CN220199610U - Flight external member with handheld cloud platform - Google Patents
Flight external member with handheld cloud platform Download PDFInfo
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- CN220199610U CN220199610U CN202322021610.7U CN202322021610U CN220199610U CN 220199610 U CN220199610 U CN 220199610U CN 202322021610 U CN202322021610 U CN 202322021610U CN 220199610 U CN220199610 U CN 220199610U
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- 238000001746 injection moulding Methods 0.000 description 1
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Abstract
The utility model discloses a flight kit with a handheld cradle head, wherein the handheld cradle head is detachably arranged on a flight device, a first camera is arranged on the handheld cradle head, and a second camera is arranged on the flight device; in the use process, the handheld shooting can be selected through the handheld cradle head according to the use requirement, the handheld cradle head can also be inserted and installed on the flying device to form the flying cradle head, the flying device drives the handheld cradle head to carry out flying tracking shooting, and the flying device can also carry out independent tracking shooting; the flight device can realize palm take-off and landing by arranging flight blades in the blade protection cover; the portable shooting device can randomly switch the handheld mode or the flight mode according to shooting use requirements, and is simple and compact in structure, small in size, light in weight, convenient to carry and high in safety coefficient.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to a flight kit with a handheld cradle head.
Background
Along with the development of science and technology and resident living standard, the requirements for photographic recording of life, entertainment, holidays, group parties, major events, social activities and other scenes are higher and higher; in order to improve the photographic effect, the mode of combining the handheld device and unmanned aerial vehicle tracking shooting is generally adopted for multiparty shooting. The handheld cradle head and the unmanned aerial vehicle tracking shooting equipment in the prior art can only be used independently respectively, and the shooting mode cannot be switched at any time according to shooting use requirements.
The handheld holder and the flight suite in the prior art, such as the prior art with the patent application number of CN202080069839.4 and the patent name of CN202080069839.4, have huge structure, occupy more space and are inconvenient to carry; and its horn and screw are all exposed outside, because the screw needs to protect high-speed rotation in the flight, easily causes human injury or equipment damage accident, has the potential safety hazard.
Disclosure of Invention
In order to solve the problems in the prior art, the utility model aims to provide a flight kit with a handheld cradle head, which can randomly switch a handheld mode or a flight mode according to shooting use requirements, and has the advantages of simple and compact structure and high safety coefficient.
The technical scheme adopted by the utility model is as follows:
a flight external member with a handheld cradle head,
comprises a handheld cradle head, a flying part and a supporting part;
the flight part is used for providing flight power; the flying part is embedded in the hollow inner cavity of the supporting part, and a convection channel is arranged on the supporting part corresponding to the flying part in a penetrating way;
the handheld cradle head is provided with a first camera and/or the flying device is provided with a second camera;
the handheld cradle head comprises a supporting part and is characterized in that a placement bin is arranged on the supporting part and used for detachably placing and accommodating the handheld cradle head, and a first camera of the handheld cradle head extends out of the supporting part.
Further, the supporting part comprises a first supporting component and a second supporting component which are symmetrically arranged, and the placement bin is arranged in a spacing space between the first supporting component and the second supporting component.
Further, the flight part is provided with an even number of groups of flight blades; the inside of first supporting component and second supporting component sets up one set of or multiunit flight paddle respectively, and every group flight paddle is embedded to be set up in the inside of first supporting component or second supporting component respectively through the motor, and the position that corresponds every group flight paddle on first supporting component and the second supporting component runs through respectively and is provided with the convection current passageway for first supporting component and second supporting component constitute the paddle safety cover.
Further, the first supporting component is a groove box-shaped structure with an openable or closable top plate; at least a top plate of the first supporting component is provided with a plurality of first hollowed-out slotted holes, and a bottom plate of the first supporting component is provided with a plurality of second hollowed-out slotted holes, so that a convection channel is formed;
the shapes and the numbers of the first hollowed-out slotted holes are different from those of the second hollowed-out slotted holes, and the projection of each first hollowed-out slotted hole in the vertical direction is overlapped with the projection part of the second hollowed-out slotted hole in the corresponding position in the vertical direction.
Still further, the inner chamber of first supporting component is provided with two sets of flight paddles, and every flight paddle of group sets up on first supporting component's bottom plate through the motor respectively.
Still further, the structure of the second supporting component is formed by symmetrically arranging the structure of the first supporting component around the longitudinal center line of the placement bin.
