CN207466984U - The device for quickly disassembling of unmanned plane - Google Patents
The device for quickly disassembling of unmanned plane Download PDFInfo
- Publication number
- CN207466984U CN207466984U CN201721525962.4U CN201721525962U CN207466984U CN 207466984 U CN207466984 U CN 207466984U CN 201721525962 U CN201721525962 U CN 201721525962U CN 207466984 U CN207466984 U CN 207466984U
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- China
- Prior art keywords
- cover
- spacing ring
- quick
- unmanned plane
- electrical connector
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Abstract
The utility model is related to a kind of device for quickly disassembling of unmanned plane, including：First Quick-dismantle component, the second Quick-dismantle component for connecting the first Quick-dismantle component and the locking piece being connected on the first Quick-dismantle component or the second Quick-dismantle component.First Quick-dismantle component includes：First cover, the fixing sleeve being connected in the first cover, the first electrical connector being connected in the first cover and the spacing ring for being fixed by socket set；It is rotatable that spacing ring is relatively fixed set；Spacing ring is equipped with the first fixture block；Second Quick-dismantle component includes：The second electrical connector for being socketed the second cover of spacing ring and being connected in the second cover；Second cover relative limit ring is rotatable；Second cover is equipped with the second fixture block；Second electrical connector and the first electrical connector are releasable connection；Position of the locking piece for elastic reset structure and for locking spacing ring.The device for quickly disassembling of above-mentioned unmanned plane by way of rotary stopper, can realize the quick dismounting at the fuselage end and carry end of unmanned plane, improve working efficiency.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, more particularly to a kind of device for quickly disassembling of unmanned plane.
Background technology
Unmanned plane is that one kind is usually used in fixed point and the scenes such as shoots, jettisonings, observing, rescuing.General unmanned plane mainly includes：
Fuselage end and the carry end for being connected to fuselage end.According to the difference of action, it is sometimes necessary to fuselage end or carry end
Debugged or replaced, that mean that fuselage end and hang over end between need assembly and disassembly repeatedly.Traditional unmanned owner
If being attached fuselage end and carry end by screw, inconvenient profit, the occupancy regular hour is needed to come repeatedly tight
It locks or unscrews screw, working efficiency is low.
Utility model content
Based on this, the utility model provides a kind of device for quickly disassembling of unmanned plane, by way of rotary stopper, realizes nothing
Quick disassembly and assembly between man-machine fuselage end and carry end improves working efficiency.
A kind of device for quickly disassembling of unmanned plane, including：
First Quick-dismantle component；First Quick-dismantle component includes：First cover, the fixing sleeve being connected in the first cover, connection
The first electrical connector in the first cover and in the fixing sleeve and the spacing ring for being fixed by socket set；Spacing ring is relatively solid
Surely it covers rotatable；Spacing ring is equipped with the first fixture block；
Connect the second Quick-dismantle component of the first Quick-dismantle component；Second Quick-dismantle component includes：It is socketed the second cover of spacing ring
With the second electrical connector being connected in the second cover；Second cover relative limit ring is rotatable；Second cover is equipped with the second card
Block；Second cover and spacing ring are removably snapped connection by the second fixture block and the realization of the first fixture block；Second electrical connector with
First electrical connector is releasable connection；And
The locking piece being connected on the first Quick-dismantle component or the second Quick-dismantle component；Locking piece is elastic reset structure and is used for
Lock the position of spacing ring.
The device for quickly disassembling of above-mentioned unmanned plane, during use between the fuselage end of unmanned plane and carry end.Wherein, first
Quick-dismantle component is mounted on one in fuselage end or carry end, and the second Quick-dismantle component is then mounted in fuselage end or carry end
Another, locking piece can be mounted on the first Quick-dismantle component or the second Quick-dismantle component as needed.The limit of first Quick-dismantle component
Position ring and the second Quick-dismantle component the second cover between for socket and can relative rotation, meanwhile, utilize first on spacing ring
When the second fixture block on fixture block and the second cover causes spacing ring turn to designated position with the mutual snapping of the second cover, also,
When spacing ring reaches the position with the second cover snapping, locking piece locks the position of spacing ring.In addition, it is electrically connected using first
Fitting and the second electrical connector realize being electrically connected between fuselage end and carry end.It is when needing that the first Quick-dismantle component and second is fast
When tearing component separation open, resetted as long as locking piece is compressed, can rotary spacing ring so that the first fixture block and the second fixture block are wrong
It opens, and the first electrical connector is detached with the second electrical connector.By above-mentioned design, by way of rotary stopper, just
It can realize the quick dismounting at the fuselage end and carry end of unmanned plane, improve working efficiency.
