CN207698007U - The second shock-damping connector of unmanned plane is identified applied to powder - Google Patents
The second shock-damping connector of unmanned plane is identified applied to powder Download PDFInfo
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- CN207698007U CN207698007U CN201721427379.XU CN201721427379U CN207698007U CN 207698007 U CN207698007 U CN 207698007U CN 201721427379 U CN201721427379 U CN 201721427379U CN 207698007 U CN207698007 U CN 207698007U
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- stationary plane
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Abstract
The utility model discloses a kind of the second shock-damping connectors identifying unmanned plane applied to powder, including：Second fixed component, second fixed component are fixedly connected across the 11st stationary plane with support cylinder, and second fixed component and the 11st stationary plane are mutually perpendicular to；Second compliant member, second compliant member are fixedly connected with second fixed component, monitor component, and the second compliant member moves between second fixed component and the monitor component；Wherein, second fixed component and second compliant member are mutually perpendicular to.Rigid connection in the prior art between support base and monitor component is substituted for flexible connection by the utility model, when realizing that unmanned plane carries out multi-angle or multi-pose flight in the air, the flexible connection between support base and monitor component will not be caused to wear, have the characteristics that maintenance cost is cheap and job safety performance is high.
Description
Technical field
The utility model belongs to technical field of safety protection, more particularly to a kind of to identify the second of unmanned plane applied to powder
Shock-damping connector.
Background technology
The great workshop in part in society often stores a large amount of valuable mechanical equipments, is especially provided with research and development base
Ground or research and development centre have further related to a large amount of know-how.For above-mentioned workshop, a kind of effective monitor mode is in nothing
Man-machine monitor component installed above (camera), and identity device of the installation with mark action are identified suspect,
Then it assists subsequent arresting work.
However, since unmanned plane flies dynamic uncertainty in the air, it is this directly that monitor component (camera) is hard
Property be mounted on when being fixed on the support base (including support cylinder and tripod) of uav bottom so that unmanned plane carries out in the air
When multi-angle or multi-pose flight, easily between support base (including support cylinder and tripod) and monitor component (camera)
Rigid connection cause to wear, maintenance cost it is relatively high and influence unmanned plane normal monitoring operation.
Utility model content
The utility model provides a kind of the second shock-damping connector applied to powder mark unmanned plane, to solve existing skill
Rigid connection in art between support base (including support cylinder and tripod) and monitor component (camera) easily causes abrasion skill
Art defect.
In order to solve the above technical problems, the utility model provides a kind of the second damping applied to powder mark unmanned plane
Connector, second shock-damping connector include：Second fixed component, second fixed component pass through the 11st stationary plane and
Support cylinder is fixedly connected, and second fixed component and the 11st stationary plane are mutually perpendicular to；Second compliant member, it is described
Second compliant member is fixedly connected with second fixed component, monitor component, and the second compliant member is fixed described second
It is moved between component and the monitor component；Wherein, second fixed component and second compliant member are mutually perpendicular to.
Optionally, second fixed component includes：Third fixing piece, one end of the third fixing piece pass through described the
11 stationary planes are fixedly connected with the support cylinder；The other end of the third fixing piece and second compliant member are fixed
Connection；One end of 4th fixing piece, the 4th fixing piece passes through the 11st stationary plane and the support cylinder to fix company
It connects；The other end of 4th fixing piece is fixedly connected with second compliant member.
Optionally, the third fixing piece is mutually perpendicular to the 11st stationary plane.
Optionally, the 4th fixing piece is mutually perpendicular to the 11st stationary plane.
Optionally, the third fixing piece and the 4th fixing piece are mutually parallel.
Optionally, second compliant member includes：Third movable plate；4th movable plate；Third flexible piece, the third
Flexible piece passes through the third movable plate and the 4th movable plate to be flexibly connected；4th flexible piece, the 4th flexible piece are worn
Cross the third movable plate and the 4th movable plate flexible connection；Wherein, the third movable plate is moved relative to the described 4th
Movable plate is removable.
