CN208665546U - Quick Release attachment device and unmanned plane equipped with the device - Google Patents
Quick Release attachment device and unmanned plane equipped with the device Download PDFInfo
- Publication number
- CN208665546U CN208665546U CN201821187982.XU CN201821187982U CN208665546U CN 208665546 U CN208665546 U CN 208665546U CN 201821187982 U CN201821187982 U CN 201821187982U CN 208665546 U CN208665546 U CN 208665546U
- Authority
- CN
- China
- Prior art keywords
- connector
- hole
- connecting pin
- bolt
- attachment device
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
The utility model discloses a kind of Quick Release attachment device and equipped with the unmanned plane of the device, it is related to unmanned plane technical field of auxiliary equipment, including the first connector and the second connector to be linked together by Quick-dismantle component；The Quick-dismantle component includes bolt, and the bolt is equipped with the through-hole axially penetrated through, and sliding is equipped with connecting pin in the through-hole, and the through-hole is stretched out at the both ends of the connecting pin；The pilot hole for being connected to the through-hole is radially provided on the bolt, the fixing piece that the connecting pin can be fixed in the through-hole when being equipped with the connecting pin described in no external force pull in the pilot hole；First connector is equipped with threaded hole, and the bolt thread is assemblied in the threaded hole；The position that the threaded hole is corresponded on second connector is equipped with pin hole, and the end of the connecting pin is inserted into the pin hole after stretching out the bolt.The utility model is not needed by external tool, can quickly dismount carry, time saving and energy saving.
Description
Technical field
The utility model relates to unmanned plane technical field of auxiliary equipment, in particular to a kind of Quick Release attachment device and be equipped with should
The unmanned plane of device.
Background technique
Unmanned plane refers to the not manned vehicle using radio robot and the presetting apparatus provided for oneself manipulation, extensively
It is general to be applied to take photo by plane, agricultural, disaster relief, observe the industries such as wild animal, mapping.Some carries can be had on unmanned plane,
Such as PTZ camera, bracket, cantilever are all made of between the fuselage body of unmanned plane and these carries are threadedly coupled at present,
Required when carry dismounting by external tool, such as spanner, screwdriver, dismounting is more complex, time-consuming and laborious.
Utility model content
For disadvantages described above, the purpose of the utility model is to provide a kind of Quick Release attachment device and equipped with nobody of the device
Machine, this Quick Release attachment device and the unmanned plane equipped with the device are not needed by external tool, it will be able to carry is quickly dismounted,
It is time saving and energy saving, it is convenient and efficient.
To achieve the goals above, the technical solution of the utility model is:
A kind of Quick Release attachment device, including the first connector and the second connector to be linked together by Quick-dismantle component；Institute
Stating Quick-dismantle component includes bolt, and the bolt is equipped with the through-hole axially penetrated through, and sliding is equipped with connecting pin in the through-hole, described
The through-hole is stretched out at the both ends of connecting pin；The pilot hole for being connected to the through-hole, the pilot hole are radially provided on the bolt
The fixing piece that the connecting pin can be fixed on when being inside equipped with the connecting pin described in no external force pull in the through-hole；It is described
First connector is equipped with threaded hole, and the bolt thread is assemblied in the threaded hole；Institute is corresponded on second connector
The position for stating threaded hole is equipped with pin hole, and the end of the connecting pin is inserted into the pin hole after stretching out the bolt.
Wherein, the connecting pin is equipped with axially extending sliding slot, the fixation when there is connecting pin described in external force pull
It is slided in the sliding slot end of part.
Wherein, the fixing piece is the rivet being mounted in the pilot hole, the end that the rivet is positioned in the chute
Portion side is arranged with gum cover, and the outer diameter of the gum cover is greater than the width dimensions of the sliding slot.
Wherein, the trench bottom of the sliding slot is pasted with foam.
Wherein, the sliding slot extends to the other end by one end of the connecting pin, and the both ends of the sliding slot are equipped with circle
Arc cell wall；The pilot hole is located on the nut of the bolt, and the nut, which is equipped with, to be led in the connecting pin from described
The escape groove that can be rotated by 90 ° around the rivet when being extracted out in hole.
Wherein, first connector is ring structure, and second connector is and the first connector shape phase
Same lid-like, first connector are set in the outside of second connector, and the Quick-dismantle component is along described first
The circumferential direction of connector and second connector is at least provided with two.
Wherein, the position that the inside of first connector corresponds to the threaded hole is axially arranged with guide groove, and described second
The gib block matched with the guide groove is axially arranged on the outside of connector, the pin hole is located on the gib block.
Wherein, the first connector outer sheath is equipped with cricoid third connector, corresponds to institute on the third connector
The position for stating threaded hole is equipped with the via hole passed through for the bolt.
Wherein, the upper end of the third connector, which is equipped with, extends to axle center and offsets with the lateral surface of first connector
Edge, the lateral surface that the hole wall of the threaded hole protrudes first connector extends to the inside of the third connector
Face, the position that the threaded hole is corresponded on the edge are equipped with evacuation notch.
A kind of unmanned plane is connected between the fuselage body and carry of the unmanned plane by above-mentioned Quick Release attachment device, institute
The fuselage body for stating unmanned plane is connect by fastener with first connector, and the carry passes through fastener and described second
Connector connection.
After above-mentioned technical proposal, the beneficial effects of the utility model are:
Since the utility model Quick Release attachment device includes the first connector and second to be linked together by Quick-dismantle component
Connector；Quick-dismantle component includes bolt, and bolt is equipped with the through-hole axially penetrated through, and sliding is equipped with connecting pin, connecting pin in through-hole
Both ends stretch out through-hole；It is radially provided with the pilot hole of connection through-hole on bolt, is equipped in pilot hole and connects in no external force pull
The fixing piece that connecting pin can be fixed on when outbound in through-hole；First connector is equipped with threaded hole, and bolt thread is assemblied in
In threaded hole；The position that threaded hole is corresponded on second connector is equipped with pin hole, and the end of connecting pin is inserted into pin after stretching out bolt
In hole.When the first connector of progress is connect for the first time with the second connector, first connecting pin is inserted into the through-hole of bolt, will be consolidated
Determine part to be installed in pilot hole, connecting pin can slide axially in through-hole under the pull effect of external force at this time, without outer masterpiece
Used time fixing piece can fix connecting pin, prevent it from sliding in the axial direction, and Quick-dismantle component is completed.Then bolt is filled
It is fitted in the threaded hole of the first connector, takes out connecting pin outward, not fully extract out, as shown in fig. 6, by the second connector
Pin hole is corresponding with the threaded hole of the first connector, and then connecting pin is fully inserted into bolt, and the end of connecting pin is pierced by spiral shell
It will be inserted into pin hole after bolt, the second connector and the first connector will be linked together.To by the first connector and second
When connector is split, it is only necessary to the two can be separated to connecting pin extraction, also only need to pull and push connecting pin just when being again coupled to
It may be implemented, not need that the dismounting that the first connector is connect with second, time saving province can be quickly finished by external tool
Power, it is convenient and efficient.
Due to using above-mentioned Quick Release attachment device to connect between the fuselage body and carry of the utility model unmanned plane, thus
It does not need by external tool, it will be able to carry is quickly dismounted, it is time saving and energy saving, it is convenient and efficient.
In conclusion the utility model Quick Release attachment device and the unmanned plane equipped with the device solve in the prior art without
The dismounting of man-machine carry is complicated, time-consuming and laborious technical problem, the utility model Quick Release attachment device and nobody equipped with the device
Machine is not needed by external tool, can quickly dismount carry, time saving and energy saving, convenient and efficient.
Detailed description of the invention
Fig. 1 is the decomposition texture schematic diagram of the utility model Quick Release attachment device；
Fig. 2 is the constitutional diagram of Fig. 1；
Fig. 3 is the line A-A cross-sectional view of Fig. 2；
Fig. 4 is the line B-B cross-sectional view of Fig. 2；
Fig. 5 is the portion the C enlarged drawing of Fig. 4；
Fig. 6 is the status diagram when connecting pin of the utility model Quick Release attachment device is transferred to；
Fig. 7 is the status diagram after the connecting pin of the utility model Quick Release attachment device is transferred to and is rotated by 90 °；
Fig. 8 is the top view of Fig. 7；
Fig. 9 is the partial structural diagram of the utility model unmanned plane；
In figure: 10, the first connector, 12, mounting portion, the 120, first mounting hole, 14, guide groove, 16, threaded hole, 18, mark
Know slot, the 20, second connector, the 22, second mounting hole, 24, gib block, 26, pin hole, 28, land, 280, boss, 30, third company
Fitting, 32, edge, 320, evacuation notch, 34, via hole, 40, Quick-dismantle component, 42, bolt, 420, pilot hole, 422, escape groove,
44, connecting pin, 440, pin handle, 442, pin rod, 444, sliding slot, 460, rivet, 462, gum cover, 48, foam, 50, fuselage fixed plate,
60, PTZ camera, 62, holder mounting hole, 70, mounting screw, 100, Quick Release attachment device.