The first cover is equipped with spaced first convex block in one of the embodiments,；Spacing ring the first cover of direction
One end be equipped be arranged at intervals and dislocation matching the first convex block the second convex block；First convex block and the second convex block cooperate to limit
Make the first cover and the relative position of spacing ring.First convex block and the second convex block are used to limit the rotating range of spacing ring, to keep away
Exempt from maloperation and the efficiency that dallies over one's work.
Locking piece includes in one of the embodiments,：The elastic component of button and connection button；Button is provided with limiting
The pillar that ring convex are stretched；Spacing ring is equipped with the limit hole being inserted into for pillar towards one end of locking piece.Under the action of elastic component, press
Key protrudes out in its natural state towards spacing ring, and when pillar is directed at limit hole, pillar will be inserted into limit hole, this
When spacing ring position be locked.When needing to unlock spacing ring, then limit hole is exited by pressing keys pillar.
Locking piece further includes in one of the embodiments,：Pressing plate；Elastic component is between pressing plate and button.Pressing plate is used
In the stroke of limitation button.
The one end of fixing sleeve far from the first cover is equipped with the first bulge loop in one of the embodiments,；Spacing ring is towards the
One end of one cover is equipped with the second bulge loop for being abutted with the first bulge loop, and the second bulge loop be located at the first bulge loop and the first cover it
Between.When fixing sleeve and spacing ring are socketed so that spacing ring is limited between fixing sleeve and the first cover, and spacing ring is avoided to make
With coming off in the process.
The first electrical connector includes in one of the embodiments,：The first circuit board being connected in the first cover and company
The first electric connector being connected on first circuit board；First electric connector is set towards the second electrical connector.Utilize electric connector
Patch realize dismountable electrical connection.
The first electric connector is shockproof movement connector in one of the embodiments,.Shockproof movement connector can assemble
When reduce vibrations.
The second electrical connector includes in one of the embodiments,：The second circuit board being connected in the second cover and company
Connect the second electric connector on the second circuit board；Second electric connector is set towards the first electrical connector.Utilize electric connector
Patch realize dismountable electrical connection.
The second electric connector is shockproof movement connector in one of the embodiments,.Shockproof movement connector can assemble
When reduce vibrations.
In one of the embodiments, the second cover away from one end of spacing ring be equipped with third bulge loop；Third bulge loop
Abut one end that the first fixture block deviates from the second fixture block.When the first fixture block and the second fixture block snapping, it is convex that the first fixture block is located at third
Between ring and the second fixture block, spacing ring is avoided to come off.
Description of the drawings
Fig. 1 is a kind of schematic diagram one of the device for quickly disassembling of the unmanned plane of embodiment of the utility model；
Fig. 2 is the schematic diagram two of the device for quickly disassembling of unmanned plane shown in FIG. 1；
Fig. 3 is the schematic diagram three of the device for quickly disassembling of unmanned plane shown in FIG. 1；
Fig. 4 is the schematic diagram crossed by the device for quickly disassembling along line A-A of unmanned plane shown in FIG. 1；
Fig. 5 is the decomposition diagram one of the device for quickly disassembling of unmanned plane shown in FIG. 1；
Fig. 6 is the decomposition diagram two of the device for quickly disassembling of unmanned plane shown in FIG. 1；
Fig. 7 is the exploded perspective view of the device for quickly disassembling of unmanned plane shown in FIG. 1；
Fig. 8 is the schematic diagram one of the spacing ring in the device for quickly disassembling of unmanned plane shown in FIG. 1；
Fig. 9 is the schematic diagram two of the spacing ring in the device for quickly disassembling of unmanned plane shown in FIG. 1；
The meaning of each label is in attached drawing：
The device for quickly disassembling of 10- unmanned planes；
The first Quick-dismantle components of 20-, the first covers of 21-, 22- fixing sleeves, the first electrical connectors of 23-, 24- spacing rings, 25-
One convex block, the first fixture blocks of 26-, the second convex blocks of 27-, the first bulge loops of 28-, the second bulge loops of 29-, 210- first circuit boards, 211-
One electric connector, the first screws of 212-, 213- anti-skid chequers, 214- limit holes, the first mounting holes of 215-；
The second Quick-dismantle components of 30-, the second covers of 31-, the second electrical connectors of 32-, the second fixture blocks of 33-, 34- third bulge loops,
35- second circuit boards, the second electric connectors of 36-, the second screws of 37-, the second mounting holes of 38-；
40- locking pieces, 41- buttons, 42- elastic components, 43- pillars, 44- pressing plates, 45- third screws.
