CN209023148U - A kind of device for quickly disassembling applied to unmanned plane carry - Google Patents
A kind of device for quickly disassembling applied to unmanned plane carry Download PDFInfo
- Publication number
- CN209023148U CN209023148U CN201821688582.7U CN201821688582U CN209023148U CN 209023148 U CN209023148 U CN 209023148U CN 201821688582 U CN201821688582 U CN 201821688582U CN 209023148 U CN209023148 U CN 209023148U
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- CN
- China
- Prior art keywords
- unmanned plane
- fixed
- mounting hole
- quickly disassembling
- fixed lobe
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Abstract
The utility model relates to a kind of unmanned plane carry fields, specially a kind of device for quickly disassembling applied to unmanned plane carry, including be installed on the body of unmanned plane connector and damping, be fixed on connector circumferential direction and be set in distance fixed lobe, be fixedly connected with carry installation part, be fixed on installation part and be rotationally connected with the pivot protrusion of fixed lobe, locking piece, fixed lobe and pivot protrusion side have coaxial the first mounting hole and the second mounting hole, and locking piece is arranged in the first mounting hole and the second mounting hole.Threaded connection in the prior art is replaced by mortise-tenon joint, not only convenient disassembly and long service life.
Description
Technical field
The utility model relates to a kind of unmanned plane carry fields, and in particular to a kind of fast dismounting applied to unmanned plane carry
It sets.
Background technique
UAV is to utilize radio robot and the process control provided for oneself referred to as " unmanned plane " (" UAV ")
The not manned vehicle of device manipulation.The purposes of unmanned plane depends on the carry module of unmanned plane, and the different module of carry can be with
Complete different tasks.Carry video camera, the achievable tasks such as take photo by plane；Carry infrared camera, achievable power-line patrolling etc. are appointed
Business；Carry remote sensing equipment, achievable mapping task.If single task role, a frame unmanned plane can be completed, if task is cumbersome
Need how carry disparate modules quickly replace module just at stubborn problem when meeting different demands.
Conventional method is all that unmanned plane and carry are linked together by bolt, due to needing to be replaced frequently different extensions
It carries, so bolt needs often disassembly, due to misoperation in disassembly process, easily leads to stripped thread phenomenon, so that hanging
It carries and is not connected firmly with the body of unmanned plane, during unmanned plane during flying, carry may be from falling from high altitude.
Utility model content
In view of the deficienciess of the prior art, the purpose of this utility model is to provide a kind of applied to unmanned plane carry
Device for quickly disassembling can quickly and easily replace carry.
To achieve the above object, the utility model provides following technical solution:
A kind of device for quickly disassembling applied to unmanned plane carry includes the connector and damping machine for being installed on the body of unmanned plane
Structure, the installation part being fixedly connected with carry, is fixed on installation part at the fixed lobe for being fixed on connector circumferential direction and being set in distance
And it is rotationally connected with the pivot protrusion of fixed lobe, locking piece, fixed lobe and pivot protrusion side have coaxial
One mounting hole and the second mounting hole, locking piece are arranged in the first mounting hole and the second mounting hole.
By using above-mentioned technical proposal, when carry to be installed, pivot protrusion rotates on fixed lobe, when the second peace
It fills hole and when coaxial the first mounting hole, locking piece is inserted into the first mounting hole and the second mounting hole, so that pivot protrusion and consolidating
Determine protrusion to be fixed together, can so not have to bolt can be such that carry is installed on the body of unmanned plane, extend unmanned plane and hang
The service life of the device for quickly disassembling of load.
The utility model is further arranged to: the limit convex abutted with fixed lobe radial end face is fixed on installation part
It rises.
By using above-mentioned technical proposal, fixed lobe and pivot protrusion are relatively rotated, when fixed lobe radial end face with
When retention bead end face abuts, fixed lobe will not be rotated further by, so that the first mounting hole is corresponding with the second mounting hole, locking
Part can pass through the first mounting hole and the second mounting hole, facilitate installation.
The utility model is further arranged to: locking piece is the self-locking type index pin for being threadedly connected to fixed lobe.
By using above-mentioned technical proposal, locking piece is the model of Shenzhen Wei Qi precision machinery Co., Ltd production
The self-locking type index pin of VCN220, self-locking type index pin successively includes button, the fixed section being threadedly coupled with the first mounting hole, interior
Glissile segment that is embedding and being slidably connected to fixed section, when fixed lobe to be locked and pivot protrusion, then release button, glissile segment are worn
If the second mounting hole；When to remove pivot protrusion from fixed lobe, then button is pulled out, glissile segment is received out of second mounting hole
It backs into fixed section, keeps under pull-out state, button is rotated by 90 °, then glissile segment can be made to keep retracted mode；Release lock
When determining state, need to only pull-out state kept to be rotated by 90 °.
