CN209839634U - Unmanned aerial vehicle image acquisition equipment intelligent regulation device - Google Patents
Unmanned aerial vehicle image acquisition equipment intelligent regulation device Download PDFInfo
- Publication number
- CN209839634U CN209839634U CN201920729295.4U CN201920729295U CN209839634U CN 209839634 U CN209839634 U CN 209839634U CN 201920729295 U CN201920729295 U CN 201920729295U CN 209839634 U CN209839634 U CN 209839634U
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- image acquisition
- aerial vehicle
- unmanned aerial
- acquisition equipment
- 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
Landscapes
- Studio Devices (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle image acquisition equipment intelligent regulation device, through the cooperation of a motor, a first screw rod, a telescopic link and a lantern ring, the first screw rod is driven to rotate after the motor is started, the motor can move back and forth, the motor can drive a slide rod to move back and forth through the cooperation of a first bearing and the slide rod, through the cooperation of the slide rod and a pan-tilt head, the pan-tilt head is driven by the motor to move as well, through the electrical connection of a gyroscope sensor, a control device and the motor, when the pan-tilt head moves relatively, the motor is controlled to rotate through the control device, so that the relative rest of the pan-tilt head and an unmanned aerial vehicle Z shaft is achieved, the image acquisition equipment can keep X, Y shaft and the unmanned aerial vehicle relatively still through the cooperation of the pan-tilt head and the motor, the image acquisition equipment can move X, Y, Z shafts, so that the image acquisition equipment and the unmanned aerial vehicle can keep, the imaging effect of the image acquisition equipment is improved, and the working efficiency is improved.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle image acquisition technical field, concrete field is an unmanned aerial vehicle image acquisition equipment intelligent regulation device.
Background
The unmanned aerial vehicle aerial image has the advantages of high definition, large scale, small area and high availability. The unmanned aerial vehicle image acquisition equipment is particularly suitable for acquiring aerial images (roads, railways, rivers, reservoirs, coastlines and the like) in banded regions, the unmanned aerial vehicle provides a remote sensing platform which is convenient to operate and easy to transfer to a place, take-off and landing are less limited by the place, the unmanned aerial vehicle can take off and land on playgrounds, highways or other open grounds, the unmanned aerial vehicle image acquisition equipment is good in stability and safety and very easy to transfer to the place, but the existing unmanned aerial vehicle image acquisition equipment cannot effectively counteract shaking generated when the unmanned aerial vehicle flies, the phenomenon that the images are taken are not clear frequently occurs, the problem is slightly solved due to the occurrence of the cradle head, but the cradle head only can enable the image acquisition equipment to keep X, Y relatively still, the relative still on the Z axis cannot be kept, the shooting effect is still not good enough, the problem can be solved by shooting for multiple times, and the working efficiency.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle image acquisition equipment intelligent regulation device to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: an intelligent adjusting device of unmanned aerial vehicle image acquisition equipment comprises a shell, wherein the front side wall of the shell is provided with an opening, the lower surface of the shell is fixedly connected with an unmanned aerial vehicle, the upper surface of an inner cavity of the shell is fixedly connected with one end of a first partition plate, the right side wall of the inner cavity of the shell is fixedly connected with one end of a second partition plate, the other end of the first partition plate is fixedly connected with the other end of the second partition plate, the rear ends of the first partition plate and the second partition plate are fixedly connected with the rear side wall of the inner cavity of the shell, the side wall of the first partition plate is provided with a sliding groove, a sliding rod is inserted in the sliding groove in a sliding manner, one end of the sliding rod, which is positioned on the right side of the first partition plate, is fixedly connected with a clamping device, the lower part of the clamping device is fixedly connected with a first sliding block, the front end of the clamping device is fixedly connected with a gyroscope sensor, the other end of the sliding rod is fixedly connected with a first bearing, the rear side wall of the shell is fixedly connected with a telescopic rod, the front end of the telescopic rod is fixedly connected with a motor, the output end of the motor is fixedly connected with a first screw rod, the inner wall of the first bearing is fixedly sleeved with the first screw rod, the side wall of the first screw rod is screwed with a lantern ring, the left side wall of the lantern ring is fixedly connected with the inner wall of the shell, the inner part of the clamping device is clamped with a holder, the top end of the holder is fixedly connected with an image acquisition device, the rear side wall of the inner cavity of the shell is fixedly connected with a control device which is positioned at the rear side of the clamping device, the surface fixedly connected with battery under the shell inner chamber, controlling means and the equal electric connection of battery, motor and gyroscope sensor, image acquisition equipment corresponds the setting with the opening.
