CN205971850U - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205971850U CN205971850U CN201620800992.0U CN201620800992U CN205971850U CN 205971850 U CN205971850 U CN 205971850U CN 201620800992 U CN201620800992 U CN 201620800992U CN 205971850 U CN205971850 U CN 205971850U
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- unmanned plane
- latch
- mobile
- locking rod
- locking
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Abstract
The application discloses unmanned aerial vehicle includes: the set -top cabin, the both sides in set -top cabin partially do not are equipped with to be run through the connecting rod that the set -top cabin set up, every the both ends of connecting rod are connected with the frame pole respectively perpendicularly, the top at the both ends of frame pole is equipped with the wing respectively, punishment do not is equipped with the support column in the turning position in the bottom in set -top cabin, the bottom of support column is equipped with the base, the set -top cabin the support column with the battery flat has been formed between the base, the set -top under -deck is equipped with flight control device, be equipped with cell ontology in the battery flat, cell ontology's top with flight control device connects. This disclosed unmanned aerial vehicle reliability is higher and can the fast loading and unloading unmanned aerial vehicle cargo hold.
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 a kind of
Unmanned plane.
Background technology
UAV referred to as " unmanned plane ", is to be manipulated with the presetting apparatus provided for oneself using radio robot
Not manned aircraft.No driving cabin on machine, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or
Machine tool remote control station personnel pass through the equipment such as radar, it is tracked, positions, remote control, remote measurement and Digital Transmission.Domestic logistics are no
Man-machine technology is mainly consumer level at present or the model plane transformation of the way forms, the X-type structure of mostly four to eight rotors, and cargo handling is transported
Waste time and energy.
Utility model content
In view of drawbacks described above of the prior art or deficiency are it is desirable to provide a kind of reliability higher unmanned plane.
A kind of first aspect according to the disclosure, there is provided unmanned plane, described unmanned plane includes：Machine overhead bin, described machine top
The both sides in cabin are respectively equipped with the connecting rod running through described machine overhead bin setting, and the two ends of each described connecting rod are respectively perpendicular connection
Organic hack lever, the top at the two ends of described frame bar is respectively equipped with wing；The bottom of described machine overhead bin difference at corner location
It is provided with support column, the bottom of described support column is provided with base, define between described machine overhead bin, described support column and described base
Battery flat；Be provided with described machine overhead bin and fly control device, in described battery flat, be provided with battery body, the top of described battery body with
Described winged control device connects.
Preferably, the top of described battery body is provided with self-locking joint, described battery body pass through described self-locking joint with
Described winged control device grafting is fixed.
Preferably, it is vertically connected with gripper shoe between described machine overhead bin and described base.
Preferably, the bottom of described base is provided with slide rail at the position near the front and rear of described battery flat, institute
State slide rail to be used for being slidably connected and lock unmanned plane cargo hold.
Preferably, described slide rail one end is provided with fixing latch, and described unmanned plane cargo hold is corresponding with described fixing latch
Position at be provided with mobile latch, described unmanned plane cargo hold can slide along described slide rail and pass through described mobile latch locking
Among described fixing latch.
Preferably, described slide rail is provided with the first sliding table being available for that mobile latch slides, described mobile latch
Being provided with is matched with described first sliding table merges the second sliding table being slidably connected, and described unmanned plane cargo hold passes through described
First sliding table and the second being slidably connected of sliding table and slide along described slide rail.
A kind of second aspect according to the disclosure, there is provided self-locking mechanism, including fixing latch and mobile latch, institute
State mobile latch and be provided with the first inclined plane, the upper horizontal of described first inclined plane extends and forms first level face, described
First level face is provided with locking hole；Described fixing latch is provided with can with respect to described fixing latch upwardly or downwardly
The locking rod of movement；Described in the lower end edge of described locking rod, the first inclined plane moves, and promotes described locking rod solid with respect to described
Lock stops moves up；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 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 arranged with sleeve member, described sleeve member is located at described mobile intracavity, described spring
The top of lower end and described sleeve member is fixed.