The utility model is further arranged to: fixed lobe and pivot protrusion section are L-shaped.
By using above-mentioned technical proposal, when connecting pivot protrusion and fixed lobe, by the end face of fixed lobe and rotation
The end face of protrusion abuts, and realizes that pivot protrusion rotates on fixed lobe.
The utility model is further arranged to: fixed lobe and pivot protrusion are equipped at least three pairs, and locking piece is equipped with extremely
It is three few.
By using above-mentioned technical proposal, according to triangular form stability principle, three locking pieces enable to fixed lobe and
Pivot protrusion securely fixes together, without relatively rotating.
The utility model is further arranged to: being provided with lightening hole on connector and installation part.
By using above-mentioned technical proposal, so that device for quickly disassembling is realized lighting, avoid device for quickly disassembling overweight and influence nobody
The flight reappearance of machine.
The utility model is further arranged to: damping include the support plate being fixedly connected with the body of unmanned plane and
Shock absorber part, shock absorber part include the upper plate being fixedly connected with connector, the lower plate abutted with upper end face of support plate, respectively with upper plate and
The first elastic component that lower plate is fixedly connected.
By using above-mentioned technical proposal, when unmanned plane produces strong motion in flight course, vibration can first conduct
To the support plate being attached thereto, then the lower plate being conducted on shock-absorbing support plate, the first elastic component due to elastic force, because
This can be good at the vibration for filtering out unmanned plane generation, so that vibration is not conducted to the upper plate being carried on elastic component again, makes
The vibration that unmanned plane generates will not generate vibration influence to carry object, flexible connection be realized between carry object and unmanned plane, very well
The flight job requirements for meeting carry object.
The utility model is further arranged to: support plate is provided with shock relieve vent, and lower plate lower end surface, which is fixed with, is embedded in damping
The damping protrusion in hole, shock relieve vent inner wall is circumferentially arranged with the second elastic component being fixedly connected respectively with shock relieve vent and damping protrusion.
By using above-mentioned technical proposal, the circumferential direction due to the second elastic component along shock relieve vent is arranged, so can be by nobody
The vibration of machine in the plane is filtered out by the second elastic component, and so that it will not pass to carry.
The utility model has the advantage that
1, unmanned plane and carry are fixed together by device for quickly disassembling, and the fixed lobe and pivot protrusion on device for quickly disassembling are adopted
It replaces being threadedly coupled with mortise-tenon joint, not only convenient disassembly and long service life；
2, connector and installation part are provided with lightening hole, mitigate the weight of device for quickly disassembling, and then reduce unmanned plane during flying process
In oil consumption or power consumption within the unit time；
3, the vibration that damping generates unmanned plane will not generate vibration influence to carry object, carry object and unmanned plane it
Between realize flexible connection, meet the flight job requirements of carry object well.
Detailed description of the invention
Fig. 1 is the schematic perspective view of the utility model；
Fig. 2 is the structural schematic diagram of the utility model fixed part；
Appended drawing reference: 1, connector；2, damping；3, fixed lobe；4, installation part；5, pivot protrusion；6, locking piece；
7, the first mounting hole；8, the second mounting hole；9, fixed part；10, rotation section；11, retention bead；12, lightening hole；13, support plate；
14, shock absorber part；15, upper plate；16, lower plate；17, the first elastic component；18, shock relieve vent；19, damping protrusion；20, the second elastic component；
21, button；22, fixed section；23, glissile segment；24, the first connecting column；25, the first threaded hole；26, the second connecting column；27, run through
Hole；28, bolt.
Specific embodiment
The utility model is described further referring to attached drawing.
As shown in Figure 1, a kind of device for quickly disassembling applied to unmanned plane carry includes being fixedly connected with the body of unmanned plane
Fixed part 9, be fixedly connected with carry and relative to fixed part 9 rotate rotation section 10, for locking fixed part 9 and rotation section 10
The locking piece 6 of relative position.
Rotation section 10 is rotated relative to fixed part 9, and carry drives rotation section 10 to rotate, and then can rotate and be assembled to fixed part
Rigging position on 9, locking piece 6 lock, and realize the installation of carry.Equally, carry can be de- from its rigging position by rotation
From, and then realize disassembly.
