CN106931834A - Low latitude unmanned plane microwave injures device - Google Patents
Low latitude unmanned plane microwave injures device Download PDFInfo
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- CN106931834A CN106931834A CN201710264203.5A CN201710264203A CN106931834A CN 106931834 A CN106931834 A CN 106931834A CN 201710264203 A CN201710264203 A CN 201710264203A CN 106931834 A CN106931834 A CN 106931834A
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- unmanned plane
- outer barrel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Constitution Of High-Frequency Heating (AREA)
Abstract
The present invention relates to High-Power Microwave field, the good low latitude unmanned plane microwave of particularly a kind of simple structure, easy to use and damage effectiveness injures device.It includes the high voltage unit, high energy pulse generator, multistage oscillator and the transmitting antenna that are sequentially connected.Unmanned plane microwave in low latitude of the invention injures device, by high voltage unit, high energy pulse generator, the cooperation of multistage oscillator and transmitting antenna etc., transmitting antenna is allowed to launch High-Power Microwave, carry out the electronic system of contactless long-range attack unmanned plane and taking pictures for carrying, recording, the electronic equipments such as video recording, its mechanism of action is using the radiation coupling of Mechanism of High Power Microwave Pulse, make to induce the pulse voltage for exceeding well over its rated operational voltage value on the circuit of target electronic device and element, realize the permanent damage to target, reach and injure unmanned plane purpose, with simple structure, the characteristics of easy to use and damage effectiveness is good.
Description
Technical field
The present invention relates to high power ripple field, the good low latitude of particularly a kind of simple structure, easy to use and damage effectiveness
Unmanned plane microwave injures device.
Background technology
Unmanned plane for human lives bring great convenience while, also bring many safety problems.In particular with state
The interior such as skill upgrading of big boundary SUAV and price reduction, are scouted using civilian inexpensive low latitude SUAV and threaten quick
The potential safety hazards such as sensillary area domain gradually increase.Military field, SUAV low latitude approaches scouting event and gradually increases, civilian neck
Domain, unmanned plane is strayed into airport landing line events and also emerges in an endless stream, and has greatly threatened military and public safety.It is low in order to break through
Empty unmanned plane, mainstream technology at this stage, including electronic interferences, laser weapon, " killer " unmanned plane, conventional kinetic energy weapon and
" " day net " is arrested etc..
The mechanism of action of electronic interferences mode is the GPS and Communication Control link by disturbing unmanned plane, reaches and forces nothing
Man-machine landing out of control or purpose of making a return voyage.This mode does not cause substantive damage to UAS, when interference signal disappears
Afterwards, unmanned plane can again carry out reconnaissance mission.Simultaneously as low-cost unmanned machine wide variety, control link frequency band range compared with
Width, the interference effect for unknown model unmanned aerial vehicle control system is less obvious.
Laser weapon makes full use of monochromatic laser energy, collimation, high-power technical characterstic, is reached using the accumulative effect of heat energy
Purpose is injured to unmanned plane.But due to laser alignment characteristic requirements, to it is matched use penetrate and take aim at and mesh refers to system accuracy
It is required that higher.And existing long-range low latitude Mini-Unmanned Aerial Vehicles Detection Techniques, radar combination photodetection means are generally used,
Because the RCS of SUAV is generally less than 0.001 square meter, cause to penetrate the system of taking aim at and be difficult to meet mesh and refer to requirement.In addition, high-energy
The use occasion limitation of laser is more, is used in densely populated urban inner, it is easy to reveal laser energy, cause personnel
Additional injury.
" killer " unmanned plane carries jamming equipment using our UAS, flies, approaches and disturb to attack small-sized nothing
Man-machine system.Its mechanism of action is identical with using electronic interferences mode, but in view of my unmanned plane preparation, landing work schedule,
Break through ageing poor.
Conventional kinetic energy weapon and " day net " are arrested and unmanned plane are realized using physical means injure and arrest, ageing poor
While, certain requirement, place and poor operation convenience are proposed to matenal supports such as ammunition and catching nets.
The content of the invention
In view of this, it is an object of the invention to overcome the deficiencies in the prior art, there is provided a kind of simple structure, easy to use
And the good low latitude unmanned plane microwave of damage effectiveness injures device.
The present invention solves its technical problem：Low latitude unmanned plane microwave injures device, including successively
The high voltage unit of connection, high energy pulse generator, multistage oscillator and transmitting antenna；
Described high voltage unit, positive and negative charging is carried out for the electric capacity to high energy pulse generator, and high voltage unit is produced
Raw high-voltage pulse, is charged using constant-current charge form to the large bulk capacitance in high energy pulse generator；
Described high energy pulse generator, output HIGH voltage pulse carries out resonant charging, high energy pulse to multistage oscillator
The amplitude and efficiency of generator output HIGH voltage pulse directly affect the amplitude and efficiency that multistage oscillator produces radiofrequency signal；
Described multistage oscillator, the energy of the high-voltage pulse of storage high energy pulse generator output, completes high-voltage pulse
Energy to radio-frequency electromagnetic pulse energy change；
Described transmitting antenna, attack area of space is radiated by the energy of radio-frequency electromagnetic pulse.
Further, for the present invention is better achieved, especially using following setting structures：Described high voltage unit includes
IGBT inversion modules and the Transformer Rectifier module coordinated with the IGBT inversion modules, the output end of described Transformer Rectifier module with
High energy pulse generator is connected.
Further, for the present invention is better achieved, especially using following setting structures：Described high energy pulse generator
Using Marx generators.
Further, for the present invention is better achieved, especially using following setting structures：Described Marx generators are used
The mode of two-way induction charging stores electric energy.
Further, for the present invention is better achieved, especially using following setting structures：Described multistage oscillator includes
Feed-in gradual change outer barrel and coupler outer barrel, resonator is combined between described feed-in gradual change outer barrel and coupler outer barrel；It is described
The end of feed-in gradual change outer barrel be provided with oil gas isolated insulation, described resonator built-in resonance device inner core；Oil gas every
Run through the connection inner core for having and extending internally and be connected with resonator inner core from insulator, described resonator inner core is connected with turn
Coupled capacitor and coupling capacitor plates in coupler outer barrel, the coupling capacitor plates are connected with transmitting antenna.
Further, for the present invention is better achieved, especially using following setting structures：Described transmitting antenna includes outer
Cylinder and the reflecting plate for being connected to the outer barrel end, the first connection inner core and second that interconnection is provided with described outer barrel connect
Connect inner core, the first described connection inner core be connected with coupling capacitor plates, described second connect inner core stretch out outer barrel end with
Reflecting plate is simultaneously connected with radiant panel；It is combined between the first described connection inner core and the junction of the second connection inner core and outer barrel
First insulator, described second connection inner core coordinates and is provided with the second insulator with expelling plate.
Further, for the present invention is better achieved, especially using following setting structures：Described reflecting plate is hollow and sets
Corresponding suction nozzle, outlet nozzle and pressure gauge are equipped with, the antenna house for covering radiant panel is connected with described reflecting plate.
Further, for the present invention is better achieved, especially using following setting structures：Described high energy pulse generator
Including the second High-Voltage Insulation sealed outer cylinder, the top of the second High-Voltage Insulation sealed outer cylinder is provided with the second upper cover plate, and bottom sets
It is equipped with the second lower cover；Mounting framework is internally provided with the second described High-Voltage Insulation sealed outer cylinder, in the mounting framework
On be provided with and charge isolation inductance and isolate electric capacity that inductance is adapted with the charging and gases at high pressure are switched.
Further, for the present invention is better achieved, especially using following setting structures：Described resonator is with feed-in gradually
Become at the cooperation of outer barrel, at the cooperation of resonator and coupler outer barrel, the cooperation of oil gas isolated insulation and feed-in gradual change outer barrel
At the cooperation of place, the second lower cover and the second High-Voltage Insulation sealed outer cylinder and outside the second upper cover plate and the second High-Voltage Insulation sealing
O-ring seal is provided with the cooperation of cylinder.
Further, for the present invention is better achieved, especially using following setting structures：Inside described multistage oscillator
The SF6 gases of the insulating coefficient for being not less than 10atm are filled inside multistage oscillator.
The beneficial effects of the invention are as follows：Unmanned plane microwave in low latitude of the invention injures device, by high voltage unit, high energy
The cooperation of impulse generator, multistage oscillator and transmitting antenna etc., allows transmitting antenna to launch High-Power Microwave, carries out contactless
The electronic equipment such as take pictures, record, recording a video of the electronic system of long-range attack unmanned plane and carrying, its mechanism of action is using height
The radiation coupling of power microwave pulse, makes to be induced on the circuit of target electronic device and element and exceeds well over its nominal operation
The pulse voltage of magnitude of voltage, realizes the permanent damage to target, reaches and injures unmanned plane purpose, with simple structure, uses
The characteristics of convenient and damage effectiveness is good.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
The accompanying drawing to be used needed for having technology description is briefly described, it should be apparent that, drawings in the following description are only this
Some embodiments of invention, for those of ordinary skill in the art, on the premise of not paying creative work, can be with
Other accompanying drawings are obtained according to these accompanying drawings.
Fig. 1 is the structured flowchart that unmanned plane microwave in low latitude of the invention injures device；
Fig. 2 is the structural representation of the multistage oscillator that unmanned plane microwave in low latitude of the invention injures device；
Fig. 3 is the structural representation of the high energy pulse generator that unmanned plane microwave in low latitude of the invention injures device；
Fig. 4 is the circuit structure diagram of the high voltage unit that unmanned plane microwave in low latitude of the invention injures device；
Fig. 5 is the circuit structure diagram of the high energy pulse generator that unmanned plane microwave in low latitude of the invention injures device；
Fig. 6 is the structural representation of the transmitting antenna that unmanned plane microwave in low latitude of the invention injures device；
In figure, the 8-the second High-Voltage Insulation sealed outer cylinder, the 9-the second upper cover plate, the 10-the second lower cover, 11-bone is installed
Frame, 12-charge isolation inductance, 13-suction nozzle, 14-pressure gauge, 15-reflecting plate, 16-outer barrel, the 17-the first insulator,
18-the first connection inner core, 19-hex bolts, 20-outlet nozzle, 22-antenna house, 23-radiant panel, in the 24-the second connection
Core, the 25-the second insulator, 27-oil gas isolated insulation, 28-feed-in gradual change outer barrel, 29-resonant switch, 30-resonance
Chamber, 32-coupling capacitor plates, 33-coupler outer barrel, 34-coupled capacitor, 35-O-shaped rubber ring, 36-resonator inner core,
38-resonator insulator, 41-connection inner core.
Specific embodiment
To make the object, technical solutions and advantages of the present invention clearer, technical scheme will be carried out below
Detailed description.Obviously, described embodiment is only one side point embodiment of the invention, rather than comprehensive embodiment.Base
Embodiment in the present invention, those of ordinary skill in the art are resulting on the premise of creative work is not made to be owned
Other embodiment, belongs to the scope that the present invention is protected.
Embodiment 1：
As shown in Figures 1 to 6, unmanned plane microwave in low latitude of the invention injures device, including be sequentially connected high voltage unit,
High energy pulse generator, multistage oscillator and transmitting antenna；
Described high voltage unit, positive and negative charging is carried out for the electric capacity to high energy pulse generator, and high voltage unit is produced
Raw high-voltage pulse, is charged using constant-current charge form to the large bulk capacitance in high energy pulse generator；
Described high energy pulse generator, output HIGH voltage pulse carries out resonant charging, high energy pulse to multistage oscillator
The amplitude and efficiency of generator output HIGH voltage pulse directly affect the amplitude and efficiency that multistage oscillator produces radiofrequency signal；
Described multistage oscillator, the energy of the high-voltage pulse of storage high energy pulse generator output, completes high-voltage pulse
Energy to radio-frequency electromagnetic pulse energy change；
Described transmitting antenna, attack area of space is radiated by the energy of radio-frequency electromagnetic pulse.