Preferably, clamping device include with slide bar fixed connection's base, the last fixed surface of base is connected with splint, the last fixed surface of base is connected with the fixed block, the fixed block is located the front side of splint, the through-hole has been seted up to the preceding lateral wall of fixed block, through-hole inner wall spiro union has the second screw rod, the second screw rod is located the one end fixedly connected with knob of fixed block front side, the fixed cover of the other end lateral wall of second screw rod has connect the second bearing, the back side fixedly connected with arc of second bearing, the back lateral wall fixedly connected with spring of arc, the quantity of spring is a plurality of, every the side all with rubber pad fixed connection behind the spring.
Preferably, the inner wall of the opening is clamped with a rubber plug.
Preferably, the rear side wall of the rubber pad is provided with convex particles.
Preferably, the telescopic link include with shell inner wall fixed connection's first festival pole, the inner wall left and right sides of first festival pole all is equipped with the second slide, two the inside sliding connection of second slide has the second slider, two the inboard of second slider all with second festival pole fixed connection.
Compared with the prior art, the beneficial effects of the utility model are that: an intelligent adjusting device for image acquisition equipment of an unmanned aerial vehicle, through a motor, a first screw rod, a telescopic rod and a lantern ring, the motor drives the first screw rod to rotate after being started, thereby achieving the purpose of enabling the motor to move back and forth, the rotating force of the first screw rod is offset through a first bearing, the motor can drive a sliding rod to move back and forth when moving through the cooperation of the first bearing and the sliding rod, the tripod head is driven by the motor to move through the cooperation of the sliding rod and the tripod head, through a gyroscope sensor on the tripod head, the control device is electrically connected with the motor, when the relative motion of the tripod head is achieved, the gyroscope sensor transmits a signal to the control device, and the motor is controlled to rotate through the control device, thereby achieving the relative rest of the tripod head and the Z axis of the unmanned aerial vehicle, the image acquisition equipment can keep X, Y relative rest with the unmanned aerial vehicle through, this device passes through the cooperation of cloud platform and motor, makes image acquisition equipment can carry out X, Y, Z triaxial motion, makes image acquisition equipment and unmanned aerial vehicle can keep the state of relative stillness, improves image acquisition equipment's formation of image effect, improves work efficiency.
Drawings
FIG. 1 is a schematic view of the main sectional structure of the present invention;
fig. 2 is a schematic view of the structure of the present invention;
FIG. 3 is a schematic view of the cross-sectional view of the present invention;
FIG. 4 is a schematic view of the structure at A in FIG. 3;
fig. 5 is a schematic cross-sectional structure diagram of the middle telescopic rod of the present invention.
In the figure: 1-shell, 2-first partition plate, 3-second partition plate, 4-sliding chute, 5-sliding rod, 6-clamping device, 601-base, 602-clamping plate, 603-fixing block, 604-through hole, 605-second screw rod, 606-knob, 607-second bearing, 608-arc plate, 609-spring, 610-rubber pad, 7-first slide block, 8-first slide way, 9-gyroscope sensor, 10-first bearing, 11-telescopic rod, 111-first section rod, 112-second section rod, 113-second slide block, 114-second slide way, 12-motor, 13-first screw rod, 14-lantern ring, 15-tripod head, 16-control device, 17-storage battery, 18-image acquisition equipment, 19-opening, 20-rubber plug, 21-convex grain.
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.
