CN211108034U - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
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- CN211108034U CN211108034U CN201921006606.0U CN201921006606U CN211108034U CN 211108034 U CN211108034 U CN 211108034U CN 201921006606 U CN201921006606 U CN 201921006606U CN 211108034 U CN211108034 U CN 211108034U
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Abstract
The utility model discloses an unmanned aerial vehicle, which comprises a body and a connecting structure, wherein the body is provided with a mounting groove for mounting the connecting structure, and a first clamping part and a first fixing part are arranged in the mounting groove; the connecting structure comprises a first mounting part and a second mounting part obliquely extending from one end of the first mounting part, the first mounting part is provided with a second clamping part, and one end of the second mounting part, which is far away from the first mounting part, is provided with a second fixing part; the first clamping part is matched with the second clamping part to fix the connecting structure in a first direction, the second fixing part is fixed on the first fixing part to fix the connecting structure in a second direction, and the first direction is perpendicular to the second direction. The utility model provides an unmanned aerial vehicle, through the cooperation of first block portion and second block portion to and the cooperation of first fixed part and second fixed part, realize installing fast and dismantling.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field especially relates to unmanned aerial vehicle.
Background
The cloud platform quick detach interface on unmanned aerial vehicle is the important structure that realizes that unmanned aerial vehicle changes different cloud platforms, but the cloud platform in-process is changed to current unmanned aerial vehicle, and the installation and the dismantlement are not convenient for.
SUMMERY OF THE UTILITY MODEL
In order to overcome the problem of being not convenient for install and dismantle when unmanned aerial vehicle changes the cloud platform among the prior art, the utility model aims to provide an unmanned aerial vehicle.
In order to achieve the above object, an embodiment of the present invention provides an unmanned aerial vehicle, which includes a body and a connection structure, wherein a mounting groove for mounting the connection structure is formed on the body, and a first engaging portion and a first fixing portion are arranged in the mounting groove; the connecting structure comprises a first mounting part and a second mounting part obliquely extending from one end of the first mounting part, the first mounting part is provided with a second clamping part, and one end of the second mounting part, which is far away from the first mounting part, is provided with a second fixing part; the first clamping part and the second clamping part are matched to fix the connecting structure in a first direction, the second fixing part is fixed to the first fixing part to fix the connecting structure in a second direction, and the first direction is perpendicular to the second direction.
Preferably, the first engaging portion is a first protrusion extending inward from a side wall of the mounting groove, and the second engaging portion is a second protrusion extending outward from a side edge of the first mounting portion.
Preferably, an included angle formed between the first mounting portion and the second mounting portion is an obtuse angle.
Preferably, unmanned aerial vehicle still includes the fastener, be equipped with first mounting hole on the first fixed part, be equipped with the second mounting hole on the second fixed part, the fastener is worn to locate first mounting hole and second mounting hole in order to with the second fixed part is fixed in on the first fixed part.
Preferably, the second fixing part is an elastic clamping piece movably connected with the second mounting part, and the first fixing part is a clamping groove matched with the elastic clamping piece.
Preferably, the unmanned aerial vehicle further comprises a cradle head which is installed on the connecting structure and used for installing the camera device.
Preferably, connection structure is still including being used for the installation the third installation department of cloud platform, the third installation department is located first installation department with the inboard of the contained angle that the second installation department formed, the one end of third installation department install in first installation department is kept away from the one end of second installation department, the other end of third installation department install in the second installation department is kept away from the one end of first installation department.
Preferably, the connecting structure further comprises a first shock absorbing member connected between a third mounting portion and the first mounting portion and a second shock absorbing member connected between the third mounting portion and the second mounting portion.
Preferably, the number of the first shock absorbing members is two, and the number of the second shock absorbing members is two; the third installation department includes installation department body and four connecting pieces, four the connecting piece by the both ends of installation department body to the outside of installation department body extends and forms, and wherein two connecting pieces are respectively through two first damper install in the both sides of first installation department, two other connecting pieces are respectively through two second damper install in the both sides of second installation department.
Preferably, the connecting structure further comprises a third shock absorbing member arranged on one side of the first mounting part, which is away from the third mounting part.
Preferably, a guide groove matched with the first mounting part is arranged in the mounting groove.
Compared with the prior art, the beneficial effects of the utility model reside in that: the installation groove is internally provided with a first clamping part and a first fixing part; set up second block portion on first installation department, set up the second fixed part on the second installation department, first block portion cooperates with second block portion with fixed connection structure in the first direction, and the second fixed part is fixed to first fixed part with fixed connection structure in the second direction on to convenient dismantlement and installation.
