CN216360021U - Cargo hold and unmanned aerial vehicle - Google Patents
Cargo hold and unmanned aerial vehicle Download PDFInfo
- Publication number
- CN216360021U CN216360021U CN202121197411.6U CN202121197411U CN216360021U CN 216360021 U CN216360021 U CN 216360021U CN 202121197411 U CN202121197411 U CN 202121197411U CN 216360021 U CN216360021 U CN 216360021U
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- cabin body
- barrel cover
- unmanned aerial
- cabin
- aerial vehicle
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- 239000000463 material Substances 0.000 claims abstract description 29
- 230000002093 peripheral effect Effects 0.000 claims abstract description 5
- 230000005484 gravity Effects 0.000 description 4
- 230000001788 irregular Effects 0.000 description 4
- 239000000725 suspension Substances 0.000 description 3
- 108010066114 cabin-2 Proteins 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a cargo hold and an unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The cargo compartment includes: the fixing device is fixedly arranged at the end part of the cabin body; the peripheral surface of the cabin body is provided with a plurality of locking holes, a plurality of locking pieces correspond to the locking holes one by one, and the locking pieces can enter the cabin body through the corresponding locking holes; the elastic bushing is detachably arranged in the cabin body; a material port is formed in the end face, away from the fixing device, of the cabin body, and the barrel cover can be transversely arranged at the material port; the fixed end of the driving device is fixedly connected with the side part of the cabin body, and the action end of the driving device is fixedly connected with the barrel cover. The cargo compartment and the unmanned aerial vehicle avoid the position change of articles in the compartment body, the balance of the unmanned aerial vehicle cannot be influenced, and the stable transportation of the unmanned aerial vehicle is ensured.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a cargo hold and an unmanned aerial vehicle.
Background
Unmanned aerial vehicle transportation that sees in the market now is used for transporting below the shoes box packing size mostly, installs the depositing that rectangular support was used for fixed goods on unmanned aerial vehicle generally.
However, in the transportation of fixed shape article, because factors such as wind speed and unmanned aerial vehicle's acceleration can lead to the position of article in the cargo hold to change to the focus has changed, influences unmanned aerial vehicle's balance, can increase the difficulty of unmanned aerial vehicle transportation.
SUMMERY OF THE UTILITY MODEL
The utility model provides a cargo hold and an unmanned aerial vehicle, which solve or partially solve the technical problems that in the prior art, the position of an object in the cargo hold is changed, so that the gravity center is changed, the balance of the unmanned aerial vehicle is influenced, and the transportation difficulty of the unmanned aerial vehicle is increased.
In order to solve the above technical problems, the present invention provides a cargo tank including: the device comprises a fixing device, a cabin body, a barrel cover, an elastic bushing, a driving device and a plurality of locking pieces; the fixing device is fixedly arranged at the end part of the cabin body; the peripheral surface of the cabin body is provided with a plurality of locking holes, a plurality of locking pieces correspond to the locking holes one by one, and the locking pieces can enter the cabin body through the corresponding locking holes; the elastic bushing is detachably arranged in the cabin body; a material port is formed in the end face, away from the fixing device, of the cabin body, and the barrel cover can be transversely arranged at the material port; the fixed end of the driving device is fixedly connected with the side part of the cabin body, and the action end of the driving device is fixedly connected with the barrel cover.
Further, the fixing device includes: a fixing frame and a fixing plate; the fixing frame is fixedly arranged on the cabin body, and a groove is formed in the fixing frame; the fixed plate is detachably connected with the fixed frame, and the fixed plate can be arranged at the groove.
Furthermore, the fixed frame is provided with a guide rail; the fixing plate is slidably disposed in the guide rail.
Further, the driving device includes: steering engines and steering wheels; the fixed end of the steering engine is fixedly connected with the side part of the cabin body, and the action end of the steering engine is fixedly connected with the steering wheel; the rudder disc is fixedly connected with the barrel cover.
Further, the action end of the steering engine is parallel to the axis of the cabin body.
Further, the driving device further includes: a rudder engine room; the rudder cabin is fixedly arranged on the side part of the cabin body; and the fixed end of the steering engine is fixedly arranged in the rudder engine cabin.
Further, the barrel cover is perpendicular to the axis of the cabin body.
Further, the size of the barrel cover is larger than or equal to that of the material opening.
Further, the cross section of the elastic bushing is in a frustum shape; the size of the end part, facing the barrel cover, of the elastic bushing is larger than the size of the end part, facing away from the barrel cover, of the elastic bushing.
Based on the same inventive concept, the application also provides an unmanned aerial vehicle which comprises the cargo hold.
One or more technical solutions provided in the embodiments of the present application have at least the following technical effects or advantages:
because the fixing device is fixedly arranged at the end part of the cabin body, the cabin body is fixed on the wings of the unmanned aerial vehicle through the fixing device, the suspension position of the cabin body on the unmanned aerial vehicle is ensured to be fixed, and the position movement can not occur, because the peripheral surface of the cabin body is provided with a plurality of locking holes, a plurality of locking parts correspond to a plurality of locking holes one by one, and the locking parts can enter the cabin body through the corresponding locking holes, so when the regular-shaped goods are conveyed, the locking parts pass through the locking holes to enter the cabin body and support against the regular-shaped goods, the position change of the goods in the cabin body is avoided, the balance of the unmanned aerial vehicle can not be influenced, the transportation stability of the unmanned aerial vehicle is ensured, because the elastic bush is detachably arranged in the cabin body, when the irregular-shaped goods are conveyed, the shape of the inner cavity of the elastic bush is matched with the shape of the irregular-shaped goods, and the size of the inner cavity of the elastic bush is matched with the size of the irregular-shaped goods, put into elastic bush's inner chamber with irregular shape's goods, extrude irregular shape's goods through elastic bush, avoid article position in the cabin body to change, can not influence unmanned aerial vehicle's balance, guarantee that unmanned aerial vehicle transportation is steady, because the cabin body has seted up the material mouth on deviating from fixing device's the terminal surface, the bung can set up in material mouth department with the sideslip formula, drive arrangement's stiff end and the lateral part fixed connection of the cabin body, drive arrangement's action end and bung fixed connection, so, when wanting to place goods, drive arrangement drives the bung action, open the material mouth, put into the cabin with goods internal, when goods enter into the cabin, drive arrangement drives the bung action, close the material mouth, when unmanned aerial vehicle reachs the assigned position, drive arrangement drives the bung action, open the material mouth, goods fall the assigned position under the effect of gravity.
Drawings
FIG. 1 is a schematic structural view of a cargo compartment provided by an embodiment of the present invention;
FIG. 2 is a schematic view of the structure of a fixture for the cargo tank of FIG. 1;
FIG. 3 is a schematic structural view of a fixing frame of the fixing device in FIG. 2;
FIG. 4 is a schematic structural view of a fixing plate of the fixing device in FIG. 2;
FIG. 5 is an assembled view of a drive assembly of the cargo space of FIG. 1;
FIG. 6 is a schematic view of the structure of the cargo compartment of FIG. 1;
FIG. 7 is a front view of a resilient liner of the cargo tank of FIG. 1;
fig. 8 is a top view of the elastomeric bushing of fig. 7.
Detailed Description
Referring to fig. 1, an embodiment of the present invention provides a cargo tank including: fixing device 1, cabin body 2, bung 3, elastic bush 4, drive arrangement 5 and a plurality of retaining member.
The fixing device 1 is fixedly arranged at the end part of the cabin body 2.
A plurality of locking holes are formed in the circumferential surface of the cabin body 2, a plurality of locking pieces correspond to the locking holes one to one, and the locking pieces can penetrate through the corresponding locking holes to enter the cabin body 2.
The elastic bushing 4 is detachably arranged inside the cabin 2.
The end face of the cabin body 2 departing from the fixing device is provided with a material port, and the barrel cover 3 can be arranged at the material port in a transverse moving mode.
The fixed end of the driving device 5 is fixedly connected with the side part of the cabin body 2, and the action end of the driving device 5 is fixedly connected with the barrel cover 3.
In the embodiment of the application, the fixing device 1 is fixedly arranged at the end part of the cabin body 2, so the cabin body 2 is fixed on the wing of the unmanned aerial vehicle through the fixing device 1, the suspension position of the cabin body 2 on the unmanned aerial vehicle is ensured to be fixed, the position movement can not occur, as the plurality of locking holes are arranged on the peripheral surface of the cabin body 2, the plurality of locking parts and the plurality of locking holes are in one-to-one correspondence, and the locking parts can enter the cabin body 2 through the corresponding locking holes, so when the goods in the regular shape are conveyed, the locking parts penetrate through the locking holes to enter the cabin body 2 and support the goods in the regular shape, the position change of the goods in the cabin body 2 is avoided, the balance of the unmanned aerial vehicle can not be influenced, the transportation stability of the unmanned aerial vehicle is ensured, as the elastic bushing 4 is detachably arranged in the cabin body 2, when the goods in the irregular shape are conveyed, the shape of the inner cavity of the elastic bushing 4 is matched with the shape of the goods in the irregular shape, the size of the inner cavity of the elastic bush 4 is matched with the size of the irregularly-shaped goods, the irregularly-shaped goods are placed into the inner cavity of the elastic bush 4, the irregularly-shaped goods are extruded by the elastic bush 4, the position of the goods in the cabin body 2 is prevented from changing, the balance of the unmanned aerial vehicle is not influenced, the stable transportation of the unmanned aerial vehicle is ensured, because the end surface of the cabin body 2, which is far away from the fixing device, is provided with a material port, the bucket cover 3 can be transversely arranged at the material port, the fixed end of the driving device 5 is fixedly connected with the side part of the cabin body 2, and the action end of the driving device 5 is fixedly connected with the bucket cover 3, when the goods are placed, the driving device 5 drives the bucket cover 3 to act, the material port is opened, the goods are placed into the cabin body 2, when the goods enter the cabin body 2, the driving device 5 drives the bucket cover 3 to act, the material port is closed, when the unmanned aerial vehicle reaches a designated position, the driving device 5 drives the barrel cover 3 to act, the material opening is opened, and goods fall to a specified position under the action of gravity.
Specifically, referring to fig. 2-5, the fixation device 1 comprises: a fixing frame 1-1 and a fixing plate 1-2.
The fixed mount 1-1 is fixedly arranged on the cabin body 2, and the fixed mount 1-1 is provided with a groove. In this embodiment, the shape of recess and the shape phase-match of unmanned aerial vehicle's wing, the size phase-match of the size of recess and unmanned aerial vehicle's wing.
The fixing plate 1-2 is detachably connected with the fixing frame 1-1, and the fixing plate 1-2 can be arranged at the groove.
The fixed frame 1-1 is provided with a guide rail.
The fixing plate 1-2 is slidably disposed in the guide rail.
The wings of the unmanned aerial vehicle are embedded into the grooves, the fixing plates 1-2 are placed into the guide rails, the two sides of the fixing plates 1-2 are limited through the guide rails, then the fixing plates 1-2 slide in the guide rails until the fixing plates 1-2 shield the grooves, the two ends of the fixing plates 1-2 are connected with the fixing pieces 1-1 through bolts, the limitation of the two ends of the fixing plates 1-2 is achieved, the suspension position of the cabin body 2 on the unmanned aerial vehicle is guaranteed to be fixed, and position movement cannot occur.
Referring to fig. 6, the cabin 2 is provided with a plurality of through holes for reducing weight.
Referring to fig. 5, the driving device 5 includes: steering wheel 5-1 and steering wheel.
The fixed end of the steering engine 5-1 is fixedly connected with the side part of the cabin body 2, and the action end of the steering engine 5-1 is fixedly connected with the steering wheel.
The rudder disc is fixedly connected with the barrel cover 3.
The action end of the steering engine 5-1 is parallel to the axis of the cabin body 2, so that the steering engine 5-1 can drive the barrel cover 3 to act through the steering wheel, and the material opening and closing are realized.
The drive device 5 further includes: a rudder cabin 5-2.
The rudder engine room 5-2 is fixedly arranged on the side part of the cabin body 2, the fixed end of the steering engine 5-1 is fixedly arranged in the rudder engine room 5-2, and the steering engine 5-1 is supported by the rudder engine room 5-2.
When goods are to be placed, the steering engine 5-1 drives the barrel cover 3 to act through the steering wheel disc, the material opening is opened, the goods are placed into the cabin body 2, when the goods enter the cabin body 2, the steering engine 5-1 drives the barrel cover 3 to act through the steering wheel disc 5, the material opening is closed, when the unmanned aerial vehicle reaches a specified position, the steering engine 5-1 drives the barrel cover 3 to act through the steering wheel disc, the material opening is opened, and the goods fall to the specified position under the action of gravity.
Specifically, the barrel cover 3 is perpendicular to the axis of the cabin body 2, so that the steering engine 5-1 can drive the barrel cover 3 to act through the steering wheel, and the material opening and closing of the material opening are realized.
Specifically, the size of the barrel cover 3 is larger than or equal to that of the material opening, so that the material opening can be completely shielded, and articles are prevented from falling off.
Wherein, fixedly on the bung 3 towards fixing device 1's the terminal surface be provided with the bolster, cushion article through the bolster, avoid article damage. In this embodiment, the buffer may be a rubber pad.
Specifically, referring to fig. 7 to 8, the sectional shape of the elastic bush 4 is a frustum shape. The size of the end part of the elastic bushing 4 facing the barrel cover 3 is larger than the size of the end part of the elastic bushing 4 deviating from the barrel cover 3, when the elastic bushing 4 enters the cabin body 2, the elastic bushing 4 is unfolded towards the end part of the barrel cover 3 through the elastic bushing 4, and the elastic bushing 4 is prevented from falling from the cabin body 2.
In the present embodiment, the material of the elastic bush 4 may be rubber.
The utility model further provides an unmanned aerial vehicle, the unmanned aerial vehicle adopts the cargo hold, the specific structure of the cargo hold refers to the above embodiments, and the cargo hold adopts all the technical schemes of all the above embodiments, so that the unmanned aerial vehicle at least has all the beneficial effects brought by the technical schemes of the above embodiments, and the details are not repeated.
Finally, it should be noted that the above embodiments are only for illustrating the technical solutions of the present invention and not for limiting, and although the present invention has been described in detail with reference to examples, it should be understood by those skilled in the art that modifications or equivalent substitutions may be made on the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention, which should be covered by the claims of the present invention.
Claims (10)
1. A cargo tank, comprising: the device comprises a fixing device, a cabin body, a barrel cover, an elastic bushing, a driving device and a plurality of locking pieces;
the fixing device is fixedly arranged at the end part of the cabin body;
the peripheral surface of the cabin body is provided with a plurality of locking holes, a plurality of locking pieces correspond to the locking holes one by one, and the locking pieces can enter the cabin body through the corresponding locking holes;
the elastic bushing is detachably arranged in the cabin body;
a material port is formed in the end face, away from the fixing device, of the cabin body, and the barrel cover can be transversely arranged at the material port;
the fixed end of the driving device is fixedly connected with the side part of the cabin body, and the action end of the driving device is fixedly connected with the barrel cover.
2. A cargo tank according to claim 1, wherein the securing means comprises: a fixing frame and a fixing plate;
the fixing frame is fixedly arranged on the cabin body, and a groove is formed in the fixing frame;
the fixed plate is detachably connected with the fixed frame, and the fixed plate can be arranged at the groove.
3. A cargo tank according to claim 2, wherein:
the fixed frame is provided with a guide rail;
the fixing plate is slidably disposed in the guide rail.
4. A cargo tank according to claim 1, wherein the drive means comprises: steering engines and steering wheels;
the fixed end of the steering engine is fixedly connected with the side part of the cabin body, and the action end of the steering engine is fixedly connected with the steering wheel;
the rudder disc is fixedly connected with the barrel cover.
5. A cargo tank according to claim 4, wherein:
the action end of the steering engine is parallel to the axis of the cabin body.
6. The cargo tank of claim 4 wherein the drive means further comprises: a rudder engine room;
the rudder cabin is fixedly arranged on the side part of the cabin body;
and the fixed end of the steering engine is fixedly arranged in the rudder engine cabin.
7. A cargo tank according to claim 1, wherein:
the barrel cover is perpendicular to the axis of the cabin body.
8. The cabin of claim 1, wherein:
the size of the barrel cover is larger than or equal to that of the material opening.
9. The cabin of claim 1, wherein:
the section of the elastic bushing is frustum-shaped;
the size of the end part, facing the barrel cover, of the elastic bushing is larger than the size of the end part, facing away from the barrel cover, of the elastic bushing.
10. An unmanned aerial vehicle comprising a cargo hold according to any one of claims 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121197411.6U CN216360021U (en) | 2021-05-31 | 2021-05-31 | Cargo hold and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121197411.6U CN216360021U (en) | 2021-05-31 | 2021-05-31 | Cargo hold and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216360021U true CN216360021U (en) | 2022-04-22 |
Family
ID=81189481
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121197411.6U Expired - Fee Related CN216360021U (en) | 2021-05-31 | 2021-05-31 | Cargo hold and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216360021U (en) |
-
2021
- 2021-05-31 CN CN202121197411.6U patent/CN216360021U/en not_active Expired - Fee Related
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220422 |