CN220054160U - Tripod head and unmanned aerial vehicle - Google Patents
Tripod head and unmanned aerial vehicle Download PDFInfo
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- CN220054160U CN220054160U CN202321430491.4U CN202321430491U CN220054160U CN 220054160 U CN220054160 U CN 220054160U CN 202321430491 U CN202321430491 U CN 202321430491U CN 220054160 U CN220054160 U CN 220054160U
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- 238000009434 installation Methods 0.000 claims description 17
- 238000013016 damping Methods 0.000 claims description 8
- 230000002349 favourable effect Effects 0.000 description 8
- 230000009286 beneficial effect Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
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Abstract
The utility model discloses a cradle head and an unmanned aerial vehicle, relates to the technical field of unmanned aerial vehicles, and is used for solving the problem of poor use experience of users. The cradle head comprises a mounting assembly and a driving assembly. The mounting assembly includes a plurality of mounting structures and a plurality of mounting bases. A plurality of mounting structure spare intervals set up, and a plurality of mounting structure spare all are connected with unmanned aerial vehicle detachably, and a mounting base rotationally is connected with a mounting structure spare, and a plurality of mounting base are used for installing article. The drive assembly is coupled to the one or more mounting bases and is configured to drive the mounting bases to rotate about the first axis relative to the mounting structure. The unmanned aerial vehicle is used for loading articles.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a cradle head and an unmanned aerial vehicle.
Background
In the related art, a cradle head of an unmanned aerial vehicle may be used to carry an object (e.g., a camera, a communication device, etc.). When the cradle head is used for bearing communication equipment, the current cradle head can only be used for bearing the communication equipment due to the fact that the weight of the communication equipment is large, when the communication equipment needs to change a communication target, the unmanned aerial vehicle needs to move to change the position of the communication equipment, so that the communication equipment can communicate with the target, power consumption of the unmanned aerial vehicle is improved, and use experience of a user is reduced.
Disclosure of Invention
The embodiment of the utility model provides a cradle head and an unmanned aerial vehicle, which are used for solving the problem of poor use experience of users.
In order to achieve the above purpose, the embodiment of the present utility model adopts the following technical scheme:
an embodiment of a first aspect of the present utility model provides a cradle head, including a mounting assembly and a driving assembly, where the mounting assembly includes a plurality of mounting structural members and a plurality of mounting bases, the plurality of mounting structural members are arranged at intervals, the plurality of mounting structural members are detachably connected with the unmanned aerial vehicle, one mounting base is rotatably connected with one mounting structural member, and the plurality of mounting bases are used for mounting articles; the drive assembly is coupled to the one or more mounting bases and is configured to drive the mounting bases to rotate about a first axis relative to the mounting structure.
Optionally, the driving assembly comprises one or more steering engines and one or more pull rods, one steering engine is provided with a steering engine arm, one end of the one or more pull rods is connected with the one or more mounting bases, and the other end of the one or more pull rods is connected with the steering engine arm.
Optionally, the drive assembly is detachably connected to the mounting structure.
Optionally, the mounting assembly further comprises a plurality of first connectors, and the one mounting base is connected to the one mounting structure by one first connector.
Optionally, the mounting assembly further includes a plurality of damping rotating shafts, a first mounting hole is formed in the first connecting piece, a second mounting hole matched with the first mounting hole is formed in the mounting base, and one damping rotating shaft penetrates through the first mounting hole and the second mounting hole.
Optionally, the one mounting base includes a first portion and a second portion, one end of the first portion is rotatably connected to the one mounting structure, the other end of the first portion is connected to one end of the second portion, and an included angle is formed between the first portion and the second portion.
Optionally, a plurality of third mounting holes are formed in the second portion, and the plurality of third mounting holes are arranged at intervals.
Optionally, the installation component still includes the second connecting piece, the second connecting piece is including the first connecting portion and the second connecting portion that connect gradually, the second connecting portion be in the planar projection that first connecting portion is located with first connecting portion are perpendicular, first connecting portion with installation structure detachably connects, the second connecting portion with unmanned aerial vehicle detachably connects.
Optionally, a first adjusting hole and a fourth mounting hole are formed in the second connecting portion, the second connecting portion is connected with the unmanned aerial vehicle through the fourth mounting hole, an adjusting fastener is arranged in the first adjusting hole, and the adjusting fastener is used for adjusting the size of the fourth mounting hole.