Drawings
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle provided in an embodiment of the present invention;
fig. 2 is a schematic structural diagram of an unmanned aerial vehicle at another viewing angle provided by an embodiment of the present invention;
fig. 3 is an assembly diagram of the connection structure and the unmanned aerial vehicle provided by the embodiment of the present invention;
fig. 4 is a schematic view of a fixing manner according to an embodiment of the present invention;
fig. 5 is a schematic view of a fixing manner according to another embodiment of the present invention;
fig. 6 is a schematic view of a connection structure provided in the embodiment of the present invention.
In the figure: 1. a body; 11. mounting grooves; 111. a guide groove; 12. a first engaging portion; 121. a first protrusion; 13. a first fixed part; 131. a card slot; 132. a first mounting hole; 2. a connecting structure; 21. a first mounting portion; 22. a second mounting portion; 221. connecting columns; 23. a second engaging portion; 231. a second protrusion; 24. A second fixed part; 241. an elastic fastener; 242. a second mounting hole; 25. a third mounting portion; 251. an installation position; 252. a mounting portion body; 253. a connecting member; 26. a first damper; 27. a second damping member; 28. a third damper; 3. a holder; 31. an image pickup device.
Detailed Description
In order to facilitate understanding of the present invention, the present invention will be described in more detail with reference to the accompanying drawings and specific embodiments. It will be understood that when an element is referred to as being "secured to" another element, it can 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 intervening elements may be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for descriptive purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
The present invention will be further described with reference to the accompanying drawings and the detailed description, and it should be noted that the embodiments or technical features described below can be arbitrarily combined to form a new embodiment without conflict.
As shown in fig. 1, the embodiment of the utility model provides an unmanned aerial vehicle, including fuselage 1, connection structure 2 and cloud platform 3, connection structure 2 is used for installing cloud platform 3 on fuselage 1, and cloud platform 3 is used for installing camera device 31, and camera device 31 is connected with power supply unit or the control chip electricity on the fuselage 1 to supply power and gather camera device 31's data camera device 31. It will be appreciated that the attachment structure 2 may also attach sensors or other monitoring components to the fuselage 1.
As shown in fig. 2-3, the fuselage 1 includes a nose, a tail and a plurality of wings, a mounting groove 11 for mounting the connecting structure 2 is provided on the nose, first engaging portions 12 are respectively provided on two sides of the mounting groove 11, and a first fixing portion 13 is provided at one end of the mounting groove 11 far from the nose.
The connecting structure 2 includes a first mounting portion 21 and a second mounting portion 22 extending obliquely from one end of the first mounting portion 21, wherein second engaging portions 23 are respectively disposed on two sides of the first mounting portion 21, and a second fixing portion 24 is disposed on one end of the second mounting portion 22 away from the first mounting portion 21. The first engaging portion 12 and the second engaging portion 23 cooperate to fix the connecting structure 2 in the first direction, specifically, the second engaging portion 23 is hung on the inner side/upper side of the first engaging portion 12 to be supported thereby. The second fixing portion 24 is fixed to the first fixing portion 13 to fix the connection structure 2 in a second direction, wherein the first direction is perpendicular to the second direction. In this embodiment, first direction is unmanned aerial vehicle's direction of height, and the second direction is unmanned aerial vehicle's length direction. In the mounting process, one end of the first mounting part 21, which is far away from the second mounting part 22, is aligned with the mounting groove 11, so that the first clamping part 12 and the second clamping part 23 are not overlapped in the second direction; pressing the second mounting portion 22 to make the first mounting portion 21 move toward the bottom of the mounting groove 11 until the second engaging portion 23 and the first engaging portion 12 do not overlap in the first direction, that is, the second engaging portion 23 is completely located inside/above the first engaging portion 12; the second mounting portion 22 is pushed in the second direction to move the first mounting portion 21 in the second direction, so that the second engaging portion 23 and the first engaging portion 12 at least partially overlap in the second direction, and the second engaging portion 23 is hung on the inner side/upper side of the first engaging portion 12, so that the first engaging portion 12 supports and limits the second engaging portion 23 in the first direction. The second fixing portion 24 is fixed to the first fixing portion 13, thereby fixing the connection structure 2 in the second direction. In the detaching process, the second fixing portion 24 is detached from the first fixing portion 13, the second mounting portion 22 is pushed in the opposite direction, the first mounting portion 21 is moved in the machine head direction, so that the first engaging portion 12 and the second engaging portion 23 are not overlapped in the second direction, and the connecting structure 2 can be detached. In the process of replacing the cradle head 3, the connecting structure 2 can be quickly detached from the machine body 1, and after the cradle head 3 is replaced, the connecting structure 2 is installed on the machine body 1, so that quick installation is realized, and the operation is simple.