Specific embodiment
With reference to the accompanying drawings and examples, the utility model is further described.
Orientation shown in attached drawing is subject in the orientation being related in this specification, only represents opposite positional relationship, not generation
The absolute positional relationship of table.
Embodiment one:
As shown in Figure 1, Figure 2, Fig. 3 and Fig. 4 is jointly shown, a kind of Quick Release attachment device, including is connected to one by Quick-dismantle component 40
The first connector 10 and the second connector 20 risen.The first connector 10 is ring structure, the second connector in present embodiment
20 be lid-like identical with 10 shape of the first connector, and further, the first connector 10 is annulus in present embodiment
Structure, the second connector 20 are round lid-like.First connector 10 is set in the outside of the second connector 20, sets with one heart
Set, the upper end of the first connector 10 is equipped with multiple radially-protruding ear shaped mounting portions 12, mounting portion 12 be equipped with for to even
The lower end of the first mounting hole 120 that connection mechanism (fuselage of such as unmanned plane) is connected, the second connector 20 is equipped with radially protruding
The lower end of land 28, the first connector 10 is located in land 28, the upper end end cap of the second connector 20 be equipped with for to even
The second mounting hole 22 that connection mechanism (such as carry) is connected.Week of the Quick-dismantle component 40 along the first connector 10 and the second connector 20
To setting, in order to improve the stability of connection, the preferred Quick-dismantle component 40 of present embodiment is equipped at least two, further preferably respectively
40 spaced set of Quick-dismantle component, present embodiment are set there are two for by Quick-dismantle component 40, and two Quick-dismantle components 40 connect along first
The axle center of fitting 10 and the second connector 20 is symmetrical arranged.
It should be noted that the structure of the first connector and the second connector is designed according to bindiny mechanism, it is above-mentioned
Ring structure be only the present embodiment a kind of specific embodiment, the knot of the first connector and the second connector in practical application
Structure is not limited to above-mentioned ring structure, can also be that plate structure, U-shaped structure, L-shaped structure, T-shaped structure etc. can be with, and
First connector is also not necessarily identical as the shape of the second connector, as long as it can be realized the connection of the two, while
It is not limited to circular ring structure, the side's of can also be ring or polygonal ring shape, the present embodiment does not limit the structure of connector
System.
As shown in Figure 1, Figure 2 and Fig. 5 is jointly shown, and Quick-dismantle component 40 includes bolt 42, and bolt 42 is logical equipped with what is axially penetrated through
Hole, the interior sliding of through-hole are equipped with connecting pin 44, and through-hole is stretched out at the both ends of connecting pin 44, and connecting pin 44 is located at the nut of bolt 42
One end is equipped with the pin handle 440 that size is greater than through-hole aperture, i.e. connecting pin 44 includes the pin handle 440 and pin rod 442 being wholely set, pin
Bar 442 is slidably arranged in through-hole, and pin handle 440 is located on the outside of through-hole, for holding when assembly crewman's pull connecting pin 44.Connecting pin
44 other end stretches out bolt 42, i.e. the end of the pin rod 442 of connecting pin 44 is connected by the screw rod of through hole stretching bolt 42
The length of pin 44 is greater than the length of bolt 42.The pilot hole 420 of connection through-hole, peace in pilot hole 420 are radially provided on bolt 42
Equipped with connecting pin 44 can be fixed on to the fixing piece in through-hole in no external force pull connecting pin 44, i.e. connecting pin 44 only exists
It can be slided in through-hole under external force pull, in no external force pull, connecting pin 44 will not slide axially in through-hole.
As shown in Figure 1, Figure 2 and Fig. 3 is jointly shown, and the first connector 10 is equipped with threaded hole 16, threaded hole in present embodiment
16 extend radially through the side wall of the first connector 10, and 42 Screw assembly of bolt is in threaded hole 16.Spiral shell is corresponded on second connector 20
The position of pit 16 is equipped with pin hole 26, and the size of the pin rod 442 in the aperture and connecting pin 44 of pin hole 26 is adapted, pin rod 442
End is inserted into pin hole 26 after stretching out bolt 42, so that the first connector 10 and the second connector 20 be linked together.