Still further, the second camera is disposed on the supporting portion. Still further, a control module is arranged at the rear side of the placement bin; the middle part of the bottom surface of the supporting part is provided with a TOF sensor and a VIO sensor; be provided with TYPE EC connector on the inner wall of settling the storehouse, be connected to battery and control module through TYPE EC connector when settling the storehouse and inserting handheld cloud platform.
Still further, the handheld cloud platform is including handheld portion and load portion, load portion is connected to handheld portion through adjustment mechanism, handheld portion is rectangular columnar structure.
Finally, the first camera is arranged on the load part.
The beneficial effects of the utility model are as follows:
a flight kit with a handheld cradle head, wherein the handheld cradle head is detachably arranged on a flight device, a first camera is arranged on the handheld cradle head, and a second camera is arranged on the flight device; in the use process, the handheld shooting can be selected through the handheld cradle head according to the use requirement, the handheld cradle head can also be inserted and installed on the flying device to form the flying cradle head, the flying device drives the handheld cradle head to carry out flying tracking shooting, and the flying device can also carry out independent tracking shooting; the flight device can realize palm take-off and landing by arranging flight blades in the blade protection cover; the portable shooting device can randomly switch the handheld mode or the flight mode according to shooting use requirements, and is simple and compact in structure, small in size, light in weight, convenient to carry and high in safety coefficient.
Drawings
FIG. 1 is a schematic perspective view of a flying device according to a first embodiment of the present utility model;
FIG. 2 is an exploded view of a three-dimensional structure of a flying device according to a first embodiment of the present utility model;
FIG. 3 is an enlarged schematic view of a planar structure of a flying device with a cradle head according to an embodiment of the present utility model;
FIG. 4 is an enlarged schematic view of the bottom structure of FIG. 3;
fig. 5 to 6 are enlarged schematic views of a three-dimensional structure of a flight kit with a handheld cradle head according to a second embodiment of the utility model;
FIG. 7 is an enlarged schematic view of a flight kit with a handheld cradle head according to a second embodiment of the present utility model;
FIG. 8 is an enlarged schematic view of the bottom structure of FIG. 7;
FIG. 9 is a schematic diagram illustrating a process for disassembling a handheld cradle head of a flight kit with a handheld cradle head according to a second embodiment of the present utility model;
fig. 10 is an enlarged schematic view of a three-dimensional structure of a handheld cradle head of a flight kit with the handheld cradle head according to the second embodiment of the utility model.
Detailed Description
The following description of the technical solutions in the embodiments of the present application will be made clearly and completely with reference to the accompanying drawings in the embodiments of the present application, and it is apparent that the described embodiments are only some embodiments of the present application, not all embodiments. All other embodiments, which can be made by one of ordinary skill in the art without undue burden from the present disclosure, are within the scope of the present disclosure.
The terms "first," "second," "third," and the like in this application are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number or order of technical features indicated. All directional indications (such as up, down, left, right, front, back … …) in the embodiments of the present application are merely used to explain the relative positional relationship or movement between the components in a particular posture (as shown in the drawings), etc.; it should be noted that when an element is referred to as being "fixed," "disposed" or "connected" to another element, it may be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or one or more intervening elements may also be present therebetween. The terms "vertical," "horizontal," "left," "right," and the like are used herein for illustrative purposes only and are not meant to be the only embodiment.
As shown in fig. 1 to 10, the present utility model provides an overall design scheme of a flight kit with a handheld cradle head, which comprises: firstly, providing a flying device capable of carrying a handheld cradle head, wherein the flying device is formed by combining a flying part 1 and a supporting part 2, the flying part 1 is embedded in a hollow inner cavity of the supporting part 2, and a convection channel is arranged on the supporting part 2 corresponding to the position of the flying part in a penetrating way; thereby the flight power can be provided through the flight part to realize the flight function. The supporting part 2 is provided with a placement bin 21, and the placement bin 21 is used for detachably placing and accommodating the handheld tripod head 100, so that the flying device can drive the handheld tripod head to carry out flying tracking shooting through a first camera of the handheld tripod head; and the first camera 101 of the handheld cradle head 100 stretches out to the outside of the supporting part 2, the shooting visual field of the first camera 101 cannot be influenced, the visual field range is wide, and the shooting effect is good.