An embodiment of a second aspect of the present utility model provides an unmanned aerial vehicle, the unmanned aerial vehicle comprising: the unmanned aerial vehicle comprises an unmanned aerial vehicle body and the cradle head, wherein the unmanned aerial vehicle body comprises a body and supporting legs, one ends of the supporting legs are connected with the bottom surface of the body, and the other ends of the supporting legs are used for supporting the bottom surface; the cradle head is detachably connected with the support legs.
The unmanned aerial vehicle provided by the utility model has at least the following beneficial effects: through setting up a plurality of mounting structure and a plurality of mounting base, make the atress of cloud platform can disperse on a plurality of mounting structure and a plurality of mounting base, be favorable to improving the structural strength of cloud platform to be favorable to improving the bearing capacity of cloud platform, make the cloud platform can bear heavier object. And because a mounting base is rotatably connected with a mounting structural member, the driving assembly drives the mounting base to rotate around the first axis relative to the mounting structural member, so that the mounting base can bear heavier objects and simultaneously enable the objects to rotate along with the mounting base, and therefore, communication equipment mounted on the mounting base can change positions under the condition that the position of the unmanned aerial vehicle is not changed, the communication range of the communication equipment can be increased, further improvement of the communication capacity of the communication equipment is facilitated, and the use experience of a user can be better. Meanwhile, the cradle head can be detachably connected with the unmanned aerial vehicle, so that a user can conveniently replace and maintain the cradle head, and the maintainability of the unmanned aerial vehicle is improved.
Drawings
Fig. 1 is a perspective view of a unmanned aerial vehicle according to an embodiment of the present utility model;
fig. 2 is a schematic diagram of a pan-tilt head according to an embodiment of the present utility model.
Reference numerals:
100. unmanned plane;
1. an unmanned aerial vehicle body; 11. a body;
2. a support leg;
3. a cradle head;
31. a mounting assembly; 311. installing a structural member; 312. a mounting base; 3121. a first portion; 3122. a second portion; 3123. a second mounting hole; 3124. a third mounting hole; 313. a first connector; 3131. a first mounting hole; 3132. a connection part; 3133. a fixing part; 314. damping the rotating shaft; 315. a second connector; 3151. a first connection portion; 3152. a second connecting portion; 3153. a first adjustment aperture; 3154. a fourth mounting hole;
32. a drive assembly; 321. steering engine; 3211. steering engine arm; 322. and (5) a pull rod.
Detailed Description
Embodiments of the present utility model will be described in detail below with reference to the accompanying drawings.
In the description of the present utility model, it should be understood that the directions or positional relationships indicated by the terms "center", "upper", "lower", "left", "right", "inner", "outer", etc., are based on the directions or positional relationships shown in the drawings, are merely for convenience of description and simplification of the description, and do not indicate or imply that the apparatus or element in question must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present utility model.
The terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the present utility model, unless otherwise indicated, the meaning of "a plurality" is two or more.
In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
In the related art, a cradle head of an unmanned aerial vehicle may be used to carry an object (e.g., a camera, a communication device, etc.). When the cradle head is used for bearing communication equipment, the current cradle head can only be used for bearing the communication equipment due to the fact that the weight of the communication equipment is large, when the communication equipment needs to change a communication target, the unmanned aerial vehicle needs to move to change the position of the communication equipment, so that the communication equipment can communicate with the target, power consumption of the unmanned aerial vehicle is improved, and use experience of a user is reduced.
In order to solve the technical problem, through setting up a plurality of mounting structure and a plurality of mounting base, make the atress of cloud platform can disperse on a plurality of mounting structure and a plurality of mounting base, be favorable to improving the structural strength of cloud platform to be favorable to improving the bearing capacity of cloud platform, make the cloud platform can bear heavier object. And because a mounting base is rotatably connected with a mounting structural member, the driving assembly drives the mounting base to rotate around the first axis relative to the mounting structural member, so that the mounting base can bear heavier objects and simultaneously enable the objects to rotate along with the mounting base, and therefore, communication equipment mounted on the mounting base can change positions under the condition that the position of the unmanned aerial vehicle is not changed, the communication range of the communication equipment can be increased, further improvement of the communication capacity of the communication equipment is facilitated, and the use experience of a user can be better. Meanwhile, the cradle head can be detachably connected with the unmanned aerial vehicle, so that a user can conveniently replace and maintain the cradle head, and the maintainability of the unmanned aerial vehicle is improved.
The unmanned aerial vehicle of the embodiment of the utility model is explained below.
Referring to fig. 1, fig. 1 is a perspective view of a unmanned aerial vehicle according to an embodiment of the present utility model. The embodiment of the utility model provides an unmanned aerial vehicle 100, wherein the unmanned aerial vehicle 100 can be a fixed-wing unmanned aerial vehicle, a multi-rotor unmanned aerial vehicle or the like, and the unmanned aerial vehicle 100 is taken as an example of the multi-rotor unmanned aerial vehicle.
With continued reference to fig. 1, the drone 100 includes a drone body 1 and a cradle head 3. The unmanned aerial vehicle body 1 includes a fuselage 11 and a foot 2.
Illustratively, a rotor assembly may be coupled to the fuselage 11 for driving the drone 100. The rotor assembly may include a rotor arm and a drive motor disposed at a distal end of the rotor arm, and a rotor configured to be rotated by the drive motor.
The feet 2 are used to support the fuselage. One end of the leg 2 may be connected to the bottom surface of the body, and the other end of the leg 2 is used to support the ground. The connection between the support leg 2 and the body 11 may be fixed connection or detachable connection, which is not limited in the present utility model.
The cradle head 3 is used for carrying articles. The cradle head 3 is detachably connected with the support legs 2. The arrangement is convenient for replacing and maintaining the cradle head 3, and is beneficial to improving the maintainability of the unmanned aerial vehicle 100. Meanwhile, the article can be mounted on the holder 3 when the holder 3 is detached from the support leg 2, so that the article can be mounted conveniently.
The cradle head 3 of the present utility model will be described below.
Referring to fig. 2, fig. 2 is a schematic diagram of a pan-tilt head 3 according to an embodiment of the utility model. The cradle head 3 provided by the embodiment of the utility model comprises a mounting assembly 31 and a driving assembly 32. The mounting assembly 31 includes a plurality of mounting structures 311 and a plurality of mounting bases 312. The plurality of mounting structures 311 are spaced apart. The plurality of mounting structures 311 are each detachably connected to the drone 100. That is, each mounting structure 311 is detachably connected to the leg 2 of the unmanned aerial vehicle 100. Therefore, the exchange and the maintenance between the cradle head 3 and the unmanned aerial vehicle 100 are facilitated, and the maintainability of the unmanned aerial vehicle 100 is improved. Wherein, a plurality of mounting structures 311 may be uniformly spaced apart.
With continued reference to fig. 2, exemplary mounting structures 311 are provided in two, with a gap between the two mounting structures 311, and both mounting structures 311 are removably connected to the foot 2.
With continued reference to FIG. 2, a mounting base 312 is rotatably coupled to a mounting structure 311. That is, a mounting base 312 may be rotated relative to a mounting structure 311. By adopting the connection mode of the installation structural member 311 and the installation base 312, the stress of the installation structural member 311 can be reduced, so that the installation structural strength can be ensured, the structural strength of the tripod head 3 can be higher, the tripod head 3 can bear articles with larger weight, and the bearing capacity of the tripod head 3 is improved.
With continued reference to fig. 2, a plurality of mounting bases 312 are provided for mounting articles. One article may be mounted on one mounting base 312, or a plurality of mounting bases 312 may be used to mount the same article. Therefore, by providing a plurality of mounting bases 312, the bearing capacity of the cradle head 3 is improved, so that the cradle head 3 can bear articles with larger weight.
With continued reference to fig. 2, the drive assembly 32 is coupled to one or more mounting bases 312. The drive assembly 32 is configured to drive rotation of the mounting base 312 relative to the mounting structure 311 about a first axis (e.g., the X-axis as shown in fig. 2). Therefore, the position of the communication device mounted on the mounting base 312 can be changed without changing the position of the unmanned aerial vehicle 100, so that the communication range of the communication device can be increased, thereby being beneficial to improving the communication capability of the communication device and improving the use experience of a user.
Illustratively, when the drive assembly 32 is coupled to one mounting base 312 and a plurality of mounting bases 312 are commonly mounted to an article, rotation of one mounting base 312 may cause the remaining mounting bases 312 to be commonly rotated. Thus, the number of driving assemblies 32 can be reduced, which is advantageous in reducing costs.
Also, for example, when the driving assembly 32 is connected to a plurality of mounting bases 312, one mounting base 312 may mount one article, so that the rotation angles of the articles mounted on different mounting bases 312 may be different, thereby facilitating the improvement of the operability of the pan-tilt head 3.
In some embodiments, the drive assembly 32 may also drive the mounting base 312 to rotate about a second axis (e.g., the Y-axis shown in fig. 2) relative to the mounting structure 311. Wherein the first axis is perpendicular to the second axis.
According to the cradle head 3 of the embodiment of the utility model, the stress of the cradle head 3 can be dispersed to the plurality of mounting structural members 311 and the plurality of mounting bases 312 by arranging the plurality of mounting structural members 311 and the plurality of mounting bases 312, so that the structural strength of the cradle head 3 is improved, the bearing capacity of the cradle head 3 is improved, and the cradle head 3 can bear heavier objects. And because a mounting base 312 is rotatably connected with a mounting structural member 311, the driving assembly 32 drives the mounting base 312 to rotate around the first axis relative to the mounting structural member 311, so that the mounting base 312 can bear heavy objects and simultaneously enable the objects to rotate along with the mounting base 312, and therefore, under the condition that the position of the unmanned aerial vehicle 100 is not changed, the communication equipment mounted on the mounting base 312 can be changed in position, the communication range of the communication equipment can be increased, the communication capability of the communication equipment can be improved, and the use experience of a user can be better. Meanwhile, the cradle head 3 can be detachably connected with the unmanned aerial vehicle 100, so that a user can conveniently replace and maintain the cradle head 3, and maintainability of the unmanned aerial vehicle 100 is improved.
With continued reference to FIG. 2, in some embodiments, the drive assembly 32 includes one or more steering engines 321, and one or more tie rods 322. One steering engine 321 has steering engine arms 3211. One end of one or more tie rods 322 is coupled to one or more mounting bases 312. The other end of the one or more tie rods 322 is connected to steering arms 3211. The built-in encoder of the steering engine 321 can receive PWM (pulse width modulation) signals sent by the unmanned aerial vehicle 100, the steering engine arm 3211 is controlled to rotate, and the steering engine arm 3211 is controlled to rotate to control the pull rod 322 to move towards the mounting base 312 or away from the mounting base 312 through rotation of the steering engine arm 3211, so that the mounting base machine can rotate anticlockwise or clockwise relative to the mounting structural member 311 around the first axis.
It should be noted that, one end of one pull rod 322 may be connected to one mounting base 312, and the other end of one pull rod 322 may be connected to the steering arm 3211. One end of one pull rod 322 is connected with the plurality of mounting bases 312, and the other end of one pull rod 322 is connected with the steering arm 3211. One end of a plurality of pull rods 322 is connected with one mounting base 312, and the other end of the plurality of pull rods 322 is connected with a steering arm 3211. One end of a plurality of pull rods 322 is connected with one mounting base 312, and the other end of the plurality of pull rods 322 is connected with a steering arm 3211.
With continued reference to fig. 2, the exemplary drive assembly 32 includes a steering engine 321 and a pull rod 322, one end of the pull rod 322 is coupled to a mounting base 312, and the other end of the pull rod 322 is coupled to a steering engine arm 3211. The steering engine 321 and the pull rod 322 may be located on the same side as the mounting base 312. When the mounting base 312 is required to rotate clockwise around the first axis, the unmanned aerial vehicle 100 sends a PWM signal, the built-in encoder of the steering engine 321 receives the PWM signal sent by the unmanned aerial vehicle 100, the steering engine 321 controls the rudder horn 3211 to rotate clockwise according to the received signal, and at the moment, the pull rod 322 moves in a direction away from the mounting base 312, so that the mounting base 312 is controlled to rotate clockwise around the first axis.
When the installation base 312 is required to rotate anticlockwise around the first axis, the unmanned aerial vehicle 100 sends a PWM signal, the built-in encoder of the steering engine 321 receives the PWM signal sent by the unmanned aerial vehicle 100, the steering engine 321 controls the steering engine arm 3211 to rotate anticlockwise according to the received signal, and at the moment, the pull rod 322 moves towards a direction close to the installation base 312, so that the installation base 312 is controlled to rotate anticlockwise around the first axis.