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 is provided with slideway, and the bottom of described solution closing piece is arranged with 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.
A kind of third 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, adjacent described first connecting plate and described second connection
Plate is connected by column around the corner；Described column being provided with mobile latch near corner, described mobile latch upper
Side is provided with the fixing latch being fixedly installed, and described unmanned plane cargo hold can move through described mobile latch in the horizontal direction
It is locked among described fixing latch.
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.
According to the unmanned plane of the application, because the both sides of machine overhead bin are respectively equipped with the connecting rod running through the setting of machine overhead bin,
The two ends of each connecting rod are respectively perpendicular connection organic frame bar, and the vibration of the machine overhead bin part that therefore unmanned plane is in operation is permissible
Disperseing away along connecting rod and frame bar, thus decreasing the impact to machine overhead bin for the operating vibration, improve unmanned plane
Reliability.
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 according to the embodiment of the present application；
Fig. 2 illustrates the A portion enlarged drawing in Fig. 1；
Fig. 3 illustrates the front view of the unmanned plane according to the embodiment of the present application；
Fig. 4 illustrates mobile latch and the structural representation fixing latch according to the embodiment of the present application；
The mobile latch that Fig. 5 illustrates according to the embodiment of the present application shows with the fixing structure in lockup state for the latch
It is intended to；
The mobile latch that Fig. 6 illustrates according to the embodiment of the present application shows with the fixing structure in lockup state for the latch
It is intended to；
Fig. 7 illustrates the structural representation of the unmanned plane cargo hold according to the embodiment of the present application；
Fig. 8 illustrates the structural representation at another visual angle of the unmanned plane cargo hold according to the embodiment of the present application；And
Fig. 9 illustrates the B portion enlarged drawing in Fig. 8.
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. 9, 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, a kind of unmanned plane includes machine overhead bin 1, and the both sides of machine overhead bin 1 are respectively equipped with the connecting rod 2 running through the setting of machine overhead bin, often
The two ends of individual connecting rod 2 are respectively perpendicular connection organic frame bar 3, and the top at the two ends of frame bar 3 is respectively equipped with wing 4.So, no
The vibration of the man-machine machine overhead bin 1 being in operation can disperse along connecting rod 2 and frame bar 3 and pass, thus decreasing
The impact to machine overhead bin 1 for the operating vibration, improves the reliability of unmanned plane.The bottom of machine overhead bin 1 is punished in corner location
Be not provided with support column 5, the bottom of support column 5 is provided with base 14 (showing in figure 3), machine overhead bin 1, support column 5 and base 14 it
Between define battery flat 6.So, battery flat 6 provides placement space for battery body 7, optimizes layout, decreases space wave
Take.It is provided with machine overhead bin 1 and flies control device, in battery flat 6, be provided with battery body 7, the top of battery body 7 is with winged control device even
Connect, to power for unmanned plane.Preferably, as shown in figure 3, the top of battery body 7 is provided with self-locking joint 12, battery body 7
Fixed with flying control device grafting by self-locking joint 12.
Preferably, as shown in figure 3, being vertically connected with gripper shoe 13 between machine overhead bin 1 and base 14, to play reinforcing battery
Cabin 6 and the effect supporting machine overhead bin 1.
On the basis of a kind of above-mentioned technical scheme of unmanned plane, as shown in figure 3, the bottom of base 14 is near battery flat
It is equipped with slide rail 8, slide rail 8 is used for being slidably connected and lock unmanned plane cargo hold 9 at the position of front and rear.
Preferably, as shown in Fig. 2 completing to be locked by self-locking mechanism between unmanned plane cargo hold 9 and slide rail 8.Wherein,
Self-locking mechanism includes fixing latch 10 and mobile latch 11.Slide rail is provided with fixing latch 10, and unmanned plane cargo hold sets
There is mobile latch 11, fixing latch 10 is arranged on the end of slipping into of slide rail 8, mobile latch 11 slipping into along unmanned plane cargo hold
End setting on direction, unmanned plane cargo hold 9 can be slided along slide rail 8 and pass through mobile latch 11 and be locked with fixing latch 10
Only.
