CN211543924U - Unmanned aerial vehicle cloud platform and unmanned aerial vehicle with shockproof function - Google Patents
Unmanned aerial vehicle cloud platform and unmanned aerial vehicle with shockproof function Download PDFInfo
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- CN211543924U CN211543924U CN201921961299.1U CN201921961299U CN211543924U CN 211543924 U CN211543924 U CN 211543924U CN 201921961299 U CN201921961299 U CN 201921961299U CN 211543924 U CN211543924 U CN 211543924U
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Abstract
The utility model discloses an unmanned aerial vehicle cloud platform and unmanned aerial vehicle with shockproof function, this unmanned aerial vehicle cloud platform includes first fixed bolster, the second fixed bolster, module and cloud platform main part make a video recording, first fixed bolster includes first support segment and second support segment, be equipped with the shock attenuation ball on the first support segment, the second support segment downwardly extending just forms the contained angle with first support segment from first support segment, the second fixed bolster sets firmly outside the contained angle space that second support segment just is located the contained angle, the module of making a video recording is located first support segment and is located the contained angle space of contained angle, cloud platform main part is connected in the second fixed bolster. The embodiment of the utility model provides an unmanned aerial vehicle cloud platform and unmanned aerial vehicle adopts and sets up the shock attenuation ball on the first support part that is equipped with the module of making a video recording, utilizes the shock attenuation ball can alleviate the strong wind air current in the air to the influence of unmanned aerial vehicle cloud platform to can alleviate the degree that the unmanned aerial vehicle cloud platform takes place vibrations or rocks, improve the image stability of unmanned aerial vehicle module of making a video recording.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle shockproof technical field especially relates to an unmanned aerial vehicle cloud platform machine and unmanned aerial vehicle with shockproof function.
Background
In recent years, with the vigorous development of the correlation technique and the application of an unmanned aerial vehicle (hereinafter referred to as an unmanned aerial vehicle), the camera shooting function becomes one of the necessary functions of the unmanned aerial vehicle, so that most unmanned aerial vehicles can be provided with camera shooting equipment, wherein the camera shooting equipment is mainly fixed on the unmanned aerial vehicle through a holder. When unmanned aerial vehicle flies in the high altitude, the unmanned aerial vehicle cloud platform receives the influence of the strong wind air current in the air easily, leads to the unmanned aerial vehicle cloud platform to take place violent vibrations or rock easily, and the mirror image that not only can lead to unmanned aerial vehicle's camera equipment to shoot like this is fuzzy, also can make whole camera equipment take place the skew, and then leads to shooting the scope skew of finding a view, influences camera equipment's normal use.
Consequently, in order to slow down the violent intensity that unmanned aerial vehicle cloud platform vibrations or rocked, add some shockproof structure at the unmanned aerial vehicle cloud platform at present many times, but because shockproof structure's structure is too complicated, the price is more expensive, and this not only leads to unmanned aerial vehicle's the overweight of load, causes unmanned aerial vehicle's consumed power, load grow, influences unmanned aerial vehicle's flight, has also increased unmanned aerial vehicle overall production cost moreover.
SUMMERY OF THE UTILITY MODEL
The embodiment of the utility model discloses unmanned aerial vehicle cloud platform and unmanned aerial vehicle with shockproof function can solve because of the easy violent vibrations that take place of unmanned aerial vehicle cloud platform or rock and lead to the fuzzy problem of mirror image that unmanned aerial vehicle's the module of making a video recording shot.
In order to achieve the above object, a first aspect of the present invention provides an unmanned aerial vehicle cloud platform with shockproof function, include:
the first fixing bracket comprises a first bracket part and a second bracket part, wherein a damping ball is arranged on the first bracket part, and the second bracket part extends downwards from the first bracket part and forms an included angle with the first bracket part;
the second fixing support is fixedly arranged on the second support part and is positioned outside the included angle space of the included angle;
the camera shooting module is arranged on the first support part and is positioned in the included angle space of the included angle; and
and the holder main body is connected to the second fixing support.
As an alternative, in an embodiment of the first aspect of the present invention, the first frame part is provided with a first connecting member, and the damping ball is provided with a second connecting member, and the second connecting member is connected to the first connecting member.