As Fig. 1 and Fig. 4 jointly shown in, connecting pin 44 is equipped with axially extending sliding slot 444, sliding slot in present embodiment
444 set there are two, two sliding slots 444 are symmetricly set on the two sides of connecting pin 44, the corresponding pilot hole 420 on bolt 42
There are two setting relatively, a fixing piece is respectively installed, the end of two fixing pieces is located at corresponding sliding slot in two pilot holes 420
In 444, when there is external force pull connecting pin 44, the end of fixing piece is slided in sliding slot 444, in no external force pull connecting pin
When, fixing piece is stuck in sliding slot 444, can prevent connecting pin 44 from sliding in the axial direction.
As Fig. 1 and Fig. 5 jointly shown in, preferred fixing piece is the rivet being mounted in pilot hole 420 in present embodiment
460, one end of rivet 460 is located in sliding slot 444, and rivet 460 is located at this one end side in sliding slot 444 and is arranged with gum cover 462,
The size of its outer diameter is greater than the width dimensions of sliding slot 444 after gum cover 462 is set on rivet 460, i.e., the cell wall of sliding slot 444 is to glue
Set 462 plays the role of an extruding, and gum cover 462 and sliding slot 444, which are formed, to be interference fitted, thus in no external force pull connecting pin 44
Connecting pin 44 can be fixed in through-hole, prevent it from sliding axially, guarantee the first connector 10 and the second connector 20
Between connective stability.Further preferred gum cover 462 is hard rubber set to present embodiment, can in pull connecting pin 44
There is better feel；Rivet 460 is snap rivet, and the semicircle head end of rivet 460 is located in sliding slot 444, and 462 sets of gum cover half
On rivet bar on rear side of round end, the depth of sliding slot 444 is greater than the height of cup head, so that 462 part of gum cover is located at sliding slot 444
It is interior.
It should be noted that the structure of above-mentioned fixing piece is the preferred structure of present embodiment, it is able to achieve in practical application
The structure of this function is more than above-mentioned structure, can also be the elastic card bead being mounted in pilot hole or screw thread peace
Threaded post is screwed out in pull connecting pin, screws in threaded post when needing to be fixedly connected pin by the threaded post in pilot hole
Withstand connecting pin.This two kinds of structures are the prior art, therefore are no longer described in detail in the present specification, and the present embodiment is to fixation
The structure of part and with no restriction.
As Fig. 1 and Fig. 5 jointly shown in, the trench bottom of two sliding slots 444 is pasted with foam 48, i.e., the end of rivet 460 with
Foam 48 is in contact, and foam 48 is capable of increasing the frictional force between rivet 460 and connecting pin 44, can further prevent from connecting
Pin 44 slides axially in the case where no external force pull.
Such as Fig. 1 and Fig. 5, sliding slot 444 extends to the other end by one end of connecting pin 44, and the both ends of sliding slot 444 are equipped with
Arc-shaped cell wall, i.e. sliding slot 444 do not run through connecting pin 44, arc-shaped cell wall and the gum cover 462 positioned at 444 both ends of sliding slot
Periphery is adapted, and can play the role of limit to rivet 460.
As Fig. 1, Fig. 5, Fig. 6, Fig. 7 and Fig. 8 jointly shown in, bolt 42 is arranged in present embodiment preferred fit hole 420
Be additionally provided on nut, on nut connecting pin 44 by out of through-hole extract out when can around the escape groove 422 that rivet 460 is rotated by 90 °,
When connecting pin 44 is inserted into through-hole, pin handle 440 is located in escape groove 422.Nut is hollow annular i.e. in present embodiment
The ring internal diameter of structure, nut is greater than the aperture of through-hole, that is, a counter sink has been opened on bolt 42, the big hole location of counter sink
In nut position, the aperture of counter sink is located at screw position, and through-hole is the aperture of counter sink, is equipped with two relatively on the ring of nut
A notch, this two notch together form escape groove 422, the center line of escape groove 422 and two pilot holes 420 in present embodiment
Axis line in cross-shaped, and intersection point is overlapped with the axle center of bolt 42.