With continued reference to FIG. 2, in some embodiments, the drive assembly 32 is removably coupled to the mounting structure 311. The drive assembly 32 is convenient to replace and maintain, so that the whole cradle head 3 can be prevented from being replaced, and the service life and maintainability of the cradle head 3 can be improved. And the driving component 32 is connected with the mounting structural member 311, so that additional components for mounting the driving component 32 can be avoided, the structural layout of the cradle head 3 can be optimized, and the structure of the cradle head 3 can be more compact.
Illustratively, the drive assembly 32 and the mounting structure 311 may be coupled by way of a snap fit, a fastener connection, an adhesive, or the like.
With continued reference to fig. 2, in some embodiments, the mounting structure 311 further includes a plurality of first connectors 313. A mounting base 312 is connected to a mounting structure 311 by a first connector 313. It will be appreciated that one end of the first connector 313 is connected to one mounting structure 311 and the other end of the first connector 313 is connected to a corresponding mounting base 312. Through setting up first connecting piece 313, can improve the joint strength between mounting structure 311 and the mounting base 312 to also can change the mounted position of mounting base 312 through first connecting piece 313, make cloud platform 3 can satisfy user's user demand better, thereby be favorable to improving user's use experience.
Referring to fig. 2, the first connector 313 has a fixing portion 3133 and a connecting portion 3132, the fixing portion 3133 is connected to the mounting structure 311, one end of the connecting portion 3132 is connected to the fixing portion 3133, and the other end of the connecting portion 3132 is connected to the mounting structure 311. By providing the first connecting member 313, the mounting bases 312 connected with different mounting structural members 311 can be symmetrically arranged, which is beneficial to improving the aesthetic property of the pan-tilt 3.
With continued reference to FIG. 2, in some embodiments, the mounting assembly 31 further includes a plurality of damping spindles 314. A first mounting hole 3131 is provided in one first connection member 313, and a second mounting hole 3123 is provided in the mounting base 312 corresponding to the first connection member 313, which is matched with the first mounting hole 3131. The damping rotation shaft 314 is penetrated in the first and second mounting holes 3131 and 3123. Through setting up damping pivot 314, can avoid mounting base 312 to take place to rock after rotatory to the assigned position, be favorable to improving stability and reliability after the mounting base 312 is rotatory to also can reduce the rocking of fixing the article on mounting base 312, be favorable to improving the reliability of cloud platform 3.
With continued reference to fig. 2, in some embodiments, one mounting base 312 includes a first portion 3121 and a second portion 3122. One end of the first portion 3121 is rotatably connected to the corresponding mounting structure 311, the other end of the first portion 3121 is connected to one end of the second portion 3122, and an angle is formed between the first portion 3121 and the second portion 3122. Wherein the angle between the first portion 3121 and the second portion 3122 may be a right angle. This arrangement allows for better structural strength between the mounting base 312 and the mounting structure 311 and also facilitates increased mounting area of the mounting base 312, allowing for a more secure attachment of the article to the mounting base 312.
With continued reference to fig. 2, in some embodiments, the second portion 3122 includes a plurality of third mounting holes 3124, and the plurality of third mounting holes 3124 are spaced apart. By providing a plurality of third mounting holes 3124, the article may be more securely coupled to the mounting base 312. Wherein the plurality of third mounting holes 3124 may be uniformly spaced.
With continued reference to FIG. 2, in some embodiments, the mounting assembly 31 further includes a second connector 315. The second connector 315 includes a first connecting portion 3151 and a second connecting portion 3152 connected in sequence. The projection of the second connecting portion 3152 on the plane of the first connecting portion 3151 is perpendicular to the first connecting portion 3151. The first connecting portion 3151 is detachably connected to the mounting structure 311, and the second connecting portion 3152 is detachably connected to the unmanned aerial vehicle 100. By providing the second connection 315, connection between the mounting structure 311 having different extension directions and the leg 2 of the unmanned aerial vehicle 100 is facilitated. Meanwhile, the cradle head 3 can also be stressed and transferred to the supporting legs 2, so that the bearing capacity of the cradle head 3 can be improved.
Illustratively, the second connectors 315 may be a plurality of, and the plurality of second connectors 315 may enhance the strength of the connection between the mounting structure 311 and the drone 100.
In some embodiments, the projection of the second connecting portion 3152 on the plane of the first connecting portion 3151 may be parallel to the first connecting portion 3151. Therefore, the cradle head 3 is convenient to be connected with other unmanned aerial vehicles 100, and the application range of the cradle head 3 is favorably improved.
In some embodiments, the second connecting portion 3152 has a first adjustment aperture 3153 and a fourth mounting aperture 3154 formed therein. The second connection portion 3152 is connected to the unmanned aerial vehicle 100 through the fourth mounting hole 3154. An adjusting fastener is disposed in the first adjusting hole 3153, and is used for adjusting the size of the fourth mounting hole 3154. Through setting up the fourth mounting hole 3154 of adjustable internal diameter, make tripod head 3 can be connected with stabilizer blade 2 that the internal diameter is different to be favorable to improving tripod head 3's application scope. Meanwhile, the mode of adjusting by the fastener is adopted, so that the adjustment is convenient and quick, and the operation of a user is facilitated.
In some embodiments, the structure of the first connecting portion 3151 may be the same as that of the second connecting portion 3152, so that the applicability of the pan-tilt head 3 may be further improved.
In the description of the present specification, a particular feature, structure, material, or characteristic may be combined in any suitable manner in one or more embodiments or examples.
The foregoing is merely illustrative of the present utility model, and the present utility model is not limited thereto, and any person skilled in the art will readily recognize that variations or substitutions are within the scope of the present utility model. Therefore, the protection scope of the present utility model shall be subject to the protection scope of the claims.
Claims (10)
1. The utility model provides a cloud platform is applied to unmanned aerial vehicle, its characterized in that includes:
the installation assembly comprises a plurality of installation structural members and a plurality of installation bases, wherein the installation structural members are arranged at intervals, the installation structural members are detachably connected with the unmanned aerial vehicle, one installation base is rotatably connected with one installation structural member, and the installation bases are used for installing articles;
and the driving assembly is connected with the one or more mounting bases and is used for driving the mounting bases to rotate around a first axis relative to the mounting structural member.
2. The pan-tilt of claim 1, wherein the drive assembly includes one or more steering engines, one of the steering engines having a steering arm, one end of the one or more steering engines being coupled to the one or more mounting bases, and the other end of the one or more steering engines being coupled to the steering arm.
3. The holder of claim 1, wherein the drive assembly is removably coupled to the mounting structure.
4. The holder of claim 1, wherein the mounting assembly further comprises a plurality of first connectors, the one mounting base being connected to the one mounting structure by one first connector.
5. The holder of claim 4, wherein the mounting assembly further comprises a plurality of damping shafts, a first mounting hole is formed in the first connector, a second mounting hole is formed in the mounting base and mates with the first mounting hole, and a damping shaft is disposed through the first mounting hole and the second mounting hole.
6. The holder of claim 1, wherein the one mounting base comprises a first portion and a second portion, one end of the first portion being rotatably coupled to the one mounting structure, the other end of the first portion being coupled to one end of the second portion, the first portion and the second portion having an included angle therebetween.
7. The holder of claim 6, wherein the second portion is provided with a plurality of third mounting holes, and a plurality of the third mounting holes are spaced apart.
8. The holder of claim 1, wherein the mounting assembly further comprises a second connector comprising a first connector and a second connector connected in sequence, wherein a projection of the second connector on a plane of the first connector is perpendicular to the first connector, the first connector is detachably connected to the mounting structure, and the second connector is detachably connected to the unmanned aerial vehicle.
9. The holder according to claim 8, wherein a first adjusting hole and a fourth mounting hole are formed in the second connecting portion, the second connecting portion is connected with the unmanned aerial vehicle through the fourth mounting hole, an adjusting fastener is disposed in the first adjusting hole, and the adjusting fastener is used for adjusting the size of the fourth mounting hole.
10. An unmanned aerial vehicle, comprising:
the unmanned aerial vehicle comprises an unmanned aerial vehicle body and supporting legs, wherein one ends of the supporting legs are connected with the bottom surface of the unmanned aerial vehicle body, and the other ends of the supporting legs are used for supporting the bottom surface;
and a cradle head according to any one of claims 1-9, said cradle head being removably attachable to said foot.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321430491.4U CN220054160U (en) | 2023-06-06 | 2023-06-06 | Tripod head and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321430491.4U CN220054160U (en) | 2023-06-06 | 2023-06-06 | Tripod head and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220054160U true CN220054160U (en) | 2023-11-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321430491.4U Active CN220054160U (en) | 2023-06-06 | 2023-06-06 | Tripod head and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220054160U (en) |
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2023
- 2023-06-06 CN CN202321430491.4U patent/CN220054160U/en active Active
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