Optionally, the third mobile edition and the 4th movable plate are mutually parallel.
Optionally, the third flexible piece is third spring.
Optionally, the 4th flexible piece is the 4th spring.
Optionally, the third fixing piece and the 4th fixing piece are located at the third flexible piece and the 4th flexibility
Between part.
The one or more technical solutions provided in the utility model embodiment, at least have the following technical effect that or excellent
Point：
The second shock-damping connector provided by the utility model applied to powder mark unmanned plane, by by the second fixed part
Part is fixedly connected across the 11st stationary plane with support cylinder, and second fixed component and the 11st stationary plane mutually hang down
Directly；The second compliant member and the second fixed component, monitor component are fixedly connected simultaneously, and the second compliant member is solid described second
Determine to move between component and the monitor component.This is allowed for support base in the prior art (including support cylinder and tripod)
Rigid connection between monitor component (camera) is substituted for flexible connection, realize unmanned plane carry out in the air multi-angle or
It, will not be to the flexibility between support base (including support cylinder and tripod) and monitor component (camera) even when person's multi-pose flight
It connects and causes to wear, have the characteristics that maintenance cost is cheap and job safety performance is high.
The above description is merely an outline of the technical solution of the present invention, in order to better understand the skill of the utility model
Art means, and being implemented in accordance with the contents of the specification, and in order to allow above and other purpose, feature of the utility model
It can be clearer and more comprehensible with advantage, it is special below to lift specific embodiment of the present utility model.
Description of the drawings
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is
Some embodiments of the utility model, for those of ordinary skill in the art, without creative efforts,
Other drawings may also be obtained based on these drawings.
Fig. 1 is the structural schematic diagram one that the utility model embodiment provides；
Fig. 2 is the structural schematic diagram two that the utility model embodiment provides.
Specific implementation mode
The second shock-damping connector provided by the utility model applied to powder mark unmanned plane, by by the second fixed part
Part is fixedly connected across the 11st stationary plane with support cylinder, and second fixed component and the 11st stationary plane mutually hang down
Directly；The second compliant member and the second fixed component, monitor component are fixedly connected simultaneously, and the second compliant member is solid described second
Determine to move between component and the monitor component.This is allowed for support base in the prior art (including support cylinder and tripod)
Rigid connection between monitor component (camera) is substituted for flexible connection, realize unmanned plane carry out in the air multi-angle or
It, will not be to the flexibility between support base (including support cylinder and tripod) and monitor component (camera) even when person's multi-pose flight
It connects and causes to wear, have the characteristics that maintenance cost is cheap and job safety performance is high.
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, the every other embodiment that those of ordinary skill in the art are obtained belong to what the present invention protected
Range；Involved "and/or" keyword wherein in this implementation, indicate and or two kinds of situations, in other words, the present invention is implemented
A and/or B mentioned by example, illustrate two kinds of A and B, A or B situations, describe three kinds of states present in A and B, as A and/
Or B, it indicates：It includes B to only include A not；It includes A to only include B not；Including A and B.
Meanwhile in the embodiment of the present invention, when component is referred to as " being fixed on " another component, it can be directly at another
On component or there may also be components placed in the middle.When a component is considered as " connection " another component, it can be direct
It is connected to another component or may be simultaneously present component placed in the middle.When a component is considered as " being set to " another group
Part, it can be set up directly on another component or may be simultaneously present component placed in the middle.Made in the embodiment of the present invention
Term " vertically ", " horizontal ", "left", "right" and similar statement are merely for purposes of illustration, and are not intended to
The limitation present invention.
In order to elaborate to the second shock-damping connector for being applied to powder mark unmanned plane that utility model provides, with
Support utility model technical problem to be solved, in the following, in embodiment provided by the utility model, first to being mounted with second
The powder mark unmanned plane of shock-damping connector elaborates, then during describing powder mark unmanned plane, further
Targetedly draw the second shock-damping connector provided by the utility model applied to the unmanned plane, with reach it is complete, clear,
Clear purpose.