As an optional implementation manner, in an embodiment of the first aspect of the present invention, the unmanned aerial vehicle pan-tilt further includes a third fixed bracket, the third fixed bracket is fixedly disposed on the first bracket portion, and a third connecting member is disposed on the third fixed bracket;
the upside and the downside of shock attenuation ball are equipped with respectively the second connecting piece, be located the upside the second connecting piece connect in the third connecting piece, be located the downside the second connecting piece connect in first connecting piece.
As an optional implementation manner, in an embodiment of the first aspect of the present invention, the second connecting member is a protruding block protruding from the damping ball, and the second connecting member is provided with a through groove, the first connecting member is a T-shaped protruding block, and includes an insertion portion and a stopping portion vertically connected to the insertion portion, the insertion portion is inserted into the through groove, and the stopping portion is located outside the through groove.
As an alternative implementation, in an embodiment of the first aspect of the present invention, the second frame portion is a U-shaped frame, and includes a first upright, a second upright and a first cross bar, the first cross bar is connected to the bottom of the first upright and the second upright, the first frame portion includes two second cross bars, and the two second cross bars are respectively connected to the top of the first upright and the top of the second upright and extend forward from the top of the first upright and the top of the second upright.
As an optional implementation manner, in an embodiment of the first aspect of the present invention, the third fixing bracket is a U-shaped frame, and includes a first portion, a second portion and a third portion that are connected in sequence, the first portion is fixedly disposed on one of the second cross rods, the third portion is fixedly disposed on the other of the second cross rods, and the first portion and the third portion are both provided with the third connecting member.
As an optional implementation manner, in an embodiment of the first aspect of the present invention, the third fixing frame is made of gum or silica gel.
In an alternative embodiment, in an embodiment of the first aspect of the present invention, the number of the damping balls is four, two damping balls are spaced apart from each other in the first portion, two damping balls are spaced apart from each other in the third portion, and the four damping balls are arranged in a square on the first portion.
As an optional implementation manner, in an embodiment of the first aspect of the present invention, the holder main body is rotatably disposed on the second fixing support.
As an optional implementation manner, in an embodiment of the first aspect of the present invention, the second fixed support is a hollow frame, a hollow portion of the hollow frame communicates with the included angle space of the included angle, the second fixed support is close to a position where the second support portion is connected to the first support portion, and a first rotating portion is disposed on the position, where the second support portion is connected to the first support portion, of the second fixed support.
As an optional implementation manner, in an embodiment of the first aspect of the present invention, the unmanned aerial vehicle pan-tilt further includes a support cover, the support cover is disposed on the first support portion and forms an accommodating space with the first support portion, and the third fixing support is located in the accommodating space.
As an optional implementation manner, in the embodiment of the first aspect of the present invention, the pan/tilt head main body includes the pan/tilt head main casing and locates the pan/tilt head control panel inside the pan/tilt head main casing, the pan/tilt head main casing is composed of a first pan/tilt head casing and a second pan/tilt head casing which are arranged relatively, the first pan/tilt head casing and the second pan/tilt head casing form after closing the chamber that holds of the pan/tilt head main casing, the pan/tilt head control panel is located hold in the chamber, just the pan/tilt head control panel with the camera module group electricity is.
In a second aspect, an embodiment of the present invention provides an unmanned aerial vehicle, the unmanned aerial vehicle includes an unmanned aerial vehicle body and an unmanned aerial vehicle holder as described above in the first aspect, a second support part of the unmanned aerial vehicle holder is installed to the unmanned aerial vehicle body.
Compared with the prior art, the beneficial effects of the utility model reside in that:
(1) can effectively guarantee unmanned aerial vehicle's shooting effect. The embodiment of the utility model provides a pair of unmanned aerial vehicle cloud platform and unmanned aerial vehicle with shockproof function adopts and sets up the shock attenuation ball on the first support part that is equipped with the module of making a video recording, utilizes the shock attenuation ball can alleviate the strong wind air current in the air to the influence of unmanned aerial vehicle cloud platform to can alleviate the degree that the unmanned aerial vehicle cloud platform takes place vibrations or rocks, improve the image stability of unmanned aerial vehicle module of making a video recording.