Unmanned plane microwave in low latitude of the invention injures device, by high voltage unit, high energy pulse generator, multistage vibration
The cooperation of device and transmitting antenna etc., allows transmitting antenna to launch High-Power Microwave, carries out the electricity of contactless long-range attack unmanned plane
The electronic equipment such as take pictures, record, recording a video of subsystem and carrying, its mechanism of action is using the radiation of Mechanism of High Power Microwave Pulse
Coupling, makes to induce the pulse voltage for exceeding well over its rated operational voltage value on the circuit of target electronic device and element,
The permanent damage to target is realized, is reached and is injured unmanned plane purpose, it is good with simple structure, easy to use and damage effectiveness
Feature.
Embodiment 2：
As preferred, for the present invention is better achieved, further optimize on the basis of above-described embodiment, especially use
Following setting structures：Described high voltage unit includes IGBT inversion modules and the Transformer Rectifier coordinated with the IGBT inversion modules
Module, the output end of described Transformer Rectifier module is connected with high energy pulse generator.It is worth noting that, described IGBT is inverse
The direct current of the 300V that the change termination rectification of module one is obtained or so, the alternating current stablized by IGBT inversion modules, then
Constant high voltage direct current is being exported by transformation and rectification, the constant high voltage direct current provides electricity for high energy pulse generator
Energy.
Embodiment 3：
As preferred, for the present invention is better achieved, further optimize on the basis of above-described embodiment, especially use
Following setting structures：Described high energy pulse generator uses Marx generators.
Embodiment 4：
As preferred, for the present invention is better achieved, further optimize on the basis of above-described embodiment, especially use
Following setting structures：Described Marx generators store electric energy by the way of two-way induction charging.As shown in figure 5, using height
Pressure charged with direct current coordinates the mode of inductance isolation to realize that the high efficiency of high energy pulse generator charges；Two-way grounded inductor ensures
Preferable synchronizing characteristics.
Embodiment 5：
As preferred, for the present invention is better achieved, further optimize on the basis of above-described embodiment, especially use
Following setting structures：As shown in Fig. 2 described multistage oscillator includes feed-in gradual change outer barrel 28 and coupler outer barrel 33, it is described
Feed-in gradual change outer barrel 28 and coupler outer barrel 33 between be combined with resonator 30；The end of described feed-in gradual change outer barrel 28 sets
It is equipped with oil gas isolated insulation 27, the described built-in resonance device inner core 36 of resonator 30；Running through in oil gas isolated insulation 27 has
The connection inner core 41 for extending internally and being connected with resonator inner core 36, described resonator inner core 36 is connected with turn positioned at coupling
Coupled capacitor 34 and coupling capacitor plates 32 in device outer barrel 33, the coupling capacitor plates 32 are connected with transmitting antenna., Marx hairs
Raw device output high energy pulse carries out resonant charging by connecting inner core 41 to resonator inner core 36, when resonator inner core voltage reaches
After the breakdown voltage of resonant switch 29, resonator will produce a High-Power Microwave of centre frequency about 600MHz, in order to remove deviation
The High-Power Microwave of centre frequency ± 100MHz, is provided with coupled capacitor 34 and coupling between described resonator inner core 36 and transmitting antenna
Capacitor plate 32 is closed, the coupling capacitor plates 32 are connected with transmitting antenna.The pressure of multistage oscillator inside SF6 determines resonance
The breakdown voltage of switch, the breakdown voltage of resonant switch determines the radiation field intensity of output High-Power Microwave.
Embodiment 6：
As preferred, for the present invention is better achieved, further optimize on the basis of above-described embodiment, especially use
Following setting structures：Described transmitting antenna includes outer barrel 16 and is connected to the reflecting plate 15 of the end of outer barrel 16, and described is outer
The first connection connection inner core 24 of inner core 18 and second of interconnection, the first described connection inner core 18 and coupling are provided with cylinder 16
Close capacitor plate 32 to connect, the second described connection inner core 24 stretches out the end of outer barrel 16 and reflecting plate 15 and is connected with radiant panel
23；The first insulator is combined between the junction of the first described connection connection inner core 24 of inner core 18 and second and outer barrel 16
17, described second connection inner core 24 coordinates with expelling plate and to be provided with the second insulator 25.
Embodiment 7：
As preferred, for the present invention is better achieved, further optimize on the basis of above-described embodiment, especially use
Following setting structures：As shown in figure 3, described high energy pulse generator includes the second High-Voltage Insulation sealed outer cylinder 8, this is second high
The top of pressure insulated enclosure outer barrel 8 is provided with the second upper cover plate 9, and bottom is provided with the second lower cover 10；It is high described second
That presses insulated enclosure outer barrel 8 is internally provided with mounting framework 11, and the charging isolation He of inductance 12 is provided with the mounting framework 11
Isolate electric capacity and gases at high pressure switch that inductance 12 is adapted with the charging.It is worth noting that, being high energy pulse shown in Fig. 3
The general diagram of generator, specific trickle parts such as electric capacity etc. are not drawn, and its circuit connecting relation is defined by Fig. 5.
Embodiment 8：
As preferred, for the present invention is better achieved, further optimize on the basis of above-described embodiment, especially use
Following setting structures：Described reflecting plate 15 is hollow and is provided with corresponding suction nozzle 13, outlet nozzle 20 and pressure gauge 14,
The antenna house 22 for covering radiant panel 23 is connected with described reflecting plate 15.
Embodiment 9：
As preferred, for the present invention is better achieved, further optimize on the basis of above-described embodiment, especially use
Following setting structures：At the cooperation of described resonator 30 Yu feed-in gradual change outer barrel 28, resonator 30 and coupler outer barrel 33
At cooperation, oil gas isolated insulation 27 with the cooperation of feed-in gradual change outer barrel 28 at, the second lower cover 10 it is close with the second High-Voltage Insulation
Seal at the cooperation of outer barrel 8 and be provided with O-shaped sealing at the cooperation of the second upper cover plate 9 and the second High-Voltage Insulation sealed outer cylinder 8
Circle 35, serves preferable sealing function, while also having preferable high voltage performance.
Embodiment 10：
As preferred, for the present invention is better achieved, further optimize on the basis of above-described embodiment, especially use
Following setting structures：The SF6 gas of the insulating coefficient for being not less than 10atm is filled inside described multistage oscillator internal multi-stage oscillator
Body, coordinates the spacing of the electromagnetic pulse change-over switch of appropriate regulation, it is ensured that other positions in addition to electromagnetic pulse change-over switch
Be not in puncture, so as to ensure that multistage oscillator can bear voltage more than 300KV.
The above, specific embodiment only of the invention, but protection scope of the present invention is not limited thereto, and it is any
Those familiar with the art the invention discloses technical scope in, change or replacement can be readily occurred in, should all contain
Cover within protection scope of the present invention.Therefore, protection scope of the present invention should be based on the protection scope of the described claims.
Claims (10)
1. unmanned plane microwave in low latitude injures device, it is characterised in that：Including the high voltage unit, the high energy pulse generation that are sequentially connected
Device, multistage oscillator and transmitting antenna；
Described high voltage unit, positive and negative charging is carried out for the electric capacity to high energy pulse generator, and high voltage unit produces high
Pressure pulse, is charged using constant-current charge form to the large bulk capacitance in high energy pulse generator；
Described high energy pulse generator, output HIGH voltage pulse carries out resonant charging to multistage oscillator, and high energy pulse occurs
The amplitude and efficiency of device output HIGH voltage pulse directly affect the amplitude and efficiency that multistage oscillator produces radiofrequency signal；
Described multistage oscillator, the energy of the high-voltage pulse of storage high energy pulse generator output, completes the energy of high-voltage pulse
Measure the energy conversion of radio-frequency electromagnetic pulse；
Described transmitting antenna, attack area of space is radiated by the energy of radio-frequency electromagnetic pulse.
2. unmanned plane microwave in low latitude according to claim 1 injures device, it is characterised in that：Described high voltage unit bag
Include IGBT inversion modules and the Transformer Rectifier module coordinated with the IGBT inversion modules, the output end of described Transformer Rectifier module
It is connected with high energy pulse generator.
3. unmanned plane microwave in low latitude according to claim 2 injures device, it is characterised in that：Described high energy pulse occurs
Device uses Marx generators.
4. unmanned plane microwave in low latitude according to claim 3 injures device, it is characterised in that：Described Marx generators are adopted
Electric energy is stored with the mode of two-way induction charging.
5. the low latitude unmanned plane microwave according to any one claim in Claims 1-4 injures device, and its feature exists
In：Described multistage oscillator includes feed-in gradual change outer barrel (28) and coupler outer barrel (33), described feed-in gradual change outer barrel
(28) resonator (30) is combined with and coupler outer barrel (33) between；The end of described feed-in gradual change outer barrel (28) is provided with oil
Air bound is from insulator (27), described resonator (30) built-in resonance device inner core (36)；Run through in oil gas isolated insulation (27)
There is the connection inner core (41) for extending internally and being connected with resonator inner core (36), described resonator inner core (36) is connected with turn
Coupled capacitor (34) and coupling capacitor plates (32) in coupler outer barrel (33), the coupling capacitor plates (32) and transmitting
Antenna is connected.
6. unmanned plane microwave in low latitude according to claim 5 injures device, it is characterised in that：Described transmitting antenna includes
Outer barrel (16) and the reflecting plate (15) of outer barrel (16) end is connected to, the of interconnection is provided with described outer barrel (16)
One connection inner core (18) and the second connection inner core (24), the first described connection inner core (18) is with coupling capacitor plates (32) even
Connect, the second described connection inner core (24) is stretched out outer barrel (16) end and reflecting plate (15) and is connected with radiant panel (23)；It is described
First connection inner core (18) and second connect inner core (24) junction and outer barrel (16) between be combined with the first insulator
(17), described second connection inner core (24) coordinates with expelling plate and to be provided with the second insulator (25).
7. unmanned plane microwave in low latitude according to claim 6 injures device, it is characterised in that：In described reflecting plate (15)
It is empty and be provided with corresponding suction nozzle (13), outlet nozzle (20) and pressure gauge (14), connected on described reflecting plate (15)
There is the antenna house (22) for covering radiant panel (23).
8. unmanned plane microwave in low latitude according to claim 7 injures device, it is characterised in that：Described high energy pulse occurs
Device includes the second High-Voltage Insulation sealed outer cylinder (8), and the top of second High-Voltage Insulation sealed outer cylinder (8) is provided with the second upper cover plate
(9), bottom is provided with the second lower cover (10)；Installation is internally provided with the second described High-Voltage Insulation sealed outer cylinder (8)
Skeleton (11), charging isolation inductance (12) is provided with the mounting framework (11) and is isolated inductance (12) with the charging and is adapted
Electric capacity and gases at high pressure switch.
9. unmanned plane microwave in low latitude according to claim 8 injures device, it is characterised in that：Described resonator (30) with
At the cooperation of feed-in gradual change outer barrel (28), at the cooperation of resonator (30) and coupler outer barrel (33), oil gas isolated insulation
(27) with the cooperation of feed-in gradual change outer barrel (28) at, the cooperation of the second lower cover (10) and the second High-Voltage Insulation sealed outer cylinder (8)
O-ring seal (35) is provided with the cooperation of place and the second upper cover plate (9) and the second High-Voltage Insulation sealed outer cylinder (8).
10. unmanned plane microwave in low latitude according to claim 9 injures device, it is characterised in that：Described multistage oscillator
The SF6 gases of the insulating coefficient for being not less than 10atm are filled inside internal multi-stage oscillator.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710264203.5A CN106931834A (en) | 2017-04-21 | 2017-04-21 | Low latitude unmanned plane microwave injures device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710264203.5A CN106931834A (en) | 2017-04-21 | 2017-04-21 | Low latitude unmanned plane microwave injures device |
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| CN106931834A true CN106931834A (en) | 2017-07-07 |
Family
ID=59437893
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| CN201710264203.5A Pending CN106931834A (en) | 2017-04-21 | 2017-04-21 | Low latitude unmanned plane microwave injures device |
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| CN112629328A (en) * | 2020-11-30 | 2021-04-09 | 刘诗林 | Small-caliber wide-band electromagnetic pulse radiation device |
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Application publication date: 20170707 |