Referring to fig. 1-5, the present invention provides a technical solution: an intelligent adjusting device of an unmanned aerial vehicle image acquisition device comprises a shell 1, wherein the front side wall of the shell 1 is provided with an opening 19, the lower surface of the shell 1 is fixedly connected with an unmanned aerial vehicle, the upper surface of an inner cavity of the shell 1 is fixedly connected with one end of a first partition plate 2, the right side wall of the inner cavity of the shell 1 is fixedly connected with one end of a second partition plate 3, the other end of the first partition plate 2 is fixedly connected with the other end of the second partition plate 3, the rear ends of the first partition plate 2 and the second partition plate 3 are fixedly connected with the rear side wall of the inner cavity of the shell 1, the side wall of the first partition plate 2 is provided with a sliding groove 4, a sliding rod 5 is inserted in the sliding groove 4 in a sliding manner, one end of the sliding rod 5, which is positioned on the right side of the first partition plate 2, the lower part of the clamping device 6 is fixedly connected with a first sliding block, the first slide rail 8 is connected with a first slide block 7 in a sliding manner, a gyroscope sensor 9 is fixedly connected at the front end of the clamping device 6, a first bearing 10 is fixedly connected at the other end of the slide bar 5, a telescopic rod 11 is fixedly connected at the rear side wall of the shell 1, a motor 12 is fixedly connected at the front end of the telescopic rod 11, a first screw 13 is fixedly connected at the output end of the motor 12, the inner wall of the first bearing 10 is fixedly sleeved with the first screw 13, a lantern ring 14 is screwed at the side wall of the first screw 13, the left side wall of the lantern ring 14 is fixedly connected with the inner wall of the shell 1, a tripod head 15 is clamped inside the clamping device 6, an image acquisition device 18 is fixedly connected at the top end of the tripod head 15, a control device 16 is fixedly connected at the rear side wall of the inner cavity of the shell 1, the control device 16 is positioned at the rear side of the clamping device, the control device 16 is electrically connected with the storage battery 17, the motor 12 and the gyroscope sensor 9, and the image acquisition equipment 18 is arranged corresponding to the opening 19.
The device internal parts are protected through the shell 1, the device and the unmanned aerial vehicle are kept static relatively, a photographing window is provided for the image acquisition equipment 18 through the opening 19, the sliding groove 4 and the first slide rail 8 are provided through the first partition plate 2 and the second partition plate 3, the sliding groove 4, the sliding rod 5, the first sliding block 7 and the first slide rail 8 are matched to limit the movement track, the motor 12 is started to drive the first screw 13 to rotate through the matching of the motor 12, the first screw 13, the telescopic rod 11 and the lantern ring 14, so that the motor 12 can move back and forth, the rotating force of the first screw 13 is counteracted through the first bearing 10, the sliding rod 5 can be driven to move back and forth through the matching of the first bearing 10 and the sliding rod 5, the tripod head 15 is driven by the motor 12 to move through the matching of the sliding rod 5 and the tripod head 15, and the gyroscope sensor 9 on the tripod head 15 are used for providing a photographing window for the image acquisition equipment 18, controlling means 16 and motor 12's electric connection, when reaching cloud platform 15 and taking place relative motion, gyroscope sensor 9 transmission signal gives controlling means 16 to rotate motor 12 control motor 12 through controlling means 16, thereby reach and make cloud platform 15 and unmanned aerial vehicle Y epaxial relative still, make image acquisition equipment 18 can keep X, Z on with unmanned aerial vehicle relative still through cloud platform 15. The device is supplied with electrical energy via an accumulator 17.
Specifically, the clamping device 6 includes a base 601 fixedly connected to the sliding rod 5, a clamping plate 602 is fixedly connected to the upper surface of the base 601, a fixed block 603 is fixedly connected to the upper surface of the base 601, the fixed block 603 is located on the front side of the clamping plate 602, a through hole 604 is formed in the front side wall of the fixed block 603, a second screw 605 is screwed to the inner wall of the through hole 604, a knob 606 is fixedly connected to one end of the second screw 605 located on the front side of the fixed block 603, a second bearing 607 is fixedly connected to the other end side wall of the second screw 605, an arc-shaped plate 608 is fixedly connected to the rear side end of the second bearing 607, a spring 609 is fixedly connected to the rear side wall of the arc-shaped plate 608, the number of the springs 609 is multiple, and the rear side end of each.
The clamping plate 602 and the fixing block 603 are supported by the base 601, the second screw 605 can move back and forth in the rotating process by matching the second screw 605 with the through hole 604, the second screw 605 can conveniently rotate by the knob 606, the rotating force of the second screw 605 is counteracted by the second bearing 607, so that the arc-shaped plate 608 only receives push-pull force, the clamping device 6 can clamp the pan-tilt 15 with different sizes by the spring 609 and the rubber pad 610, and the clamping effect is good.
Specifically, a rubber stopper 20 is snapped on the inner wall of the opening 19.
When not in use, the opening 19 can be sealed by the rubber plug 20 to achieve the purpose of dust prevention, and when in use, the rubber plug is taken down.