As Fig. 1 and Fig. 4 jointly shown in, the position that the inside of the first connector 10 corresponds to threaded hole 16 is axially arranged with guide groove
14, the outside of the second connector 20 is axially arranged with the gib block 24 matched with guide groove 14, and pin hole 26 is located on gib block 24.
The setting of guide groove 14 and gib block 24 can play positioning action in assembly, reduce assembly difficulty, improve assembly efficiency, together
When can play the role of the X of the first connector 10 and the second connector 20 and positioned to Y-direction.
As shown in Figure 1, Figure 2 and Fig. 4 is jointly shown, and the outside of the first connector 10 is also arranged with cricoid third connector 30,
The position that threaded hole 16 is corresponded on third connector 30 is equipped with the via hole 34 passed through for bolt 42.The upper edge of first connector 10
The position of upper corresponding threaded hole 16 is equipped with a logo slot 18, and logo slot 18 is when assembling the first connector 10 and third connector 30
Mark action is played, can be quickly directed at via hole 34 with threaded hole 16.The setting of third connector 30 can enhance connection
The intensity of device can increase the length of bolt 42, improve the reliability of attachment device.
As Fig. 1 and Fig. 3 jointly shown in, the upper end of third connector 30 be equipped with extend to axle center and with the first connector 10
The edge 32 that lateral surface offsets, the hole wall of threaded hole 16 protrude the lateral surface of the first connector 10 and extend to third connector 30
Medial surface, the position that threaded hole 16 is corresponded on edge 32 is equipped with the evacuation notch 320 that threaded hole 16 can be avoided in assembly.
The protrusion setting structure of threaded hole 16 can increase the length of threaded hole 16, to increase the company of bolt 42 and the first connector 10
The stability of connection can be improved in spreading degree.The setting at edge 32 can reduce between the first connector 10 and third connector 30
Fit-up gap, can be improved the stability of attachment device.
As Fig. 1 and Fig. 3 jointly shown in, the outside of the land 28 of the second connector 20 correspond to gib block 24 position be equipped with it is convex
The side of platform 280, boss 280 is in contact with the medial surface of 30 lower end of third connector, can equally play the second connection of reduction
Fit-up gap between part 20 and third connector 30 is conducive to the stability for improving attachment device.
Embodiment two:
As shown in figure 9, a kind of unmanned plane, originally passes through Quick Release described in embodiment one between man-machine fuselage body and carry
Attachment device 100 connects, and the fuselage body of unmanned plane is connect with the first connector 10 (referring to Fig. 1) by fastener, and carry is logical
Fastener is crossed to connect with the second connector 20 (referring to Fig. 1).
As shown in figure 9, connection type is described in detail so that carry is PTZ camera as an example in present embodiment, it is practical
The Quick Release attachment device of middle the utility model can be also used for the connection between the fuselage body of unmanned plane and bracket or cantilever, this
The utility model Quick Release can be connected dress without making creative work according to the description of this specification by field technical staff
In the connection for setting the fuselage for being applied to unmanned plane and bracket or cantilever, therefore the fuselage body about unmanned plane and bracket or cantilever
This will not be detailed here for the specific embodiment of connection.
As Fig. 1 and Fig. 9 jointly shown in, fuselage fixed plate 50 is installed on the fuselage body of unmanned plane in present embodiment,
Fuselage fixed plate 50 is fixedly connected by mounting screw 70 with the first mounting hole 120 on the first connector 10, PTZ camera
PTZ camera 60 be equipped with holder mounting hole 62 compatible with the second mounting hole 22 on the second connector 20, when assembly
The second mounting hole 22 and holder mounting hole 62 are passed through by PTZ camera and the second connector by fastener (not shown)
It is fixedly connected, to realize the fuselage body of unmanned plane and the connection of PTZ camera.
As Fig. 1, Fig. 3, Fig. 5, Fig. 6, Fig. 7, Fig. 8 and Fig. 9 jointly shown in, specific assemble flow is as follows:
In first assembly,
Step 1: the first connector 10 is linked together by mounting screw 70 with fuselage fixed plate 50.
Step 2: foam 48 is pasted into sliding slot 444, two sides is pasted altogether；Connecting pin 44 is inserted into the through-hole of bolt 42, note
Meaning not be fully inserted into bottom at this time；Gum cover 462 is inserted on rivet 460, rivet 460 is tensed using riveting gun at this time, by rivet 460
It is mounted in pilot hole 420 with gum cover 462, at this point, connecting pin 44 can be in the through-hole of bolt 42 under the pull effect of external force
It slides axially.