The flying part 1 is embedded in the hollow inner cavity of the supporting part 2, so that the palm take-off and landing can be realized; the handheld mode or the flight mode can be switched randomly according to shooting use requirements, the structure is simple and compact, and the safety coefficient is high.
The second camera 20 may also be disposed on the support part 2 of the flying device of the present utility model, so that the flying device of the present utility model may individually perform flying tracking shooting through the second camera 20.
And then the flying suite with the handheld cradle head is formed by combining the flying suite with the handheld cradle head.
The specific implementation process is as follows:
embodiment one: firstly, providing a flying device capable of carrying a handheld cradle head, which is formed by combining a flying part 1 and a supporting part 2, wherein the flying part 1 is embedded in a hollow inner cavity of the supporting part 2, and a convection channel is arranged on the supporting part 2 corresponding to the position of the flying part in a penetrating way; thereby the flight power can be provided through the flight part to realize the flight function. The supporting part 2 is provided with a placing bin 23, and the placing bin 23 is used for detachably placing and accommodating the handheld tripod head 100, so that the flying device can drive the handheld tripod head to carry out flying tracking shooting through a first camera of the handheld tripod head; and the first camera 101 of the handheld cradle head 100 stretches out to the outside of the supporting part 2, the shooting visual field of the first camera 101 cannot be influenced, the visual field range is wide, and the shooting effect is good.
Further, the main structure of the supporting part 2 is a first supporting component 21 and a second supporting component 22, the first supporting component 21 and the second supporting component 22 are symmetrically arranged, and the placement bin 23 is arranged in the interval space between the first supporting component 21 and the second supporting component 22, so that the balance performance is good.
Further, the main structure of the flight part 1 is that a plurality of groups of flight blades 11 are arranged, and the flight blades of even groups are arranged in detail, so that the flight part is convenient to be correspondingly arranged with the symmetrically arranged first support component 21 and second support component 22. That is, one or more groups of flight blades are respectively arranged in the first support component 21 and the second support component 22, each group of flight blades is respectively embedded in the first support component 21 or the second support component 22 through a motor 12, convection channels are respectively arranged on the first support component 21 and the second support component 22 corresponding to the positions of each group of flight blades 11 in a penetrating way, and rising power is generated through the convection channels when the motor drives the flight blades to rotate; meanwhile, the first supporting component 21 and the second supporting component 22 form a blade protecting cover, so that the flying blades are not exposed outside, and the flying blades cannot contact with the outer space of the blade protecting cover in the processes of taking off, landing and flying, and the safety coefficient is high.
Further, the first support member 21 is a channel box-like structure in which the top plate 211 can be opened or closed; a plurality of first hollow slots 212 are disposed on the top plate 211 of the first support assembly 21, and a plurality of second hollow slots 214 are disposed on the bottom plate 213, thereby forming a convection channel.
The shape and the number of the first hollow slots 212 on the top plate 211 are different from those of the second hollow slots 214 on the bottom plate 213, and the projection of each first hollow slot 212 in the vertical direction is overlapped with the projection part of the second hollow slot 214 in the corresponding position in the vertical direction, so that the air flow of the flight blade is ensured to be unobstructed when the flight blade rotates.
In the first embodiment, four isosceles triangle first hollow slots 212 are disposed on the top plate 211 corresponding to each group of flight blades, and the four isosceles triangle first hollow slots 212 are uniformly arranged around the center of each group of flight blades.
Four rectangular first hollowed-out slotted holes 214 are arranged on the bottom plate 212 at positions corresponding to each group of flight paddles, and four isosceles rectangular second hollowed-out slotted holes 214 are uniformly arranged around the center of each group of flight paddles.
A plurality of rectangular third hollow slots can be respectively arranged on the peripheral side walls of the first support component 21, so that the flight effect of the flight blade during rotation is further improved.
In the first embodiment, the first support component substantially forms a hollow-mesh-shaped box-shaped blade protection cover structure through the first hollow slot 212, the first hollow slot 214 and the third hollow slot 215.
Further, the structure of the second support assembly 22 is composed of the structure of the first support assembly 21 symmetrically disposed about the longitudinal center line of the placement chamber 23.
In the first embodiment, two groups of flight blades are symmetrically arranged in the inner cavity of the first support assembly, and each group of flight blades is rotatably arranged on the bottom plate of the first support assembly through a motor respectively; a group of first hollowed-out slotted holes are respectively arranged on the top plate of the first supporting component at positions corresponding to each group of flight paddles, and a group of second hollowed-out slotted holes are respectively arranged on the bottom plate at positions corresponding to each group of flight paddles; each motor is arranged on the central position of the area where a group of second hollowed-out slotted holes are positioned on the bottom plate of the first supporting component. Therefore, the first support component is also symmetrical around the transverse central line, and the second support component is also symmetrical around the transverse central line. The first supporting component and the second supporting component are symmetrically distributed around the longitudinal center line of the placement bin, so that the traveling device of the aircraft with the handheld cradle head is of a structure which is symmetrical to each other along the transverse center line and the longitudinal center line, and the balance stability performance is good.
The structure of the second supporting component 22 in the first embodiment is substantially identical to that of the first supporting component 21, so that the directions of the second supporting component and the first supporting component are not required to be distinguished in the assembling and using process, the second supporting component and the first supporting component can be combined in any direction, the production process flow is simplified, and the operation is convenient.
The first support component and the second support component are injection molding pieces, and the size is small and the weight is light.
Further, the placement cabin 23 is disposed at an upper portion of a space between the first support assembly 21 and the second support assembly 22, and the battery 24 and the second camera 20 are disposed at a lower portion of the space between the first support assembly 21 and the second support assembly 22, the second camera being a tracking camera; a control module 25 is arranged at the rear side of the placement bin 23, and a power indicator lamp 25 is arranged on the control module; a TOF sensor 26 and a VIO sensor 27 are arranged in the middle of the bottom surface of the support part 2; the battery 24, the second camera 20, the power indicator, the TOF sensor 26, the VIO sensor 27, and other electrical signal portions are all connected to the control module.
When the flying device with the handheld cradle head is independently used, tracking shooting can be realized through the TOF sensor and the VIO sensor.
And set up TYPE EC connector 28 on the inner wall of settling the storehouse, can be connected to battery and control module through TYPE EC connector when settling the storehouse and inserting handheld cloud platform, be convenient for centralized control.
In this example can carry on the flight device of handheld cloud platform, settle the storehouse and can also regard as the load storehouse to popularize and apply to can popularize and apply to other unmanned aerial vehicle application fields that need flight load.
Embodiment two: on the basis of the first embodiment, a flight kit with a handheld cradle head is provided, which is formed by combining the handheld cradle head and the flight device with the handheld cradle head 3 and the tracking shooting function, wherein the handheld cradle head 3 is detachably arranged on the flight device; the flying device provides flying power and drives the handheld cradle head 3 to realize flying tracking shooting; therefore, the flight kit with the functions of holding the cradle head and tracking shooting is formed. The handheld cradle head 3 is specifically formed by combining a handheld part 31 and a load part 32, the load part 32 is installed and connected to the end part of the handheld part 31 through an adjusting mechanism 33, and the handheld part 31 adopts a rectangular columnar structure. The load part, the handheld part and the adjusting mechanism of the handheld tripod head can directly adopt the structure of the handheld tripod head of the same type in the prior art. The first camera 30 is fixedly mounted on the load portion 32. The first camera can be arranged on the handheld cradle head through the load part, and the second camera can also be arranged on the flying device. In the use process, the handheld shooting can be selected through the handheld cradle head according to the use requirement, the handheld cradle head can also be inserted and installed on the flying device to form the flying cradle head, the flying device drives the handheld cradle head to carry out flying tracking shooting, and the flying device can also carry out independent tracking shooting; the flight device can realize palm take-off and landing by arranging flight blades in the blade protection cover; the portable shooting device can randomly switch the handheld mode or the flight mode according to shooting use requirements, and is simple and compact in structure, small in size, light in weight, convenient to carry and high in safety coefficient.
The handheld holder of the utility model can directly adopt the DJI Pocket2 type handheld holder sold in the market and the handheld holders of the same type in the prior art.
The utility model aims to provide a portable small-size handheld cradle head tracking flight kit, which is based on a small folding aircraft, and the handheld cradle head is arranged on the equipment, so that a common handheld cradle head can not only shoot in a handheld manner, but also fly, and is used as a flight cradle head.
The main technical points of the utility model are as follows:
1. the handheld cradle head and the folding aircraft are combined together, so that the cradle head can be used for shooting in a handheld manner and can be used for tracking shooting in the air;
2. the small folding aircraft can be taken down from the flight suite to be used alone in a handheld mode, and the cradle head is inserted into the flight suite to carry out flight tracking shooting when a flight view angle is needed.