It is further preferred that slide rail 8 is provided with the first sliding table 8.1 being available for that mobile latch slides, mobile locking
Block 11 is provided with to be matched with the first sliding table 8.1 and merges the second sliding table 11.1 being slidably connected, and unmanned plane cargo hold 9 passes through
Being slidably connected and slide along slide rail 8 of first sliding table 8.1 and the second sliding table 11.1.So, unmanned plane cargo hold 9 passes through
Self-locking cooperation between mobile latch 11 and fixing latch 10 has been connected on unmanned plane.
Refer to Fig. 1-Fig. 9, it illustrates the technical scheme of the unmanned plane according to the embodiment of the present application.As Fig. 4-Fig. 6 institute
Show, it illustrates the structural representation of self-locking mechanism, wherein, mobile latch 11 is provided with the first inclined plane 16, the first inclination
The upper horizontal in face 16 extends and forms first level face 17, and first level face 17 is provided with locking hole 28.On fixing latch 10
It is provided with the locking rod 15 that can move up with respect to fixing latch 10.As shown in figure 5, in mobile latch 11 water
Flat when moving closer to locking rod 15, the lower end of locking rod 15 can along the first inclined plane 16 mobile (as the dotted line position in Fig. 5
Place), thus promoting locking rod 15 to move up with respect to fixing latch 10；And the lower end working as locking rod 15 moves to the first water
During plane 17, mobile latch 11 continues to move horizontally, and it is mobile, in locking hole 28 that locking rod 15 is no longer relatively fixed latch 10
During mobile lower end to locking rod 15, locking rod 15 moves down and is locked in locking hole 28 with respect to fixing latch 10.
Locking hole can be elastic fastening set, can by locking rod fastening with wherein, and limit locking rod move.Thus, by unmanned plane
Cargo hold locking is assembled on unmanned plane.Auto-lock process is easy to operate, and can quickly realize certainly being locked into no unmanned plane cargo hold
Operation on people.
Preferably, as shown in figure 5, being provided with, in fixing latch 10, the mobile cavity being available for locking rod 15 movement, mobile intracavity
It is provided with spring 18.Spring 18 is enclosed within locking rod 19, and the upper end of spring 18 and mobile cavity are fixed, the lower end of spring 18 and locking rod
15 is fixing.So, when locking rod 15 moves up, meeting compression spring 18, there is elastic deformation in spring 18；And work as locking hole 28
When moving to locking rod 15 bottom, spring 18 recovers elastic deformation and simultaneously opens, so that locking rod 15 is under spring 18 effect
It is locked in locking hole 28.Preferably, locking rod 15 is arranged with sleeve member 19, sleeve member 19 is located at mobile intracavity, spring 18
The top of lower end and sleeve member 19 fix, the setting of sleeve member 19 is easy to spring 18 and is connected with locking rod 15.
It is further preferred that locking rod can be Telescopic rod structure, and include the first expansion link and the second expansion link.Second
Expansion link 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 first
On expansion link, the upper end of spring and mobile cavity are fixed, and the lower end of spring is fixed with the second expansion link.So, under locking rod
Along during the first inclined plane movement, the first expansion link can remain stationary as, and the second expansion link is retracted upwards, thus compressing bullet at end
Spring.In the lower end of locking rod to first level face, during the lower end of locking hole movement to locking rod, spring opens, and drives second to stretch
Contracting bar extends downwardly from, so that firm being locked among locking hole of locking rod.
