CN209126955U - Wireless communication exploration unmanned plane - Google Patents
Wireless communication exploration unmanned plane Download PDFInfo
- Publication number
- CN209126955U CN209126955U CN201820909906.9U CN201820909906U CN209126955U CN 209126955 U CN209126955 U CN 209126955U CN 201820909906 U CN201820909906 U CN 201820909906U CN 209126955 U CN209126955 U CN 209126955U
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- CN
- China
- Prior art keywords
- fuselage
- camera
- unmanned plane
- wireless communication
- telescopic cylinder
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- Geophysics And Detection Of Objects (AREA)
Abstract
The utility model relates to a kind of wireless communications to survey unmanned plane comprising: network signal tester, camera, camera, GPS positioning instrument and two undercarriages that fuselage, at least three are uniformly distributed the rotor assemblies being installed on fuselage, are installed on fuselage.Battery component and telescopic cylinder are installed, battery component is electrically connected with GPS positioning instrument, camera, telescopic cylinder in fuselage main body.Each rotor assemblies include the support arm connecting with fuselage, are installed on support arm far from the screw motor and propeller on the end of fuselage, and screw motor is connect with propeller, and screw motor is electrically connected with battery component.The foot prop that undercarriage includes the support base being installed on fuselage, is articulated on support base, foot prop are connect with telescopic cylinder.The detection precision that the wireless communication surveys unmanned plane is high, high-efficient, detects instead of artificial climbing tower, highly-safe.
Description
Technical field
The utility model relates to flight equipment technical fields, survey unmanned plane more particularly to a kind of wireless communication.
Background technique
With the fast development of wireless communication industry, relevant rudimentary allocation scale and density are also growing, such as nothing
Line base station.In order to ensure the performance and range of wireless signal covering, often wireless base station is detected, detection now is often
The progress of worker ground is either completed by worker's climbing tower.But wireless base station is often built in mountain top, ait etc.
Technical staff is not easy the position reached, and the precision that artificial ground is detected, the low efficiency that artificial climbing tower is detected is right
The physical strength of worker be one greatly test, and worker's climbing tower carry out detection there are biggish security risks.
Utility model content
Based on this, it is necessary to wireless base station Measuring error there are aiming at the problem that, provide that a kind of detection precision is high, efficiency
High, safety wireless communication surveys unmanned plane.
A kind of wireless communication exploration unmanned plane, comprising: fuselage, at least three are uniformly distributed the rotation being installed on the fuselage
Wing component, the network signal tester being installed on the fuselage, camera, camera, GPS position indicator and two undercarriages;
Battery component and telescopic cylinder be installed, the battery component and the GPS positioning instrument, are stretched camera in the fuselage main body
The electrical connection of contracting cylinder;Each rotor assemblies include the support arm connecting with the fuselage, are installed on the support arm far from institute
State the screw motor and propeller on the end of fuselage, the screw motor is connect with the propeller, the screw motor with
The battery component electrical connection;The undercarriage includes the support base being installed on the fuselage, is articulated on the support base
Foot prop, the foot prop connect with the telescopic cylinder.
Above-mentioned wireless communication surveys unmanned plane, and the rotor group being installed on fuselage is uniformly distributed including fuselage, at least three
Part, the network signal tester being installed on fuselage, camera, camera, GPS positioning instrument and two undercarriages.It is sharp when use
With the flight characteristics of unmanned plane can be controlled from distant place unmanned communication exploration unmanned plane carry network signal tester, camera,
Camera, GPS positioning instrument, which fly, carries out inspection to the periphery of wireless base station, substitutes artificial climbing tower and carries out, improve safety, examines
It surveys high-efficient.Double positioning are realized by the stereoscopic vision positioning of GPS positioning instrument positioning combination camera, and GPS signal is avoided to be hidden
After gear can not precise positioning, and network signal tester can in arbitrary height around wireless base station, radius into
Row detection, the data of detection are more perfect, and precision is high.
The network signal tester and camera are installed on the bottom of the fuselage in one of the embodiments,.
The camera, GPS positioning instrument are located at the periphery of the fuselage, the camera in one of the embodiments,
The corresponding top for being located at the camera, the corresponding top for being located at the network signal tester of the GPS positioning instrument.
The camera is diplopore camera in one of the embodiments, and the camera is high definition focal length camera.
It in one of the embodiments, further include being installed on the fuselage and accommodating case open at one end, being installed on institute
The tight locking button stating the locking belt on accommodating case side, being installed on the accommodating case other side, network signal tester position
In in the accommodating case.
The quantity of the rotor assemblies is eight groups in one of the embodiments,.
The foot prop includes cross bar, the support rod connecting with the cross bar and the support in one of the embodiments,
The pin joint seat of bar connection, the pin joint seat are arranged on the support base and connect with the telescopic cylinder.
The support base is equipped with swing duct, flexible duct, two receiving holes and two in one of the embodiments,
Stroke duct, the swing duct and the flexible hole link, two receiving holes and the swing hole link, two
The stroke duct and the flexible hole link;The pin joint seat be equipped with pivoted hole and connects bayonet socket, the pivoted hole with
The receiving hole is oppositely arranged, and the connects bayonet socket is oppositely arranged with the stroke duct and connect with the telescopic cylinder.
The foot prop further includes adapter in one of the embodiments, and the adapter is installed on the cross bar and institute
It states on the junction of support rod.
There are two cushion collars, the cushion collar to be located at the cross bar for installation on the cross bar in one of the embodiments,
On end.
Above-mentioned wireless communication surveys unmanned plane, and the rotor group being installed on fuselage is uniformly distributed including fuselage, at least three
Part, the network signal tester being installed on fuselage, camera, camera, GPS positioning instrument and two undercarriages.It is sharp when use
With the flight characteristics of unmanned plane can be controlled from distant place unmanned communication exploration unmanned plane carry network signal tester, camera,
Camera, GPS positioning instrument, which fly, carries out inspection to the periphery of wireless base station, substitutes artificial climbing tower and carries out, improve safety, examines
It surveys high-efficient.Double positioning are realized by the stereoscopic vision positioning of GPS positioning instrument positioning combination camera, and GPS signal is avoided to be hidden
After gear can not precise positioning, and network signal tester can in arbitrary height around wireless base station, radius into
Row detection, the data of detection are more perfect, and precision is high.
Detailed description of the invention
Fig. 1 is the schematic diagram of one preferred embodiment of the utility model wireless communication exploration unmanned plane;
Fig. 2 is another schematic diagram of unmanned plane of wireless communication exploration shown in Fig. 1;
Fig. 3 is the enlarged diagram in the unmanned plane of wireless communication exploration shown in Fig. 2 at circle A;
Fig. 4 is the schematic diagram of support base in the unmanned plane of wireless communication exploration shown in Fig. 2;
Fig. 5 is the schematic diagram of foot prop in the unmanned plane of wireless communication exploration shown in Fig. 2.
Attached drawing mark explanation:
100- wireless communication exploration unmanned plane, 20- fuselage, 30- rotor assemblies, 31- support arm, 32- screw motor, 33-
Propeller, 40- network signal tester, 41- accommodating case, 42- locking belt, 50- camera, 60- camera, 70-GPS positioning
Instrument, 80- undercarriage, 81- support base, 82- foot prop, 811- swing duct, and 812- stretches duct, 813- receiving hole, 814- stroke
Duct, 821- cross bar, 822- support rod, 823- pin joint seat, 824- adapter, 825- cushion collar, 826- pivoted hole, 827- connection
Bayonet.
Specific embodiment
The utility model is more fully retouched below with reference to relevant drawings for the ease of understanding the utility model,
It states.The preferred embodiment of the utility model is given in attached drawing.But the utility model can come in many different forms in fact
It is existing, however it is not limited to embodiment described herein.On the contrary, purpose of providing these embodiments is makes public affairs to the utility model
The understanding for opening content is more thorough and comprehensive.
It should be noted that it can directly on the other element when element is referred to as " being fixed on " another element
Or there may also be elements placed in the middle.When an element is considered as " connection " another element, it, which can be, is directly connected to
To another element or it may be simultaneously present centering elements.
Unless otherwise defined, all technical and scientific terms used herein are led with the technology for belonging to the utility model
The normally understood meaning of the technical staff in domain is identical.Terminology used in the description of the utility model herein only be
The purpose of description specific embodiment, it is not intended that in limitation the utility model.
Fig. 1 to Fig. 5 is please referred to, is that the wireless communication of an embodiment of the present invention surveys unmanned plane 100, the wireless communication
Exploration unmanned plane 100 is uniformly distributed the rotor assemblies 30 being installed on fuselage 20, is installed on fuselage 20 including fuselage 20, at least three
On network signal tester 40, camera 50, camera 60, GPS position indicator 70 and two undercarriages 80.Wherein network is believed
Number tester 40, camera 50 are located on the bottom of fuselage 20, and camera 60, GPS positioning instrument 70 are located at the periphery of fuselage 20
On, the corresponding top for being located at camera 50 of camera 60, the corresponding top for being located at network signal tester 40 of GPS positioning instrument 70.
Battery component (not shown) and telescopic cylinder (not shown) are installed, battery component and GPS are fixed in the fuselage 20
Position instrument 70, camera 60, telescopic cylinder electrical connection, battery component include battery, control module etc., can receive processing transmitting control
The control instruction that handle issues.
Fig. 1 and Fig. 2 are referred again to, the rotor assemblies 30 include the support arm 31 connecting with fuselage 20, are installed on support arm
Screw motor 32 and propeller 33 on 31 ends far from fuselage 20, screw motor 32 are connect with propeller 33, screw motor
32 connect with battery component.In use, battery component is powered to screw motor 32, screw motor 32 drives the rotation of propeller 23 to mention
For power, to wirelessly communicate the exploration lift-off flight of unmanned plane 100.In the present embodiment, the quantity of suspense component 30 is eight groups, this
Wireless communication exploration unmanned plane 100 is eight wing unmanned planes, flight stability and power foot.
Fig. 3 is referred again to, wireless communication exploration unmanned plane 100 further includes being installed on fuselage 20 and having opening with one end
Accommodating case 41, the locking belt 42 being installed on 41 side of accommodating case, the tight locking button being installed on 41 other side of accommodating case (are not schemed
Show), network signal tester 40 is located in accommodating case 41.In use, when needing not carry out network signal test or more
When switching network signal tester 40, so that it may locking belt 42 is removed from tight locking button, so that network signal tester 40 is removed,
Mitigate main screw lift convenient for flight.When needing replacing network signal tester 40, so that it may which locking belt 42 is from tight locking button
On remove, thus remove network signal tester 40 and by new network signal tester 40 be installed on accommodating case 41 locking locking
Taut band 42, it is quick and easy for installation.
In the present embodiment, camera 50 is high definition focal length camera, and wireless base station peripheral ring can be accurately shot with high definition
Border photo etc..Camera 60 is diplopore camera, can more accurate clearly shooting record inspection process.Wherein wirelessly communicate
Surveying unmanned plane 100 and being based on GPS signal hovering precision is vertically ± 0.5 meter, ± 1.5 meters horizontal, passes through the vision of camera 60
Positioning hovering precision is ± 0.1 meter vertical, ± 0.3 meter of level.
Fig. 4 is referred again to, the undercarriage 80 includes the support base 81 being installed on fuselage 20, is articulated on support base 81
Foot prop 82, foot prop 82 are connect with telescopic cylinder, and telescopic cylinder drives lower foot prop 82 to pack up around the swing of support base 81, convenient for flight
Progress.Further, support base 81, which is equipped with, swings duct 811, flexible 812, two, duct receiving hole 813 and two strokes
Duct 814 swings duct 811 and is connected to flexible duct 812, and two receiving holes 813 are connected to duct 811 is swung, two strokes
Duct 814 is connected to flexible duct 812.
Refer again to Fig. 5, the support rod 822 and the support rod that the foot prop 82 includes cross bar 821, connect with cross bar 821
The pin joint seat 823 of 822 connections, pin joint seat 823 are arranged on support base 81 and connect with telescopic cylinder.Further, foot prop 82
It further include adapter 824, adapter 825 is installed on the junction of cross bar 821 and support rod 822, adapter 824, pin joint seat
An aperture slots are offered on 823, such aperture slots ensure that adapter 824, pin joint seat 823 and support rod 822 connect
It connects and is hardly damaged.Further, there are two cushion collars 824, cushion collar 824 to be located at the end of cross bar 821 for installation on cross bar 821
On, so that wireless communication is surveyed damping when the landing of unmanned plane 100 is grounded, mildness is good.Further, pin joint seat 823
It is equipped with pivoted hole 826 and connects bayonet socket 817, pivoted hole 826 is oppositely arranged with receiving hole 813, connects bayonet socket 827 and stroke hole
Road 814 is oppositely arranged and connect with telescopic cylinder.In use, pin joint seat 823 passes through pivoted hole 826, receiving hole 813, drive-connecting shaft
It is mounted on support base 81, connects bayonet socket 817 is located at flexible duct 812 and connect with the telescopic rod of telescopic cylinder.
Above-mentioned wireless communication surveys unmanned plane 100, is uniformly distributed and is installed on fuselage 20 including fuselage 20, at least three
Rotor assemblies 30, the network signal tester 40 being installed on fuselage 20, camera 50, camera 60, GPS positioning instrument 70 and two
A undercarriage 80.Unmanned communication exploration unmanned plane 100 can be controlled from distant place using the flight characteristics of unmanned plane when use to carry
Network signal tester 40, camera 50, camera 60, GPS positioning instrument 70, which fly, carries out inspection to the periphery of wireless base station,
It substitutes artificial climbing tower to carry out, improves safety, detection efficiency is high.Pass through the vertical of 70 positioning combination camera 60 of GPS positioning instrument
Double positioning are realized in body vision positioning, after avoiding GPS signal from being blocked can not precise positioning, and network signal tester 40 can be with
Around the wireless base station arbitrary height, detected in radius, the data of detection are more perfect, and precision is high.
Each technical characteristic of embodiment described above can be combined arbitrarily, for simplicity of description, not to above-mentioned reality
It applies all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, all should be considered as described in this specification.
Above-described embodiments merely represent several embodiments of the utility model, the description thereof is more specific and detailed,
But it cannot be understood as the limitations to utility model patent range.It should be pointed out that for the common skill of this field
For art personnel, without departing from the concept of the premise utility, various modifications and improvements can be made, these are belonged to
The protection scope of the utility model.Therefore, the scope of protection shall be subject to the appended claims for the utility model patent.
Claims (10)
1. a kind of wireless communication surveys unmanned plane characterized by comprising fuselage, at least three be uniformly distributed be installed on it is described
Rotor assemblies on fuselage, network signal tester, camera, camera, the GPS positioning instrument and two being installed on the fuselage
A undercarriage;Battery component and telescopic cylinder be installed in the fuselage main body, the battery component and the GPS positioning instrument,
Camera, telescopic cylinder electrical connection;Each rotor assemblies include the support arm connecting with the fuselage, are installed on the support
Screw motor and propeller on end of the arm far from the fuselage, the screw motor are connect with the propeller, the spiral shell
Rotation motor is electrically connected with the battery component;The undercarriage include the support base being installed on the fuselage, be articulated in it is described
Foot prop on support base, the foot prop are connect with the telescopic cylinder.
2. wireless communication according to claim 1 surveys unmanned plane, which is characterized in that the network signal tester and photograph
Camera is installed on the bottom of the fuselage.
3. wireless communication according to claim 2 surveys unmanned plane, which is characterized in that the camera, GPS positioning instrument position
In the periphery of the fuselage, the corresponding top for being located at the camera of the camera, the GPS positioning instrument is corresponding positioned at described
The top of network signal tester.
4. wireless communication according to claim 3 surveys unmanned plane, which is characterized in that the camera is diplopore camera shooting
Head, the camera are high definition focal length camera.
5. wireless communication according to claim 1 surveys unmanned plane, which is characterized in that further include being installed on the fuselage
And accommodating case open at one end, be installed on the accommodating case side locking belt, be installed on the accommodating case other side
Tight locking button, the network signal tester are located in the accommodating case.
6. wireless communication according to claim 1 surveys unmanned plane, which is characterized in that the quantity of the rotor assemblies is eight
Group.
7. wireless communication according to claim 1 surveys unmanned plane, which is characterized in that the foot prop includes cross bar and institute
State the support rod of cross bar connection, the pin joint seat that connect with the support rod, the pin joint seat be arranged on the support base and with
The telescopic cylinder connection.
8. wireless communication according to claim 7 surveys unmanned plane, which is characterized in that the support base, which is equipped with, swings hole
Road, flexible duct, two receiving holes and two stroke ducts, the swing duct and the flexible hole link, described in two
Receiving hole and the swing hole link, two stroke ducts and the flexible hole link;The pin joint seat is equipped with
Pivoted hole and connects bayonet socket, the pivoted hole are oppositely arranged with the receiving hole, the connects bayonet socket and stroke duct phase
It connect to setting and with the telescopic cylinder.
9. wireless communication according to claim 7 surveys unmanned plane, which is characterized in that the foot prop further includes adapter,
The adapter is installed on the junction of the cross bar and the support rod.
10. wireless communication according to claim 7 surveys unmanned plane, which is characterized in that on the cross bar there are two installations
Cushion collar, the cushion collar are located in the crossbar end.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820909906.9U CN209126955U (en) | 2018-06-12 | 2018-06-12 | Wireless communication exploration unmanned plane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820909906.9U CN209126955U (en) | 2018-06-12 | 2018-06-12 | Wireless communication exploration unmanned plane |
Publications (1)
Publication Number | Publication Date |
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CN209126955U true CN209126955U (en) | 2019-07-19 |
Family
ID=67227248
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Application Number | Title | Priority Date | Filing Date |
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CN201820909906.9U Expired - Fee Related CN209126955U (en) | 2018-06-12 | 2018-06-12 | Wireless communication exploration unmanned plane |
Country Status (1)
Country | Link |
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CN (1) | CN209126955U (en) |
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2018
- 2018-06-12 CN CN201820909906.9U patent/CN209126955U/en not_active Expired - Fee Related
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Date | Code | Title | Description |
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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: 20190719 Termination date: 20210612 |
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CF01 | Termination of patent right due to non-payment of annual fee |