CN206782088U - A kind of unmanned plane article hanging structure - Google Patents
A kind of unmanned plane article hanging structure Download PDFInfo
- Publication number
- CN206782088U CN206782088U CN201720589732.8U CN201720589732U CN206782088U CN 206782088 U CN206782088 U CN 206782088U CN 201720589732 U CN201720589732 U CN 201720589732U CN 206782088 U CN206782088 U CN 206782088U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- snap ring
- connecting rod
- head rod
- grip block
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model discloses a kind of unmanned plane article hanging structure, it is fixedly connected by using head rod with unmanned plane lower body part, it is connected again by second connecting rod one end with head rod ball-joint, the other end of second connecting rod is fixedly connected with clamping device, the article of carry is needed come fixed clamp using clamping device, in addition, by being arranged the first snap ring and the second snap ring on head rod and the second connecting rod, and it is arranged limit spring between the first snap ring and the second snap ring, after unmanned plane goes up to the air, when running into air-flow rocks carry article, the screen resilience of limit spring can cause the shaking amplitude of carry article significantly to reduce, make the overall centre-of gravity shift amplitude of unmanned plane not too large, and influence the normal flight of unmanned plane, substantially increase the safety and reliability during unmanned plane during flying carry.
Description
Technical field
Unmanned plane device field is the utility model is related to, especially a kind of unmanned plane article hanging structure.
Background technology
As the popularization of SUAV and purposes are increasingly extensive, the transport of small article is carried out using unmanned plane also to be become
It is more and more common, but due to unmanned plane lighter weight itself, in conveying articles, most article is all direct carry unmanned plane
Body below transported, cause carry article to rock because unmanned plane is likely to encounter airflow influence in the air, due to hang
The center of gravity that the rocking of loading product can frequently result in unmanned plane body is unbalance, and triggers flight failure.
The content of the invention
In order to solve the deficiencies in the prior art, the purpose of this utility model be to provide one kind can constrain carry article by
Airflow influence shaking amplitude, and the unmanned plane article hanging structure of unmanned plane body center of gravity can be stablized.
In order to realize above-mentioned technical purpose, the technical solution of the utility model：
A kind of unmanned plane article hanging structure, located at unmanned plane lower body part, it includes being fixedly connected with unmanned plane bottom
Bindiny mechanism and the clamping device that is fixedly connected with bindiny mechanism, described bindiny mechanism include head rod, second connect
Extension bar, described head rod one end are fixed on unmanned plane lower body part, the other end of head rod and the second connecting rod
One end connected by ball-joint, the other end of the second connecting rod is fixedly connected with clamping device, and described clamping device includes
Inside is the grip block of hollow structure, an end margin of described grip block side be provided with the first bulge-structure and with it is first raised
Structure is relative and is slidably arranged in the sliding shoe of grip block side, and described sliding shoe is provided with extension with the end face that grip block is affixed
Extension inside to grip block, the corresponding extension top in described grip block inside is provided with the stopper slot that section is U-shaped, described
Stopper slot in be equipped with the sliding bar being fixedly connected with sliding shoe, end horizontal extension of the described sliding bar away from sliding shoe
Limited location block, is arranged with spring between described limited block and stopper slot u-shaped bottom, described spring one end is pressed on limited block
Lower surface, the other end are pressed on the u-shaped bottom of stopper slot.
Further, the described head rod other end is provided with ball head, corresponding first connection in one end of the second connecting rod
Bar ball head structure is provided with the inner fovea part with ball head rotation connection.
Further, described head rod is threadably secured connection unmanned plane lower body part, and described screw thread is thin
Pitch thread.
Further, be screwed connection between the second described connecting rod and grip block, and described screw thread is fine thread.
Further, described head rod outer peripheral face is provided with first annular inner fovea part, is covered on first annular inner fovea part
Provided with the first snap ring, the second described connecting rod outer peripheral face is provided with the second annular inner fovea part, is arranged on the second annular inner fovea part
There is the second snap ring, offset and cover with the first snap ring and the second snap ring respectively provided with both ends between first snap ring and the second snap ring
The limit spring being located on head rod and the second connecting rod.
Preferably, the first described snap ring and the second snap ring are that iron or copper material are integrally formed.
Further, described head rod and the second connecting rod be fiber glass reinforced polypropylene material, carbon fibre materials or
Polytetrafluoroethylene (PTFE) material.
Using above-mentioned technical scheme, the beneficial effects of the utility model are：By using head rod and unmanned plane
Lower body part is fixedly connected, then is connected by second connecting rod one end with head rod ball-joint, the second connecting rod it is another
End is fixedly connected with clamping device, the article of carry is needed come fixed clamp using clamping device, in addition, by head rod
With the first snap ring and the second snap ring are arranged in the second connecting rod, and be arranged limit spring between the first snap ring and the second snap ring,
After unmanned plane goes up to the air, when running into air-flow rocks carry article, the screen resilience of limit spring can cause rocking for carry article
Amplitude significantly reduces, and makes the overall centre-of gravity shift amplitude of unmanned plane not too large, and influences the normal flight of unmanned plane, carries significantly
Safety and reliability during high unmanned plane during flying carry.
Brief description of the drawings
The utility model is further elaborated with reference to the accompanying drawings and detailed description：
Fig. 1 is the simplified diagram of the utility model structure；
Fig. 2 is the front schematic view of the utility model clamping device.
Embodiment
As shown in Fig. 1 to one of 2, the utility model structure is located at the bottom of unmanned plane main body 1, and it includes and unmanned plane bottom
The bindiny mechanism 2 being fixedly connected and the clamping device 3 being fixedly connected with bindiny mechanism 2, described bindiny mechanism 2 include first and connected
Extension bar 21, the second connecting rod 23, described one end of head rod 21 are fixed on the bottom of unmanned plane main body 1, head rod 21
One end of the other end and the second connecting rod 23 be connected 22 by ball-joint, the other end and the clamping device 3 of the second connecting rod 23
It is fixedly connected, described clamping device 3 includes the internal grip block 31 for hollow structure, one end of the described side of grip block 31
Edge is provided with the first bulge-structure 312 and relative with the first bulge-structure 312 and be slidably arranged in the sliding shoe of the side of grip block 3
32, described sliding shoe 32 is provided with the extension extended to inside grip block 3, described clamping with the end face that grip block 3 is affixed
The stopper slot 311 that section is U-shaped is provided with above the corresponding extension in the inside of block 3, is equipped with described stopper slot 311 and sliding shoe
32 sliding bars 33 being fixedly connected, described end horizontal of the sliding bar 33 away from sliding shoe 32 is extended with limited block 331, described
Limited block 331 and stopper slot 311U shapes bottom surface between be arranged with spring 34, described one end of spring 34 is pressed on limited block 331
Lower surface, the other end are pressed on the u-shaped bottom of stopper slot 311, by pulling sliding shoe 32 to make sliding shoe 32 on grip block 3
Chute 35 enter line slip and back-moving spring 34, it would be desirable to the article of carry is clamped in the first bulge-structure 312 and sliding shoe 32
Between, because the tensile force of spring 34 enables article reliably to be clamped.
Further, the described other end of head rod 21 is provided with ball head 22, one end of the second connecting rod 23 corresponding the
The structure of one connecting rod, 21 ball head 22 is provided with the inner fovea part being rotatablely connected with ball head 22.
Further, described head rod 21 is threadably secured the bottom of connection unmanned plane main body 1, and described screw thread is
Fine thread.
Further, be screwed connection between the second described connecting rod 23 and grip block 31, and described screw thread is closely-pitched
Screw thread.
Further, the described outer peripheral face of head rod 21 is provided with first annular inner fovea part, on first annular inner fovea part
The first snap ring 211 is arranged with, the described outer peripheral face of the second connecting rod 23 is provided with the second annular inner fovea part, the second annular inner fovea part
On be arranged with the second snap ring 231, be provided between the snap ring 231 of the first snap ring 211 and second both ends respectively with the first snap ring 211
Offseted with the second snap ring 231 and be set in the limit spring 24 in the connecting rod 23 of head rod 21 and second, it is preferred that be described
The first snap ring 211 and the second snap ring 231 be that iron or copper material are integrally formed.
Further, the described connecting rod 23 of head rod 21 and second is fiber glass reinforced polypropylene material, carbon fiber material
Matter or polytetrafluoroethylene (PTFE) material.
The utility model uses above-mentioned technical scheme, consolidates by using head rod 21 and the bottom of unmanned plane main body 1
Fixed connection, then be connected by the one end of the second connecting rod 23 with the ball-joint of head rod 21, the other end of the second connecting rod 23 is consolidated
Surely clamping device 3 is connected, the article of carry is needed come fixed clamp using clamping device 3, in addition, by head rod 21
With the first snap ring 211 and the second snap ring 231 are arranged in the second connecting rod 23, and between the first snap ring 211 and the second snap ring 231
Limit spring 24 is arranged, after unmanned plane goes up to the air, when running into air-flow rocks carry article, the screen resilience of limit spring 24 can make
The shaking amplitude for obtaining carry article significantly reduces, and makes the overall centre-of gravity shift amplitude of unmanned plane not too large, and influences unmanned plane
Normal flight, substantially increase the safety and reliability during unmanned plane during flying carry.
Specific embodiment of the present utility model is the foregoing described, it will be appreciated by those of skill in the art that this is only
Be for example, those skilled in the art is on the premise of without departing substantially from principle of the present utility model and essence, can be to this reality
The mode of applying makes various changes or modifications, but these changes and modification each fall within the scope of protection of the utility model.
Claims (7)
- A kind of 1. unmanned plane article hanging structure, located at unmanned plane lower body part, it is characterised in that：It includes and unmanned plane bottom The bindiny mechanism being fixedly connected and the clamping device being fixedly connected with bindiny mechanism, described bindiny mechanism include the first connection Bar, the second connecting rod, described head rod one end are fixed on unmanned plane lower body part, the other end of head rod and One end of two connecting rods is connected by ball-joint, and the other end of the second connecting rod is fixedly connected with clamping device, described clamping Mechanism include it is internal be hollow structure grip block, an end margin of described grip block side be provided with the first bulge-structure and with First bulge-structure is relative and is slidably arranged in the sliding shoe of grip block side, the end face that described sliding shoe is affixed with grip block Provided with the extension extended to inside grip block, the limit that section is U-shaped is provided with inside described grip block above corresponding extension Position groove, is equipped with the sliding bar being fixedly connected with sliding shoe, end of the described sliding bar away from sliding shoe in described stopper slot The horizontal-extending limited location block in portion, is arranged with spring between described limited block and stopper slot u-shaped bottom, described spring one end supports Limited block lower surface is pressed in, the other end is pressed on the u-shaped bottom of stopper slot.
- A kind of 2. unmanned plane article hanging structure according to claim 1, it is characterised in that：Described head rod is another One end is provided with ball head, and one end of the second connecting rod corresponds to head rod ball head structure and is provided with and ball head rotation connection Inner fovea part.
- A kind of 3. unmanned plane article hanging structure according to claim 1, it is characterised in that：Described head rod leads to The connection unmanned plane lower body part that is screwed is crossed, described screw thread is fine thread.
- A kind of 4. unmanned plane article hanging structure according to claim 1, it is characterised in that：Described the second connecting rod with Be screwed connection between grip block, and described screw thread is fine thread.
- A kind of 5. unmanned plane article hanging structure according to claim 1, it is characterised in that：Outside described head rod Side face is provided with first annular inner fovea part, and the first snap ring, the second described connecting rod periphery are arranged with first annular inner fovea part Face is provided with the second annular inner fovea part, and the second snap ring, first snap ring and the second snap ring are arranged with the second annular inner fovea part Between offseted respectively with the first snap ring and the second snap ring provided with both ends and be set in the limit on head rod and the second connecting rod Position spring.
- A kind of 6. unmanned plane article hanging structure according to claim 5, it is characterised in that：The first described snap ring and Two snap rings are that iron or copper material are integrally formed.
- A kind of 7. unmanned plane article hanging structure according to claim 1, it is characterised in that：Described head rod and Second connecting rod is fiber glass reinforced polypropylene material, carbon fibre materials or polytetrafluoroethylene (PTFE) material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720589732.8U CN206782088U (en) | 2017-05-24 | 2017-05-24 | A kind of unmanned plane article hanging structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720589732.8U CN206782088U (en) | 2017-05-24 | 2017-05-24 | A kind of unmanned plane article hanging structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206782088U true CN206782088U (en) | 2017-12-22 |
Family
ID=60712881
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720589732.8U Expired - Fee Related CN206782088U (en) | 2017-05-24 | 2017-05-24 | A kind of unmanned plane article hanging structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206782088U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113697109A (en) * | 2021-09-29 | 2021-11-26 | 上海扩博智能技术有限公司 | Unmanned aerial vehicle mounting device and system and operation method of mounting system |
-
2017
- 2017-05-24 CN CN201720589732.8U patent/CN206782088U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113697109A (en) * | 2021-09-29 | 2021-11-26 | 上海扩博智能技术有限公司 | Unmanned aerial vehicle mounting device and system and operation method of mounting system |
| CN113697109B (en) * | 2021-09-29 | 2024-03-26 | 上海扩博智能技术有限公司 | Unmanned aerial vehicle mounting device, unmanned aerial vehicle mounting system and operation method of unmanned aerial vehicle mounting system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171222 Termination date: 20200524 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |