CN206437219U - Signal shielding unmanned plane - Google Patents
Signal shielding unmanned plane Download PDFInfo
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- CN206437219U CN206437219U CN201621413418.6U CN201621413418U CN206437219U CN 206437219 U CN206437219 U CN 206437219U CN 201621413418 U CN201621413418 U CN 201621413418U CN 206437219 U CN206437219 U CN 206437219U
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- Prior art keywords
- signal shielding
- unmanned plane
- aircraft base
- signal
- fixed
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- 238000004146 energy storage Methods 0.000 claims abstract description 26
- 238000006243 chemical reaction Methods 0.000 claims abstract description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 230000002265 prevention Effects 0.000 claims description 2
- 230000005611 electricity Effects 0.000 claims 1
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 4
- 238000004891 communication Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000010295 mobile communication Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
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- Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)
Abstract
The utility model is related to a kind of signal shielding unmanned plane, including：Unmanned plane body；The unmanned plane body includes aircraft base；Fixing device, described fixing device one end is fixed on the aircraft base, and the other end is used for fixed signal and shields device；The signal shielding device, is fixed on the aircraft base by the fixing device；The signal shielding device is used to realize signal shielding function；Photovoltaic module；It is arranged on the top of the aircraft base；The photovoltaic module is used to convert the solar into electric energy；And energy storage device, it is connected with the photovoltaic module；The energy storage device is used to store the electric energy that the photovoltaic module conversion comes；The energy storage device is additionally operable to the power supply for electrical equipment into the signal shielding unmanned plane.The shielding coverage of above-mentioned signal shielding unmanned plane is compared with wide and shield effectiveness is preferable.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, more particularly to a kind of signal shielding unmanned plane.
Background technology
With the development of science and technology, mobile communication is increasingly popularized, the mobile device such as mobile phone is had become in people's life not
The means of communication that can or lack.But in some special secrets and the higher occasion of safety requirements, it is necessary to using signal shielding device
Signal interference shielding is carried out to the means of communication in the occasion.Traditional signal shielding device is all integrally fixed on above ground structure,
Limited coverage area is shielded, shield effectiveness can not meet actual shielding needs well.
Utility model content
Based on this, it is necessary to provide a kind of shielding coverage compared with the wide and preferable signal shielding unmanned plane of shield effectiveness.
A kind of signal shielding unmanned plane, including：Unmanned plane body；The unmanned plane body includes aircraft base；It is fixed
Device, described fixing device one end is fixed on the aircraft base, and the other end is used for fixed signal and shields device；The signal
Device is shielded, is fixed on by the fixing device on the aircraft base；The signal shielding device is used to realize signal shielding
Function；Photovoltaic module；It is arranged on the top of the aircraft base；The photovoltaic module is used to convert the solar into electric energy；
And energy storage device, it is connected with the photovoltaic module；The energy storage device is used to store the electric energy that the photovoltaic module conversion comes；
The energy storage device is additionally operable to the power supply for electrical equipment into the signal shielding unmanned plane.
Above-mentioned signal shielding unmanned plane, signal shielding device is mounted in by fixing device the aircraft bottom of unmanned plane body
On seat, so that signal shielding device can be moved to above the building for needing to carry out signal shielding region with unmanned plane
Row signal shielding, signal shielding coverage is wider.Synchronous signal shielding device, which is located at signal obstacle when above building, to be reduced,
So that it has preferable shield effectiveness.Also, photovoltaic module is provided with the top of aircraft base, so as to will too
Sun, which can be converted to, gives energy storage device energy supply after electric energy, extend the endurance of unmanned plane, so as to meet signal shielding duration demand.
In one of the embodiments, the fixing device includes support baseboard and is connected at least with the support baseboard
Two lateral columns；The one end not being connected at least two lateral columns with the support baseboard is fixed on the aircraft base；
The signal shielding device is fixed between the support baseboard and at least two lateral columns.
In one of the embodiments, wherein one lateral column at least two lateral columns is adjustable lateral column；It is described can
Adjust position of the lateral column on the support baseboard and the aircraft base can be synchronously close or remote to another lateral column.
In one of the embodiments, at least two lateral columns are copper post.
In one of the embodiments, undercarriage and drive device are additionally provided with the aircraft base；The driving
Device is used to carry out folding and unfolding control to the undercarriage, to cause the undercarriage when the signal shielding device works in receipts
The state of rising.
In one of the embodiments, the drive device is worm gear pole；The undercarriage is fixed on the worm gear pole.
In one of the embodiments, it is provided with adjusting knob on the signal shielding device；The adjusting knob is used to adjust
Save the working frequency range of the signal shielding device.
In one of the embodiments, the working signal frequency range of the signal shielding device includes 2G frequency ranges, 3G frequency ranges and 4G
Frequency range.
In one of the embodiments, it is additionally provided with power-supply controller of electric in the aircraft base；The power-supply controller of electric
For being overcharged and Cross prevention to the energy storage device.
In one of the embodiments, it is additionally provided with electric power source distribution device in the aircraft base；The electric power source distribution device
Exported after carrying out voltage conversion to the output voltage of the energy storage device for the voltage according to needed for each electrical equipment to corresponding
Electrical equipment.
Brief description of the drawings
Fig. 1 be an embodiment in signal shielding unmanned plane schematic perspective view；
Fig. 2 be Fig. 1 in signal shielding unmanned plane top view；
Fig. 3 be Fig. 1 in signal shielding unmanned plane front view；
Fig. 4 be Fig. 1 in signal shielding unmanned plane side view；
Fig. 5 be Fig. 1 in signal shielding unmanned plane another state schematic diagram；
Fig. 6 is the power control circuit schematic diagram in an embodiment.
Embodiment
In order that the purpose of this utility model, technical scheme and advantage are more clearly understood, below in conjunction with accompanying drawing and implementation
Example, the utility model is further elaborated.It should be appreciated that specific embodiment described herein is only to explain
The utility model, is not used to limit the utility model.
It should be noted that when element is referred to as " being fixed on " another element, it can be directly in another element liter
It is high that or can also have element placed in the middle.When an element is considered as " connection " another element, it can be direct
It is connected to another element or may be simultaneously present centering elements.On the contrary, when element be referred to as " directly existing " another element " on "
When, in the absence of intermediary element.Term as used herein " vertically ", " level ", "left", "right" and similar statement are only
It is for illustrative purposes.
Referring to Fig. 1, the signal shielding unmanned plane in the embodiment includes unmanned plane body 100, fixing device 200, signal
Shield device 300 and photovoltaic module 400.Wherein, signal shielding device 300 is fixed on unmanned plane body 100 by fixing device 200
On, photovoltaic module 400 is similarly disposed on unmanned plane body 100.
Unmanned plane body 100 is used to realize the common functions such as the autonomous flight of unmanned plane.Unmanned plane body 100 includes flight
Device base 110, support shaft 120, propeller pedestal 130 and propeller 140.Energy storage device 112 is provided with aircraft base 110
(not showing in Fig. 1, referring to Fig. 6).Energy storage device 112 can be battery.Energy storage device 112 be used for whole signal shielding nobody
Each power supply for electrical equipment in machine.The one end of support shaft 120 is fixed on aircraft base 110, the other end and propeller pedestal 130
It is fixedly connected.Support shaft 120 is multiple, and is symmetrically distributed on aircraft base 110, so that it is guaranteed that unmanned plane body 100 exists
Stationarity in flight course.In the present embodiment, support shaft 120 is six.Six support shafts 120 are symmetrically distributed in aircraft
The surrounding of base 110.Propeller 140 is fixed on propeller pedestal 130.Electron speed regulator is provided with propeller pedestal 130
And motor.Electron speed regulator is used to be adjusted the rotating speed of motor, and then controls the rotating speed of the rotor of propeller 140.Specifically
Ground, electron speed regulator is connected by wire with the control device in aircraft base 110, so that right under control of the control means
Motor speed is controlled, and finally the state of flight to unmanned plane is adjusted.
One end of fixing device 200 is fixed on the bottom of aircraft base 110, and the other end is then used for fixed signal and shields device
300.Fixing device 200 signal shielding device 300 can be fixed using conventional fixed structure.In the present embodiment, Gu
Determining device 200 includes support baseboard 210 and at least two lateral columns 220, as shown in Figure 3.One end of at least two lateral columns 220 with
Support baseboard 210 is fixedly connected, and the other end is then fixed on aircraft base 110.Signal shielding device 300 is then fixed on support
Between bottom plate 210 and at least two lateral columns 220.In one embodiment, the quantity of lateral column 220 is two, and two lateral columns 220 are equal
With certain elasticity, so as to can be deformed upon when being acted on by external force, facilitate user installation signal shielding device 300；When outer
When power is cancelled, then restore to the original state the fixation realized to signal shielding device 300 in the presence of elastic restoring force.In another embodiment
In, signal shielding device 300 can also be fixed on support baseboard 210 by equipment such as screws, to strengthen signal shielding device 300
Mounting stability.In one embodiment, it is adjustable lateral column to have a lateral column 220 at least two lateral columns 220, namely it can be
Synchronizing moving is carried out on support baseboard 210 and aircraft base 110, it is such as close or remote to another lateral column 220, so that convenient
Signal shielding device 300 is installed and fixed.In the present embodiment, lateral column 220 is copper post, so as to strengthen signal shielding
Effect.
Signal shielding device 300 is used to realize signal shielding function.Signal shielding device 300 can be to common communications band such as
2G (CDMA, GSM, DCS and TD-SCDMA etc.) frequency range, 3G frequency ranges and 4G frequency ranges etc. produce interference, realize signal shielding.At this
In embodiment, adjusting knob 310 is provided with signal shielding device 300.Adjusting knob 310 is used for the work that Regulate signal shields device
Frequency range, so as to be shielded to the signal of target frequency bands.Signal shielding device 300 is that high power signals shield device, its transmission power
Larger, interference range is wide, so that its effective shield ranges is up to 500 meters.
In the present embodiment, undercarriage 150 and drive device 160 are additionally provided with aircraft base 110, as shown in Figure 3.
Undercarriage 120 is fixed on aircraft base 110 by drive device 160.Drive device 160 is used to carry out undercarriage 120
Folding and unfolding is controlled.Drive device 160 can be worm gear pole.Therefore, drive device 160 can drive undercarriage by the rotation of itself
120 carry out folding and unfolding control.Therefore, when signal shielding device 300 works, drive undercarriage 120 to be at by drive device 160
Collapsed state, as shown in Figure 5.By the way that undercarriage 150 is packed up, it is possible to reduce shadow of the undercarriage 150 to signal shielding device 300
Ring, so that signal shielding device 300 has preferable signal shielding effect.Drive device 160 can pass through aircraft base
Control device in 110 is controlled.
The top of aircraft base 110 is additionally provided with photovoltaic module 400.In the present embodiment, aircraft base 110 is circle
Dish structure, photovoltaic module 400 is also disc structure.Photovoltaic module 400 is used to convert the solar into after electric energy to export to energy storage
Device 112 is stored.The electric energy supplement of energy storage device 112 can be continuously given using photovoltaic module 400, so as to extend nothing
Man-machine cruising time, and be not limited within traditional 30~45 minutes, so as to meet the need of signal shielding duration very well
Ask.
In the present embodiment, power-supply controller of electric 114 and electric power source distribution device 116 are additionally provided with aircraft base 110, such as schemed
Shown in 6.Wherein, power-supply controller of electric 114 is connected with energy storage device 112, and electric power source distribution device 116 is connected to energy storage device 112 and each
Between electrical equipment.Power-supply controller of electric 114 can be controlled to the discharge and recharge of energy-storage battery, and it is overcharged and crossed put
Protection, to extend the service life of energy storage device 112.Electric power source distribution device 116 is used to carry out the output voltage of energy storage device 112
Exported after voltage conversion to corresponding electrical equipment, so as to meet the utilization voltage demand of each electrical equipment.In the present embodiment,
Energy storage device 112 is detachable, thus without using when can be dismantled, and then it is charged by household electric.
Above-mentioned signal shielding unmanned plane, unmanned plane body 100 is mounted in by signal shielding device 300 by fixing device 200
Aircraft base 110 on need to carry out signal shielding region so that signal shielding device 300 can be moved to unmanned plane
Building above to carry out signal shielding, signal shielding coverage is wider.Synchronous signal shielding device 300 is located on building
Signal obstacle is reduced when square, so that it has preferable shield effectiveness.Also, the top of aircraft base 110 is set
There is photovoltaic module 400, energized so as to convert the solar into after electric energy to energy storage device 112, extend the continuation of the journey of unmanned plane
Ability, can meet signal shielding duration demand.
Each technical characteristic of embodiment described above can be combined arbitrarily, to make description succinct, not to above-mentioned reality
Apply 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, the scope of this specification record is all considered to be.
Embodiment described above only expresses several embodiments of the present utility model, and it describes more specific and detailed,
But therefore it can not be interpreted as the limitation to utility model patent scope.It should be pointed out that for the common skill of this area
For art personnel, without departing from the concept of the premise utility, various modifications and improvements can be made, these are belonged to
Protection domain of the present utility model.Therefore, the protection domain of the utility model patent should be determined by the appended claims.
Claims (10)
1. a kind of signal shielding unmanned plane, it is characterised in that including：
Unmanned plane body；The unmanned plane body includes aircraft base；
Fixing device, described fixing device one end is fixed on the aircraft base, and the other end is used for fixed signal and shields device；
The signal shielding device, is fixed on the aircraft base by the fixing device；The signal shielding device is used for
Realize signal shielding function；
Photovoltaic module；It is arranged on the top of the aircraft base；The photovoltaic module is used to convert the solar into electric energy；With
And
Energy storage device, is connected with the photovoltaic module；The energy storage device is used to store the electric energy that the photovoltaic module conversion comes；
The energy storage device is additionally operable to the power supply for electrical equipment into the signal shielding unmanned plane.
2. signal shielding unmanned plane according to claim 1, it is characterised in that the fixing device include support baseboard and
At least two lateral columns being connected with the support baseboard；The one end not being connected at least two lateral columns with the support baseboard
It is fixed on the aircraft base；The signal shielding device is fixed between the support baseboard and at least two lateral columns.
3. signal shielding unmanned plane according to claim 2, it is characterised in that wherein one at least two lateral columns
Root lateral column is adjustable lateral column；Position of the adjustable lateral column on the support baseboard and the aircraft base can synchronously to
Another lateral column is close or remote.
4. signal shielding unmanned plane according to claim 2, it is characterised in that at least two lateral columns are copper post.
5. signal shielding unmanned plane according to claim 1, it is characterised in that be additionally provided with the aircraft base
Fall frame and drive device；The drive device is used to carry out folding and unfolding control to the undercarriage, to cause the undercarriage in institute
Collapsed state is in when stating the work of signal shielding device.
6. signal shielding unmanned plane according to claim 5, it is characterised in that the drive device is worm gear pole；It is described
Undercarriage is fixed on the worm gear pole.
7. signal shielding unmanned plane according to claim 1, it is characterised in that be provided with regulation on the signal shielding device
Knob；The adjusting knob is used for the working frequency range for adjusting the signal shielding device.
8. signal shielding unmanned plane according to claim 7, it is characterised in that the working signal frequency of the signal shielding device
Section includes 2G frequency ranges, 3G frequency ranges and 4G frequency ranges.
9. signal shielding unmanned plane according to claim 1, it is characterised in that be additionally provided with electricity in the aircraft base
Source controller；The power-supply controller of electric is used to overcharge the energy storage device and Cross prevention.
10. signal shielding unmanned plane according to claim 1, it is characterised in that be additionally provided with the aircraft base
Electric power source distribution device；The electric power source distribution device enters for the voltage according to needed for each electrical equipment to the output voltage of the energy storage device
Exported after row voltage conversion to corresponding electrical equipment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621413418.6U CN206437219U (en) | 2016-12-21 | 2016-12-21 | Signal shielding unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621413418.6U CN206437219U (en) | 2016-12-21 | 2016-12-21 | Signal shielding unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206437219U true CN206437219U (en) | 2017-08-25 |
Family
ID=59647605
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621413418.6U Expired - Fee Related CN206437219U (en) | 2016-12-21 | 2016-12-21 | Signal shielding unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206437219U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20210300590A1 (en) * | 2020-03-26 | 2021-09-30 | Seiko Epson Corporation | Unmanned aircraft |
-
2016
- 2016-12-21 CN CN201621413418.6U patent/CN206437219U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20210300590A1 (en) * | 2020-03-26 | 2021-09-30 | Seiko Epson Corporation | Unmanned aircraft |
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| PP01 | Preservation of patent right | ||
| PP01 | Preservation of patent right |
Effective date of registration: 20200623 Granted publication date: 20170825 |
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| PD01 | Discharge of preservation of patent | ||
| PD01 | Discharge of preservation of patent |
Date of cancellation: 20230623 Granted publication date: 20170825 |
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| 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: 20170825 |