- 2 are please referred to Fig.1, the powder mark unmanned plane that the utility model embodiment provides includes：First shock-damping connector 4,
Second shock-damping connector 5, drive component 1, ejection assemblies 2, support base 3, monitor component 6.In order to the utility model embodiment
The powder mark unmanned plane provided elaborates, and illustrates respectively into row information to each component part below.
For unmanned plane part, in the utility model embodiment, unmanned plane can be the nothing of any specific flight function
Man-machine, such as multi-rotor unmanned aerial vehicle, fixed-wing unmanned plane, unmanned helicopter etc., the utility model embodiment does not limit.
For earth station part, in the utility model embodiment, earth station has wireless communication function, for controlling nothing
Man-machine flight.
For 1 part of drive component, the driving component 1 includes：Charger 12, for powering；Driver 11, and it is described
Charger 12 connects；Receiver 13 is connect with the charger 12 and the driver 11 respectively, and is carried out with the earth station
Signal transmits；Figure passes device 14, is connect with the charger 12, and is carried out respectively with the monitor component 6 and the earth station
Signal transmits；First shell 15, the first shell 15 include the first stationary plane 151 and the second stationary plane 152；And the power supply
Device 12, the driver 11, the receiver 13 and the figure pass device 14 and are both secured in the first shell 15, described
First shell 15 is fixedly connected by first stationary plane 151 with first shock-damping connector 4；The first shell 15 is logical
Second stationary plane 152 is crossed to be fixedly connected with the support base 3.
Specifically, charger 12 can be supplying cell, for passing device 14 etc. to driver 11, receiver 13, figure
The equipment powered is needed to be powered, receiver 13 is the signal receiving device for having signal receiving function, and figure passes device 14
Respectively signal transmission is carried out with earth station.It is noted that figure, which passes device 14, can pass through signal transmitter-receiver 102 and ground
It is transmitted into row information at face station.The first stationary plane 151 and the second stationary plane 152 of the first shell 15 are two opposites.Institute
It states charger 12 to be fixed at first stationary plane 151, and the charger 12 is parallel with first stationary plane 151.
The driver 11 is fixed on second stationary plane 152, and the driver 11 and second stationary plane 152 are mutually flat
Row.The first shell 15 further includes：8th stationary plane 153 and the 9th stationary plane 154；Wherein, 153 He of the 8th stationary plane
The opposition distribution of 9th stationary plane 154, and it is located at the centre of first stationary plane 151 and second stationary plane 152, make
First stationary plane 151, second stationary plane 152, the 8th stationary plane 153 and the 9th stationary plane 154 is obtained to close
It encloses to form the rectangular first shell 15；The figure passes device 14 and is fixed on the 9th stationary plane 154；The driving
Device 11 is also fixed on the 8th stationary plane 153, and positioned at second stationary plane 152 and the 8th stationary plane 153
At angle position.First shock-damping connector 4 is fixedly connected across the first shell 15 with the charger 12.
In addition, on the 9th stationary plane 154 of first shell 15, it is additionally provided with electricity display screen 7, is connected with charger 12
It connects, is used for the remaining capacity of real-time display charger 12.
Further, the ejection assemblies 2 include：Second shell 21, the second shell 21 include third stationary plane 211
With the 4th stationary plane 212；The second shell 21 is fixed on by the third stationary plane 211 in the first shell 15；Powder
Last throwing arm 22 is fixed in the second shell 21, and is connect with the driver 11；And the driver 11 drive it is described
Powder throwing arm 22 carries out powderject；Go out powder chamber 23, it is described go out powder chamber 23 include the 5th stationary plane 231, the 6th stationary plane 232
With the 7th stationary plane 233, and it is described go out powder chamber 23 pass through the 5th stationary plane 231 and the 4th stationary plane 212 and fix and connect
Connect, it is described go out powder chamber 23 be fixedly connected with the first shell 15 by the 6th stationary plane 212, it is described go out powder chamber 23 pass through
7th stationary plane 233 is fixedly connected with the support base 3；Wherein, the powder that the powder throwing arm 22 sprays is by described
Go out powder chamber 23 to spray to target object.