In conjunction with shown in Fig. 1 and 2, fixed part 9 includes successively from top to bottom damping 2, connector 1, is fixed on connector 1
Circumferential direction and three fixed lobes 3 being set in distance, 3 section of fixed lobe are L-shaped.Damping 2 includes the machine with unmanned plane
The support plate 13 and shock absorber part 14 that body is fixedly connected, shock absorber part 14 include the upper plate 15 being fixedly connected with connector 1 and support plate
The lower plate 16 of 13 upper surfaces abutting, the first elastic component 17 being fixedly connected respectively with upper plate 15 and lower plate 16.As shown in Fig. 2, branch
Fagging 13 is provided with shock relieve vent 18, and 16 lower end surface of lower plate is fixed with the damping protrusion 19 for being embedded in shock relieve vent 18,18 inner wall of shock relieve vent
Circumferentially arranged with the second elastic component 20 being fixedly connected respectively with shock relieve vent 18 and damping protrusion 19.First elastic component 17 is damping
Ball, the second elastic component 20 are spring.
As shown in Figure 1, the first connecting column 24 is equipped between the body bottom end (not shown) and support plate 13 of unmanned plane,
First connecting column, 24 both ends are provided with the first threaded hole 25, and the body bottom end of support plate 13 and unmanned plane is provided with and the first threaded hole 25
The first coaxial connecting hole (not shown), bolt 28 pass through the first connecting hole and are threadedly coupled with the first threaded hole 25.So
The body bottom end of support plate 13 and unmanned plane is fixed together.As shown in Fig. 2, being equipped with the between upper plate 15 and connector 1
Two connecting columns 26, lower plate 16 are provided with the through hole 27 with 26 clearance fit of the second connecting column, and 26 both ends of the second connecting column are provided with
Two threaded hole (not shown)s, connector 1 and upper plate 15 are provided with second connecting hole coaxial with the second threaded hole and (do not show in figure
Out), bolt 28 passes through the second connecting hole and is threadedly coupled with the second threaded hole.Such upper plate 15 and connector 1 are fixedly connected on one
It rises.
As shown in Figure 1, vibration, which can be first conducted to, to be attached thereto when unmanned plane produces strong motion in flight course
Support plate 13, then the lower plate 16 being conducted on shock-absorbing support plate 13, the first elastic component 17 is due to elastic force, energy
The vibration of enough vertical directions for filtering out unmanned plane generation well, since the second elastic component 20 is set along the circumferential direction of shock relieve vent 18
It sets, so can filter out the vibration of unmanned plane in the plane by the second elastic component 20, be conducted to vibration will not again and hold
The upper plate 15 being loaded on elastic component, make unmanned plane generate vibration will not to carry object generate vibration influence, carry object and nobody
Flexible connection is realized between machine, meets the flight job requirements of carry object well.
As shown in Figure 1, between rotation section 10 includes the installation part 4 being fixedly connected with carry, is fixed on 4 circumferential direction of installation part and is in
Every three pivot protrusions 5 of setting, 5 section of pivot protrusion is L-shaped.It is fixed on installation part 4 and is supported with 3 radial end face of fixed lobe
The retention bead 11 connect.Fixed lobe 3 and 5 side of pivot protrusion have coaxial three pair of first mounting hole 7 and the second peace
Hole 8 is filled, is equipped with internal screw thread in the first mounting hole 7.Locking piece 6 is the model of Shenzhen Wei Qi precision machinery Co., Ltd production
The self-locking type index pin of VCN220, self-locking type index pin successively includes button 21, the fixed section that is threadedly coupled with the first mounting hole 7
22, embed and be slidably connected to the glissile segment 23 of fixed section 22.
When carry to be installed, the end face of fixed lobe 3 is abutted with the end face of pivot protrusion 5, realizes that pivot protrusion 5 exists
It is rotated on fixed lobe 3.When 3 radial end face of fixed lobe is abutted with 11 end face of retention bead, fixed lobe 3 will not turn again
Dynamic, so that the first mounting hole 7 and the second mounting hole 8 are coaxial, release button 21, glissile segment 23 wears the second mounting hole 8；When will be from
When removing pivot protrusion 5 on fixed lobe 3, then button 21 is pulled out, glissile segment 23 is received out of second mounting hole 8 and backs into fixation
It in section 22, keeps under pull-out state, button 21 is rotated by 90 °, then glissile segment 23 can be made to keep retracted mode；Unlock state
When, need to only pull-out state kept to be rotated by 90 °.