Preferably, as Figure 4-Figure 6, fixing latch 10 top is provided with solution closing piece 20, and solution closing piece 20 can be with respect to solid
Lock stops 10 moves horizontally, and solution closing piece is provided with the second inclined plane 22, and the upper horizontal of the second inclined plane 22 extends formation the
Two horizontal planes 21.Second inclined plane 22 and the second horizontal plane 21 are provided with the solution locked groove 23 of up/down perforation fixed solution closing piece, locking
The top of bar is located in unblock groove.Preferably, the periphery of fixing latch 10 is provided with slideway 25, and the bottom of solution closing piece is arranged with
Slide plate 24, slide plate 24 is slidably connected with the slideway 25 of correspondence position, so that solution closing piece can be along fixing latch level
Mobile.So, as shown in fig. 6, when solution closing piece 20 moves horizontally, the top of locking rod 15 can be with respect to solution locked groove 23 level
And move up；Under the promotion of solution closing piece 20, the top of locking rod 15 is moved to the second horizontal plane 21 along the second inclined plane 22,
Such that it is able to lift the top of locking rod 15 so that locking hole 28 is left in the lower end of locking rod 15, release lockup state.Release
After lockup state, unmanned plane cargo hold 9 disassembles from unmanned plane.
Preferably, the top of locking rod 15 is provided with locking cap 26, the bottom of locking cap 26 and the second inclined plane 22 and second
Horizontal plane 21 contacts, and is easy to solution closing piece and lifts locking cap 26 by the effect of the second inclined plane 22 and the second horizontal plane 21,
Thus unlocking locking rod.
It is further preferred that the top of fixing latch 10 is provided with stopper section 27 in the side near the second horizontal plane 21,
Stopper section 27 can release formula with solution closing piece and offset.As shown in fig. 6, solve closing piece move horizontally lift locking rod when, solution closing piece from
Opening and closing stopper 26；And when locking rod is in lockup state, as shown in figure 5, solution closing piece is offseted with stopper section 26, thus limiting solution
The movement of closing piece.
Refer to Fig. 1-Fig. 9, it illustrates the technical scheme of the unmanned plane according to the embodiment of the present application.As Fig. 7-Fig. 9 institute
Show, unmanned plane cargo hold includes one group of first connecting plate 29 being parallel to each other and one group of second connecting plate 30 being parallel to each other, adjacent
The first connecting plate 29 and the second connecting plate 30 connected by column 31 around the corner, column 31 can be rectangular in shape, column 31
Both sides connect corresponding first connecting plate 29 and the second connecting plate 30 respectively, so, the first connecting plate 29 and the second connecting plate
30 cargo components constituting integral type passing through column 31, assembled simple, it is easy to operate.Preferably, under column 31
Portion is provided with heel brace block 32, and heel brace block 32 is supported between the both sides of column 31, to the first connecting plate 29 and the second connecting plate 30
Arrive position-limiting action.It is further preferred that heel brace block 32 bottom is provided with roller, so, unmanned plane can be in ground moving.
Preferably, as shown in Figure 8 and Figure 9, column 31 is being provided with mobile latch 11 near corner, mobile latch 11
Top be provided with the fixing latch 10 being fixedly installed.Wherein, fixing latch 10 is fixedly installed on slide rail 8, and slide rail 8 sets
There is the first sliding table 8.1 being available for that mobile latch 11 slides, and also be provided with and the first sliding table on mobile latch 11
8.1 match merges the second sliding table 11.1 being slidably connected.Mobile latch 11 can be by the first sliding table 8.1 and the
Being slidably connected between two sliding tables 11.1, and slide along slide rail 8 level and be locked among fixing latch 10, this
Sample, the self-locking cooperation that unmanned plane cargo hold passes through between mobile latch 11 and fixing latch 10 has been connected to unmanned plane
On.
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, described unmanned plane includes：Machine overhead bin, the both sides of described machine overhead bin are respectively equipped with runs through described machine top
The connecting rod of cabin setting, the two ends of each described connecting rod are respectively perpendicular connection organic frame bar, the top at the two ends of described frame bar
Portion is respectively equipped with wing；The bottom of described machine overhead bin is respectively equipped with support column at corner location, and the bottom of described support column sets
There is base, between described machine overhead bin, described support column and described base, define battery flat；It is provided with described machine overhead bin and fly control dress
Put, in described battery flat, be provided with battery body, the top of described battery body is connected with described winged control device.