As shown in fig. 3, in an embodiment, the first engaging portion 12 is a first protrusion 121 extending inward from a sidewall of the mounting groove 11, the second engaging portion 23 is a second protrusion 231 extending outward from a side edge of the first mounting portion 21, and when the first protrusion 121 overlaps the second protrusion 231, the first protrusion 121 supports the second protrusion 231. In other embodiments, the first engaging portion 12 may be a convex pillar, the second engaging portion 23 is provided with a through hole matching with the convex pillar, and the first engaging portion 12 and the second engaging portion 23 are overlapped to form the through hole sleeved on the convex pillar.
As shown in fig. 4, in an embodiment, the second fixing portion 24 is an elastic fastening member 241 movably connected to the second mounting portion 22, wherein the second mounting portion 22 is provided with a connection post 221, a connection hole is formed at a connection end of the elastic fastening member 241 connected to the second mounting portion 22, the connection hole is sleeved on the connection post 221, a V-shaped fastening structure is disposed at a free end of the elastic fastening member 241 far away from the second mounting portion 22, the first fixing portion 13 is a slot 131 matched with the elastic fastening member 241, and the V-shaped fastening structure of the elastic fastening member 241 is fastened in the slot 131 to fix the connection structure 2 in the second direction.
As shown in fig. 5, in another embodiment, the unmanned aerial vehicle further includes a fastening member 4, the first fixing portion 13 is provided with a first mounting hole 132, the second fixing portion 24 is provided with a second mounting hole 242, and the fastening member 4 is inserted into the first mounting hole 132 and the second mounting hole 242 to fix the second fixing portion 24 on the first fixing portion 13.
As shown in fig. 6, the included angle between the first mounting portion 21 and the second mounting portion 22 is preferably an obtuse angle, which facilitates the detachment and installation. The connecting structure 2 further comprises a third mounting part 25 for mounting the holder 3, the third mounting part 25 is arranged at the inner side of an included angle formed by the first mounting part 21 and the second mounting part 22, one end of the third mounting part 25 is mounted at one end of the first mounting part 21 far away from the second mounting part 22, and the other end of the third mounting part 25 is mounted at one end of the second mounting part 22 far away from the first mounting part 21. The third installation part 25 is provided with an installation position 251 for installing the cloud platform 3, and the cloud platform 3 is installed on the third installation part 25, so that the connection structure 2 is prevented from damaging the cloud platform 3 in the installation and disassembly processes.
As shown in fig. 6, the connecting structure 2 further includes a first damper 26 connected between the third mounting portion 25 and the first mounting portion 21 and a second damper 27 connected between the third mounting portion 25 and the second mounting portion 22. Preferably, the number of the first shock-absorbing members 26 is two, and the number of the second shock-absorbing members 27 is two; the third mounting portion 25 includes a mounting portion body 252 and four connecting members 253, the four connecting members 253 are formed by extending two ends of the mounting portion body 252 to the outer side of the mounting portion body 252, wherein two connecting members 253 are respectively mounted on two sides of the first mounting portion 21 through two first shock absorbing members 26, the other two connecting members 253 are respectively mounted on two sides of the second mounting portion 22 through two second shock absorbing members 27, and a shock absorbing effect is achieved between the third mounting portion 25 and the first and second mounting portions 21 and 22, so as to prevent the damage of the horizontal shock to the pan/tilt head 3 during flight. The connection structure 2 further comprises a third shock-absorbing member 28 arranged on a side of the first mounting portion 21 away from the third mounting portion 25, so as to prevent damage to the pan/tilt head 3 caused by vertical vibration during flight.
As shown in fig. 4, be equipped with the guide slot 111 with first installation department 21 looks adaptation on the mounting groove 11, first installation department 21 aims at behind the guide slot 111 can slide to the unmanned aerial vehicle aircraft nose direction, realizes installing fast.
The utility model provides an unmanned aerial vehicle makes first installation department 21 slide in mounting groove 11 through pressing down second installation department 22, forms the mode that first block portion 12 and second block portion 23 overlapped and set up, and first block portion 12 plays the limiting displacement to second block portion 23, and fixed connection structure 2 on the first direction is fixed in second fixed part 24 again on first fixed part 13 to fixed connection structure 2 in the second direction, convenient dismantlement and installation.
The above embodiments are only preferred embodiments of the present invention, and the protection scope of the present invention cannot be limited thereby, and any insubstantial changes and substitutions made by those skilled in the art based on the present invention are all within the protection scope of the present invention.
Claims (11)
1. An unmanned aerial vehicle is characterized by comprising a body and a connecting structure, wherein the body is provided with a mounting groove for mounting the connecting structure, and a first clamping part and a first fixing part are arranged in the mounting groove; the connecting structure comprises a first mounting part and a second mounting part obliquely extending from one end of the first mounting part, the first mounting part is provided with a second clamping part, and one end of the second mounting part, which is far away from the first mounting part, is provided with a second fixing part; the first clamping part and the second clamping part are matched to fix the connecting structure in a first direction, the second fixing part is fixed to the first fixing part to fix the connecting structure in a second direction, and the first direction is perpendicular to the second direction.
2. The unmanned aerial vehicle of claim 1, wherein the first engaging portion is a first protrusion extending inwardly from a side wall of the mounting groove, and the second engaging portion is a second protrusion extending outwardly from a side edge of the first mounting portion.
3. An unmanned aerial vehicle as defined in claim 1, wherein an included angle formed between the first mounting portion and the second mounting portion is an obtuse angle.
4. The unmanned aerial vehicle of claim 1, further comprising a fastener, wherein a first mounting hole is disposed on the first fixing portion, a second mounting hole is disposed on the second fixing portion, and the fastener is disposed through the first mounting hole and the second mounting hole to fix the second fixing portion to the first fixing portion.
5. The unmanned aerial vehicle of claim 1, wherein the second fixing portion is an elastic buckle movably connected with the second mounting portion, and the first fixing portion is a slot matched with the elastic buckle.
6. The drone of claim 1, further comprising a pan-tilt mounted on the connection structure for mounting a camera device.
7. The unmanned aerial vehicle of claim 6, wherein the connection structure further comprises a third installation part for installing the pan/tilt head, the third installation part is arranged at the inner side of an included angle formed by the first installation part and the second installation part, one end of the third installation part is installed at one end of the first installation part far away from the second installation part, and the other end of the third installation part is installed at one end of the second installation part far away from the first installation part.
8. The unmanned aerial vehicle of claim 7, wherein the connection structure further comprises a first shock absorber connected between a third mount and the first mount and a second shock absorber connected between the third mount and the second mount.
9. The drone of claim 8, wherein the first shock absorbing members are two in number and the second shock absorbing members are two in number; the third installation department includes installation department body and four connecting pieces, four the connecting piece by the both ends of installation department body to the outside of installation department body extends and forms, and wherein two connecting pieces are respectively through two first damper install in the both sides of first installation department, two other connecting pieces are respectively through two second damper install in the both sides of second installation department.
10. An unmanned aerial vehicle as defined in claim 7, wherein the connection structure further includes a third shock absorber disposed on a side of the first mounting portion facing away from the third mounting portion.
11. An unmanned aerial vehicle as defined in claim 1, wherein a guide slot adapted to the first mounting portion is provided in the mounting slot.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921006606.0U CN211108034U (en) | 2019-06-28 | 2019-06-28 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921006606.0U CN211108034U (en) | 2019-06-28 | 2019-06-28 | Unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN211108034U true CN211108034U (en) | 2020-07-28 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921006606.0U Active CN211108034U (en) | 2019-06-28 | 2019-06-28 | Unmanned aerial vehicle |
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| CN (1) | CN211108034U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110329525A (en) * | 2019-06-28 | 2019-10-15 | 深圳市道通智能航空技术有限公司 | A kind of unmanned plane and its assemble method |
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2019
- 2019-06-28 CN CN201921006606.0U patent/CN211108034U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110329525A (en) * | 2019-06-28 | 2019-10-15 | 深圳市道通智能航空技术有限公司 | A kind of unmanned plane and its assemble method |
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Address after: 518055 Shenzhen, Guangdong, Nanshan District Xili street, No. 1001, Zhiyuan Road, B1 9. Patentee after: Shenzhen daotong intelligent Aviation Technology Co.,Ltd. Address before: 518055 Shenzhen, Guangdong, Nanshan District Xili street, No. 1001, Zhiyuan Road, B1 9. Patentee before: AUTEL ROBOTICS Co.,Ltd. |