Further include fan 24 it should be noted that in ejection assemblies 2, the fan 24 be fixed on it is described go out powder chamber 23
It is interior, and the blowing direction of the fan 24 with it is described go out the direction of dusting of powder chamber 23 it is identical.Preferably, the fan 24 is fixed
At the 6th stationary plane 232.The second shell 21 includes：Flour opening, the flour opening setting are fixed the described 4th
On face；It is described go out powder chamber 23 include：Powder entering hole 25 and powder injection hole 26, the powder entering hole are arranged on the 5th stationary plane, and
The powder entering hole is mutually connected with the flour opening.The powder injection hole be arranged it is described go out powder chamber end, and with it is the described 6th solid
It is fixed to be distributed in face of vertical.
Further, the support base 3 includes：Support cylinder 61, the support cylinder 61 include the tenth stationary plane 611,
11st stationary plane 612 and the 12nd stationary plane 613；The first shell 15 is fixed on institute by second stationary plane 152
It states on the tenth stationary plane 611；It is described go out powder chamber 23 be fixed on the tenth stationary plane 611 by the 7th stationary plane 233；
Second shock-damping connector 5 is fixed on the 11st stationary plane 612；Tripod 62, the tripod 62 are fixed on described
On 12 stationary planes 613.
In addition, first shock-damping connector 4 includes：First fixed component, first fixed component pass through described the
One stationary plane 151 is fixedly connected with the driver 11, and first fixed component and first stationary plane are mutually perpendicular to；
First compliant member, first compliant member are movably fixed in first fixed component so that the first flexible part
Part can be relatively moved relative to first fixed component.First fixed component includes：First fixing piece 411, described
One end of one fixing piece is fixedly connected across first stationary plane with the driver；The other end of first fixing piece and
First compliant member is fixedly connected；One end of second fixing piece 412, second fixing piece passes through first stationary plane
It is fixedly connected with the driver；The other end of second fixing piece is fixedly connected with first compliant member.Described
One fixing piece is mutually perpendicular to first stationary plane.Second fixing piece is mutually perpendicular to first stationary plane.It is described
First fixing piece and second fixing piece are mutually parallel.First compliant member includes：First movement plate 42；Second movement
Plate 43；First flexible piece 44, first flexible piece pass through the first movement plate and second movable plate to be flexibly connected；The
Two flexible pieces 45, second flexible piece pass through the first movement plate and second movable plate to be flexibly connected；Wherein, institute
It is removable relative to second movable plate to state first movement plate.The first movement version and second movable plate are mutually flat
Row.First flexible piece is the first spring.Second flexible piece is second spring.First fixing piece and described second
Fixing piece is between first flexible piece and second flexible piece.
It should be pointed out that between the first shock-damping connector 4 and first shell 15, in practical applications for basis
Distance of the flexible modulation first shell 15 relative to uav bottom is actually needed, as a kind of realization method, in the second movement
Between plate 43 and first shell 15, it is additionally provided with a telescopic rod 8,8 built-in flexible spring of telescopic rod can be extended or be contracted
It is short.One end of telescopic rod 8 is fixedly connected with the first fixed component, namely is fixed with the first fixing piece 411 and the second fixing piece 412
Connection, the other end are fixedly connected with the second movable plate 43.
Second shock-damping connector 5 includes：Second fixed component, second fixed component pass through the 11st stationary plane
612 are fixedly connected with support cylinder 61, and second fixed component and the 11st stationary plane are mutually perpendicular to；Second flexible part
Part, second compliant member are fixedly connected with second fixed component, monitor component 6, and the second compliant member is described
It is moved between second fixed component and the monitor component；Wherein, second fixed component and second compliant member
It is mutually perpendicular to.Second fixed component includes：One end of third fixing piece 511, the third fixing piece passes through the described tenth
One stationary plane is fixedly connected with the support cylinder；The other end of the third fixing piece and second compliant member, which are fixed, to be connected
It connects；One end of 4th fixing piece 512, the 4th fixing piece passes through the 11st stationary plane and the support cylinder to fix company
It connects；The other end of 4th fixing piece is fixedly connected with second compliant member.