Step 3: 30 sets of third connector are attached on the first connector 10, pay attention to for via hole 34 being aligned with logo slot 18,
Guarantee that via hole 34 is overlapped with 16 axle center of threaded hole.
Step 4: by the installation to via hole 34 and threaded hole 16 of bolt 42, by the first connector 10 and third connector 30
It links together.
The assembled bolt 42 of step 2 is initially passed through into via hole 34, after be threaded into hole 16, will will be even when being screwed into bolt
It draws outside outbound 44 in maximum travel position shown in fig. 6, is then rotated down 90 °, make to change in longitudinal connecting pin 44 originally
Direction rotates in a circumferential direction to transverse direction as shown in fig. 7, connecting pin 44 can be equivalent to Simple spanner at this time, and bolt 42 can be made quick
And what is fastened locks the first connector 10 and third connector 30.
Step 5: connecting pin 44 is threaded to position shown in Fig. 6 again, installation at this time is connected with the second connection of PTZ camera
Part 20, by the position of the logo slot 18 on 24 the first connector of aligned in position 10 of gib block of the second connector 20, by gib block
24 are inserted into guide groove 14, and the second connector 20 is assembled in the first connector 10.
Step 6: connecting pin 44 is directly pushed into the through-hole of bolt 42, the end of connecting pin 44 is inserted into second at this time
In pin hole 26 on connector 20, the first installation of the PTZ camera of unmanned plane is so far completed.
It only needs connecting pin 44 dialing out to position shown in fig. 6 out of bolt 42 if it is when splitting, it can be by second
Connector 20 is taken out out of first connector 10, so that PTZ camera be removed from unmanned plane；Similarly, when then will install
Only need to carry out above-mentioned step five and step 6, it is simple and convenient, it is no longer necessary to, can be quickly complete by external tool
It is time saving and energy saving at the dismounting of PTZ camera, it is convenient and efficient.
The name of the first connector, the second connector and third connector that are related in this specification is intended merely to distinguish
Three does not represent positional relationship, assemble sequence etc. between three.
The utility model is not limited to above-mentioned specific embodiment, and those skilled in the art visualize from above-mentioned
Hair, without creative labor, the various transformation made are all fallen within the protection scope of the utility model.
Claims (10)
1. Quick Release attachment device, which is characterized in that
Including the first connector and the second connector to be linked together by Quick-dismantle component；
The Quick-dismantle component includes bolt, and the bolt is equipped with the through-hole axially penetrated through, and sliding is equipped with connection in the through-hole
Pin, the through-hole is stretched out at the both ends of the connecting pin；
It is radially provided with the pilot hole for being connected to the through-hole on the bolt, is equipped in the pilot hole described in no external force pull
The fixing piece that the connecting pin can be fixed on when connecting pin in the through-hole；
First connector is equipped with threaded hole, and the bolt thread is assemblied in the threaded hole；
The position that the threaded hole is corresponded on second connector is equipped with pin hole, and the bolt is stretched out in the end of the connecting pin
After be inserted into the pin hole.
2. Quick Release attachment device according to claim 1, which is characterized in that the connecting pin is equipped with axially extending cunning
Slot, when there is connecting pin described in external force pull, the end of the fixing piece is slided in the sliding slot.
3. Quick Release attachment device according to claim 2, which is characterized in that the fixing piece is to be mounted on the pilot hole
Interior rivet, the end side that the rivet is positioned in the chute are arranged with gum cover, and the outer diameter of the gum cover is greater than institute
State the width dimensions of sliding slot.
4. Quick Release attachment device according to claim 3, which is characterized in that the trench bottom of the sliding slot is pasted with foam.
5. Quick Release attachment device according to claim 3, which is characterized in that the sliding slot is prolonged by one end of the connecting pin
The other end is extended to, and the both ends of the sliding slot are equipped with arc-shaped cell wall；The pilot hole is located on the nut of the bolt, institute
It states nut and is equipped with the escape groove that can be rotated by 90 ° around the rivet when the connecting pin is extracted out out of described through-hole.
6. Quick Release attachment device according to any one of claims 1 to 5, which is characterized in that first connection
Part is ring structure, and second connector is lid-like identical with the first connector shape, first connection
Part is set in the outside of second connector, week of the Quick-dismantle component along first connector and second connector
To at least provided with two.
