CN208344527U - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
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- CN208344527U CN208344527U CN201820460877.2U CN201820460877U CN208344527U CN 208344527 U CN208344527 U CN 208344527U CN 201820460877 U CN201820460877 U CN 201820460877U CN 208344527 U CN208344527 U CN 208344527U
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- container
- fuselage
- lock tongue
- unmanned plane
- cargo hold
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Abstract
The utility model discloses a kind of unmanned planes, including fuselage and container, the cargo hold that can accommodate the container is equipped in the fuselage, the tank top is equipped with container entrance, lockable mechanism is equipped in the fuselage and lockable mechanism part is protruded into cargo hold, lock corresponding with the lockable mechanism is provided on the container lateral wall, so that container protrudes into lockable mechanism and lock in cargo hold and locks.The utility model has the beneficial effects that unmanned plane described in the utility model; by the way that cargo hold is arranged; container can be made to obtain the protection in multiple directions; on the other hand; by the way that lockable mechanism is arranged on fuselage and lock is arranged on container; it can guarantee that container is relatively stable in cargo hold, be reduced as far as jolting and shaking for container in flight course.
Description
Technical field
The utility model relates to unmanned plane logistics technology, it particularly relates to a kind of unmanned plane.
Background technique
With the development of unmanned air vehicle technique, the application prospect on logistics transportation is also expected.In the prior art, nothing
Man-machine loading is usually the mode transported after tying up cargo on unmanned plane, or by cargo hoisting in unmanned plane
The mode that lower section is transported lacks the protection to transport article during unmanned plane during flying.For example, Publication No.
The patent application of CN106828937A discloses a kind of hooking type loading unmanned plane, is hung by the suspension hook of lower section to cargo
It takes, after hanging cargo, drives rack bar reversion to move up suspension hook by driving motor, realize lifting cargo flight.Existing nothing
Man-machine not have to provide special accommodation space for cargo, cargo is largely exposed to outside in transport, can not cope with severe
Environment and weather, also, not stable enough using the fixed cargo of the mode of suspension hook or binding, cargo be easy because jolt and shake by
Damage.
For the problems in the relevant technologies, currently no effective solution has been proposed.
Utility model content
For above-mentioned technical problem in the related technology, the utility model proposes a kind of unmanned planes, can protect cargo not
It is influenced by unmanned plane external environment, guarantees cargo smooth transport under state of flight.
To realize the above-mentioned technical purpose, the technical solution of the utility model is achieved in that
A kind of unmanned plane, including fuselage and container, the fuselage is interior to be equipped with the cargo hold that can accommodate the container, the goods
Bilge portion is equipped with container entrance, is equipped with lockable mechanism in the fuselage and lockable mechanism part is protruded into cargo hold, outside the container
Lock corresponding with the lockable mechanism is provided on side wall, so that container protrudes into lockable mechanism and lock in cargo hold and locks.
Preferably, the container inlet is equipped with the cargo hold inner wall to the unmanned plane internal stretch.
Preferably, it is connected between the cargo hold inner wall and the container entrance by chamfering structure.
Preferably, under loading state, the gap between the cargo hold inner wall and container side wall becomes smaller gradually from bottom to up.
Preferably, the bottom of the container, which is equipped with to match with the chamfering structure, makes the container that can not continue up shifting
Dynamic position limiting structure.
Preferably, the lockable mechanism includes lock tongue and driving device, and the lock includes recessed portion, the driving device
The lock tongue can be driven to protrude into or leave the recessed portion.
Preferably, the lock includes lock tongue pushing part, the process that the lock tongue pushing part is moved up in the container
The middle press lock tongue, after the lock tongue pushing part is by the lock tongue, the lock tongue automatically extends into the recessed portion.
Preferably, the recessed portion includes the first groove and the second groove setting up and down, the lock tongue pushing part setting
Between the first groove and the second groove, and the first groove and the second groove have the straight upper wall for limiting the lock tongue
Face.
Preferably, the fuselage includes fuselage girder, the upper covering of the covering fuselage roof and the covering fuselage bottom
The lower covering in portion, the container entrance are provided on the lower covering.
Preferably, under loading state, the bottom of the fuselage and the container bottom constitute smooth curved surface.
The utility model has the beneficial effects that unmanned plane described in the utility model can be such that container obtains by the way that cargo hold is arranged
Protection on to multiple directions, on the other hand, by the way that lockable mechanism is arranged on fuselage and lock, Neng Goubao are arranged on container
It demonstrate,proves that container is relatively stable in cargo hold, is reduced as far as jolting and shaking for container in flight course.
Unmanned plane described in the utility model can better ensure that container in transportational process by the way that cargo hold inner wall is arranged
In stability, also, container mounting during, cargo hold inner wall can play guiding function.
Unmanned plane described in the utility model can guide container to be rapidly articulated to cargo hold by the way that chamfering structure is arranged
It is interior.
Unmanned plane described in the utility model can be realized automatic locking during loading container, keep unmanned plane fast
Speed enters loading state, decontrols container using electric drive lockable mechanism during unloading load-carrying box, completes automatic unloading, dress
The process for carrying and unloading load-carrying box avoids manual operation completely, realizes efficient operation.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Needed in attached drawing be briefly described, it should be apparent that, the accompanying drawings in the following description is only the utility model
Some embodiments for those of ordinary skill in the art without creative efforts, can also be according to this
A little attached drawings obtain other attached drawings.
Fig. 1 is structural schematic diagram of the unmanned plane described in the utility model embodiment under loading state；
Fig. 2 is the structural schematic diagram of fuselage；
Fig. 3 is main view of the unmanned plane described in the utility model embodiment under loading state；
Fig. 4 is the main view under fuselage and container discrete state；
Fig. 5 is that container passes through the state before lockable mechanism；
Fig. 6 is container by the state of lockable mechanism；
Fig. 7 is that container passes through the state after lockable mechanism；
Fig. 8 is the cross-sectional view of container；
Fig. 9 is the enlarged drawing of circle B in Fig. 3；
Figure 10 is the enlarged drawing of circle A in Fig. 2；
Figure 11 is the side view of lockable mechanism；
Figure 12 is the top view of unmanned plane first half.
In figure: 1. unmanned planes；10. fuselage；20. container；30. lockable mechanism；40. lock；
11. cargo hold inner wall；12. chamfering structure；13. gap；14. fuselage girder；Covering on 15.；16. lower covering；
21. position limiting structure；22. recessed portion；23. lock tongue pushing part；
221. first grooves；222. second grooves；223. first upper wall surfaces；224. second upper wall surfaces；
31. lock tongue.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art's every other embodiment obtained, all belongs to
In the range of the utility model protection.
As shown in Figure 1, being a kind of structural representation of the unmanned plane 1 described in the utility model embodiment under loading state
Figure, unmanned plane 1 include fuselage 10 and container 20, are equipped with the cargo hold that can accommodate container 20 in fuselage 10,10 bottom of fuselage is equipped with
Container entrance is equipped with lockable mechanism 30 in fuselage 10 and lockable mechanism 30 partially protrudes into cargo hold, is arranged on 20 lateral wall of container
There is lock 40 corresponding with lockable mechanism 30, so that container 20 protrudes into lockable mechanism 30 and lock 40 in cargo hold and locks.
After container 20 enters cargo hold from container entrance, lockable mechanism 30 is fixed by container 20 and locking with lock 40
Firmly, the top and side of container 20 are all protected by fuselage, to mitigate the external environment such as rainwater and wind to container 20
Influence, lockable mechanism 30 makes container 20 and fuselage 10 keeps relatively-stationary state in flight course, and reduction is jolted and shaken
It is dynamic.
Preferably, as shown in figure 12, lockable mechanism 30 there are two setting in fuselage 10, respectively consolidates the two sides of container 20
It is fixed.
Specifically, as shown in Fig. 2, fuselage 10 includes fuselage girder 14, the upper covering 15 at 10 top of covering fuselage and covering
The lower covering 16 of 10 bottom of fuselage, container entrance are provided on lower covering 16, and lockable mechanism 30 is mounted on fuselage girder 14, from
The side of container 20 carries out locking to container 20.
As the further improvement of the utility model embodiment, as shown in Fig. 2, container inlet is equipped with to the inside of fuselage 10
The cargo hold inner wall 11 of extension.During container 20 is moved upwardly into cargo hold, cargo hold inner wall 11 is that container 20 provides guiding
Effect, after container 20 enters cargo hold, container 20 is auxiliarily fixed in cargo hold inner wall 11, is further ensured that flight course container 20 and machine
Relatively-stationary state between body 10.
As the further improvement of the utility model embodiment, as shown in Fig. 3,9, between cargo hold inner wall 11 and container entrance
It is connected by chamfering structure 12.When container 20 moves up, even if container 20 without being directed at container entrance, container 20 completely
Cargo hold can be promptly slid by contacting with chamfering structure 12, realize the quick mounting of container 20.
As the further improvement of the utility model embodiment, as shown in figure 9, under loading state, cargo hold inner wall 11 with
Gap 13 between 20 side wall of container becomes smaller gradually from bottom to up.This structure can further make container 20 more easily right
Quasi- container entrance helps the quick mounting for realizing container 20.Specifically, cargo hold inner wall 11 and vertical direction have certain folder
Angle, the angle slowly reduce from bottom to up, and 11 bottom end of cargo hold inner wall and vertical direction angle are 15 °, 11 top of cargo hold inner wall with
Vertical direction angle is 7 °.The side wall of container 20 and vertical direction also have certain angle, the side wall top of container 20 with it is vertical
Angular separation is 0 °, and the side wall bottom end of container 20 and vertical direction angle are 6.8 °, in this way, under loading state, cargo hold inner wall
It just will form the gap 13 to become smaller gradually from bottom to up between 11 and 20 side wall of container.Container 20 more moves upwards, scope of activities
More become smaller, state is more stable.
As the further improvement of the utility model embodiment, as shown in figure 9, the bottom of container 20 is equipped with and chamfering structure
12 match, the position limiting structure 21 that continue to move up container 20 can not.When container 20 is moved up to a certain extent, limit
Bit architecture 21 is stuck on chamfering structure 12, in case container 20 excessively gos deep into cargo hold.
As shown in Figure 10,11, lockable mechanism 30 includes lock tongue 31 and driving device (not shown), as shown in figure 4, lock 40
Including recessed portion 22, driving device can drive lock tongue 31 to protrude into or leave the recessed portion 22.As shown in figure 3, in loading shape
Under state, lock tongue 31 protrudes into recessed portion 22, fixes container 20.
As shown in figure 4, lock 40 further includes lock tongue pushing part 23, the process that lock tongue pushing part 23 is moved up in container 20
Middle press lock tongue 31, after lock tongue pushing part 23 is by lock tongue 31, lock tongue 31 automatically extends into recessed portion 22.Fig. 5~7 are shown respectively
Lock tongue pushing part 23 passes through the state before, during and after lock tongue 31.Lock tongue pushing part 23 has acclivitous face, lock tongue 31
Head has the face that tilts down, during container 20 moves up, acclivitous face can press and push to
Under inclined face, so that lock tongue 31 is moved horizontally unlock.As shown in figure 5, lock tongue 31 is in the top of container 20, as shown in fig. 6, container
20 during moving up lock tongue pushing part 23 press lock tongue 31, lock tongue 31 to moving on the outside of container 20, as shown in fig. 7,
After lock tongue pushing part 23 passes through lock tongue 31, lock tongue 31 is automatically stretched in recessed portion 22.Specific set-up mode can be,
For example, spring (not shown) is arranged between the tail portion and lockable mechanism shell 32 of lock tongue 31, which makes lock tongue 31 in spring
With the trend mobile to container 20 when being compressed, during lock tongue pushing part 23 passes through lock tongue 31, spring is compressed, lock tongue
After pushing part 23 passes through lock tongue 31, the power for squeezing spring disappears, and spring pushes 31 return of lock tongue to be locked in recessed portion 22, completes certainly
Dynamic locking process.
As shown in figure 8, recessed portion 22 includes the first groove 221 and the second groove 222 setting up and down, lock tongue pushing part 23
It is arranged between the first groove 221 and the second groove 222, and the first groove 221 and the second groove 22 are respectively provided with for limiting
Straight the first upper wall surface 223 and the second upper wall surface 224 of lock tongue 31.Lock tongue 31 can be locked on the first groove 221, can also
To be locked on the second groove 222.When lock tongue 31 is locked on the first groove 221, container 20 is partially protruded into cargo hold, works as lock
When tongue 31 is locked on the second groove 222, container 20 is fully inserted into cargo hold.
As the further improvement of the utility model embodiment, as shown in figure 3, under loading state, the bottom of fuselage 10
Smooth curved surface is constituted with 20 bottom of container.Specifically, the bottom of the lower covering 16 Yu container 20 of 10 bottom of fuselage constitutes smooth
Curved surface, smooth curved surface can reduce the resistance of air under state of flight, guarantee that unmanned plane is whole during transportation
Stability.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Within the spirit and principle of utility model, any modification, equivalent replacement, improvement and so on should be included in the utility model
Protection scope within.
Claims (10)
1. a kind of unmanned plane, which is characterized in that including fuselage and container, the goods that can accommodate the container is equipped in the fuselage
Cabin, the tank top are equipped with container entrance, are equipped with lockable mechanism in the fuselage and lockable mechanism part is protruded into cargo hold, institute
It states and is provided with lock corresponding with the lockable mechanism on container lateral wall, so that container protrudes into lockable mechanism and lock in cargo hold
Locking.
2. unmanned plane according to claim 1, which is characterized in that the container inlet is equipped with prolongs to the fuselage interior
The cargo hold inner wall stretched.
3. unmanned plane according to claim 2, which is characterized in that pass through between the cargo hold inner wall and the container entrance
Chamfering structure connection.
4. unmanned plane according to claim 3, which is characterized in that under loading state, the cargo hold inner wall and container side
Gap between wall becomes smaller gradually from bottom to up.
5. unmanned plane according to claim 4, which is characterized in that the bottom of the container is equipped with and the chamfering structure phase
Cooperate the position limiting structure that continue to move up the container can not.
6. unmanned plane according to claim 1, which is characterized in that the lockable mechanism includes lock tongue and driving device, institute
Stating lock includes recessed portion, and the driving device can drive the lock tongue to protrude into or leave the recessed portion.
7. unmanned plane according to claim 6, which is characterized in that the lock includes lock tongue pushing part, and the lock tongue pushes away
Dynamic portion presses the lock tongue during container moves up, after the lock tongue pushing part is by the lock tongue, institute
It states lock tongue and automatically extends into the recessed portion.
8. unmanned plane according to claim 7, which is characterized in that the recessed portion include the first groove setting up and down and
Second groove, the lock tongue pushing part is arranged between the first groove and the second groove, and the first groove and the second groove have
For limiting the straight upper wall surface of the lock tongue.
9. unmanned plane according to claim 1, which is characterized in that the fuselage includes fuselage girder, the covering fuselage
The upper covering at top and the lower covering of the covering fuselage bottom, the container entrance are provided on the lower covering.
10. unmanned plane according to claim 1, which is characterized in that under loading state, the bottom of the fuselage with it is described
Container bottom constitutes smooth curved surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820460877.2U CN208344527U (en) | 2018-04-03 | 2018-04-03 | Unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820460877.2U CN208344527U (en) | 2018-04-03 | 2018-04-03 | Unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208344527U true CN208344527U (en) | 2019-01-08 |
Family
ID=64885935
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820460877.2U Active CN208344527U (en) | 2018-04-03 | 2018-04-03 | Unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208344527U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109878725A (en) * | 2019-03-31 | 2019-06-14 | 拓攻（南京）机器人有限公司 | A kind of fixed-wing logistics unmanned plane |
| CN114212235A (en) * | 2021-12-30 | 2022-03-22 | 西安京东天鸿科技有限公司 | Aircraft, cargo carrying system, aircraft dismounting method and aircraft mounting method |
-
2018
- 2018-04-03 CN CN201820460877.2U patent/CN208344527U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109878725A (en) * | 2019-03-31 | 2019-06-14 | 拓攻（南京）机器人有限公司 | A kind of fixed-wing logistics unmanned plane |
| CN114212235A (en) * | 2021-12-30 | 2022-03-22 | 西安京东天鸿科技有限公司 | Aircraft, cargo carrying system, aircraft dismounting method and aircraft mounting method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210716 Address after: 518000 5th floor, block B, building 1, software industry base, Yuehai street, Nanshan District, Shenzhen City, Guangdong Province Patentee after: Fengyi Technology (Shenzhen) Co.,Ltd. Address before: 518000 Xuefu Road (south) and Baishi Road (east) intersection of Nanshan District, Shenzhen City, Guangdong Province, 6-13 floors, Block B, Shenzhen Software Industry Base Patentee before: SF TECHNOLOGY Co.,Ltd. |