2. unmanned plane according to claim 1 is it is characterised in that the top of described battery body is provided with self-locking joint, institute
State battery body to fix with described winged control device grafting by described self-locking joint.
3. unmanned plane according to claim 1 is it is characterised in that be vertically connected between described machine overhead bin and described base
Gripper shoe.
4. the unmanned plane according to claim 1-3 any one claim is it is characterised in that the bottom of described base is being leaned on
It is provided with slide rail, described slide rail is used for being slidably connected and lock unmanned plane goods at the position of front and rear of closely described battery flat
Cabin.
5. unmanned plane according to claim 4 is it is characterised in that described slide rail one end is provided with fixing latch, described nothing
Man-machine cargo hold is provided with mobile latch at position corresponding with described fixing latch, and described unmanned plane cargo hold can be along described slide rail
Slide and be locked among described fixing latch by described mobile latch.
6. unmanned plane according to claim 5 is available for what mobile latch slided it is characterised in that described slide rail is provided with
First sliding table, described mobile latch is provided with to be matched with described first sliding table and merges the second slip being slidably connected
Table top, described unmanned plane cargo hold is slided along described slide rail by described first sliding table and the second being slidably connected of sliding table
Dynamic.
7. unmanned plane according to claim 6 is it is characterised in that described mobile latch is provided with the first inclined plane, institute
The upper horizontal stating the first inclined plane extends formation first level face, and described first level face is provided with locking hole；Described fixation
Latch is provided with the locking rod that can move up with respect to described fixing latch；The lower end edge of described locking rod
Described first inclined plane moves, and promotes described locking rod to move up with respect to described fixing latch；Under described locking rod
During the extremely close described locking hole mobile along described first level face of end, described locking rod moves downwards with respect to described fixing latch
Move and be locked in described locking in the hole.
8. unmanned plane according to claim 7 is available for described locking rod it is characterised in that being provided with described fixing latch
The mobile cavity of movement, described mobile intracavity is provided with spring, described spring housing on described locking rod, the upper end of described spring and institute
State mobile cavity to fix, the lower end of described spring is fixed with described locking rod.
9. unmanned plane cargo hold according to claim 8 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, the top of described locking rod is provided with locking cap, described lock
Only the bottom of cap is contacted with described second inclined plane and described second horizontal plane.
10. unmanned plane cargo hold according to claim 9 it is characterised in that described fixing latch fixing lock stops outer
It is provided with slideway week, 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,
The top of described fixing latch being provided with stopper section near the side of described second horizontal plane, described stopper section and described unblock
Block can release formula and offset.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620800992.0U CN205971850U (en) | 2016-07-28 | 2016-07-28 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620800992.0U CN205971850U (en) | 2016-07-28 | 2016-07-28 | Unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205971850U true CN205971850U (en) | 2017-02-22 |
Family
ID=58026976
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620800992.0U Withdrawn - After Issue CN205971850U (en) | 2016-07-28 | 2016-07-28 | Unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205971850U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106081110A (en) * | 2016-07-28 | 2016-11-09 | 顺丰科技有限公司 | A kind of unmanned plane |
| CN109649660A (en) * | 2019-03-14 | 2019-04-19 | 北京三快在线科技有限公司 | A kind of unmanned plane handling system, unmanned plane and loading/unloading platform |
-
2016
- 2016-07-28 CN CN201620800992.0U patent/CN205971850U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106081110A (en) * | 2016-07-28 | 2016-11-09 | 顺丰科技有限公司 | A kind of unmanned plane |
| CN106081110B (en) * | 2016-07-28 | 2019-06-11 | 顺丰科技有限公司 | A kind of unmanned plane |
| CN109649660A (en) * | 2019-03-14 | 2019-04-19 | 北京三快在线科技有限公司 | A kind of unmanned plane handling system, unmanned plane and loading/unloading platform |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20170222 Effective date of abandoning: 20190611 |