CN207141392U - Unmanned plane unmanned vehicle system is used in nature reserve area monitoring - Google Patents
Unmanned plane unmanned vehicle system is used in nature reserve area monitoring Download PDFInfo
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- CN207141392U CN207141392U CN201720852850.3U CN201720852850U CN207141392U CN 207141392 U CN207141392 U CN 207141392U CN 201720852850 U CN201720852850 U CN 201720852850U CN 207141392 U CN207141392 U CN 207141392U
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- arm
- lever arm
- unmanned plane
- fixed
- upper plate
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Abstract
The utility model discloses a kind of nature reserve area monitoring unmanned plane unmanned vehicle system; the system includes unmanned plane; the unmanned plane includes the objective table for being arranged on its bottom; it is provided with below the objective table and automatically controls latch assembly, the latch assembly that automatically controls suspends unmanned vehicle, unmanned plane carrier's unmanned plane during flying in midair by cotton rope; when reaching presumptive area; latch assembly release is automatically controlled, the unmanned vehicle suspended in midair thereon falls, enters directly into region to be monitored and start to monitor.
Description
Technical field
It the utility model is related to a kind of monitoring nature reserve area equipment, and in particular to a kind of nature reserve area monitoring nothing
Man-machine-unmanned vehicle system.
Background technology
Existence is in various wild animals and wild plant in nature reserve area, for scientific research or to locality
Ecological environment be provided with shield of trying hard to keep, be required in time in detail understand nature reserve area in environmental aspect, and it is many when
Operating personnel is waited to be difficult to go deep into nature reserve area；At present, conventional mode is monitored by unmanned plane, allows unmanned plane to fly over
Or hover over above nature reserve area, so as to obtain related data, still, many nature reserve areas have very dense clump
Woods, unmanned plane are difficult to fly in jungle, it is easy to which collision is crashed, but if only viewed from above, many important informations are but
It can not know；In addition, if send compact robot or unmanned vehicle to be monitored from ground, generally require to pass by far
Distance get to specified location, necessary not only for expend for a long time, sometimes can also be because of not enough power supply or road surface
The reason such as be difficult to walk and failure, so far, are badly in need of a kind of new protection zone environmental monitoring system that can solve the problem that above mentioned problem.
For these reasons, the present inventor furthers investigate to existing protection zone monitoring device, to it is to be designed go out
A kind of new monitoring and protecting area system that can solve the problem that above mentioned problem.
Utility model content
In order to overcome above mentioned problem, present inventor has performed studying with keen determination, a kind of nature reserve area monitoring nothing is designed
Man-machine-unmanned vehicle system, the system include unmanned plane, and the unmanned plane includes the objective table for being arranged on its bottom, in the load
It is provided with below thing platform and automatically controls latch assembly, the latch assembly that automatically controls suspends unmanned vehicle in midair by cotton rope, nobody
Machine carrier's unmanned plane during flying, when reaching presumptive area, latch assembly release is automatically controlled, the unmanned vehicle pendant suspended in midair thereon
Fall, enter directly into region to be monitored and start to monitor, so as to complete the utility model.
Specifically, the purpose of this utility model is to provide a kind of nature reserve area monitoring unmanned plane-unmanned vehicle system
System,
The system includes unmanned plane 1,
The unmanned plane includes the objective table 2 for being arranged on its bottom,
It is provided with below the objective table and automatically controls latch assembly 3,
The latch assembly 3 that automatically controls suspends unmanned vehicle 5 in midair by cotton rope 4.
Wherein, the latch assembly 3 that automatically controls includes latch door 31 and pin rod 32, wherein, the latch door 31 is cut
Face is in inverted U, including two baffle plates, and the through hole that supply and marketing bar 32 passes through, one end position of cotton rope 4 are all offered on two baffle plates
Between two baffle plates, and it is wrapped on the pin rod 32.
Wherein, the latch assembly 3 that automatically controls also includes power part 33 and drive link 34, wherein, power part can drive
The reciprocally swinging of drive link 34 being attached thereto, the drive link 34 are also connected with pin rod 32；
Control pin rod 32 through the through hole on latch door 31 or control pin rod 32 from latch door 31 by power box 33
Through hole in remove.
Wherein, unmanned plane 1 includes frame 11 and is arranged on the protective cover 12 of frame top,
The protective cover 12 is overall round and smooth cover body protruding upward,
Control chip 13 and antenna 14 are provided with the top surface inside the protective cover,
The frame 11 includes upper plate 15 and lower shoe 16,
The cantilever of connection propeller 6 is provided between the upper plate 15 and lower shoe 16.
Wherein, the cantilever includes fixed arm and lever arm,
The fixed arm includes left fixed arm 21 and right fixed arm 22,
The lever arm includes the left front lever arm 23 and left back lever arm 24 for being located at the left both sides of fixed arm 21 respectively,
The lever arm also includes the lever arm after lever arm 25 before the right side of the right both sides of fixed arm 22 and the right side respectively
26,
The fixed arm all one end are fixedly mounted between upper plate 15 and lower shoe 16, and the other end stretches out and at it
On propeller 6 is installed；
The lever arm all one end are installed in rotation between upper plate 15 and lower shoe 16, and the other end stretches out simultaneously
Propeller 6 is installed thereon.
Wherein, it is additionally provided with paddle arm fixed seat 7 between the upper plate 15 and lower shoe 16；
The neck 8 for accommodating lever arm is offered in the paddle arm fixed seat 7.
Wherein, the section of the neck 8 is in cyclotomy shape, the diameter dimension of the cyclotomy and the diameter dimension one of lever arm
Cause.
Wherein, paddle arm fixed seat, and neck 8 in the paddle arm fixed seat are respectively arranged with each lever arm both sides
Opening direction is both facing to the lever arm；
Each lever arm can only be swung between the paddle arm fixed seat of its both sides.
Wherein, fixed arm and lever arm all include hollow connecting rod, and wire is laid in the hollow connecting rod.
Wherein, the bottom of the objective table 2 is provided with magic tape 9.
Beneficial effect includes possessed by the utility model：
(1) according to can be nobody in nature reserve area monitoring unmanned plane-unmanned vehicle system provided by the utility model
Machine and unmanned plane each the advantages of bring into play, can with it is air-ground integrated execution inspection task；
(2) set according to nature reserve area monitoring provided by the utility model with unmanned plane-unmanned vehicle system on unmanned plane
Swingable lever arm is equipped with, operating position can be rocked in flight, reception position can be rocked in storage, can
Meet normal navigation needs, additionally it is possible to which be easy to carry transport.
(3) it is every on unmanned plane according to nature reserve area monitoring provided by the utility model with unmanned plane-unmanned vehicle system
Individual lever arm both sides are all respectively arranged with paddle arm fixed seat, and each lever arm can only be put between the paddle arm fixed seat of its both sides
It is dynamic, the hunting range of lever arm is limited by paddle arm fixed seat, and lever arm is fixed by paddle arm fixed seat, make its no matter
Receiving state or working condition can be consolidated without unexpected swing.
Brief description of the drawings
Fig. 1 shows nature reserve area monitoring unmanned plane-unmanned vehicle according to a kind of preferred embodiment of the utility model
Remove the top view after protective cover when unmanned plane is in state of flight in system；
Fig. 2 shows nature reserve area monitoring unmanned plane-unmanned vehicle according to a kind of preferred embodiment of the utility model
Remove the top view after protective cover when unmanned plane is in receiving state in system；
Fig. 3 shows nature reserve area monitoring unmanned plane-unmanned vehicle according to a kind of preferred embodiment of the utility model
System removes the side view after unmanned plane cantilever；
Fig. 4 shows nature reserve area monitoring unmanned plane-unmanned vehicle according to a kind of preferred embodiment of the utility model
Overall structure side view during system unmanned plane working condition；
Fig. 5 shows nature reserve area monitoring unmanned plane-unmanned vehicle according to a kind of preferred embodiment of the utility model
Latch assembly structural representation is automatically controlled in system.
Drawing reference numeral explanation：
1- unmanned planes
11- frames
12- protective covers
13- control chips
14- antennas
15- upper plates
16- lower shoes
The left fixed arms of 21-
The right fixed arms of 22-
The left front lever arms of 23-
The left back lever arms of 24-
Lever arm before the 25- right sides
Lever arm behind the 26- right sides
2- objective tables
3- automatically controls latch assembly
31- latch doors
32- pin rods
33- power parts
34- drive links
4- cotton ropes
5- unmanned vehicles
6- propellers
7- paddle arm fixed seats
8- necks
9- magic tapes
Embodiment
The utility model is further described below by drawings and examples.It is new by these explanations, this practicality
The characteristics of type and advantage will become more apparent from clearly.
Special word " exemplary " is meant " being used as example, embodiment or illustrative " herein.Here as " exemplary "
Illustrated any embodiment should not necessarily be construed as preferred or advantageous over other embodiments.Although each of embodiment is shown in the drawings
In terms of kind, but unless otherwise indicated, it is not necessary to accompanying drawing drawn to scale.
According to nature reserve area monitoring provided by the utility model unmanned plane-unmanned vehicle system, as shown in Figure 1, Figure 2, Fig. 3,
Shown in Fig. 4 and Fig. 5, the system includes unmanned plane 1, and the unmanned plane includes the objective table 2 for being arranged on its bottom, in the load
It is provided with below thing platform and automatically controls latch assembly 3, the latch assembly 3 that automatically controls suspends unmanned vehicle 5 in midair by cotton rope 4.
Wherein it is preferred to it is respectively arranged with magic tape 9 at the top of the bottom of the objective table 2 and upper plate 15.This Shen
Please described in magic tape be also known as VELCRO, be a kind of conventional connection auxiliary material, molecule mother two sides, be simultaneously small, flexible fibre
Dimension circle hair, another side is the seta of harder buckle, other components can be removably easily bundled in into unmanned plane frame
On, such as reserve battery, working equipment.
Preferably, the objective table includes a flat board, the through hole of various shapes is offered on the flat board, in order to make
Objective table be connected in several ways with other components so that objective table can carry a variety of components, with satisfaction nobody
The different work requirements of machine, such as can on objective table carry video camera, infrared thermoviewer, sound wave monitoring device, air monitoring device
Etc. equipment, will then automatically control latch assembly 3 in the application and be fixedly mounted on objective table, certainly, may be used also on objective table
To install other equipment simultaneously.
In one preferred embodiment, the latch assembly 3 that automatically controls can be unclamped to cotton rope 4 in predetermined instant
Fixation so that cotton rope 4 comes off；
Preferably, as shown in Figure 5, the latch assembly 3 that automatically controls includes latch door 31 and pin rod 32, wherein, institute
The section for stating latch door 31 is in inverted U, including two baffle plates, and the through hole that supply and marketing bar 32 passes through all is offered on two baffle plates,
Described one end of cotton rope 4 is wrapped on the pin rod 32 between two baffle plates.
It is further preferred that the latch assembly 3 that automatically controls also includes power part 33 and drive link 34, wherein, power
Portion can drive the reciprocally swinging of drive link 34 being attached thereto, and the drive link 34 is also connected with pin rod 32；Wherein, the drive link
Connected between 34 and pin rod 32 by another rod member, the rod member is adjusting rod 35, the adjusting rod 35 respectively with drive link 34
It is be hinged with pin rod 32, it can rotate against.
Control pin rod 32 through the through hole on latch door 31 or control pin rod 32 from latch door 31 by power box 33
Through hole in remove, so as to fixed cotton rope or unclamp cotton rope.
In one preferred embodiment, the unmanned plane includes frame 11 and is arranged on the protective cover 12 of frame top,
The protective cover 12 is overall round and smooth cover body protruding upward, it is preferable that protective cover fringe region surrounds figure
Shape is consistent with the shape of frame top surface edge.
Control chip 13 and antenna 14 are provided with the top surface inside the protective cover, the antenna is used to receive and pass
Information is passed, so that wireless telecommunications connect between unmanned plane and GCU, the control chip 13 can include leading
Model plane block and calculating processing module, state of flight can be adjusted according to the control instruction on ground so that unmanned plane is according to predetermined
Track target position；
The frame 11 includes upper plate 15 and lower shoe 16, and upper plate 15 and lower shoe 16 are oppositely arranged in parallel, and two
Person's size shape is basically identical, leaves preset distance therebetween；
Preferably, control chip 13 and antenna 14 are all arranged on protective cover 12 by magic tape；
The lower edge of the protective cover 12 is attached on upper plate 15, is left between the control chip 13 and upper plate 15 pre-
Determine space, predetermined space to be left between the antenna 14 and upper plate 15, so as to reduce the vibration on upper plate for control
The interference of chip and antenna.
The cantilever of connection propeller 6 is provided between the upper plate 15 and lower shoe 16.
The cantilever includes fixed arm and lever arm, and as shown in Figures 1 and 2, the fixed arm includes left fixed arm 21
With right fixed arm 22, the lever arm includes the left front lever arm 23 positioned at the left both sides of fixed arm 21 and left back activity respectively
Arm 24, the lever arm also include the lever arm 26 after lever arm 25 before the right side of the right both sides of fixed arm 22 and the right side respectively；
Preferably, the fixed arm is identical with the length of lever arm, is symmetrical set.
The fixed arm all one end are fixedly mounted between upper plate 15 and lower shoe 16, and the other end stretches out and at it
On propeller 6 is installed；Propeller quantity is consistent with the quantity of arm, and the arm refers to fixed arm and lever arm.
The rotation of the lever arm can only be the region between upper plate 15 and lower shoe, along with upper plate 15 and under
The parallel track of bottom plate is rotated, and is also referred to as swung.
In one preferred embodiment, as shown in Fig. 1, Fig. 3, Fig. 4, the upper plate 15 and lower shoe 16 it
Between be additionally provided with paddle arm fixed seat 7；
The neck 8 for accommodating lever arm is offered in the paddle arm fixed seat 7.Limitation lever arm is fixed by the neck.
Preferably, the section of the cantilever is rounded, and the section of the neck 8 is in cyclotomy shape.
It is further preferred that the diameter dimension of the cyclotomy is consistent with the diameter dimension of lever arm.
It is highly preferred that the cyclotomy is big cyclotomy.
Cyclotomy described in the utility model is the major name in art of mathematics, specifically special in plane geometry
Industry title, it is meant that is cut into two halves with straight line incising circular, circle, if this straight line by the center of circle, two
The individual figure obtained by circle cutting can all be referred to as semicircle；If this straight line is not by the center of circle, the two are by justifying cutting
Obtained figure all shapes are referred to as cyclotomy, and wherein larger one of area is referred to as big cyclotomy.
By the way that the section of neck 8 is arranged into cyclotomy shape, it can preferably fix lever arm, in not big enough the feelings of external force
Lever arm can not be departed from from neck under condition, so that it is guaranteed that frame lever arm in state of flight will not be swung.
In one preferred embodiment, paddle arm fixed seat is respectively arranged with each lever arm both sides, and it is described
The opening direction of neck 8 is both facing to the lever arm in paddle arm fixed seat；Each lever arm can only be consolidated in the paddle arm of its both sides
Swung between reservation.By setting activity/hunting range of two each lever arms of paddle arm fixed seat to be fixed, and
Particular location when its working condition and receiving state is also defined.
In one preferred embodiment, as shown in Figure 2, during the frame storage of unmanned plane, the left front He of lever arm 23
Left back lever arm 24 is all close to left fixed arm 21；Before the right side behind lever arm 25 and the right side lever arm 26 all close to right fixed arm 22；
During the frame expansion of unmanned plane, that is, when unmanned plane works, as shown in fig. 1, left front lever arm 23 and left back
Lever arm 24 is all away from left fixed arm 21；Before the right side behind lever arm 25 and the right side lever arm 26 all away from right fixed arm 22.
In one preferred embodiment, fixed arm and lever arm all include hollow connecting rod, described hollow
Wire is laid in connecting rod.The wire one end is connected with the main body between upper plate 15 and lower shoe 16, the other end and spiral
Oar is connected, so as to which the power supply in main body and control instruction etc. are passed into propeller, and due to the protection of connecting rod, the wire
It is hardly damaged, wherein, the control instruction can be as caused by the control chip.
In one preferred embodiment, the fixed arm and lever arm are all telescopic, so as in activity
The nearly fixed arm of arm rest later can further retraction volume.
In one preferred embodiment, the equipment of protection zone monitoring is provided with the unmanned vehicle 5, is such as imaged
Machine, temperature element etc., it is preferable that be additionally provided with auto take-up on the unmanned vehicle, the device can in unmanned vehicle
Automatically cotton rope 4 is packed up behind land, prevents cotton rope 4 from disturbing the action of unmanned vehicle.
, it is necessary to explanation, the finger such as term " on ", " under ", " interior ", " outer " " preceding " " rear " in description of the present utility model
The orientation or position relationship shown is based on the orientation or position relationship under utility model works state, is for only for ease of description
The utility model and simplified description, rather than indicate or imply that signified device or element must be with specific orientation, Yi Te
Fixed azimuth configuration and operation, therefore it is not intended that to limitation of the present utility model.
The utility model is illustrated above in association with preferred embodiment, but these embodiments are only models
Example property, only play illustrative effect.On this basis, a variety of replacements and improvement can be carried out to the utility model, these
Each fall within the scope of protection of the utility model.
Claims (10)
1. unmanned plane-unmanned vehicle system is used in a kind of nature reserve area monitoring, it is characterised in that
The system includes unmanned plane (1),
The unmanned plane includes the objective table (2) for being arranged on its bottom,
It is provided with below the objective table and automatically controls latch assembly (3),
The latch assembly (3) that automatically controls suspends unmanned vehicle (5) in midair by cotton rope (4).
2. system according to claim 1, it is characterised in that
The latch assembly (3) that automatically controls includes latch door (31) and pin rod (32), wherein, the section of the latch door (31)
In inverted U, including two baffle plates, the through hole that supply and marketing bar (32) passes through, described cotton rope (4) one end are all offered on two baffle plates
Between two baffle plates, and it is wrapped on the pin rod (32).
3. system according to claim 2, it is characterised in that
The latch assembly (3) that automatically controls also includes power part (33) and drive link (34), wherein, power part can drive therewith
Connected drive link (34) reciprocally swinging, the drive link (34) are also connected with pin rod (32)；
Pin rod (32) is controlled through the through hole on latch door (31) by power part (33) or controls pin rod (32) from latch door
(31) removed in the through hole on.
4. system according to claim 1, it is characterised in that
Unmanned plane (1) includes frame (11) and is arranged on the protective cover (12) of frame top,
The protective cover (12) is overall round and smooth cover body protruding upward,
Control chip (13) and antenna (14) are provided with the top surface inside the protective cover,
The frame (11) includes upper plate (15) and lower shoe (16),
The cantilever of connection propeller (6) is provided between the upper plate (15) and lower shoe (16).
5. system according to claim 4, it is characterised in that
The cantilever includes fixed arm and lever arm,
The fixed arm includes left fixed arm (21) and right fixed arm (22),
The lever arm includes the left front lever arm (23) positioned at left fixed arm (21) both sides and left back lever arm respectively
(24),
The lever arm also includes the lever arm after lever arm (25) before the right side of right fixed arm (22) both sides and the right side respectively
(26),
Each fixed arm all one end are fixedly mounted between upper plate (15) and lower shoe (16), the other end stretch out and
Propeller (6) is installed thereon；
Each lever arm all one end are installed in rotation between upper plate (15) and lower shoe (16), and the other end stretches out
And propeller (6) is installed thereon.
6. system according to claim 4, it is characterised in that
Paddle arm fixed seat (7) is additionally provided between the upper plate (15) and lower shoe (16)；
The neck (8) for accommodating lever arm is offered on the paddle arm fixed seat (7).
7. system according to claim 6, it is characterised in that
The section of the neck (8) is in cyclotomy shape, and the diameter dimension of the cyclotomy is consistent with the diameter dimension of lever arm.
8. system according to claim 6, it is characterised in that
Be respectively arranged with paddle arm fixed seat in each lever arm both sides, and in the paddle arm fixed seat neck (8) openings
To both facing to the lever arm；
Each lever arm can only be swung between the paddle arm fixed seat of its both sides.
9. system according to claim 3, it is characterised in that
Fixed arm and lever arm all include hollow connecting rod, and wire is laid in the hollow connecting rod.
10. system according to claim 1, it is characterised in that
The bottom of the objective table (2) is provided with magic tape (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720852850.3U CN207141392U (en) | 2017-07-14 | 2017-07-14 | Unmanned plane unmanned vehicle system is used in nature reserve area monitoring |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720852850.3U CN207141392U (en) | 2017-07-14 | 2017-07-14 | Unmanned plane unmanned vehicle system is used in nature reserve area monitoring |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207141392U true CN207141392U (en) | 2018-03-27 |
Family
ID=61675440
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720852850.3U Expired - Fee Related CN207141392U (en) | 2017-07-14 | 2017-07-14 | Unmanned plane unmanned vehicle system is used in nature reserve area monitoring |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207141392U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109250115A (en) * | 2018-11-12 | 2019-01-22 | 云南电网有限责任公司红河供电局 | Multi-rotor unmanned aerial vehicle power grid high-altitude working safety rope hooking method |
-
2017
- 2017-07-14 CN CN201720852850.3U patent/CN207141392U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109250115A (en) * | 2018-11-12 | 2019-01-22 | 云南电网有限责任公司红河供电局 | Multi-rotor unmanned aerial vehicle power grid high-altitude working safety rope hooking method |
| CN109250115B (en) * | 2018-11-12 | 2023-09-29 | 云南电网有限责任公司红河供电局 | Multi-rotor unmanned aerial vehicle power grid aerial work safety rope hanging method |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180327 Termination date: 20210714 |