17; the horizontal tangent plane of bracing piece 4 and spliced pole 17 is equilateral triangle structure, when adjusting monitoring head 1's height, rotates adjusting screw 16, and under the screw thread closes the effect soon, spliced pole 17 can remove along adjusting chamber 15, and chassis 8 ground connection, therefore the height of bracing piece 4 can change, monitoring head 1's high change.
Specifically, according to fig. 1 and fig. 3, in this embodiment, the adjusting assembly 9 further includes a hand wheel 19, a driving bevel gear 20 and a driven bevel gear 21, the hand wheel 19 is disposed on the support rod 4 through a bearing support frame, the driving bevel gear 20 is fixed on a central shaft of the hand wheel 19 and is located in the adjusting cavity 15, the driven bevel gear 21 is fixed on the adjusting screw 16 and is engaged with the driving bevel gear 20, when the height of the monitoring head 1 is adjusted, the hand wheel 19 is rotated, the driving bevel gear 20 is rotated by the hand wheel 19, and the adjusting screw 16 is driven to rotate by the driven bevel gear 21 under the engagement relationship, under the screwing action of the threads, the connecting column 17 moves along the adjusting cavity 15, the chassis 8 is grounded, so that the height of the support rod 4 is changed, and the height of the monitoring head 1 is changed.
Specifically, according to fig. 1 and fig. 2, in the present embodiment, the locking assembly includes a locking screw 12, the locking screw 12 is screwed and fixed on the ferrule 5 through threads, a pushing piece 13 is mounted on an insertion end of the locking screw 12 by using a bearing, a knob 11 is fixed at an outer end of the locking screw 12, when the height of the ferrule 5 needs to be adjusted, the locking screw 12 is firstly unscrewed, and after the height of the ferrule 5 is adjusted, the locking screw 12 is screwed, so that the pushing piece 13 is tightly attached to the outer wall of the support rod 4.
Specifically, according to fig. 1 and 2, in the present embodiment, the anti-slip rubber pad 14 is adhered and fixed on the surface of the pushing piece 13, so as to increase the friction force, thereby further improving the stability of the height-adjusted ferrule 5.
Specifically, as shown in fig. 1 and 4, the present embodiment further includes a linkage assembly 10, where the linkage assembly 10 includes a sleeve 22, a connecting rod 23 and a collar 24, the connecting rod 23 is provided with three rings and fixed on the outer wall of the sleeve 22 at equal intervals, and the collar 24 is hinged at an end of the connecting rod 23; the support rod 4 can run through the sleeve 22, and the stabilizing support leg 6 can run through the lantern ring 24, so, when the height of the hoop 5 is reduced, or one of the stabilizing support legs 6 is turned towards the outside, under the effect of the linkage assembly 10, the three stabilizing support legs 6 are turned over simultaneously, and the same inclination angle is ensured, so that the stability of supporting the equipment can be further improved.
The utility model discloses a theory of operation and use flow: the utility model discloses an unmanned aerial vehicle control monitoring radar, when using, place the device in suitable position department, the stabilizing support leg 6 expandes certain angle to insert ground awl 7 and stabilize equipment, utilize monitoring head 1 to monitor unmanned aerial vehicle, to the actual use needs, can utilize adjusting part 9 to adjust the height of bracing piece 4, in order to adjust the height of monitoring head 1;
in addition, when heightening monitoring head 1, after the altitude mixture control of monitoring head 1 was good, remove the locking subassembly, pull out ground awl 7 earlier, adjust cuff 5 along bracing piece 4 downwards, at this moment, insert ground awl 7 into ground again if need, need the outside upset stabilizing support leg 6, enlarge the holding area, improve the stability of supporting to equipment.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle control monitoring radar, includes monitoring head (1), mount pad (2) and revolving stage (3), mount pad (2) are installed revolving stage (3) top surface, monitoring head (1) utilize the pivot to install on mount pad (2), its characterized in that: the device is characterized by further comprising a support rod (4) and a hoop (5), wherein the hoop (5) is sleeved on the support rod (4), the outer wall of the hoop (5) is hinged with three stable support legs (6) which are distributed in an annular and equidistant mode, the bottom end of each stable support leg (6) is hinged with a ground cone (7), and three groups of locking assemblies which are distributed in an annular and equidistant mode are mounted on the hoop (5); an adjusting component (9) for adjusting the height of the supporting rod (4) is arranged in the supporting rod (4).
2. The unmanned aerial vehicle regulation monitoring radar of claim 1, wherein: the adjusting assembly (9) comprises an adjusting screw rod (16) and a connecting column (17), a base plate (8) is fixed at the bottom end of the connecting column (17), an adjusting cavity (15) capable of accommodating the connecting column (17) is formed in the supporting rod (4), the adjusting screw rod (16) is supported and installed in the adjusting cavity (15) through a bearing, and a threaded deep groove (18) matched with the adjusting screw rod (16) is formed in the connecting column (17); the transverse sections of the support rod (4) and the connecting column (17) are both rectangular structures.
3. The unmanned aerial vehicle regulation monitoring radar of claim 2, wherein: adjusting part (9) still include hand wheel (19), initiative umbelliform gear (20) and driven umbelliform gear (21), hand wheel (19) are established through bearing support frame on bracing piece (4), initiative umbelliform gear (20) are fixed on the center pin of hand wheel (19) and be in adjust in chamber (15), driven umbelliform gear (21) are fixed adjusting screw (16) are last and with initiative umbelliform gear (20) meshing links to each other.
4. The unmanned aerial vehicle regulation monitoring radar of claim 1, wherein: the locking assembly comprises a locking screw rod (12), the locking screw rod (12) is screwed and fixed on the hoop (5) through threads, a push sheet (13) is installed on the embedding end of the locking screw rod (12) through a bearing, and a knob (11) is fixed at the outer end of the locking screw rod (12).
5. The unmanned aerial vehicle regulation monitoring radar of claim 4, wherein: and an anti-slip rubber gasket (14) is bonded and fixed on the surface of the push sheet (13).
6. The unmanned aerial vehicle regulation monitoring radar of claim 1, wherein: the linkage assembly (10) comprises a sleeve (22), three connecting rods (23) and a sleeve ring (24), the connecting rods (23) are annularly and equidistantly fixed on the outer wall of the sleeve (22), and the sleeve ring (24) is hinged to the end part of the connecting rod (23); the support rod (4) may extend through the sleeve (22) and the stabilizing support leg (6) may extend through the collar (24).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022648549.5U CN213517531U (en) | 2020-11-17 | 2020-11-17 | Unmanned aerial vehicle control monitoring radar |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022648549.5U CN213517531U (en) | 2020-11-17 | 2020-11-17 | Unmanned aerial vehicle control monitoring radar |
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| CN213517531U true CN213517531U (en) | 2021-06-22 |
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| CN202022648549.5U Active CN213517531U (en) | 2020-11-17 | 2020-11-17 | Unmanned aerial vehicle control monitoring radar |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115338678A (en) * | 2022-09-21 | 2022-11-15 | 马鞍山市皖晓旅游用品制造有限责任公司 | Horizontal numerical control lathe |
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2020
- 2020-11-17 CN CN202022648549.5U patent/CN213517531U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115338678A (en) * | 2022-09-21 | 2022-11-15 | 马鞍山市皖晓旅游用品制造有限责任公司 | Horizontal numerical control lathe |
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