Specific embodiment
For the ease of understanding the utility model, the utility model is more fully retouched below with reference to relevant drawings
It states.The preferred embodiment of the utility model is given in attached drawing.But the utility model can in many different forms come in fact
It is existing, however it is not limited to embodiment described herein.On the contrary, the purpose for providing these embodiments is the public affairs made to the utility model
Open the understanding more thorough and comprehensive of content.
It should be noted that when element is referred to as " being fixed on " another element, it can be directly on another element
Or there may also be elements placed in the middle.When an element is considered as " connection " another element, it can be directly connected to
To another element or it may be simultaneously present centering elements.
Unless otherwise defined, all of technologies and scientific terms used here by the article is led with belonging to the technology of the utility model
The normally understood meaning of technical staff in domain is identical.It is only in the term used in the description of the utility model herein
The purpose of description specific embodiment, it is not intended that in limitation the utility model.
It is a kind of schematic diagram of the device for quickly disassembling 10 of unmanned plane of the utility model referring to Fig. 1 to Fig. 9.
The device for quickly disassembling 10 of the unmanned plane, including：First Quick-dismantle component 20, the second Quick Release for connecting the first Quick-dismantle component 20
Component 30 and the locking piece 40 being connected on the first Quick-dismantle component 20.Wherein, the first Quick-dismantle component 20 is used to connect unmanned plane
Fuselage end, and the second Quick-dismantle component 30 is used to connect the carry end of unmanned plane, and the first Quick-dismantle component 20 and the second Quick Release
It is releasable connection between component 30, locking piece 40 is then for the first Quick-dismantle component 20 and the assembling phase interlocking of the second Quick-dismantle component 30
It is fixed.It should be noted that in other embodiments, locking piece 40 can also be connected on the second Quick-dismantle component 30.And first is fast
It can also be the carry end for connecting unmanned plane to tear component 20 open, and correspondingly, the second Quick-dismantle component 30 can also be connected to unmanned plane
Fuselage end.Hereafter above-mentioned each structure in the present embodiment is illustrated in more detail：
First Quick-dismantle component 20 includes：First cover 21, is connected to first at the fixing sleeve 22 being connected in the first cover 21
The first electrical connector 23 in cover 21 and in the fixing sleeve 22 and be fixed by socket 22 spacing ring 24.First cover
21 are equipped with spaced first convex block 25.It is rotatable and equipped with the first fixture block 26 that spacing ring 24 is relatively fixed set 22.Spacing ring
24 are equipped with the second convex block 27 for being arranged at intervals and misplacing the first convex block 25 of matching towards one end of the first cover 21.First convex block 25
It cooperates to limit the first cover 21 and the relative position of spacing ring 24 with the second convex block 27.In addition, in the present embodiment, Gu
Surely 22 one end far from the first cover 21 of set are additionally provided with the first bulge loop 28, and one end of spacing ring 24 towards the first cover 21 is then set
There is the second bulge loop 29 abutted with the first bulge loop 28, and the second bulge loop 29 is between the first bulge loop 28 and the first cover 21.The
One electrical connector 23 includes：The first circuit board 210 that is connected in the first cover 21 and be connected on first circuit board 210 the
One electric connector 211, and the first electric connector 211 is set towards the second electrical connector 32.In the present embodiment, first circuit board
210 be PCBA, and the first electric connector 211 is socket connector and is shockproof movement connector.In addition, 22 and first circuit of fixing sleeve
Plate 210 is by 212 releasable connection of the first screw in the first cover 21.The outside of spacing ring 24 is equipped with anti-skid chequer 213.First lid
Body 21 is equipped with the first mounting hole 215 being connect for the fuselage end with unmanned plane.
Second Quick-dismantle component 30 includes：It is socketed the second cover 31 and be connected in the second cover 31 second of spacing ring 24
Electrical connector 32.Second cover, 31 relative limit ring 24 is rotatable and equipped with the second fixture block 33.Second cover 31 and spacing ring 24
It is realized by the second fixture block 33 and the first fixture block 26 and removably snapped connection.In addition, in the present embodiment, the second cover 31
Third bulge loop 34 is equipped with away from one end of spacing ring 24.Third bulge loop 34 abuts one that the first fixture block 26 deviates from the second fixture block 33
End.Second electrical connector 32 and the first electrical connector 23 are releasable connection.In the present embodiment, the second electrical connector 32 includes：
The second circuit board 35 being connected in the second cover 31 and the second electric connector 36 being connected on second circuit board 35, and second
Electric connector 36 is set towards the first electrical connector 23.In the present embodiment, second circuit board 35 be PCBA, the second electric connector
36 are male seat connector and are shockproof movement connector.In addition, second circuit board 35 by 37 releasable connection of the second screw second
In cover 31.Second cover 31 is equipped with the second mounting hole 38 being connect for the carry end with unmanned plane,
Position of the locking piece 40 for elastic reset structure and for locking spacing ring 24.In the present embodiment, locking piece 40
Including：The button 41 and the elastic component 42 of connection button 41 being slidably connected in the first cover 21.Button 41 is provided with limiting
The pillar 43 that ring 24 protrudes out, correspondingly, spacing ring 24 are equipped with the limit hole being inserted into for pillar 43 towards one end of locking piece 40
214.Elastic component 42 is spring, in other embodiments, or elastic rubber or shrapnel etc..In the present embodiment, it locks
Part 40 further includes：Pressing plate 44 of the releasable connection in the first cover 21, and elastic component 42 is between pressing plate 44 and button 41.
In addition, pressing plate 44 by 45 releasable connection of third screw in the first cover 21.
The device for quickly disassembling 10 of above-mentioned unmanned plane, during use between the fuselage end of unmanned plane and carry end.Wherein,
One Quick-dismantle component 20 is mounted on one in fuselage end or carry end, and the second Quick-dismantle component 30 is then mounted on fuselage end or carry
Another in end, locking piece 40 can be mounted on the first Quick-dismantle component 20 or the second Quick-dismantle component 30 as needed.First
Between second cover 31 of 24 and second Quick-dismantle component 30 of spacing ring of Quick-dismantle component 20 for socket and can relative rotation, together
When, using the second fixture block 33 on the first fixture block 26 and the second cover 31 on spacing ring 24 so that 24 turn of spacing ring is to specified
During position with 31 mutual snapping of the second cover, also, when spacing ring 24 is reached with the position of 31 snapping of the second cover, locking piece
40 lock the position of spacing ring 24, the first Quick-dismantle component 20 and 30 stable connection of the second Quick-dismantle component and have anti-during locking
The advantages of vibrations.In addition, the electricity between fuselage end and carry end is realized using the first electrical connector 23 and the second electrical connector 32
Connection.When needing to detach the first Quick-dismantle component 20 with the second Quick-dismantle component 30, as long as locking piece 40 is compressed reset,
With rotary spacing ring 24 so that the first fixture block 26 and the second fixture block 33 are staggered, and the first electrical connector 23 is electrically connected with second
Part 32 detaches.By above-mentioned design, by way of rotary stopper, the fuselage end of unmanned plane and carry end can be realized
Quick dismounting, improve working efficiency.
In addition, the first convex block 25 and the second convex block 27 are used to limit the rotating range of spacing ring 24, to avoid maloperation
Dally over one's work efficiency.Under the action of elastic component 42, button 41 protrudes out in its natural state towards spacing ring 24, and works as pillar
During 43 alignment limit hole 214, pillar 43 will be inserted into limit hole 214, and the position of spacing ring 24 is locked at this time.Work as needs
When unlocking spacing ring 24, then limit hole 214 is exited by 41 pillar 43 of pressing keys.Pressing plate 44 is used to limit button
41 stroke.When fixing sleeve 22 and spacing ring 24 are socketed so that spacing ring 24 be limited in 22 and first cover 21 of fixing sleeve it
Between, spacing ring 24 is avoided to come off in use.Using electric connector patch realize dismountable electrical connection, and select
Shockproof movement connector can reduce vibrations in assembling.When the first fixture block 26 and the second 33 snapping of fixture block, the first fixture block 26
Between 34 and second fixture block 33 of third bulge loop, spacing ring 24 is avoided to come off.
Each technical characteristic of above example can be combined arbitrarily, to make description succinct, not to above-described embodiment
In each technical characteristic it is all possible combination be all described, as long as however, the combination of these technical characteristics be not present lance
Shield is all considered to be the range of this specification record.
Above example only expresses the preferred embodiment of the utility model, and description is more specific and detailed, but
Can not the limitation to utility model patent range therefore be interpreted as.It should be pointed out that the ordinary skill for this field
For personnel, without departing from the concept of the premise utility, various modifications and improvements can be made, these belong to this
The protection domain of utility model.Therefore, the protection domain of the utility model patent should be determined by the appended claims.
Claims (10)
1. a kind of device for quickly disassembling of unmanned plane, it is characterised in that：Including：
First Quick-dismantle component；First Quick-dismantle component includes：First cover, the fixing sleeve being connected in first cover,
The limiting of the first electrical connector and the socket fixing sleeve being connected in first cover and in the fixing sleeve
Ring；The relatively described fixing sleeve of the spacing ring is rotatable；The spacing ring is equipped with the first fixture block；
Connect the second Quick-dismantle component of first Quick-dismantle component；Second Quick-dismantle component includes：It is socketed the spacing ring
Second cover and the second electrical connector being connected in second cover；The relatively described spacing ring of second cover can revolve
Turn；Second cover is equipped with the second fixture block；Second cover and the spacing ring pass through second fixture block and described
The realization of one fixture block removably snaps connection；Second electrical connector is releasable connection with first electrical connector；And
The locking piece being connected on first Quick-dismantle component or the second Quick-dismantle component；The locking piece for elastic reset structure and
For locking the position of the spacing ring.
2. the device for quickly disassembling of unmanned plane according to claim 1, which is characterized in that first cover, which is equipped with, to be arranged at intervals
The first convex block；The spacing ring, which is equipped with to be arranged at intervals and misplace towards one end of first cover, matches first convex block
The second convex block；First convex block and second convex block cooperate to limit first cover and the spacing ring
Relative position.
3. the device for quickly disassembling of unmanned plane according to claim 1, which is characterized in that the locking piece includes：Button and company
Connect the elastic component of the button；The button is provided with the pillar that the spacing ring protrudes out；The spacing ring is towards the lock
The one end for determining part is equipped with the limit hole being inserted into for the pillar.
4. the device for quickly disassembling of unmanned plane according to claim 3, which is characterized in that the locking piece further includes：Pressing plate；Institute
Elastic component is stated between the pressing plate and the button.
5. the device for quickly disassembling of unmanned plane according to claim 1, which is characterized in that the fixing sleeve is far from the described first lid
There is the first bulge loop in one end of body；The spacing ring is equipped with the abutted with first bulge loop towards one end of first cover
Two bulge loops, and second bulge loop is between first bulge loop and first cover.
6. the device for quickly disassembling of unmanned plane according to claim 1, which is characterized in that first electrical connector includes：Even
The first circuit board being connected in first cover and the first electric connector being connected on the first circuit board；Described first
Electric connector is set towards second electrical connector.
7. the device for quickly disassembling of unmanned plane according to claim 6, which is characterized in that first electric connector is against shock
Connector.
8. the device for quickly disassembling of unmanned plane according to claim 1, which is characterized in that second electrical connector includes：Even
The second circuit board being connected in second cover and the second electric connector being connected on the second circuit board；Described second
Electric connector is set towards first electrical connector.
9. the device for quickly disassembling of unmanned plane according to claim 8, which is characterized in that second electric connector is against shock
Connector.
10. the device for quickly disassembling of unmanned plane according to claim 1, which is characterized in that deviating from for second cover is described
One end of spacing ring is equipped with third bulge loop；The third bulge loop abuts one that first fixture block deviates from second fixture block
End.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721525962.4U CN207466984U (en) | 2017-11-15 | 2017-11-15 | The device for quickly disassembling of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721525962.4U CN207466984U (en) | 2017-11-15 | 2017-11-15 | The device for quickly disassembling of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207466984U true CN207466984U (en) | 2018-06-08 |
Family
ID=62260692
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721525962.4U Expired - Fee Related CN207466984U (en) | 2017-11-15 | 2017-11-15 | The device for quickly disassembling of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207466984U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108001695A (en) * | 2017-11-15 | 2018-05-08 | 深圳市科比特航空科技有限公司 | The device for quickly disassembling of unmanned plane |
| CN108583851A (en) * | 2018-06-29 | 2018-09-28 | 拓攻（南京）机器人有限公司 | A kind of Quick Release undercarriage and the multi-rotor unmanned aerial vehicle containing it |
-
2017
- 2017-11-15 CN CN201721525962.4U patent/CN207466984U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108001695A (en) * | 2017-11-15 | 2018-05-08 | 深圳市科比特航空科技有限公司 | The device for quickly disassembling of unmanned plane |
| CN108583851A (en) * | 2018-06-29 | 2018-09-28 | 拓攻（南京）机器人有限公司 | A kind of Quick Release undercarriage and the multi-rotor unmanned aerial vehicle containing it |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180608 Termination date: 20211115 |
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| CF01 | Termination of patent right due to non-payment of annual fee |