(2) The whole weight of the unmanned aerial vehicle can be lightened. The unmanned aerial vehicle cloud platform and unmanned aerial vehicle of this embodiment adopt shell structure's fixed damping ball of fixed bolster, make a video recording module and cloud platform main part, and the fixed bolster matter is light and simple structure, is favorable to alleviateing unmanned aerial vehicle's whole weight for unmanned aerial vehicle's flight is lighter and more graceful, more stable.
(3) Can improve unmanned aerial vehicle flight's stability and security. The utility model discloses an unmanned aerial vehicle cloud platform and unmanned aerial vehicle, through the mode with cloud platform main part rotatable coupling in second fixed bolster, when installing the unmanned aerial vehicle cloud platform in the unmanned aerial vehicle body, can rotate the position of cloud platform main part with the adjustment cloud platform main part according to the barycenter of unmanned aerial vehicle body for the unmanned aerial vehicle cloud platform is closer to the barycenter of unmanned aerial vehicle body, thereby can make unmanned aerial vehicle's flight more stable safety.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle pan-tilt provided by the first embodiment of the present invention;
fig. 2 is an exploded schematic view of an unmanned aerial vehicle pan-tilt provided by the first embodiment of the present invention;
fig. 3 is a schematic structural diagram of a first bracket according to an embodiment of the present invention;
fig. 4 is another schematic structural diagram of the unmanned aerial vehicle cloud platform that the embodiment of the utility model provides a provide.
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.
In the present invention, the terms "upper", "lower", "left", "right", "front", "rear", "top", "bottom", "inner", "outer", "middle", "vertical", "horizontal", "lateral", "longitudinal", and the like indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings. These terms are used primarily to better describe the invention and its embodiments, and are not intended to limit the indicated devices, elements or components to a particular orientation or to be constructed and operated in a particular orientation.
Moreover, some of the above terms may be used to indicate other meanings besides the orientation or positional relationship, for example, the term "on" may also be used to indicate some kind of attachment or connection relationship in some cases. The specific meaning of these terms in the present invention can be understood by those of ordinary skill in the art as appropriate.
Furthermore, the terms "mounted," "disposed," "provided," "connected," and "connected" are to be construed broadly. For example, it may be a fixed connection, a removable connection, or a unitary construction; can be a mechanical connection, or an electrical connection; may be directly connected, or indirectly connected through intervening media, or may be in internal communication between two devices, elements or components. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
Furthermore, the terms "first," "second," and the like, are used primarily to distinguish one device, element, or component from another (the specific nature and configuration may be the same or different), and are not used to indicate or imply the relative importance or number of the indicated devices, elements, or components. "plurality" means two or more unless otherwise specified.
The technical solution of the present invention will be further described with reference to the following embodiments and the accompanying drawings.
Example one
Please refer to fig. 1 to 3 together, an embodiment of the present invention provides an unmanned aerial vehicle pan-tilt with shockproof function, this unmanned aerial vehicle pan-tilt 1 includes first fixed bolster 10, second fixed bolster 11, camera module 12 and pan-tilt main body 13, this first fixed bolster 10 includes first support part 101 and second support part 102, wherein, be equipped with damping ball 14 on the first support part 101, second support part 102 extends downwards from first support part 101 and forms the contained angle with first support part 101, second fixed bolster 11 sets firmly outside second support part 102 and is located the contained angle space of contained angle, camera module 12 locates first support part 101 and is located the contained angle space of contained angle, pan-tilt main body 13 is connected in second fixed bolster 11.
Wherein, the damping ball 14 can be made of soft materials such as silica gel and rubber; the camera module 12 can be an infrared camera module and/or a visible light camera module.
The adoption sets up the mode of shock attenuation ball 14 on the first support part 101 that is equipped with the module 12 of making a video recording, can utilize the cushioning effect of shock attenuation ball 14 to alleviate the strong wind air current in the air to the influence of unmanned aerial vehicle cloud platform 1 to can alleviate the degree that unmanned aerial vehicle cloud platform 1 takes place vibrations or rocks, improve the image stability of unmanned aerial vehicle camera module 12, obtain the higher picture of definition or video.
