CN220996795U - Unmanned aerial vehicle who possesses camera shock-absorbing function - Google Patents
Unmanned aerial vehicle who possesses camera shock-absorbing function Download PDFInfo
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- CN220996795U CN220996795U CN202322917085.7U CN202322917085U CN220996795U CN 220996795 U CN220996795 U CN 220996795U CN 202322917085 U CN202322917085 U CN 202322917085U CN 220996795 U CN220996795 U CN 220996795U
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- unmanned aerial
- aerial vehicle
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- buffer
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- 238000013016 damping Methods 0.000 claims abstract description 11
- 230000017525 heat dissipation Effects 0.000 claims abstract description 10
- 239000007787 solid Substances 0.000 claims description 5
- 239000003292 glue Substances 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 23
- 230000000903 blocking effect Effects 0.000 abstract description 11
- 235000017166 Bambusa arundinacea Nutrition 0.000 description 4
- 235000017491 Bambusa tulda Nutrition 0.000 description 4
- 241001330002 Bambuseae Species 0.000 description 4
- 235000015334 Phyllostachys viridis Nutrition 0.000 description 4
- 239000011425 bamboo Substances 0.000 description 4
- 238000001125 extrusion Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000011435 rock Substances 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a camera damping function, which comprises a support, wherein four groups of lantern rings are fixed on the outer side of the support, a screw is arranged in the lantern rings, a camera body is arranged at one end of the support, an antenna is arranged at the other end of the support, a socket is arranged at one side of the antenna, an interface is arranged at the bottom position of the support, heat dissipation grooves are formed in the central position of the bottom of the support, a convenient operation mechanism is arranged on the surface of the support, the convenient operation mechanism comprises a groove, a dismounting assembly and a blocking cover, and a buffer mechanism is arranged on the outer side of the camera body and consists of a support frame and a buffer component. The utility model not only improves the shooting effect of the camera body when the unmanned aerial vehicle is used, improves the convenience degree when the unmanned aerial vehicle is used, but also improves the heat dissipation effect when the unmanned aerial vehicle is used.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a camera damping function.
Background
The unmanned aerial vehicle can take off like a common plane under radio remote control or launch and lift off by using a booster rocket, can be brought to the air by a host machine to put in flight, can automatically land in the same way as the landing process of the common plane during recovery, and can also be recovered by using a parachute or a barrier net for remote control.
The camera is generally arranged on the surface of the unmanned aerial vehicle, a certain gap is generally reserved between the camera and the unmanned aerial vehicle, and the unmanned aerial vehicle is easy to shake during use, so that the shooting effect of the camera during use of the unmanned aerial vehicle is influenced; the connection socket of the unmanned aerial vehicle is generally hidden and inconvenient to connect with the connecting wire, and the antenna is not easy to quickly disassemble and assemble by the general unmanned aerial vehicle, so that the SD card is inconvenient to install, and the convenience degree of the unmanned aerial vehicle in use is reduced; the unmanned aerial vehicle can generate heat when using, and general unmanned aerial vehicle is difficult to dispel the heat fast to influence the radiating effect when unmanned aerial vehicle uses easily.
Disclosure of utility model
The utility model aims to provide an unmanned aerial vehicle with a camera damping function, which aims to solve the problems of poor shooting effect, low convenience and poor heat dissipation effect of a camera when the unmanned aerial vehicle is used in the background art.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an unmanned aerial vehicle who possesses camera shock-absorbing function, includes the support, the outside of support is fixed with four groups lantern rings, the inside of lantern ring is provided with the screw, the one end at the support is installed to the screw, the one end of support is provided with the camera body, the other end of support is provided with the antenna, one side of antenna is provided with the socket, the one end at the support is installed to the socket, the interface is installed to the bottom position department of support, the interface is type-c structure, the heat dissipation groove has all been seted up to the central point department of support bottom, the surface of support is provided with operating device of being convenient for, operating device's inside of being convenient for includes recess, dismouting subassembly and fender lid, the outside of camera body is provided with buffer gear, buffer gear comprises support frame and buffer unit.
Preferably, the surface of the support is provided with a groove, the groove is positioned on one side of the interface, one end of the support is rotationally connected with a blocking cover, the blocking cover is matched with the support in a mutually covering way, and the blocking cover is positioned on the outer side of the socket.
Preferably, the antenna is detachably connected with the bracket through a dismounting assembly, and the dismounting assembly consists of an elastic clamping strip, an adjusting screw cylinder and a fixing stud.
Preferably, a fixing stud is fixed on the surface of the bracket, an adjusting screw barrel is sleeved on the surface of the fixing stud, and the adjusting screw barrel is in threaded fit with the fixing stud.
Preferably, the inner walls at the top positions of the fixing studs are all fixed with elastic clamping strips, and one ends of the elastic clamping strips extend to the inside of the adjusting screw cylinder and are tightly attached to the surface of the antenna.
Preferably, the camera body is provided with a support frame on both sides, the surface of the support frame is fixedly connected with the surface of the support frame, and a buffer part is arranged in the support frame.
Preferably, the inside of buffer unit is including solid fixed ring, spliced pole and buffer piece, the inside of support frame is fixed with solid fixed ring, gu the inside of fixed ring glues and have the buffer piece, the surface of buffer piece closely laminates with the surface of camera body.
Preferably, the two sides of the camera body are both fixedly provided with connecting columns, and one end of each connecting column is fixedly connected with the surface of the buffer block.
Compared with the prior art, the utility model has the beneficial effects that: this unmanned aerial vehicle that possesses camera shock-absorbing function has not only improved the shooting effect of unmanned aerial vehicle when using the camera body, has improved the degree of convenience when unmanned aerial vehicle uses, has improved the radiating effect when unmanned aerial vehicle uses moreover;
1. Through being provided with buffer gear, the spliced pole is inserted and is fixed inside the buffer block, makes the buffer block hug closely in the both sides of camera body under the effect of spliced pole, can cushion the camera body, avoids the camera body to rock and influences the shooting effect to realize unmanned aerial vehicle to the buffer function of camera body, thereby improved the shooting effect of camera body when unmanned aerial vehicle uses;
2. through being provided with convenient operating device, because the interface is type-c structure, be convenient for the user to insert the connecting wire, be convenient for the user under the effect of recess installs the SD card, simultaneously, rotatable fender lid is opened with the fender lid, make things convenient for connecting wire and socket connection, simultaneously, adjust the screw barrel and extrude the elastic holding strip this moment, make the elastic holding strip press from both sides tightly fixedly with the antenna, if need dismantle the antenna, rotatable adjust the screw barrel, adjust the screw barrel shrink to the inside of fixed double-screw bolt under the screw-thread fit of fixed double-screw bolt with the adjustment screw barrel, make elastic holding strip one end lose the extrusion force, make the elastic holding strip keep away from the antenna, can take off the antenna afterwards, in order to realize unmanned aerial vehicle's function of being convenient for operation, thereby the degree of convenience when unmanned aerial vehicle uses has been improved;
3. Through being provided with the radiating groove, there is heat production when unmanned aerial vehicle uses, at this moment, can carry out heat conduction to the support under the effect of radiating groove, accelerate air circulation to accelerate the radiating rate of support, with the high-efficient heat dissipation function of realization unmanned aerial vehicle, thereby improved the radiating effect when unmanned aerial vehicle uses.
Drawings
FIG. 1 is a schematic view of a three-dimensional appearance structure of the present utility model;
FIG. 2 is a schematic view of a front cross-sectional structure of the present utility model;
FIG. 3 is an enlarged schematic view of a buffer mechanism according to the present utility model;
Fig. 4 is an enlarged schematic view of the convenient operating mechanism of the present utility model.
In the figure: 1. a bracket; 101. a collar; 102. an antenna; 103. a propeller; 104. a camera body; 105. an interface; 106. a socket; 2. the operation mechanism is convenient; 201. a groove; 202. disassembling and assembling the assembly; 2021. an elastic clamping strip; 2022. adjusting the screw cylinder; 2023. fixing a stud; 203. a blocking cover; 3. a buffer mechanism; 301. a support frame; 302. a buffer member; 3021. a fixing ring; 3022. a connecting column; 3023. a buffer block; 4. a heat sink.
Detailed Description
The technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the drawings in the embodiments of the present utility model, and it is apparent that the described embodiments are only some embodiments of the present utility model, not all embodiments, and furthermore, the terms "first", "second", "third", "up, down, left, right", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance. Meanwhile, in the description of the present utility model, unless explicitly stated and defined otherwise, the terms "connected", "connected" and "connected" should be interpreted broadly, and for example, may be fixedly connected, detachably connected, or integrally connected; the mechanical connection and the electrical connection can be adopted; all other embodiments, which may be directly or indirectly through intermediaries, which may be obtained by a person of ordinary skill in the art without inventive effort based on the embodiments of the present utility model are within the scope of the present utility model.
The utility model provides a structure of an unmanned aerial vehicle with a camera damping function, as shown in fig. 1 and 2, comprising a bracket 1, wherein four groups of lantern rings 101 are fixed on the outer side of the bracket 1, a propeller 103 is arranged in the lantern rings 101, the propeller 103 is arranged at one end of the bracket 1, a camera body 104 is arranged at one end of the bracket 1, an antenna 102 is arranged at the other end of the bracket 1, a socket 106 is arranged at one side of the antenna 102, the socket 106 is arranged at one end of the bracket 1, an interface 105 is arranged at the bottom position of the bracket 1, the interface 105 is of a type-c structure, and radiating grooves 4 are formed in the central position of the bottom of the bracket 1.
During the use, there is heat production when unmanned aerial vehicle uses, at this moment, can carry out heat conduction to support 1 under the effect of heat dissipation groove 4, accelerates the circulation of air to accelerate the radiating rate of support 1, in order to realize unmanned aerial vehicle's high-efficient heat dissipation function.
Further, as shown in fig. 2 and 4, the surface of the bracket 1 is provided with a convenient operation mechanism 2, the interior of the convenient operation mechanism 2 comprises a groove 201, a dismounting component 202 and a blocking cover 203, the surface of the bracket 1 is provided with the groove 201, the groove 201 is located at one side of the interface 105, one end of the bracket 1 is rotationally connected with the blocking cover 203, the blocking cover 203 is mutually covered and matched with the bracket 1, the blocking cover 203 is located at the outer side of the socket 106, the antenna 102 is detachably connected with the bracket 1 through the dismounting component 202, the dismounting component 202 is composed of an elastic clamping strip 2021, an adjusting screw 2022 and a fixing screw 2023, the surface of the bracket 1 is fixedly provided with the fixing screw 2023, the surface of the fixing screw 2023 is sleeved with the adjusting screw 2022, the adjusting screw 2022 is mutually matched with the fixing screw 2023, the inner wall at the top position of the fixing screw 2023 is fixedly provided with the elastic clamping strip 2021, and one end of the elastic clamping strip 2021 extends to the interior of the adjusting screw 2022 and is tightly adhered to the surface of the antenna 102.
During the use, because interface 105 is type-c structure, the user of being convenient for inserts the connecting wire, be convenient for the user under the effect of recess 201 installs the SD card, simultaneously, rotatable shield 203 opens shield 203, make things convenient for the connecting wire to be connected with socket 106, simultaneously, adjust spiral shell section of thick bamboo 2022 and extrude elasticity holding strip 2021 this moment, make elasticity holding strip 2021 press from both sides tightly fixedly antenna 102, if need dismantle antenna 102, rotatable adjust spiral shell section of thick bamboo 2022, adjust spiral shell section of thick bamboo 2022 shrink to the inside of fixing stud 2023 under the screw-thread fit of adjust spiral shell section of thick bamboo 2022 and fixing stud 2023, make elasticity holding strip 2021 one end lose the extrusion force, make elasticity holding strip 2021 keep away from antenna 102, afterwards can take off antenna 102, in order to realize unmanned aerial vehicle convenient operation's function.
Further, as shown in fig. 3, a buffer mechanism 3 is disposed on the outer side of the camera body 104, the buffer mechanism 3 is composed of a support frame 301 and a buffer member 302, the support frame 301 is disposed on two sides of the camera body 104, the surface of the support frame 301 is fixedly connected with the surface of the support frame 1, the buffer member 302 is disposed in the support frame 301, a fixing ring 3021, a connecting column 3022 and a buffer block 3023 are disposed in the buffer member 302, the fixing ring 3021 is fixed in the support frame 301, the buffer block 3023 is adhered to the fixing ring 3021, the surface of the buffer block 3023 is tightly adhered to the surface of the camera body 104, connecting columns 3022 are fixed on two sides of the camera body 104, and one end of the connecting column 3022 is fixedly connected with the surface of the buffer block 3023.
When the camera head is used, the connecting column 3022 is fixedly inserted into the buffer block 3023, the buffer block 3023 is tightly attached to two sides of the camera head body 104 under the action of the connecting column 3022, the camera head body 104 can be buffered, the camera head body 104 is prevented from shaking, the shooting effect is prevented from being influenced, and the buffer function of the unmanned aerial vehicle to the camera head body 104 is achieved.
Working principle: during the use, can shoot at first under the effect of camera body 104, at this moment, spliced pole 3022 inserts and fixes inside buffer block 3023, makes buffer block 3023 hug closely in the both sides of camera body 104 under spliced pole 3022's effect, can cushion camera body 104, avoids camera body 104 to rock and influences the shooting effect to realize unmanned aerial vehicle to the buffer function of camera body 104, thereby the shooting effect of camera body 104 when unmanned aerial vehicle uses has been improved.
Simultaneously, there is heat production when unmanned aerial vehicle uses, at this moment, can carry out heat conduction to support 1 under the effect of heat dissipation groove 4, accelerates the circulation of air to accelerate the radiating rate of support 1, with the high-efficient heat dissipation function of realization unmanned aerial vehicle, thereby improved the radiating effect when unmanned aerial vehicle uses.
Meanwhile, because the interface 105 is of a type-c structure, a user is convenient to access a connecting wire, the user is convenient to install the SD card under the action of the groove 201, meanwhile, the blocking cover 203 can be rotated, the blocking cover 203 is opened, the connecting wire is convenient to connect with the socket 106, meanwhile, the adjusting screw cylinder 2022 extrudes the elastic clamping strip 2021, the elastic clamping strip 2021 clamps and fixes the antenna 102, if the antenna 102 needs to be disassembled, the adjusting screw cylinder 2022 can be rotated, the adjusting screw cylinder 2022 is contracted into the inside of the fixing stud 2023 under the threaded fit of the adjusting screw cylinder 2022 and the fixing stud 2023, one end of the elastic clamping strip 2021 loses extrusion force, the elastic clamping strip 2021 is far away from the antenna 102, and then the antenna 102 can be taken down, so that the unmanned aerial vehicle is convenient to operate, and therefore the convenience degree of the unmanned aerial vehicle in use is improved, and the unmanned aerial vehicle is finally used.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present utility model may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (8)
1. Unmanned aerial vehicle that possesses camera shock-absorbing function, including support (1), its characterized in that: the utility model discloses a camera, including support (1), support (2), support (1), four sets of lantern rings (101) are fixed with in the outside of the support (1), the inside of lantern ring (101) is provided with screw (103), screw (103) are installed in the one end of support (101), the one end of support (1) is installed in one side of antenna (102) is provided with socket (106), interface (105) are installed in the bottom position department of support (1), interface (105) are type-c structure, heat dissipation groove (4) are all seted up in the central point department of support (1) bottom, the surface of support (1) is provided with operating mechanism (2) of being convenient for, the inside of operating mechanism (2) is including recess (201), dismouting subassembly (202) and fender lid (203), the outside of camera body (104) is provided with buffer gear (3), buffer gear (3) comprise support frame (301) and buffer part (302).
2. The unmanned aerial vehicle with camera damping function according to claim 1, wherein: the surface of support (1) has seted up recess (201), recess (201) are located one side of interface (105), the one end rotation of support (1) is connected with keeps off lid (203), keep off lid (203) and support (1) mutually lid and connect the cooperation, keep off lid (203) are located the outside of socket (106).
3. The unmanned aerial vehicle with camera damping function according to claim 2, wherein: the antenna (102) is detachably connected with the bracket (1) through a disassembly and assembly component (202), and the disassembly and assembly component (202) consists of an elastic clamping strip (2021), an adjusting screw cylinder (2022) and a fixing stud (2023).
4. The unmanned aerial vehicle with camera damping function according to claim 3, wherein: the surface of the bracket (1) is fixedly provided with a fixing stud (2023), the surface of the fixing stud (2023) is sleeved with an adjusting screw cylinder (2022), and the adjusting screw cylinder (2022) is in threaded fit with the fixing stud (2023).
5. The unmanned aerial vehicle with camera damping function according to claim 4, wherein: the inner walls of the top positions of the fixing studs (2023) are respectively fixed with an elastic clamping strip (2021), and one end of each elastic clamping strip (2021) extends to the inside of the adjusting screw cylinder (2022) and is tightly attached to the surface of the antenna (102).
6. The unmanned aerial vehicle with camera damping function according to claim 1, wherein: both sides of camera body (104) all are provided with support frame (301), the surface of support frame (301) is fixed connection with the surface of support (1), the inside of support frame (301) is provided with buffer unit (302).
7. The unmanned aerial vehicle with camera damping function according to claim 6, wherein: the inside of buffer unit (302) is including solid fixed ring (3021), spliced pole (3022) and buffer piece (3023), the inside of support frame (301) is fixed with solid fixed ring (3021), the inside of solid fixed ring (3021) glues and glues has buffer piece (3023), the surface of buffer piece (3023) closely laminates with the surface of camera body (104).
8. The unmanned aerial vehicle with camera damping function according to claim 7, wherein: connecting columns (3022) are fixed on two sides of the camera body (104), and one end of each connecting column (3022) is fixedly connected with the surface of each buffer block (3023).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322917085.7U CN220996795U (en) | 2023-10-30 | 2023-10-30 | Unmanned aerial vehicle who possesses camera shock-absorbing function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322917085.7U CN220996795U (en) | 2023-10-30 | 2023-10-30 | Unmanned aerial vehicle who possesses camera shock-absorbing function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220996795U true CN220996795U (en) | 2024-05-24 |
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ID=91114668
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322917085.7U Active CN220996795U (en) | 2023-10-30 | 2023-10-30 | Unmanned aerial vehicle who possesses camera shock-absorbing function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220996795U (en) |
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2023
- 2023-10-30 CN CN202322917085.7U patent/CN220996795U/en active Active
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