Specifically, the rear sidewall of the rubber pad 610 is provided with a convex particle 21.
The friction force is increased by the convex particles 21, so that the purpose of increasing the clamping effect is achieved.
Specifically, the telescopic rod 11 includes the first section of pole 111 with shell 1 inner wall fixed connection, the inner wall left and right sides of first section of pole 111 all is equipped with second slide 114, two the inside sliding connection of second slide 114 has second slider 113, two the inboard of second slider 113 all with second section of pole 112 fixed connection.
Through the cooperation of the first section rod 111, the second section rod 112, the second sliding block 113 and the second sliding way 114, the telescopic rod 11 can only do telescopic motion and can not rotate, and the phenomenon that the motor 12 body rotates and the device fails is prevented.
The working principle is as follows: through the cooperation of motor 12, first screw 13, telescopic link 11 and lantern ring 14, make motor 12 drive first screw 13 rotatory after starting, thereby reach the mesh that can make motor 12 back-and-forth movement, offset the revolving force of first screw 13 through first bearing 10, can drive slide bar 5 fore-and-aft movement when making motor 12 move through the cooperation of first bearing 10 and slide bar 5, through the cooperation of slide bar 5 and cloud platform 15, make cloud platform 15 receive motor 12's drive and move equally, through the electrical connection of gyroscope sensor 9 on cloud platform 15, controlling means 16 and motor 12, when reaching cloud platform 15 and taking place relative motion, gyroscope sensor 9 transmits the signal to controlling means 16, and control motor 12 through controlling means 16 and rotate, thereby reach and make cloud platform 15 and unmanned aerial vehicle Z epaxial relative stillness, make image acquisition equipment 18 can keep X, through cloud platform 15, And the Y is relatively static with the unmanned aerial vehicle.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides an unmanned aerial vehicle image acquisition equipment intelligent regulation device, includes shell (1), its characterized in that: the unmanned aerial vehicle is characterized in that an opening (19) is formed in the front side wall of the shell (1), the lower surface of the shell (1) is fixedly connected with an unmanned aerial vehicle, one end of a first partition plate (2) is fixedly connected to the upper surface of an inner cavity of the shell (1), one end of a second partition plate (3) is fixedly connected to the right side wall of the inner cavity of the shell (1), the other end of the first partition plate (2) is fixedly connected with the other end of the second partition plate (3), the rear ends of the first partition plate (2) and the second partition plate (3) are fixedly connected with the rear side wall of the inner cavity of the shell (1), a sliding groove (4) is formed in the side wall of the first partition plate (2), a sliding rod (5) is inserted in the sliding groove (4), a clamping device (6) is fixedly connected to one end, located on the right side of the first partition plate (2), of the clamping device (6), and a first, the upper surface of the second partition plate (3) is provided with a first slide way (8), the first slide way (8) is connected with a first sliding block (7) in a sliding manner, the front end of the clamping device (6) is fixedly connected with a gyroscope sensor (9), the other end of the slide rod (5) is fixedly connected with a first bearing (10), the rear side wall of the shell (1) is fixedly connected with a telescopic rod (11), the front end of the telescopic rod (11) is fixedly connected with a motor (12), the output end of the motor (12) is fixedly connected with a first screw rod (13), the inner wall of the first bearing (10) is fixedly sleeved with the first screw rod (13), the side wall of the first screw rod (13) is screwed with a lantern ring (14), the left side wall of the lantern ring (14) is fixedly connected with the inner wall of the shell (1), and a tripod head (15) is clamped inside the clamping device (6), top fixedly connected with image acquisition equipment (18) of cloud platform (15), lateral wall fixedly connected with controlling means (16) behind the inner chamber of shell (1), controlling means (16) are located the rear side of clamping device (6), surface fixedly connected with battery (17) under shell (1) inner chamber, controlling means (16) and battery (17), motor (12) and the equal electric connection of gyroscope sensor (9), image acquisition equipment (18) correspond the setting with opening (19).