Wherein, the third fixing piece 511 is mutually perpendicular to the 11st stationary plane.4th fixing piece 512 with
11st stationary plane is mutually perpendicular to.The third fixing piece and the 4th fixing piece are mutually parallel.Described second is flexible
Component includes：Third movable plate 52；4th movable plate 53；Third flexible piece 54, the third flexible piece are moved across the third
Movable plate and the 4th movable plate flexible connection；4th flexible piece 55, the 4th flexible piece pass through the third movable plate and
The 4th movable plate flexible connection；Wherein, the third movable plate is removable relative to the 4th movable plate.The third
Mobile edition and the 4th movable plate are mutually parallel.The third flexible piece is third spring.4th flexible piece is the 4th
Spring.The third fixing piece and the 4th fixing piece are between the third flexible piece and the 4th flexible piece.
It should be noted that in the utility model embodiment, the first shock-damping connector 4 and the second shock-damping connector 5 can
To be not understood as the damping connection component of the utility model embodiment.Meanwhile in order to enable the first shock-damping connector 4 and unmanned plane
Between it is easy to connect, and also for avoiding the first shock-damping connector 4 from being worn because long-time is connect with unmanned plane,
One shock-damping connector 4 and unmanned plane can also add an engagement plate 103 namely engagement plate 103 and first movement plate 42 is fixed
Connection, the first shock-damping connector 4 are fixed on by the engagement plate 103 on unmanned plane, and the area of engagement plate 103 is less than first and moves
The area of movable plate 42.
Likewise, in order to enable easy to connect between the second shock-damping connector 5 and support cylinder 61, and also for avoiding
Two shock-damping connectors 5 are worn due to long-time is connect with support cylinder 61, in the second shock-damping connector 5 and support cylinder 61
Between can also add a terminal pad 10 namely terminal pad 10 is fixedly connected with the 4th movable plate 53, the second shock-damping connector
5 are fixed on by the terminal pad 10 in support cylinder 61, and the area of terminal pad 10 is more than the area of the 4th movable plate 53.
The monitor component 6 includes：Camera, the camera are fixed on second shock-damping connector.Wherein, it shines
Camera passes device 14 with figure by transmission line 9 and connect, for information transmission, and since transmission line 9 is exposed in external environment, in order to
Transmission line 9 is avoided to be damaged because long-term exposed, in the utility model embodiment, the outside of transmission line 9 is additionally provided with one
Layer protective layer.It should be noted that in the utility model embodiment, the second shell is in hollow cylindrical.It is described go out powder
Chamber is in hollow cylindrical.It is described go out powder chamber and the second shell be mutually perpendicular to.
As can be seen from the above description, a kind of the second damping applied to powder mark unmanned plane provided by the utility model connects
Fitting, including：Second fixed component, second fixed component are fixedly connected across the 11st stationary plane with support cylinder, institute
It states the second fixed component and the 11st stationary plane is mutually perpendicular to；Second compliant member, second compliant member and described
Second fixed component, monitor component are fixedly connected, and the second compliant member is in second fixed component and the monitor component
Between move；Wherein, second fixed component and second compliant member are mutually perpendicular to.During actual job,
By the way that the second fixed component is fixedly connected across the 11st stationary plane with support cylinder, second fixed component and described
11 stationary planes are mutually perpendicular to；The second compliant member and the second fixed component, monitor component are fixedly connected simultaneously, and second is flexible
Component moves between second fixed component and the monitor component.This is allowed for the (packet of support base in the prior art
Including support cylinder and tripod) rigid connection between monitor component (camera) is substituted for flexible connection, realize that unmanned plane exists
When aerial progress multi-angle or multi-pose flight, support base (including support cylinder and tripod) and monitor component (will not be shone
Camera) between flexible connection cause to wear, have the characteristics that maintenance cost is cheap and job safety performance is high.
Although the preferred embodiment of the utility model has been described, once a person skilled in the art knows basic
Creative concept, then additional changes and modifications may be made to these embodiments.It is wrapped so the following claims are intended to be interpreted as
It includes preferred embodiment and falls into all change and modification of the scope of the utility model.
Obviously, those skilled in the art the utility model embodiment can be carried out various modification and variations without departing from
The spirit and scope of the utility model embodiment.In this way, if these modifications and variations of the utility model embodiment belong to this
Within the scope of utility model claims and its equivalent technologies, then the utility model is also intended to exist comprising these modification and variations
It is interior.
Claims (10)
1. a kind of the second shock-damping connector applied to powder mark unmanned plane, which is characterized in that second shock-damping connector
Including：
Second fixed component, second fixed component are fixedly connected across the 11st stationary plane with support cylinder, and described second
Fixed component and the 11st stationary plane are mutually perpendicular to；
Second compliant member, second compliant member is fixedly connected with second fixed component, monitor component, and second is soft
Property component between second fixed component and the monitor component move；
Wherein, second fixed component and second compliant member are mutually perpendicular to.
2. the second shock-damping connector as described in claim 1, which is characterized in that second fixed component includes：
One end of third fixing piece, the third fixing piece passes through the 11st stationary plane and the support cylinder to fix company
It connects；The other end of the third fixing piece is fixedly connected with second compliant member；
One end of 4th fixing piece, the 4th fixing piece passes through the 11st stationary plane and the support cylinder to fix company
It connects；The other end of 4th fixing piece is fixedly connected with second compliant member.
3. the second shock-damping connector as claimed in claim 2, it is characterised in that：
The third fixing piece is mutually perpendicular to the 11st stationary plane.
4. the second shock-damping connector as claimed in claim 2, it is characterised in that：
4th fixing piece is mutually perpendicular to the 11st stationary plane.
5. the second shock-damping connector as claimed in claim 2, it is characterised in that：
The third fixing piece and the 4th fixing piece are mutually parallel.
6. the second shock-damping connector as claimed in claim 2, which is characterized in that second compliant member includes：
Third movable plate；
4th movable plate；
Third flexible piece, the third flexible piece pass through the third movable plate and the 4th movable plate to be flexibly connected；
4th flexible piece, the 4th flexible piece pass through the third movable plate and the 4th movable plate to be flexibly connected；
Wherein, the third movable plate is removable relative to the 4th movable plate.
7. the second shock-damping connector as claimed in claim 6, it is characterised in that：
The third mobile edition and the 4th movable plate are mutually parallel.
8. the second shock-damping connector as claimed in claim 7, it is characterised in that：
The third flexible piece is third spring.
9. the second shock-damping connector as claimed in claim 8, it is characterised in that：
4th flexible piece is the 4th spring.
10. the second shock-damping connector as claimed in claim 9, it is characterised in that：
The third fixing piece and the 4th fixing piece are between the third flexible piece and the 4th flexible piece.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721427379.XU CN207698007U (en) | 2017-10-31 | 2017-10-31 | The second shock-damping connector of unmanned plane is identified applied to powder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721427379.XU CN207698007U (en) | 2017-10-31 | 2017-10-31 | The second shock-damping connector of unmanned plane is identified applied to powder |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207698007U true CN207698007U (en) | 2018-08-07 |
Family
ID=63021789
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721427379.XU Expired - Fee Related CN207698007U (en) | 2017-10-31 | 2017-10-31 | The second shock-damping connector of unmanned plane is identified applied to powder |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207698007U (en) |
-
2017
- 2017-10-31 CN CN201721427379.XU patent/CN207698007U/en not_active Expired - Fee Related
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180807 Termination date: 20181031 |
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| CF01 | Termination of patent right due to non-payment of annual fee |