Working principle: rotation section 10 is rotated relative to fixed part 9, and carry drives rotation section 10 to rotate, when 3 diameter of fixed lobe
When abutting to end face with 11 end face of retention bead, the first mounting hole 7 and the second mounting hole 8 are coaxial, release and 3 screw thread of fixed lobe
The button 21 of the self-locking type index pin of connection makes glissile segment 23 wear the second mounting hole 8, realizes the installation of carry.Pull out button
21, glissile segment 23 is received out of second mounting hole 8 backs into fixed section 22 and then realizes that carry can be quickly from unmanned plane
It disassembles.For cumbersome when carry is assembled and disassembled, user is able to achieve to the quick despatch of carry.
The above is only the preferred embodiment of the utility model, and the protection scope of the utility model is not limited merely to
Above-described embodiment, technical solution belonging to the idea of the present invention belong to the protection scope of the utility model.It should refer to
Out, for those skilled in the art, it is without departing from the principle of the utility model it is several improvement and
Retouching, these improvements and modifications also should be regarded as the protection scope of the utility model.
Claims (8)
1. a kind of device for quickly disassembling applied to unmanned plane carry, which is characterized in that the fast dismounting applied to unmanned plane carry
Connector (1) and damping (2) including the body bottom end that is installed on unmanned plane are set, connector (1) circumferential direction is fixed on and is in
Spaced fixed lobe (3), the installation part (4) being fixedly connected with carry are fixed on installation part (4) and are rotationally connected with solid
The pivot protrusion (5) of fixed protrusion (3), locking piece (6), fixed lobe (3) and pivot protrusion (5) side have coaxial the
One mounting hole (7) and the second mounting hole (8), locking piece (6) are arranged in the first mounting hole (7) and the second mounting hole (8).
2. a kind of device for quickly disassembling applied to unmanned plane carry according to claim 1, it is characterized in that: the installation part
(4) retention bead (11) abutted with fixed lobe (3) radial end face is fixed on.
3. a kind of device for quickly disassembling applied to unmanned plane carry according to claim 2, it is characterized in that: the locking piece
It (6) is the self-locking type index pin for being threadedly connected to fixed lobe (3).
4. a kind of device for quickly disassembling applied to unmanned plane carry according to claim 2, it is characterized in that: the fixed lobe
(3) and pivot protrusion (5) section is L-shaped.
5. a kind of device for quickly disassembling applied to unmanned plane carry according to claim 1, it is characterized in that: the fixed lobe
(3) and pivot protrusion (5) is equipped at least three pairs, and locking piece (6) is equipped at least three.
6. a kind of device for quickly disassembling applied to unmanned plane carry according to claim 1, it is characterized in that: the connector
(1) and on installation part (4) it is provided with lightening hole (12).
7. a kind of device for quickly disassembling applied to unmanned plane carry according to claim 1, it is characterized in that: the damping
It (2) include the support plate (13) being fixedly connected with the body of unmanned plane and shock absorber part (14), shock absorber part (14) includes and connector
(1) upper plate (15) that is fixedly connected, the lower plate (16) abutted with support plate (13) upper surface, respectively with upper plate (15) and lower plate
(16) the first elastic component (17) being fixedly connected.
8. a kind of device for quickly disassembling applied to unmanned plane carry according to claim 7, it is characterized in that: the support plate
(13) it is provided with shock relieve vent (18), lower plate (16) lower end surface is fixed with the damping protrusion (19) for being embedded in shock relieve vent (18), shock relieve vent
(18) inner wall is circumferentially arranged with the second elastic component (20) being fixedly connected respectively with shock relieve vent (18) and damping raised (19).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821688582.7U CN209023148U (en) | 2018-10-17 | 2018-10-17 | A kind of device for quickly disassembling applied to unmanned plane carry |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821688582.7U CN209023148U (en) | 2018-10-17 | 2018-10-17 | A kind of device for quickly disassembling applied to unmanned plane carry |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209023148U true CN209023148U (en) | 2019-06-25 |
Family
ID=66906736
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821688582.7U Expired - Fee Related CN209023148U (en) | 2018-10-17 | 2018-10-17 | A kind of device for quickly disassembling applied to unmanned plane carry |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209023148U (en) |
-
2018
- 2018-10-17 CN CN201821688582.7U patent/CN209023148U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190625 Termination date: 20201017 |