7. Quick Release attachment device according to claim 6, which is characterized in that described in the inside of first connector is corresponding
The position of threaded hole is axially arranged with guide groove, is axially arranged on the outside of second connector and leads with what the guide groove matched
To item, the pin hole is located on the gib block.
8. Quick Release attachment device according to claim 6, which is characterized in that the first connector outer sheath is equipped with ring-type
Third connector, the position that the threaded hole is corresponded on the third connector is equipped with the via hole passed through for the bolt.
9. Quick Release attachment device according to claim 8, which is characterized in that the upper end of the third connector is equipped with to axis
The hole wall at the edge that the heart extends and offsets with the lateral surface of first connector, the threaded hole protrudes first connector
Lateral surface extend to the medial surface of the third connector, the position that the threaded hole is corresponded on the edge is equipped with evacuation and lacks
Mouthful.
10. unmanned plane, which is characterized in that pass through any power of claim 1 to 9 between the fuselage body and carry of the unmanned plane
Benefit requires the Quick Release attachment device connection, and the fuselage body of the unmanned plane is connected by fastener and first connector
It connects, the carry is connect by fastener with second connector.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821187982.XU CN208665546U (en) | 2018-07-25 | 2018-07-25 | Quick Release attachment device and unmanned plane equipped with the device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821187982.XU CN208665546U (en) | 2018-07-25 | 2018-07-25 | Quick Release attachment device and unmanned plane equipped with the device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208665546U true CN208665546U (en) | 2019-03-29 |
Family
ID=65829664
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821187982.XU Active CN208665546U (en) | 2018-07-25 | 2018-07-25 | Quick Release attachment device and unmanned plane equipped with the device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208665546U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110561496A (en) * | 2019-08-28 | 2019-12-13 | 龙岩学院 | connecting device for quick mounting and dismounting of flying manipulator |
| CN113998131A (en) * | 2021-11-26 | 2022-02-01 | 昌河飞机工业（集团）有限责任公司 | Universal hanging rack for helicopter ventral |
-
2018
- 2018-07-25 CN CN201821187982.XU patent/CN208665546U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110561496A (en) * | 2019-08-28 | 2019-12-13 | 龙岩学院 | connecting device for quick mounting and dismounting of flying manipulator |
| CN110561496B (en) * | 2019-08-28 | 2024-03-19 | 龙岩学院 | A connecting device for flying manipulator installs and dismantles fast |
| CN113998131A (en) * | 2021-11-26 | 2022-02-01 | 昌河飞机工业（集团）有限责任公司 | Universal hanging rack for helicopter ventral |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208665546U (en) | Quick Release attachment device and unmanned plane equipped with the device | |
| US20120005858A1 (en) | Wheel assembly with single fixing arm | |
| CN204646924U (en) | A kind of spring detent | |
| CN103749071B (en) | The rotatory and extending device of grass-mowing machine | |
| CN205499230U (en) | Bassinet T dismantles structure to group | |
| CN206129848U (en) | Bolt and fixed knot construct | |
| CN205639226U (en) | From taking fixed wrench type bolt | |
| CN209260832U (en) | A kind of Fast Installation structure of tap | |
| CN104421264B (en) | Telescopic mechanism and blade-rotating fan comprising same | |
| CN203468132U (en) | Heaven and earth column adopting telescopic pipe structure | |
| CN202953167U (en) | Unmanned aerial vehicle with wing inserted fixing device | |
| CN208702851U (en) | A kind of attachment device between two bar | |
| CN104858827B (en) | Spanner clamping and drawing device | |
| CN201115946Y (en) | Covering and fixing structure of adapting rod | |
| CN203986398U (en) | A kind of easy mounting shoe buckle | |
| CN210599697U (en) | Novel clamp spring for mounting turbocharger pressure shell | |
| CN204363365U (en) | A kind of stainless steel cabinet of foolproof installation | |
| CN203697860U (en) | Caster with detaching structure | |
| CN207039240U (en) | Using the mobile device of more power technologies | |
| CN205166850U (en) | Piston uide bushing device | |
| CN205093086U (en) | Flower hoe that conveniently carries | |
| CN203902286U (en) | Transmission operating lever and automobile | |
| CN203880047U (en) | Rapidly-riveting device for automotive transmission label | |
| CN205438429U (en) | Valve seat mounting device | |
| CN207336824U (en) | ST optical connector assembling tools |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |