CN210083572U - Searchlighting mechanism for agricultural unmanned aerial vehicle - Google Patents
Searchlighting mechanism for agricultural unmanned aerial vehicle Download PDFInfo
- Publication number
- CN210083572U CN210083572U CN201920278008.2U CN201920278008U CN210083572U CN 210083572 U CN210083572 U CN 210083572U CN 201920278008 U CN201920278008 U CN 201920278008U CN 210083572 U CN210083572 U CN 210083572U
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- searchlight
- connecting plate
- vertical
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Landscapes
- Catching Or Destruction (AREA)
Abstract
The utility model discloses a searchlight mechanism for agricultural unmanned aerial vehicle, including unmanned aerial vehicle body, connecting plate, searchlight and buffer, the below of unmanned aerial vehicle body is provided with the connecting plate, the vertical section of connecting plate sets up to "U" type, vertical bolt and unmanned aerial vehicle body fixed connection are passed through to the horizontal portion of connecting plate, the outer lane of the vertical bearing frame of fixedly connected with in the circular through-hole that two sets of vertical portions of connecting plate adjacent side bore established, the equal fixed welding of inner circle of two sets of vertical bearing frames has the axis of rotation, installs the searchlight between two sets of axis of rotation, and the fixed welding of one end of searchlight has the commentaries on classics board in a set of axis of rotation, the fixed device of fixing of side fixedly connected with and commentaries on classics board of vertical portion of connecting plate, the buffer. The searchlighting mechanism for the agricultural unmanned aerial vehicle can adjust the illumination effect, so that the agricultural unmanned aerial vehicle is suitable for various use environments.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to searchlighting mechanism for agricultural unmanned aerial vehicle.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like. In the agricultural work at night, need large-scale searchlight to throw light on, go on in some special work, need diversified illumination, just need use unmanned aerial vehicle to provide the illumination this time, but traditional unmanned aerial vehicle can't realize the illuminating effect of high strength, and the illuminating effect is not adjustable.
Therefore, in order to meet the current situation, the search mechanism for the agricultural unmanned aerial vehicle needs to be designed and produced urgently to meet the actual use requirement.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an agricultural unmanned aerial vehicle is with searchlighting mechanism to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a searchlight mechanism for an agricultural unmanned aerial vehicle comprises an unmanned aerial vehicle body, a connecting plate, searchlights and a buffer device, wherein the connecting plate is arranged below the unmanned aerial vehicle body, the vertical section of the connecting plate is set to be U-shaped, the transverse part of the connecting plate is fixedly connected with the unmanned aerial vehicle body through vertical bolts, the outer rings of vertical bearing seats are fixedly connected in circular through holes drilled in the adjacent sides of two groups of vertical parts of the connecting plate, rotating shafts are fixedly welded on the inner rings of the two groups of vertical bearing seats, the searchlights are installed between the two groups of rotating shafts, one ends, away from the searchlights, of the rotating plates are fixedly welded on one ends of the rotating shafts, and the sides of the vertical parts of the connecting plate;
the bottom fixed welding of unmanned aerial vehicle body has the buffer of four groups of rectangle array arrangements, buffer's lower half rotates and is connected with the universal wheel.
Preferably, fixing device includes fixed plate and puller bolt, the vertical section of fixed plate sets up to "L" type, the vertical portion of fixed plate bores and is equipped with horizontal screw hole, and horizontal screw hole female connection has the puller bolt, the side of changeing the board is bored and is equipped with the horizontal through-hole that the multiunit was arranged at commentaries on classics board side annular array, and the one end setting of puller bolt is in a set of horizontal through-hole of changeing the board.
Preferably, the periphery of the rotating plate is provided with anti-skid grains convenient to rotate, and the side surface of the rotating plate is further provided with angle scale marks.
Preferably, buffer includes hollow tube, compression spring and montant, the one end of montant and the bottom fixed connection of unmanned aerial vehicle body, the other end setting of montant is at the inner chamber of hollow tube, the bottom of hollow tube sets up to closed structure, pass through compression spring fixed connection between the bottom of montant and the horizontal inner wall of hollow tube.
Preferably, the bottom of searchlight is connected with the camera through L shaped plate, also be connected with the battery through L shaped plate in the unmanned aerial vehicle body.
The utility model discloses a technological effect and advantage: this searchlight mechanism for agricultural unmanned aerial vehicle, fixing device through the setting, the position of the horizontal through-hole of the fixed commentaries on classics board of adjustment jack bolt, make the orientation angle regulation of searchlight become simple, and utilize the fixed plate to make fixed very stable, orientation angle and the distance of unmanned aerial vehicle body and target ground through the adjustment searchlight, make the illuminating effect change, thereby adapt to multiple service environment, buffer and the universal wheel through the setting, make the take-off and landing of unmanned aerial vehicle body become safety, meet under the special circumstances, buffer's buffering and the removal of universal wheel make searchlight and camera obtain the protection, reduce its possibility that receives the damage, this searchlight mechanism for agricultural unmanned aerial vehicle, can obtain the regulation to the effect of illumination, thereby adapt to multiple service environment.
Drawings
Fig. 1 is a front view of the present invention;
fig. 2 is a schematic structural view of the fixing device of the present invention;
fig. 3 is a sectional view of the buffering device of the present invention.
In the figure: 1 unmanned aerial vehicle body, 2 connecting plates, 4 searchlights, 5 commentaries on classics board, 6 fixing device, 7 buffer, 8 universal wheels, 9 fixed plates, 10 puller bolts, 11 horizontal through-holes, 12 hollow tubes, 13 compression spring, 14 montants, 15L shaped plates, 16 cameras, 17 batteries.
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.
Unless defined otherwise, all references to up, down, left, right, front, back, inner and outer directions herein are to be interpreted as referring to up, down, left, right, front, back, inner and outer directions in the drawings to which the invention is applied, and all references are hereby incorporated herein by reference.
The utility model provides a searchlight mechanism for an agricultural unmanned aerial vehicle as shown in figures 1-3, which comprises an unmanned aerial vehicle body 1, a connecting plate 2, a searchlight 4 and a buffer device 7, a connecting plate 2 is arranged below the unmanned aerial vehicle body 1, the vertical section of the connecting plate 2 is U-shaped, the transverse part of the connecting plate 2 is fixedly connected with the unmanned aerial vehicle body 1 through a vertical bolt, the outer rings of vertical bearing seats are fixedly connected in circular through holes drilled in the adjacent sides of two groups of vertical parts of the connecting plate 2, rotating shafts are fixedly welded on the inner rings of the two groups of vertical bearing seats, a searchlight 4 is installed between the two groups of rotating shafts, the searchlight 4 is set as a sea king powerful searchlight, a rotating plate 5 is fixedly welded at one end of one group of rotating shafts, which is far away from the searchlight 4, the side surface of the vertical part of the connecting plate 2 is fixedly connected with a fixing device 6 fixed with the rotating plate 5;
the fixed welding of bottom of unmanned aerial vehicle body 1 has four groups of buffer 7 that the rectangle array was arranged, buffer 7's lower half rotates and is connected with universal wheel 8.
Specifically, fixing device 6 includes fixed plate 9 and puller bolt 10, the vertical section of fixed plate 9 sets up to "L" type, the vertical portion of fixed plate 9 bores and is equipped with horizontal screw hole, and horizontal screw hole female connection has puller bolt 10, the side of changeing board 5 is bored and is equipped with the horizontal through-hole 11 that the multiunit was being changeed 5 side ring array and is arranged, and the one end setting of puller bolt 10 is in a set of horizontal through-hole 11 of changeing board 5, and the fixed rotation that makes changeing board 5 through puller bolt 10 is adjusted more conveniently.
Specifically, the periphery of the rotating plate 5 is provided with anti-skid grains convenient to rotate, and the side surface of the rotating plate 5 is further provided with angle scale marks, so that the rotating angle can be clear, controllable and controllable.
Specifically, buffer 7 includes hollow tube 12, pressure spring 13 and montant 14, the one end of montant 14 and the bottom fixed connection of unmanned aerial vehicle body 1, the other end setting of montant 14 is at the inner chamber of hollow tube 12, the bottom of hollow tube 12 sets up to closed structure, pass through pressure spring 13's elasticity through pressure spring 13 fixed connection between the bottom of montant 14 and the horizontal inner wall of hollow tube 12, make it obtain the buffer capacity, the rotation of the universal wheel of setting has also reduced the resistance of horizontal direction.
Specifically, the bottom of searchlight 4 is connected with camera 16 through L shaped plate 15, also be connected with battery 17 through L shaped plate 15 in the unmanned aerial vehicle body 1, through the position of adjusting battery 17 for holistic focus can be adjusted.
Concretely, this searchlight mechanism for agricultural unmanned aerial vehicle, utilize vertical bolt with connecting plate 2 and 1 fixed connection of unmanned aerial vehicle body, then rotate commentaries on classics board 5 and make the orientation of searchlight 4 adjust reasonable position, rotate top tight bolt 10, make top tight bolt 10 support the inner wall of the transverse through-hole 11 of commentaries on classics board, thereby realize searchlight 4's fixed, whether select the bottom installation camera 16 at searchlight 4 as required, adjust the position of battery 17, make the centre of gravity position adjust central point as far as possible, under meetting special circumstances, take place to fall the machine and cross falling, utilize the rotation of universal wheel 8 and pressure spring 13's elasticity, make whole certain buffer capacity that obtains, and then searchlight 4 and camera 16 in the four buffer of group 7 of protection.
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 and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.
Claims (5)
1. The utility model provides a searchlight mechanism for agricultural unmanned aerial vehicle, includes unmanned aerial vehicle body (1), connecting plate (2), searchlight (4) and buffer (7), its characterized in that: a connecting plate (2) is arranged below the unmanned aerial vehicle body (1), the vertical section of the connecting plate (2) is set to be U-shaped, the transverse part of the connecting plate (2) is fixedly connected with the unmanned aerial vehicle body (1) through a vertical bolt, the outer rings of vertical bearing seats are fixedly connected in circular through holes drilled in the adjacent sides of two groups of vertical parts of the connecting plate (2), rotating shafts are fixedly welded on the inner rings of the two groups of vertical bearing seats, a searchlight (4) is installed between the two groups of rotating shafts, one end, far away from the searchlight (4), of one group of rotating shafts is fixedly welded with a rotating plate (5), and a fixing device (6) fixed with the rotating plate (5) is fixedly connected to the side of the vertical part of the connecting;
the bottom fixed welding of unmanned aerial vehicle body (1) has buffer (7) that four groups of rectangle arrays were arranged, the lower half of buffer (7) rotates and is connected with universal wheel (8).
2. The searchlighting mechanism for an agricultural unmanned aerial vehicle according to claim 1, wherein: fixing device (6) are including fixed plate (9) and puller bolt (10), the vertical section of fixed plate (9) sets up to "L" type, the vertical portion of fixed plate (9) bores and is equipped with horizontal screw hole, and horizontal screw hole female connection has puller bolt (10), the side of changeing board (5) is bored and is equipped with horizontal through-hole (11) that the multiunit was being changeed board (5) side annular array and is arranged, and the one end setting of puller bolt (10) is in a set of horizontal through-hole (11) of changeing board (5).
3. The searchlighting mechanism for an agricultural unmanned aerial vehicle according to claim 1, wherein: the anti-skidding lines convenient to rotate are arranged on the periphery of the rotating plate (5), and angle scale marks are further arranged on the side face of the rotating plate (5).
4. The searchlighting mechanism for an agricultural unmanned aerial vehicle according to claim 1, wherein: buffer (7) include hollow tube (12), compression spring (13) and montant (14), the one end of montant (14) and the bottom fixed connection of unmanned aerial vehicle body (1), the other end setting of montant (14) is at the inner chamber of hollow tube (12), the bottom of hollow tube (12) sets up to closed structure, through compression spring (13) fixed connection between the bottom of montant (14) and the horizontal inner wall of hollow tube (12).
5. The searchlighting mechanism for an agricultural unmanned aerial vehicle according to claim 1, wherein: the bottom of searchlight (4) is connected with camera (16) through L shaped plate (15), also be connected with battery (17) through L shaped plate (15) in unmanned aerial vehicle body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920278008.2U CN210083572U (en) | 2019-03-06 | 2019-03-06 | Searchlighting mechanism for agricultural unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920278008.2U CN210083572U (en) | 2019-03-06 | 2019-03-06 | Searchlighting mechanism for agricultural unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210083572U true CN210083572U (en) | 2020-02-18 |
Family
ID=69471525
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920278008.2U Expired - Fee Related CN210083572U (en) | 2019-03-06 | 2019-03-06 | Searchlighting mechanism for agricultural unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210083572U (en) |
-
2019
- 2019-03-06 CN CN201920278008.2U patent/CN210083572U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104590556B (en) | A kind of folding unmanned plane | |
| CN108146639B (en) | High-speed parachute landing system and method for recycling small and medium unmanned aerial vehicle and ejection parachute | |
| CN105035339B (en) | Zoom-type unmanned plane | |
| CN202657252U (en) | Vehicle-mounted flying frame | |
| CN210083572U (en) | Searchlighting mechanism for agricultural unmanned aerial vehicle | |
| CN205022913U (en) | Carry image signal collection system's flight equipment | |
| CN211969733U (en) | Unmanned aerial vehicle is with frame shock-absorbing structure that plays | |
| CN109760830B (en) | Environment surveying is with three leg module combination formula rotor unmanned aerial vehicle that prop | |
| CN213768958U (en) | Vertical take-off and landing fixed wing unmanned aerial vehicle | |
| CN215285257U (en) | A unmanned aerial vehicle for piping lane surveys | |
| CN211167391U (en) | Unmanned aerial vehicle undercarriage with transfer wheel | |
| CN211223860U (en) | Special indoor safe flying device of unmanned aerial vehicle | |
| CN212500950U (en) | Rescue unmanned aerial vehicle life buoy delivery device | |
| CN110758723B (en) | Unmanned aerial vehicle convenient to receive and release undercarriage | |
| CN208325627U (en) | A kind of anticollision is taken photo by plane remote sensing unmanned plane | |
| CN215794447U (en) | Unmanned aerial vehicle that multi-angle was noiseless shoots | |
| CN214649091U (en) | A unmanned aerial vehicle for piping lane surveys | |
| CN108001678B (en) | A variable rotor connecting device for unmanned aerial vehicle | |
| CN216102832U (en) | Unmanned aerial vehicle cloud platform quick detach device | |
| CN219001828U (en) | Unmanned aerial vehicle does investigation extinguishing device | |
| CN212074418U (en) | Unmanned aerial vehicle for geographic exploration | |
| CN220082669U (en) | Airport airspace management and control device | |
| CN112793777A (en) | Unmanned aerial vehicle with adjustable paddle angle | |
| CN215475727U (en) | Unmanned aerial vehicle flight buffer stop | |
| CN216805796U (en) | Unmanned aerial vehicle of AI intelligent control box loads |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200218 |