2. The intelligent adjusting device for the unmanned aerial vehicle image acquisition equipment according to claim 1, characterized in that: the clamping device (6) comprises a base (601) fixedly connected with the sliding rod (5), the upper surface of the base (601) is fixedly connected with a clamping plate (602), the upper surface of the base (601) is fixedly connected with a fixing block (603), the fixing block (603) is positioned at the front side of the clamping plate (602), the front side wall of the fixing block (603) is provided with a through hole (604), a second screw rod (605) is screwed on the inner wall of the through hole (604), a knob (606) is fixedly connected at one end of the second screw rod (605) positioned at the front side of the fixed block (603), a second bearing (607) is fixedly sleeved on the side wall of the other end of the second screw rod (605), the rear side end of the second bearing (607) is fixedly connected with an arc-shaped plate (608), the rear side wall of the arc-shaped plate (608) is fixedly connected with a plurality of springs (609), the number of the springs (609) is multiple, and the rear side end of each spring (609) is fixedly connected with a rubber pad (610).
3. The intelligent adjusting device for the unmanned aerial vehicle image acquisition equipment according to claim 1, characterized in that: the inner wall of the opening (19) is clamped with a rubber plug (20).
4. The intelligent adjusting device for the unmanned aerial vehicle image acquisition equipment according to claim 2, characterized in that: the rear side wall of the rubber pad (610) is provided with convex particles (21).
5. The intelligent adjusting device for the unmanned aerial vehicle image acquisition equipment according to claim 1, characterized in that: telescopic link (11) include with shell (1) inner wall fixed connection's first festival pole (111), the inner wall left and right sides of first festival pole (111) all is equipped with second slide (114), two the inside sliding connection of second slide (114) has second slider (113), two the inboard of second slider (113) all with second festival pole (112) fixed connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920729295.4U CN209839634U (en) | 2019-05-21 | 2019-05-21 | Unmanned aerial vehicle image acquisition equipment intelligent regulation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920729295.4U CN209839634U (en) | 2019-05-21 | 2019-05-21 | Unmanned aerial vehicle image acquisition equipment intelligent regulation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209839634U true CN209839634U (en) | 2019-12-24 |
Family
ID=68897752
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920729295.4U Expired - Fee Related CN209839634U (en) | 2019-05-21 | 2019-05-21 | Unmanned aerial vehicle image acquisition equipment intelligent regulation device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209839634U (en) |
-
2019
- 2019-05-21 CN CN201920729295.4U patent/CN209839634U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106394919A (en) | Rotor wing unmanned aerial vehicle with angle-adjustable aerial photography camera and storage structure | |
| CN108423164A (en) | A kind of clamshell phone unmanned plane | |
| CN205113735U (en) | Electronic fixed wing uavs of three camera oblique photography | |
| CN209839634U (en) | Unmanned aerial vehicle image acquisition equipment intelligent regulation device | |
| CN113716056A (en) | Camera linkage that civil unmanned aerial vehicle was taken photo by plane | |
| CN114701655A (en) | Data acquisition device based on unmanned aerial vehicle survey and drawing | |
| CN205396569U (en) | Unmanned vehicles with battery formula counter weight device | |
| CN207725613U (en) | A kind of unmanned plane with camera function | |
| CN219468052U (en) | Photogrammetry airborne multi-view stereoscopic aviation remote sensing device | |
| CN210979131U (en) | Adjustable 3D camera shooting pan-tilt | |
| CN112623208B (en) | Unmanned aerial vehicle for aerial photography | |
| CN109515729A (en) | A kind of unmanned plane camera mounting support and aerial surveying camera of photographing | |
| CN212968066U (en) | Unmanned aerial vehicle data transmission directional antenna | |
| CN214690245U (en) | Automatic rotating device for oblique photogrammetry | |
| CN205877612U (en) | Adjustable support and contain camera device of this support | |
| CN111470057A (en) | Unmanned aerial photography device capable of freely adjusting shooting angle | |
| CN113277082A (en) | Unmanned aerial vehicle is patrolled and examined to electric power | |
| CN216887225U (en) | Unmanned aerial vehicle for engineering survey | |
| CN210284127U (en) | Panoramic lifting vehicle-mounted holder | |
| CN113306703A (en) | But balanced survey and drawing unmanned aerial vehicle of automatically regulated | |
| CN216035183U (en) | Unmanned aerial vehicle oblique photography integration data acquisition equipment | |
| CN220243561U (en) | Adjustable limit structure of camera | |
| CN215862768U (en) | Portable installed stability augmentation monitoring device | |
| CN219257725U (en) | A photographic arrangement for unmanned aerial vehicle survey and drawing | |
| CN110677570A (en) | Four-eye pan-tilt camera based on thermal infrared technology |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191224 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |