CN205971861U - Unmanned aerial vehicle cargo hold - Google Patents
Unmanned aerial vehicle cargo hold Download PDFInfo
- Publication number
- CN205971861U CN205971861U CN201620801260.3U CN201620801260U CN205971861U CN 205971861 U CN205971861 U CN 205971861U CN 201620801260 U CN201620801260 U CN 201620801260U CN 205971861 U CN205971861 U CN 205971861U
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- Prior art keywords
- cargo hold
- connecting plate
- unmanned plane
- latch
- locking
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Abstract
The application discloses unmanned aerial vehicle cargo hold, unmanned aerial vehicle cargo hold includes: a set of first connecting plate that is parallel to each other and a set of second connecting plate that is parallel to each other, the bottom of a set of first connecting plate and a set of second connecting plate is sealed by the bottom plate, and adjacent first connecting plate and second connecting plate pass through the stand connection in the corner, at least one first connecting plate is equipped with removal locking piece in the turning position that is close to a department, and the top of removing the locking piece is equipped with fixed locking piece, and fixed locking piece can set up on the slide rail of unmanned aerial vehicle body, and unmanned aerial vehicle cargo hold can follow slide rail horizontal migration and pass through to remove locking piece and fixed locking piece locking. The utility model provides an unmanned aerial vehicle cargo hold can fast loading and unloading and auto -lock.
Description
Technical field
The disclosure relates generally to logistics transportation and in particular to using the logistics transportation field of unmanned plane, more particularly, to unmanned
Machine cargo hold.
Background technology
At present, logistics unmanned plane cargo hold mostly is easy cargo component, and directly adopts mode connects for screw to unmanned plane,
Or bundle to unmanned plane.The handling of this cargo hold are cumbersome, and can not realize quick despatch and the self-locking of cargo hold.
Utility model content
In view of drawbacks described above of the prior art or not enough it is desirable to provide a kind of unmanned plane being capable of quick despatch and self-locking
Cargo hold.
A kind of first aspect according to the disclosure, there is provided unmanned plane cargo hold, described unmanned plane cargo hold includes：One group mutual
The first parallel connecting plate and one group of second connecting plate being parallel to each other, the first connecting plate described in a group and the second company described in a group
The bottom of fishplate bar is closed by base plate, and adjacent described first connecting plate and described second connecting plate are around the corner by column even
Connect；At least one described first connecting plate is provided with mobile latch in the corner location near, described mobile latch
Top is provided with fixing latch, and described fixing latch may be provided on the slide rail of unmanned plane body, and described unmanned plane cargo hold can
Move horizontally and pass through described mobile latch and described fixing latch locking along described slide rail.
Preferably, described column is rectangular in shape, and the both sides of described column connect corresponding first connecting plate and second respectively
Connecting plate, the bottom of described column is provided with heel brace block, and described heel brace block is supported between the both sides of described column.
Preferably, described heel brace block bottom is provided with roller.
A kind of second aspect according to the disclosure, there is provided self-locking mechanism, described self-locking mechanism include fixing latch and
Mobile latch, described mobile latch is provided with the first inclined plane, and the upper horizontal of described first inclined plane extends formation the
One horizontal plane, described first level face is provided with locking hole；Described fixing latch is provided with can be with respect to described fixing locking
The locking rod that block moves up；Described in the lower end edge of described locking rod, the first inclined plane moves, and promotes described locking
Bar moves up with respect to described fixing latch；First level face described in the lower end edge of described locking rod is mobile extremely close described
During locking hole, described locking rod moves down with respect to described fixing latch and is locked in described locking in the hole.
Preferably, it is provided with the mobile cavity being available for described locking rod movement in described fixing latch, described mobile intracavity sets
There is spring, described spring housing on described locking rod, fixed with described mobile cavity by the upper end of described spring, the lower end of described spring
Fix with described locking rod.
Preferably, described locking rod is Telescopic rod structure, and includes the first expansion link and the second expansion link；Described spring housing
It is located on described first expansion link, the lower end of described spring is fixed with described second expansion link；Described second expansion link is set in
Extend downwardly from can or upwards retract on described first expansion link and with respect to described first expansion link.
Preferably, described fixing latch top is provided with solution closing piece, and described solution closing piece can be with respect to described fixing latch
Move horizontally, described solution closing piece is provided with the second inclined plane, the upper horizontal of described second inclined plane extends and forms the second level
Face, described second inclined plane and described second horizontal plane are provided with the solution locked groove of fixed solution closing piece described in up/down perforation, described lock
The top of stopping bar is located in described solution locked groove, and mobile extremely described along described second inclined plane when described solution closing piece moves horizontally
Second horizontal plane.
Preferably, the top of described locking rod is provided with locking cap, the bottom of described locking cap and described second inclined plane and
Described second horizontal plane contacts.
Preferably, the periphery of described fixing latch fixing lock stops is provided with slideway, and the bottom of described solution closing piece symmetrically sets
There is slide plate, described slide plate is slidably connected with the described slideway of correspondence position.
Preferably, the top of described fixing latch is provided with stopper section in the side near described second horizontal plane, described
Stopper section can release formula with described solution closing piece and offset.
According to the unmanned plane cargo hold of the application, because unmanned plane cargo hold can move through mobile latch in the horizontal direction
It is locked among fixing latch, therefore, it is possible to realize quick despatch and the self-locking of unmanned plane cargo hold.
Brief description
By reading the detailed description that non-limiting example is made made with reference to the following drawings, other of the application
Feature, objects and advantages will become more apparent upon：
Fig. 1 illustrates the structural representation of the unmanned plane cargo hold according to the embodiment of the present application；
Fig. 2 illustrates the structural representation at another visual angle of the unmanned plane cargo hold according to the embodiment of the present application；
Fig. 3 illustrates the A portion enlarged drawing in Fig. 2；
The structure of mobile latch and fixing latch that Fig. 4 illustrates the unmanned plane cargo hold according to the embodiment of the present application is shown
It is intended to；
Fig. 5 illustrates the mobile latch of the unmanned plane cargo hold according to the embodiment of the present application and fixes latch in locking shape
Structural representation during state；And
Fig. 6 illustrates the mobile latch of the unmanned plane cargo hold according to the embodiment of the present application and fixes latch in locking shape
Structural representation during state.
Specific embodiment
With reference to the accompanying drawings and examples the application is described in further detail.It is understood that this place is retouched
The specific embodiment stated is used only for explaining relevant utility model, rather than the restriction to this utility model.Further need exist for explanation
, for the ease of description, in accompanying drawing, illustrate only the part related to utility model.
It should be noted that in the case of not conflicting, the embodiment in the application and the feature in embodiment can phases
Mutually combine.To describe the application below with reference to the accompanying drawings and in conjunction with the embodiments in detail.
Refer to Fig. 1-Fig. 6, it illustrates the technical scheme of the unmanned plane cargo hold according to the embodiment of the present application.As Fig. 1-figure
Shown in 3, unmanned plane cargo hold includes one group of first connecting plate 1 being parallel to each other and one group of second connecting plate 2 being parallel to each other, one group
The bottom of the first connecting plate and one group of second connecting plate is closed by base plate, the top of one group of first connecting plate and one group of second connecting plate
Portion can be unenclosed construction, is easy to be placed and taken out goods.It is of course also possible to one group of first connecting plate and one group second are connected
The top seal of fishplate bar, and the loading door of goods is arranged wherein on first connecting plate or the second connecting plate.Adjacent
One connecting plate 1 and the second connecting plate 2 are connected by column 3 around the corner, and column 3 can be rectangular in shape, and the both sides of column 3 are respectively
Connect corresponding first connecting plate 1 and the second connecting plate 2, so, the first connecting plate 1 and the second connecting plate 2 company by column 3
Connect the cargo component defining integral type, assembled simple, it is easy to operate.Preferably, the bottom of column 3 is provided with heel brace block 4, heel brace
Block 4 is supported between the both sides of column 3, serves position-limiting action to the first connecting plate 1 and the second connecting plate 2.Further preferably
Ground, heel brace block 4 bottom is provided with roller, and so, unmanned plane can be in ground moving.
On the basis of the technical scheme of above-mentioned unmanned plane cargo hold, as shown in Figures 2 and 3, unmanned plane cargo hold and slide rail it
Between locking is connected by self-locking mechanism, self-locking mechanism includes fixing latch 6 and mobile latch 5.First connecting plate is close
Corner location (being right side in Fig. 2) at one is provided with mobile latch 5, and the top of mobile latch 5 is provided with fixing latch 6.
Wherein, unmanned plane cargo hold general with unmanned plane body assembly connection, therefore, fixation latch 6 can be fixedly installed on unmanned plane
On the slide rail 7 of body.It is of course also possible to as needed fixing latch 6 is fixedly installed on the slide rail of different devices.No
Man-machine cargo hold can move along slide rail, when at the mobile position to fixing latch 6 of mobile latch 5, completes locking.Enter
One step ground, slide rail 7 is provided with the first sliding table 7.1 being available for that mobile latch 5 slides, and also is provided with mobile latch 5
Match with the first sliding table 7.1 and merge the second sliding table 5.1 being slidably connected.Mobile latch 5 can be sliding by first
Being slidably connected between dynamic table top 7.1 and the second sliding table 5.1, and slide along slide rail 7 level and be locked in fixing locking
Among block 6, so, the self-locking cooperation that unmanned plane cargo hold passes through between mobile latch 5 and fixing latch 6 is connected to
On slide rail 7, it is achieved thereby that rapidly self-locking connects to unmanned plane body by unmanned plane cargo hold.
Refer to Fig. 1-Fig. 6, it illustrates the technical scheme of the unmanned plane cargo hold according to the embodiment of the present application.As Fig. 4-figure
Shown in 6, mobile latch 5 is provided with the first inclined plane 8, and the upper horizontal of the first inclined plane 8 extends and forms first level face 9,
First level face 9 is provided with locking hole 21.Fixing latch 6 is provided with and upwardly or downwardly can move with respect to fixing latch 6
Dynamic locking rod 10.As shown in figure 5, when mobile latch 5 moves horizontally close to locking rod 10, the lower end of locking rod 10 is permissible
Mobile (at the dotted line position in Fig. 5) along the first inclined plane 8, thus promoting locking rod 10 with respect to fixing latch 6 upwards
Mobile；And when the lower end of locking rod 10 moves to first level face 9, mobile latch 5 continues to move horizontally, locking rod 10 is not
It is relatively fixed latch 6 movement again, when the lower end of locking hole 21 movement to locking rod 10, locking rod 10 is with respect to fixing locking
Block 6 moves down and is locked in locking hole 21.Locking hole 21 can be elastic fastening set, can fasten and it locking rod
In, and limit locking rod movement.Thus, the locking of unmanned plane cargo hold is assembled on unmanned plane.Thus, unmanned plane cargo hold is locked
It is assembled to slide rail, or even on unmanned plane.Auto-lock process is easy to operate, and can quickly realize self-locking operation.
On the basis of the technical scheme of above-mentioned unmanned plane cargo hold, as shown in figure 5, be provided with fixing latch 6 to be available for locking
The mobile cavity of stopping bar 10 movement, mobile intracavity is provided with spring 11.Spring 11 is enclosed within locking rod 10, the upper end of spring 11 and movement
Chamber is fixed, and the lower end of spring 11 is fixing with locking rod 10.So, when locking rod 10 moves up, meeting compression spring 11, spring
11 generation elastic deformations；And when locking hole 21 moves to locking rod 10 bottom, spring 11 recovers elastic deformation and simultaneously opens, thus
Locking rod 10 is locked in locking hole 21 under spring 11 effect.Preferably, locking rod 10 is arranged with sleeve member 12, set
Barrier part 12 is located at mobile intracavity, and the top of the lower end of spring 11 and sleeve member 12 is fixed, and spring 11 is easy in the setting of sleeve member 12
It is connected with locking rod 10.
Preferably, locking rod can be Telescopic rod structure, and includes the first expansion link and the second expansion link.Second expansion link
It is set on the first expansion link and can extend downwardly from respect to the first expansion link or retract upwards.Spring is set in the first expansion link
On, the upper end of spring and mobile cavity are fixed, and the lower end of spring is fixed with the second expansion link.So, the lower end of locking rod along
When first inclined plane is mobile, the first expansion link can remain stationary as, and the second expansion link is retracted upwards, thus compression spring.?
The lower end of locking rod to first level face, during the lower end of locking hole movement to locking rod, spring opens, drive the second expansion link to
Under stretch out, so that firm being locked among locking hole of locking rod.
On the basis of the technical scheme of above-mentioned unmanned plane cargo hold, as Figure 4-Figure 6, fixing latch 6 top is provided with
Solution closing piece 13, solution closing piece 13 can move horizontally with respect to fixing latch 6, and solution closing piece is provided with the second inclined plane 15, and second inclines
The upper horizontal on inclined-plane 15 extends and forms the second horizontal plane 14.Second inclined plane 15 and the second horizontal plane 14 are provided with up/down perforation
The solution locked groove 16 of fixed solution closing piece, the top of locking rod is located in unblock groove.Preferably, the periphery of fixing latch 6 is provided with cunning
Road 18, the bottom of solution closing piece is arranged with slide plate 17, and slide plate 17 is slidably connected with the slideway of correspondence position, so that solution closing piece
Can move horizontally along fixing latch.So, when solving closing piece 13 and moving horizontally, the top of locking rod 10 can be with respect to
Solution locked groove 16 level simultaneously moves up；Under the promotion of solution closing piece 13, the top of locking rod 10 is mobile extremely along the second inclined plane 15
Second horizontal plane 14, such that it is able to lift the top of locking rod 10 so that locking hole 21 is left in the lower end of locking rod 10, releases
Lockup state.After releasing lockup state, unmanned plane cargo hold disassembles from slide rail.
Preferably, the top of locking rod 10 is provided with locking cap 19, the bottom of locking cap 19 and the second inclined plane 15 and second
Horizontal plane 14 contacts, and is easy to solution closing piece and lifts locking cap 19 by the effect of the second inclined plane 15 and the second horizontal plane 14,
Thus unlocking locking rod.
It is further preferred that the top of fixing latch 6 is provided with stopper section 20 in the side near the second horizontal plane 14, only
Stopper 20 can release formula with solution closing piece and offset.As shown in fig. 6, when solution closing piece moves horizontally and lifts locking rod, solution closing piece leaves
Stopper section 20；And when locking rod is in lockup state, as shown in figure 5, solution closing piece is offseted with stopper section 20, thus limiting unblock
The movement of block.
Above description is only the preferred embodiment of the application and the explanation to institute's application technology principle.People in the art
Member is it should be appreciated that involved utility model scope is however it is not limited to the particular combination of above-mentioned technical characteristic in the application
Technical scheme, also should cover in the case of without departing from described application design, by above-mentioned technical characteristic or its equivalent feature simultaneously
The other technical schemes carrying out combination in any and being formed.Such as features described above and (but not limited to) disclosed herein have class
The technical scheme replaced mutually and formed like the technical characteristic of function.
Claims (10)
1. a kind of unmanned plane cargo hold, described unmanned plane cargo hold includes：One group of first connecting plate being parallel to each other and one group mutually flat
Second connecting plate of row, the first connecting plate described in a group and the bottom of the second connecting plate described in a group are closed by base plate, adjacent
Described first connecting plate and described second connecting plate are connected by column around the corner；At least one described first connecting plate is leaning on
Corner location at nearly one is provided with mobile latch, and the top of described mobile latch is provided with fixing latch, described fixing lock
Stops may be provided on the slide rail of unmanned plane body, and described unmanned plane cargo hold can move horizontally along described slide rail and by described shifting
Dynamic latch and described fixing latch locking.
2. unmanned plane cargo hold according to claim 1 is it is characterised in that described column is rectangular in shape, and the two of described column
Side connects corresponding first connecting plate and the second connecting plate respectively, and the bottom of described column is provided with heel brace block, and described heel brace block props up
Support between the both sides of described column.
3. unmanned plane cargo hold according to claim 2 is it is characterised in that described heel brace block bottom is provided with roller.
4. the unmanned plane cargo hold according to claim 1-3 any one claim is it is characterised in that described mobile latch
It is provided with the first inclined plane, the upper horizontal of described first inclined plane extends and forms first level face, on described first level face
It is provided with locking hole；Described fixing latch is provided with the locking that can move up with respect to described fixing latch
Bar；Described in the lower end edge of described locking rod first inclined plane move, promote described locking rod with respect to described fixing latch to
Upper movement；During the mobile extremely close described locking hole in first level face described in the lower end edge of described locking rod, described locking rod is relatively
Move down in described fixing latch and be locked in described locking in the hole.
5. unmanned plane cargo hold according to claim 4 is available for described lock it is characterised in that being provided with described fixing latch
The mobile cavity of stopping bar movement, described mobile intracavity is provided with spring, described spring housing on described locking rod, the upper end of described spring
Fix with described mobile cavity, the lower end of described spring is fixed with described locking rod.
6. unmanned plane cargo hold according to claim 5, it is characterised in that described locking rod is Telescopic rod structure, and includes
First expansion link and the second expansion link；Described spring is set on described first expansion link, the lower end of described spring and described the
Two expansion links are fixed；Described second expansion link is set on described first expansion link and can be downward with respect to described first expansion link
Stretch out or retract upwards.
7. unmanned plane cargo hold according to claim 6 is it is characterised in that described fixing latch top is provided with solution closing piece,
Described solution closing piece can move horizontally with respect to described fixing latch, and described solution closing piece is provided with the second inclined plane, and described second
The upper horizontal of inclined plane extends and forms the second horizontal plane, and described second inclined plane and described second horizontal plane are provided with and pass through up and down
Lead to the solution locked groove of described fixed solution closing piece, the top of described locking rod is located in described solution locked groove, and in described solution closing piece level
Along mobile extremely described second horizontal plane of described second inclined plane when mobile.
8. unmanned plane cargo hold according to claim 7 is it is characterised in that the top of described locking rod is provided with locking cap, institute
The bottom stating locking cap is contacted with described second inclined plane and described second horizontal plane.
9. unmanned plane cargo hold according to claim 8 is it is characterised in that the periphery of described fixing latch fixing lock stops
It is provided with slideway, the bottom of described solution closing piece is arranged with slide plate, and described slide plate is slidably connected with the described slideway of correspondence position.
10. unmanned plane cargo hold according to claim 9 is it is characterised in that the top of described fixing latch is near institute
The side stating the second horizontal plane is provided with stopper section, and described stopper section can release formula with described solution closing piece and offset.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620801260.3U CN205971861U (en) | 2016-07-28 | 2016-07-28 | Unmanned aerial vehicle cargo hold |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620801260.3U CN205971861U (en) | 2016-07-28 | 2016-07-28 | Unmanned aerial vehicle cargo hold |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205971861U true CN205971861U (en) | 2017-02-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620801260.3U Active CN205971861U (en) | 2016-07-28 | 2016-07-28 | Unmanned aerial vehicle cargo hold |
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| CN (1) | CN205971861U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106114866A (en) * | 2016-07-28 | 2016-11-16 | 顺丰科技有限公司 | Unmanned plane cargo hold |
| CN107355455A (en) * | 2017-07-27 | 2017-11-17 | 顺丰科技有限公司 | One kind carrying lock and locking, unlocking method |
| CN109110133A (en) * | 2018-09-07 | 2019-01-01 | 佛山皖和新能源科技有限公司 | A kind of plural serial stage shipping unmanned aerial vehicle body |
-
2016
- 2016-07-28 CN CN201620801260.3U patent/CN205971861U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106114866A (en) * | 2016-07-28 | 2016-11-16 | 顺丰科技有限公司 | Unmanned plane cargo hold |
| CN106114866B (en) * | 2016-07-28 | 2019-02-01 | 顺丰科技有限公司 | Unmanned plane cargo hold |
| CN107355455A (en) * | 2017-07-27 | 2017-11-17 | 顺丰科技有限公司 | One kind carrying lock and locking, unlocking method |
| CN109110133A (en) * | 2018-09-07 | 2019-01-01 | 佛山皖和新能源科技有限公司 | A kind of plural serial stage shipping unmanned aerial vehicle body |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210805 Address after: 518063 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: 518061 Intersection of Xuefu Road (south) and Baishi Road (east) in Nanshan District, Shenzhen City, Guangdong Province, 6-13 floors, Block B, Shenzhen Software Industry Base Patentee before: SF TECHNOLOGY Co.,Ltd. |
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| TR01 | Transfer of patent right |