Furthermore, in this patent, unmanned aerial vehicle cloud platform 1 can be applied to on the unmanned aerial vehicle. When the unmanned aerial vehicle cloud platform 1 of this embodiment is carried on unmanned aerial vehicle (not shown), because first fixed bolster 10 and the second fixed bolster 11 of fixed shock attenuation ball 14, camera module 12 and cloud platform main part 13 adopt shell structure, light in weight and simple structure are favorable to alleviateing unmanned aerial vehicle's whole weight for unmanned aerial vehicle's flight is lighter, more stable.
As shown in fig. 2 and 3, in the present embodiment, the second frame portion 102 may be a U-shaped frame, and includes a first upright 102a, a second upright 102b, and a first cross bar 102c, wherein the first cross bar 102c is connected to the bottom of the first upright 102a and the second upright 102b, and the first frame portion 101 may include two second cross bars which are respectively connected to the top of the first upright 102a and the second upright 102b and respectively extend forward from the top of the first upright 102a and the second upright 102 b. That is to say, first fixed bolster 10 that first support part 101 and second support part 102 connect formation is hollow frame, and this is favorable to alleviateing the weight of first fixed bolster 10 to can reduce the weight of unmanned aerial vehicle cloud platform 1, the flight of the unmanned aerial vehicle of being convenient for.
Further, in order to fix the shock-absorbing ball 14 to the first frame portion 101, the first frame portion 101 is provided with a first connector 103, and the shock-absorbing ball 14 is provided with a second connector 141 connected to the first connector 103. Specifically, the second connecting member 141 is a protruding block protruding from the damping ball 14, and the second connecting member 141 is provided with a through groove, the first connecting member 103 may be a T-shaped protruding block, the first connecting member 103 includes an insertion portion and a stopping portion vertically connected to the insertion portion, the insertion portion is inserted into the through groove, and the stopping portion is located outside the through groove.
The shock absorption balls 14 are fixed on the first support part 101 in an inserting mode, so that the shock absorption balls 14 can be quickly installed on the first support part 101, simplicity and convenience are realized, and the installation efficiency of the shock absorption balls 14 is improved; but also facilitates the removal of the shock-absorbing ball 14 from the first bracket part 101, facilitating the replacement and maintenance of the shock-absorbing ball 14.
Further, in order to fix the damping balls 14 on the first bracket portion 101 more firmly, the unmanned aerial vehicle pan/tilt head 1 further includes a third fixing bracket 15. The third fixing bracket 15 is fixedly arranged on the first bracket part 101, and a third connecting member 151 is arranged on the third fixing bracket 15. Specifically, the upper and lower sides of the shock-absorbing ball 14 are respectively provided with a second connector 141, the second connector 141 on the upper side is connected to a third connector 151, and the second connector 141 on the lower side is connected to the first connector 103.
As can be seen from the above description, the third connecting member 151 of the third fixing bracket 15 may also preferably be a T-shaped protrusion, which also includes an inserting portion 151a and a stopping portion 151b vertically connected to the inserting portion 151a, wherein the inserting portion 151a is inserted into the through groove, and the stopping portion 151b is located outside the through groove.
In the present embodiment, in order to further improve the shock-proof effect of the shock-absorbing ball 14, the material of the third fixing bracket 15 is preferably soft material such as gum or silica gel.
Further, in order to protect the third fixing bracket 15 from being damaged by other external substances, the unmanned aerial vehicle holder 1 further includes a bracket cover 16. Specifically, the bracket cover 16 covers the first bracket portion 101 and forms an accommodating space with the first bracket portion 101, and the third fixing bracket 15 is located in the accommodating space. This not only helps to protect the third fixing bracket 15 and improve the service life of the third fixing bracket 15, but also makes the overall structure of the first bracket portion 101 more compact and reduces the occupied space of the first bracket portion 101.
Further, in order to further reduce the mass of the first fixing bracket 10, the third fixing bracket 15 may be a U-shaped frame. Specifically, the third fixing bracket 15 includes a first portion 15a, a second portion 15b and a third portion 15c, which are connected in sequence, the first portion 15a is fixedly disposed on one of the second cross bars of the first bracket portion 101, the third portion 15c is fixedly disposed on the other second cross bar of the first bracket portion 101, and the first portion 15a and the third portion 15c are both provided with a third connecting member 151.
