CN216994865U - A carrier centre gripping fixing device for unmanned aerial vehicle - Google Patents
A carrier centre gripping fixing device for unmanned aerial vehicle Download PDFInfo
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- CN216994865U CN216994865U CN202122769304.2U CN202122769304U CN216994865U CN 216994865 U CN216994865 U CN 216994865U CN 202122769304 U CN202122769304 U CN 202122769304U CN 216994865 U CN216994865 U CN 216994865U
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- unmanned aerial
- aerial vehicle
- sliding
- support
- rod
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- 230000000694 effects Effects 0.000 claims description 4
- 238000013016 damping Methods 0.000 description 8
- 239000000463 material Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
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Abstract
The utility model provides a carrier clamping and fixing device for an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. According to the utility model, the springs are elastically connected to the upper end and the lower end of the outer side of the supporting rod B close to the outer side of the sliding rod, when a user controls the unmanned aerial vehicle to land after aerial photography processing is carried out in the air, the user controls the unmanned aerial vehicle to descend, the supporting frame is in contact with the ground, the sliding rod is pushed to slide on the outer side of the supporting rod B through the sliding block, the springs are pressed and rebounded, and the supporting frame is prevented from being impacted too much while the vibration generated by the unmanned aerial vehicle is weakened.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a clamping and fixing device for a carrier of an unmanned aerial vehicle.
Background
A drone is a device that flies without a human being, using radio remote control devices and self-contained programs.
Wherein, the research shows that the patent number is CN 201920988183.0A damping clamping mechanism of unmanned aerial vehicle, the damping clamping mechanism of the unmanned aerial vehicle is provided with the landing gear device and the damping device, so that when the unmanned aerial vehicle rises and falls, firstly, the base is contacted with the ground, if the vibration is large, the elastic force of the damping spring and the friction force between the sliding plug and the inner wall of the hollow rod can greatly buffer the vibration force, so that the unmanned aerial vehicle is more stable when rising and falling, the carried precise electronic equipment is protected, and by arranging the damping mechanism, the driving mechanism and the air duct, when the unmanned aerial vehicle rises and falls to generate vibration force, the base drives the damping spring and the sliding plug to contact with the supporting column, the damping spring deforms, the supporting column pushes the sliding plug to extrude air in the hollow rod into the cylinder, the air pressure borne by the telescopic end of the electric telescopic cylinder is increased, and the clamping device is pushed to clamp the tool more tightly; wherein, the deficiency points are as follows:
this kind of unmanned aerial vehicle shock attenuation fixture is when the user uses, because mobilizable between this dead lever and the centre gripping arm, can make the holder behind the centre gripping article, can cause the centre gripping article of holder centre gripping to cause to rock because of unmanned aerial vehicle's shake between this dead lever and the centre gripping arm for it is too nimble between this dead lever and the centre gripping arm, cause not hard up easily, make fixed effect relatively poor.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the problem that the fixing effect of the damping clamping mechanism of the unmanned aerial vehicle is poor in the background, and therefore the utility model provides the clamping and fixing device for the object carrier of the unmanned aerial vehicle.
In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides a carrier centre gripping fixing device for unmanned aerial vehicle, includes unmanned aerial vehicle, mount, unmanned aerial vehicle bottom fixed mounting has the mount, the mount bottom is provided with adjustment mechanism, the mount both ends all are provided with bradyseism mechanism.
Preferably, adjustment mechanism comprises bracing piece A, backup pad A, spout, backup pad B, slider, mount bottom fixed mounting has bracing piece A, bracing piece A outside both ends all slide through the slider and be provided with backup pad A, and pass through bolted connection between backup pad A and the bracing piece A, the equal fixed mounting of backup pad A bottom opposite face has the spout, be provided with backup pad B between the spout, the equal fixed mounting in backup pad B both ends has the slider, the slider agrees with to slide and sets up in the spout inboard, the equal fixed mounting in both ends has bracing piece C about the backup pad B outer wall, bracing piece C outside both ends all slide through the slider and be provided with splint, and pass through bolted connection between bracing piece C and the slider, the splint opposite face all forms a complete set and is provided with the clamp groove.
Preferably, bradyseism mechanism comprises bracing piece B, spring, support frame and slide bar, the equal fixed mounting in mount both ends has bracing piece B, bracing piece B has a plurality of, and is the equidistance and sets up side by side, the mount both ends all are provided with the support frame, the equal fixed mounting in support frame top opposite face has the slide bar, the slide bar has a plurality of, and is and sets up side by side, and the slide bar slides through the slider and sets up in the bracing piece B outside, the equal elastic connection in both ends is close to the slide bar outside about the bracing piece B outside has the spring.
Preferably, the support frame is made of PVC.
Preferably, the support frame is made of PC.
The utility model provides a carrier clamping and fixing device for an unmanned aerial vehicle, which has the following beneficial effects:
1. this kind of a carrier centre gripping fixing device for unmanned aerial vehicle can make the user arrange backup pad B in between the spout back through being provided with spout and slider, stimulates backup pad A and slides in the bracing piece A outside through the slider, makes backup pad B both ends slider slide in two spouts after, the user fixes through the bolt between with backup pad A and the bracing piece A.
2. This kind of a carrier centre gripping fixing device for unmanned aerial vehicle can make the user promote splint and move towards relative direction through the slider through being provided with splint, contacts behind the camera is in the double-layered inslot of splint back, and the user passes through the bolt fastening between with bracing piece C and the slider.
Drawings
Fig. 1 is a schematic view of a front view structure of an unmanned aerial vehicle of the present invention;
FIG. 2 is a schematic view of a front perspective structure of the chute of the present invention;
FIG. 3 is an enlarged schematic view of the structure at A in FIG. 1 according to the present invention;
fig. 4 is a schematic side view of the unmanned aerial vehicle of the present invention;
fig. 5 is a schematic front perspective view of the splint of the present invention.
In FIGS. 1-5: 1. an unmanned aerial vehicle; 101. a fixed mount; 102. a support rod A; 103. a support plate A; 104. a chute; 105. a support bar B; 1051. a spring; 2. a support plate B; 201. a slider; 202. a support bar C; 203. a splint; 3. a support frame; 301. a slide bar.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1 to 5, in an embodiment of the present invention, a carrier clamping and fixing device for an unmanned aerial vehicle includes an unmanned aerial vehicle 1 and a fixing frame 101, wherein the fixing frame 101 is fixedly installed at the bottom of the unmanned aerial vehicle 1, an adjusting mechanism is installed at the bottom of the fixing frame 101, and two ends of the fixing frame 101 are both provided with a cushioning mechanism.
Referring to fig. 1-3, in this embodiment: the adjusting mechanism is composed of a supporting rod A102, a supporting plate A103, a sliding groove 104, a supporting plate B2 and a sliding block 201;
Referring to fig. 1, 3, 5, in the present embodiment: equal fixed mounting in both ends has bracing piece C202 about the backup pad B2 outer wall, bracing piece C202 outside both ends all slide through the slider and are provided with splint 203, and pass through bolted connection between bracing piece C202 and the slider, splint 203 opposite face all forms a complete set and is provided with double-layered groove, after the user carries out centre gripping with backup pad B2 and fixes, arrange the camera in between the splint 203, at this moment the user promotes splint 203 and removes towards relative direction through the slider, contact behind the camera be in the double-layered inslot of splint 203, the user passes through the bolt fastening between with bracing piece C202 and the slider.
Referring to fig. 1 and 4, in the present embodiment: the cushioning mechanism consists of a support rod B105, a spring 1051, a support frame 3 and a sliding rod 301;
two ends of the fixing frame 101 are both fixedly provided with a plurality of support rods B105, the support rods B105, and are arranged in parallel at equal intervals, the two ends of the fixed frame 101 are both provided with the supporting frames 3, the opposite surfaces of the top of the supporting frames 3 are both fixedly provided with a plurality of sliding rods 301, and are arranged in parallel, the sliding rod 301 is arranged outside the supporting rod B105 in a sliding way through a sliding block, the upper end and the lower end of the outer side of the supporting rod B105 close to the outer side of the sliding rod 301 are elastically connected with a spring 1051, when the user holds the camera and controls the unmanned aerial vehicle 1 to fly in the air for aerial photography and needs to land, the user controls the unmanned aerial vehicle 1 to descend, so that after the support frame 3 contacts the ground, the sliding rod 301 is pushed to slide outside the support rod B105 through the sliding block, pressing spring 1051 and making spring 1051 kick-back, when will make the vibrations that unmanned aerial vehicle 1 produced weaken, make support frame 3 can not receive too big striking.
Referring to fig. 1 and 4, in the present embodiment: unmanned aerial vehicle 1 passes through control panel and battery electric connection.
Referring to fig. 1 and 4, in the present embodiment: the 3 materials of support frame are PVC, have the pliability good, the difficult fragile characteristic because of the PVC material, can make 1 descends of user control unmanned aerial vehicle, makes the 3 striking that contact ground produced of support frame, can not make support frame 3 cause cracked.
As shown in fig. 1 and 4, in the embodiment of the present invention, in addition to the support frame 3 made of PVC, the support frame 3 is made of PC, and because the PC has the characteristics of light weight and high strength, the user can control the unmanned aerial vehicle 1 to descend, so that the support frame 3 contacts with the ground to generate impact, the support frame 3 cannot be cracked, and meanwhile, the support frame 3 is made of PC with impact resistance, and because the hardness is higher, when the support frame 3 contacts with the ground, the support frame 3 can resist larger impact generated after contacting with the ground, so that the support frame 3 is not easy to damage.
When the carrier clamping and fixing device for the unmanned aerial vehicle is used, firstly, when a user needs to fix a camera on the unmanned aerial vehicle 1 for aerial photography, the user places a supporting plate B2 between the sliding grooves 104, pulls the supporting plate A103 to slide on the outer side of the supporting rod A102 through the sliding blocks, enables the sliding blocks 201 at two ends of the supporting plate B2 to slide into the two sliding grooves 104, then, the user fixes the supporting plate A103 and the supporting rod A102 through bolts, then, the user places the camera between the clamping plates 203, pushes the clamping plates 203 to move towards opposite directions through the sliding blocks, after contacting the camera, the user places the camera in the clamping grooves of the clamping plates 203, then, the user fixes the supporting rod C202 and the sliding blocks through the bolts, finally, after the user controls the unmanned aerial vehicle 1 for clamping the camera to fly in the air for aerial photography, when landing is needed, the user controls the unmanned aerial vehicle 1 to descend, make support frame 3 contact ground after, will promote slide bar 301 and pass through the slider in the gliding of bracing piece B105 outside, pressure move spring 1051 and make spring 1051 kick-back, will make the vibrations that unmanned aerial vehicle 1 produced weaken, carry out safety and stability's landing.
The above are only preferred embodiments of the present invention, and it should be noted that, for those skilled in the art, it can make several changes and modifications without departing from the concept of the present invention, and these should also be considered as the protection scope of the present invention, which will not affect the effect of the implementation of the present invention and the practicability of the patent.
Claims (3)
1. The utility model provides a carrier centre gripping fixing device for unmanned aerial vehicle, includes unmanned aerial vehicle (1), mount (101), unmanned aerial vehicle (1) bottom fixed mounting has mount (101), its characterized in that: the bottom of the fixed frame (101) is provided with an adjusting mechanism, and two ends of the fixed frame (101) are provided with a cushioning mechanism;
the adjusting mechanism consists of a support rod A (102), a support plate A (103), a sliding groove (104), a support plate B (2) and a sliding block (201);
the bottom of the fixing frame (101) is provided with a support rod A (102), two ends of the outer side of the support rod A (102) are respectively and movably provided with a support plate A (103) through a sliding block, the support plate A (103) is connected with the support rod A (102) through a bolt, opposite surfaces of the bottom of the support plate A (103) are respectively provided with a sliding groove (104), a support plate B (2) is arranged between the sliding grooves (104), two ends of the support plate B (2) are respectively provided with a sliding block (201), and the sliding blocks (201) are arranged on the inner side of the sliding grooves (104) in a fit and sliding mode;
the upper end and the lower end of the outer wall of the supporting plate B (2) are respectively provided with a supporting rod C (202), the two ends of the outer side of the supporting rod C (202) are respectively movably provided with a clamping plate (203) through a sliding block, the supporting rod C (202) is connected with the sliding block through a bolt, and the opposite surfaces of the clamping plates (203) are respectively provided with a clamping groove in a matched manner;
the cushioning mechanism consists of a support rod B (105), a spring (1051), a support frame (3) and a sliding rod (301);
mount (101) both ends all are provided with bracing piece B (105), bracing piece B (105) have a plurality of, and are the equidistance and set up side by side, mount (101) both ends all are provided with support frame (3), support frame (3) top opposite face all is provided with slide bar (301), slide bar (301) have a plurality of, and are and set up side by side, and slide bar (301) set up in bracing piece B (105) outside through the slider activity, the equal elastic connection in both ends is close to slide bar (301) outside about bracing piece B (105) outside has spring (1051).
2. The carrier clamp fixture of claim 1, wherein: the support frame (3) is made of PVC.
3. The carrier clamp fixture of claim 1, wherein: the support frame (3) is made of PC.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122769304.2U CN216994865U (en) | 2021-11-12 | 2021-11-12 | A carrier centre gripping fixing device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122769304.2U CN216994865U (en) | 2021-11-12 | 2021-11-12 | A carrier centre gripping fixing device for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216994865U true CN216994865U (en) | 2022-07-19 |
Family
ID=82380797
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122769304.2U Expired - Fee Related CN216994865U (en) | 2021-11-12 | 2021-11-12 | A carrier centre gripping fixing device for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216994865U (en) |
-
2021
- 2021-11-12 CN CN202122769304.2U patent/CN216994865U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220719 |
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| CF01 | Termination of patent right due to non-payment of annual fee |