3. The flight kit is provided with a full-protection shell, is safe and reliable, and can take off and land on the palm;
4. the kit is of modular design
The utility model is not limited to the above-described alternative embodiments, and any person who may derive other various forms of products in the light of the present utility model, however, any changes in shape or structure thereof, all falling within the technical solutions defined in the scope of the claims of the present utility model, fall within the scope of protection of the present utility model.
Claims (10)
1. A flight external member that has handheld cloud platform concurrently which characterized in that: the flying device comprises a handheld cradle head, a flying part and a supporting part, wherein the flying part and the supporting part are combined to form the flying device;
the flight part is used for providing flight power; the flying part is embedded in the hollow inner cavity of the supporting part, and a convection channel is arranged on the supporting part corresponding to the flying part in a penetrating way;
the handheld cradle head is provided with a first camera and/or the flying device is provided with a second camera; the handheld cradle head comprises a supporting part and is characterized in that a placement bin is arranged on the supporting part and used for detachably placing and accommodating the handheld cradle head, and a first camera of the handheld cradle head extends out of the supporting part.
2. The flight kit with the handheld cradle head as set forth in claim 1, wherein: the supporting part comprises a first supporting component and a second supporting component which are symmetrically arranged, and the placement bin is arranged in a spacing space between the first supporting component and the second supporting component.
3. The flight kit with the handheld cradle head as set forth in claim 2, wherein: the flying part is provided with an even number of flying blades; the inside of first supporting component and second supporting component sets up one set of or multiunit flight paddle respectively, and every group flight paddle is embedded to be set up in the inside of first supporting component or second supporting component respectively through the motor, and the position that corresponds every group flight paddle on first supporting component and the second supporting component runs through respectively and is provided with the convection current passageway for first supporting component and second supporting component constitute the paddle safety cover.
4. A flight kit with a handheld pan-tilt as claimed in claim 3, wherein: the first supporting component is a groove box-shaped structure with an openable top plate or a closable top plate; at least a top plate of the first supporting component is provided with a plurality of first hollowed-out slotted holes, and a bottom plate of the first supporting component is provided with a plurality of second hollowed-out slotted holes, so that a convection channel is formed;
the shapes and the numbers of the first hollowed-out slotted holes are different from those of the second hollowed-out slotted holes, and the projection of each first hollowed-out slotted hole in the vertical direction is overlapped with the projection part of the second hollowed-out slotted hole in the corresponding position in the vertical direction.
5. The flight kit with the handheld cradle head as set forth in claim 4, wherein: the inner cavity of the first supporting component is provided with two groups of flight blades, and each group of flight blades is arranged on the bottom plate of the first supporting component through a motor.
6. The flight kit with the handheld cradle head as set forth in claim 5, wherein: the structure of the second supporting component is formed by symmetrically arranging the structure of the first supporting component around the longitudinal center line of the placement bin.
7. The flight kit with the handheld cradle head as set forth in claim 6, wherein: the second camera is arranged on the supporting part.
8. The flight kit with the handheld cradle head as set forth in claim 2, wherein: the said; the rear side of the placement bin is provided with a control module; the middle part of the bottom surface of the supporting part is provided with a TOF sensor and a VIO sensor; be provided with TYPE EC connector on the inner wall of settling the storehouse, handheld cloud platform cartridge can be connected to battery and control module through TYPE EC connector when settling the storehouse.
9. The flight kit with the handheld cradle head as set forth in claim 1, wherein: the handheld cradle head comprises a handheld part and a load part, wherein the load part is connected to the handheld part through an adjusting mechanism, and the handheld part is of a rectangular columnar structure.
10. The flight kit with the handheld cradle head as set forth in claim 1, wherein: the first camera is arranged on the load part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322021610.7U CN220199610U (en) | 2023-07-28 | 2023-07-28 | Flight external member with handheld cloud platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322021610.7U CN220199610U (en) | 2023-07-28 | 2023-07-28 | Flight external member with handheld cloud platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220199610U true CN220199610U (en) | 2023-12-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322021610.7U Active CN220199610U (en) | 2023-07-28 | 2023-07-28 | Flight external member with handheld cloud platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220199610U (en) |
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2023
- 2023-07-28 CN CN202322021610.7U patent/CN220199610U/en active Active
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