In the present embodiment, the number of the damping balls 14 may preferably be four, wherein two damping balls 14 are spaced apart from each other in the first portion 15a, and the other two damping balls 14 are spaced apart from each other in the third portion 15 c. In order to avoid shock attenuation ball 14 overall arrangement centroid to be far away from the centrobaric distance of unmanned aerial vehicle cloud platform 1, and lead to unmanned aerial vehicle cloud platform 1 to take place to rotate and produce vibration or rock around its self focus, influence the condition of the shooting of module 12 of making a video recording, preferably, four shock attenuation balls 14 are the square arrangement setting on first support portion 101.
Adopt such layout mode, can be so that the square centroid that the geometric centre of four shock attenuation balls 14 constitutes be close to the focus of unmanned aerial vehicle cloud platform 1 or be close with the focus coincidence of unmanned aerial vehicle cloud platform 1 to can reduce the condition of the vibrations or the rocking of unmanned aerial vehicle cloud platform 1, and then make shock attenuation ball 14 reach better shockproof effect, effectively improve the stability of unmanned aerial vehicle cloud platform 1.
Further, as shown in fig. 1 to 3, each of the shock-absorbing balls 14 includes a front side 14a and a rear side 14b, wherein the front side 14a of the shock-absorbing ball 14 refers to a side of the shock-absorbing ball 14 disposed toward one of the second cross bars 101a, and the rear side 14a of the shock-absorbing ball 14 refers to a side of the shock-absorbing ball 14 disposed away from one of the second cross bars 101 a. For the damping ball 14 connected to the third link 151 of the first portion 15a, the stopper 151b of the third link 151 is located at the front side of the damping ball 14, and the stopper of the first link 103 is located at the rear side of the damping ball 14; and, with respect to the damping ball 14 connected to the third link 151 of the third portion 15c, the stopper 151b of the third link 151 is located at the rear side of the damping ball 14, and the stopper of the first link 103 is located at the front side of the damping ball 14.
This cross-connection is advantageous in further improving the fixing effect and stability of the damping ball 14 and the first frame portion 101 to prevent the damping ball 14 from being separated from the first frame portion 101.
Referring to fig. 1, 2 and 4, fig. 4 is a schematic structural view of the unmanned aerial vehicle pan-tilt head in fig. 1, in which the pan-tilt head main body rotates a certain angle relative to the second support portion. In the present embodiment, the pan/tilt head main body 13 is rotatably provided on the second fixing bracket 11. Specifically, the second stationary bracket 11 is provided with a first rotating portion 111 near the connection of the second bracket portion 102 and the first bracket portion 101, and the head main body 13 is provided with a second rotating portion 133, wherein the first rotating portion 111 is rotatably connected to the second rotating portion 133, for example: the first rotating portion 111 may be two shaft holes formed in the second fixing bracket 11, and the second rotating portion 133 may be a rotating shaft, wherein two ends of the rotating shaft are rotatably connected to the two shaft holes, respectively. Adopt such a mode, be favorable to installing unmanned aerial vehicle cloud platform 1 in the unmanned aerial vehicle body time, can rotate cloud platform main part 13 according to the barycenter of unmanned aerial vehicle body to the position of adjustment cloud platform main part 13 makes unmanned aerial vehicle cloud platform 1 more be close to unmanned aerial vehicle's barycenter, thereby can make unmanned aerial vehicle's flight more stable safety.
Further, this second fixed bolster 11 can be the cavity frame, and the well kenozooecium of second fixed bolster 11 communicates in the contained angle space of contained angle, is favorable to further lightening the quality of first fixed bolster 10, makes things convenient for unmanned aerial vehicle's flight.
In this embodiment, the main body 13 includes the main body and locates the internal portion of main body of the cloud platform control panel 132, and the main body of the cloud platform comprises relative first cloud platform casing 131a and second cloud platform casing 131b that set up, and first cloud platform casing 131a forms the chamber that holds of the main body of the cloud platform after closing with second cloud platform casing 131b, and cloud platform control panel 132 locates and holds in the chamber, and cloud platform control panel 132 is connected with camera module 12 electricity.
In order to change the shooting direction of the camera module 12, the camera module 12 is convenient to shoot at multiple angles, and the unmanned aerial vehicle holder 1 further comprises a driving device 12 a. Specifically, the driving device 12a is fixed on the first frame portion 101, the driving device 12a can be located outside the space with the included angle, and the camera module 12 is connected to the driving device 12 a. Can drive the module of making a video recording 12 through drive arrangement 12a and take place to rotate to change the shooting direction of module of making a video recording 12, make things convenient for the shooting of module of making a video recording 12 more.
The drive device 12a may be a motor, among others.
The embodiment of the utility model provides a pair of unmanned aerial vehicle cloud platform with shockproof function adopts and sets up the shock attenuation ball on the first support part that is equipped with the module of making a video recording, utilizes the shock attenuation ball can alleviate the strong wind air current in the air to the influence of unmanned aerial vehicle cloud platform to can alleviate the degree that the unmanned aerial vehicle cloud platform takes place vibrations or rocks, improve the image stability of unmanned aerial vehicle module of making a video recording.
Furthermore, because the utility model is used for the first fixed bolster of fixed shock attenuation ball, the module of making a video recording is the U-shaped support to and the second fixed bolster that is used for fixed cloud platform main part is the cavity frame, is favorable to alleviateing unmanned aerial vehicle's whole weight, makes unmanned aerial vehicle's flight lighter and graceful, more stable.
Example two
Please refer to fig. 1 and fig. 2 again, embodiment two of the present invention provides an unmanned aerial vehicle, which includes an unmanned aerial vehicle body and an unmanned aerial vehicle cradle head as described in the above embodiment one, wherein the second support part 11 of the unmanned aerial vehicle cradle head 1 is installed on the unmanned aerial vehicle body. Specifically, this second support part 11's bottom is equipped with installation department 17, and wherein this installation department 17 is equipped with screw hole 171, and when the second support part 11 of unmanned aerial vehicle cloud platform 1 was installed to the unmanned aerial vehicle body on, mainly adopt bolt 18 and screw hole 171's cooperation to be connected the installation department 17 of second support part 11 and fix on the unmanned aerial vehicle body.
To sum up, the embodiment of the utility model provides a pair of unmanned aerial vehicle cloud platform and unmanned aerial vehicle with shockproof function adopts to set up the shock attenuation ball on the first support part that is equipped with the module of making a video recording, utilizes the strong wind air current that the shock attenuation ball can alleviate in the air to the influence of unmanned aerial vehicle cloud platform to can alleviate the degree that the unmanned aerial vehicle cloud platform takes place vibrations or rocks, improve the image stability of unmanned aerial vehicle module of making a video recording.
Furthermore, the utility model discloses an unmanned aerial vehicle cloud platform and unmanned aerial vehicle, through the mode with cloud platform main part rotatable coupling in second fixed bolster, when installing the unmanned aerial vehicle cloud platform in the unmanned aerial vehicle body, can rotate the position of cloud platform main part with the adjustment cloud platform main part according to the barycenter of unmanned aerial vehicle body for the unmanned aerial vehicle cloud platform is closer to the barycenter of unmanned aerial vehicle body, thereby can make unmanned aerial vehicle's flight more stable safety.
The unmanned aerial vehicle cradle head with the shockproof function and the unmanned aerial vehicle disclosed by the embodiment of the invention are described in detail above, the principle and the implementation mode of the invention are explained by applying specific examples in the text, and the description of the above embodiments is only used for helping to understand the principle and the core idea of the invention; meanwhile, for the general technical personnel in the field, according to the idea of the present invention, there are changes in the specific implementation and application scope, to sum up, the content of the present specification should not be understood as the limitation of the present invention.
Claims (13)
1. The utility model provides an unmanned aerial vehicle cloud platform with shockproof function which characterized in that includes:
the first fixing bracket comprises a first bracket part and a second bracket part, wherein a damping ball is arranged on the first bracket part, and the second bracket part extends downwards from the first bracket part and forms an included angle with the first bracket part;
the second fixing support is fixedly arranged on the second support part and is positioned outside the included angle space of the included angle;
the camera shooting module is arranged on the first support part and is positioned in the included angle space of the included angle; and
and the holder main body is connected to the second fixing support.
2. An unmanned aerial vehicle holder as defined in claim 1, wherein the first frame portion is provided with a first connector, and the shock absorbing ball is provided with a second connector, the second connector being connected to the first connector.
3. The unmanned aerial vehicle holder of claim 2, further comprising a third stationary gantry, the third stationary gantry being fixedly attached to the first frame portion, the third stationary gantry having a third connector;
the upside and the downside of shock attenuation ball are equipped with respectively the second connecting piece, be located the upside the second connecting piece connect in the third connecting piece, be located the downside the second connecting piece connect in first connecting piece.
4. The unmanned aerial vehicle holder of claim 3, wherein the second connecting member is a protrusion protruding from the damping ball, and the second connecting member is provided with a through groove, the first connecting member is a T-shaped protrusion and comprises an insertion portion and a stopping portion vertically connected with the insertion portion, the insertion portion is inserted into the through groove, and the stopping portion is located outside the through groove.
5. The unmanned aerial vehicle holder of claim 3 or 4, wherein the second support portion is a U-shaped support including a first upright, a second upright, and a first cross bar, the first cross bar being connected to the bottom of the first upright and the second upright, the first support portion including two second cross bars, the two second cross bars being connected to the top of the first upright and the second upright, respectively, and extending forward from the top of the first upright and the second upright, respectively.
6. The unmanned aerial vehicle cloud platform of claim 5, wherein, the third fixed bolster is U-shaped frame, includes first portion, second portion and the third portion that connects gradually, first portion set firmly in one of them second horizontal pole, the third portion set firmly in another one the second horizontal pole, and first portion and the third portion all are equipped with the third connecting piece.
7. An unmanned aerial vehicle holder according to claim 3 or 4, wherein the third fixing bracket is made of gum or silica gel.
8. An unmanned aerial vehicle holder as defined in claim 6, wherein the number of the shock absorbing balls is four, two shock absorbing balls are spaced apart from each other in the first portion, two shock absorbing balls are spaced apart from each other in the third portion, and the four shock absorbing balls are arranged in a square array on the first portion.
9. An unmanned aerial vehicle holder according to any one of claims 2 to 4, wherein the holder body is rotatably mounted on the second fixed support.
10. The unmanned aerial vehicle cloud platform of claim 9, wherein the second fixed bolster is hollow frame, and wherein the hollow portion communicates in the contained angle space of contained angle, the second fixed bolster is close to the position of second support part with first support part junction and is equipped with first rotation portion, the cloud platform main part is equipped with the second rotation portion, first rotation portion with the rotation of second rotation portion is connected.
11. An unmanned aerial vehicle holder as claimed in claim 3 or 4, wherein the unmanned aerial vehicle holder further comprises a support cover, the support cover is disposed on the first support portion and forms an accommodation space with the first support portion, and the third fixing support is located in the accommodation space.
12. The unmanned aerial vehicle cloud platform of any one of claims 1 to 4, wherein, the cloud platform main part includes the main casing body of cloud platform and locates the cloud platform control panel of the main casing body of cloud platform, the main casing body of cloud platform comprises relative first cloud platform casing and the second cloud platform casing that sets up, the first cloud platform casing forms the chamber that holds of the main casing body of cloud platform with the second cloud platform casing after closing, the cloud platform control panel is located in holding the chamber, and the cloud platform control panel is connected with the module electricity of making a video recording.
13. An unmanned aerial vehicle comprising an unmanned aerial vehicle body and an unmanned aerial vehicle pan/tilt head as claimed in any one of claims 1 to 12, the second support portion of the unmanned aerial vehicle pan/tilt head being mounted to the unmanned aerial vehicle body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921961299.1U CN211543924U (en) | 2019-11-13 | 2019-11-13 | Unmanned aerial vehicle cloud platform and unmanned aerial vehicle with shockproof function |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921961299.1U CN211543924U (en) | 2019-11-13 | 2019-11-13 | Unmanned aerial vehicle cloud platform and unmanned aerial vehicle with shockproof function |
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| CN211543924U true CN211543924U (en) | 2020-09-22 |
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| CN201921961299.1U Active CN211543924U (en) | 2019-11-13 | 2019-11-13 | Unmanned aerial vehicle cloud platform and unmanned aerial vehicle with shockproof function |
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