CN109921845A - Wirelessly communicate detection system - Google Patents
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- CN109921845A CN109921845A CN201910297465.0A CN201910297465A CN109921845A CN 109921845 A CN109921845 A CN 109921845A CN 201910297465 A CN201910297465 A CN 201910297465A CN 109921845 A CN109921845 A CN 109921845A
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Abstract
The present invention provides a kind of wireless communication detection systems, are related to field of communication technology.A kind of wireless communication detection system, comprising: multiple groups flight instruments and multiple groups are for drawing the traction device of flight instruments；By combining cable connection between flight instruments and traction device described in each group described in each group；Flight instruments described in multiple groups can form honeycomb system in high-altitude；The storehouse of hanging of signal equipment is provided on the flight instruments, and hung described in each group the signal equipment on storehouse can with carried out wireless communication between the signal equipment that is hung described in surrounding on storehouse.Efficiently solve the problems such as communication system in the prior art cannot transmit signal at a distance.
Description
Technical field
The present invention relates to fields of communication technology, more particularly, to a kind of wireless communication detection system.
Background technique
In the prior art, overocean communications is to be realized by multiple marine mast, and marine mast are solid using seabed
Determine stake to be fixed, project amount is huge, and cost is very high, and due to maritime environment complexity, the factors such as sea wind wave are numerous, lead to sea
Upper communication is difficult, also, is not suitable for transmitting signal at a distance.
Overocean communications can also be realized by multiple satellites, however, satellite communication narrow bandwidth, signal difference and delay are longer,
It needs many satellites that could cover coverage comprehensively, keeps communications cost very high.
In addition, overocean communications can also be communicated using submarine optical fiber cable, however, submarine optical fiber cable can only solve the logical of both ends land
Letter problem can not solve marine communication issue.
Based on problem above, propose a kind of to put into communication system small, that communication efficiency is good and be particularly important.
The information disclosed in the background technology section is intended only to deepen understanding of the general background technology to the present invention, and
It is not construed as recognizing or implying in any form that the information constitutes the prior art known to those skilled in the art.
Summary of the invention
The purpose of the present invention is to provide a kind of wireless communication detection system, with solve the problems, such as it is above-mentioned at least one.
In order to solve the above-mentioned technical problem, the technological means that the present invention takes are as follows:
A kind of wireless communication detection system provided by the invention, comprising: multiple groups flight instruments and multiple groups are for drawing flight
The traction device of device；
By combining cable connection between flight instruments and traction device described in each group described in each group；
Flight instruments described in multiple groups can form honeycomb system in high-altitude；
The storehouse of hanging of signal equipment is provided on the flight instruments, and the signal equipment on storehouse is hung described in each group can
With carried out wireless communication between the signal equipment that is hung described in surrounding on storehouse.
As a kind of further technical solution, the signal equipment includes multiple groups radar and multi-unit message antenna；
Radar described in multiple groups is arranged in a ring on the flight instruments；
The communication antenna is arranged in a ring on the flight instruments.
As a kind of further technical solution, the flight instruments bottom is provided with holder；
Radar described in multiple groups is uniformly arranged on the holder；
Communication antenna described in multiple groups is uniformly arranged on the holder.
As a kind of further technical solution, the radar is set as six groups, and per adjacent two groups described in radar it
Between angle be 60 °；
The communication antenna is set as six groups, and often the angle between communication antenna described in adjacent two groups is 60 °.
As a kind of further technical solution, centered on wherein flight instruments described in one group, the group flight dress
Flight instruments described in being distributed six groups around setting, and flight instruments described in six groups of surrounding surround hexagon；
Centered on the signal equipment on wherein flight instruments described in one group, divide around the group signal equipment
Signal equipment described in six groups of cloth, and signal equipment described in six groups of surrounding surrounds hexagon；Signal equipment described in two adjacent groups it
Between can be mutually located and signal and data transmitting.
As a kind of further technical solution, slightly determine by radio between signal equipment described in two adjacent groups
Position, and point-to-point communication is carried out by laser or millimeter wave.
As a kind of further technical solution, the flight instruments include body, multiple groups wing and multiple groups screw wing；
Wing described in multiple groups is symmetricly set on the left and right sides of the body；
The screw wing is arranged on the body, and screw wing described in multiple groups is symmetricly set on the left and right two of the body
Side.
As a kind of further technical solution, the wing is set as two groups, and wing described in two groups and the body
Form scholar's character form structure；
The screw wing is set as four groups, and screw wing described in every two groups is symmetricly set on the institute at left and right sides of the body
It states on wing.
As a kind of further technical solution, the tail portion of the body is provided with the wind for stablizing the flight instruments
To rudder.
As a kind of further technical solution, the flight instruments integrally use carbon fibre materials.
Compared with prior art, technical advantage possessed by a kind of wireless communication detection system provided by the invention are as follows:
A kind of wireless communication detection system provided by the invention, including multiple groups flight instruments and multiple groups traction device, wherein
Connection is realized by combining cable between each group flight instruments and each group traction device, and flight instruments flight is in hundred meters of height as a result,
When empty, traction device can draw flight instruments by combining cable, to limit the flight range of each group flight instruments；Also,
It can be by control signal and electrical energy transportation to flight instruments, to realize control and confession to flight instruments by combination cable
Can, guarantee that flight instruments can be smoothly in hundred meters of high airflights.
Further, hanging for each group flight instruments is provided with signal equipment on storehouse, can be realized and appoints by signal equipment
Communication function between one flight instruments and around other flight instruments, including be mutually located, mutually transmit data etc..
When signal equipment energy of the multiple groups flight instruments when hundred meters of height form honeycomb system in the air, on multiple groups flight instruments
Enough hundred meters of height at sea form cellular cordless communication network system in the air, so as to realize the covering of marine network, greatly
The speed and quality of marine transmitting signal is improved greatly；Meanwhile being communicated compared to traditional marine mast, eliminate construction seabed
The trouble of spud pile reduces enforcement difficulty and cost, and not will receive the influence of marine complex environment such as wave, to reduce
The enforcement difficulty of overocean communications, also, by the covering of marine network, network coverage area is expanded, thus, increase letter
Number transmission range solves the problems, such as that traditional marine mast are not suitable for transmitting signal at a distance；In addition, compared to defending
Star transmits signal, solves the problems, such as satellite communication narrow bandwidth, signal difference, and reduce time delay and communications cost；It removes
Other than this, additionally it is possible to effectively solve the problems, such as that submarine optical fiber cable communication is only adapted to the communication of both ends land, in turn, efficiently solve sea
The problem of upper communication.
Detailed description of the invention
It, below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art be briefly described, it should be apparent that, it is described below
Attached drawing is some embodiments of the present invention, for those of ordinary skill in the art, before not making the creative labor
It puts, is also possible to obtain other drawings based on these drawings.
Fig. 1 is the schematic diagram of wireless communication detection system provided in an embodiment of the present invention；
Fig. 2 is the schematic diagram of flight instruments provided in an embodiment of the present invention, combination cable and traction device；
Fig. 3 is the first schematic diagram of flight instruments provided in an embodiment of the present invention；
Fig. 4 is the second schematic diagram of flight instruments provided in an embodiment of the present invention.
Icon:
100- flight instruments；110- body；120- wing；130- screw wing；140- wind direction rudder；
200- combines cable；210- fiber optic cable；220- cable；230- rope；
300- traction device；310- floats dish；320- mass；
400- signal equipment；410- radar；420- communication antenna；430- holder；
500- control unit；600- power supply unit.
Specific embodiment
Technical solution of the present invention is clearly and completely described below in conjunction with attached drawing, it is clear that described implementation
Example is a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill
Personnel's every other embodiment obtained without making creative work, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that term " center ", "upper", "lower", "left", "right", "vertical",
The orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" be based on the orientation or positional relationship shown in the drawings, merely to
Convenient for description the present invention and simplify description, rather than the device or element of indication or suggestion meaning must have a particular orientation,
It is constructed and operated in a specific orientation, therefore is not considered as limiting the invention.In addition, term " first ", " second ",
" third " is used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
To be mechanical connection, it is also possible to be electrically connected；It can be directly connected, can also can be indirectly connected through an intermediary
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition
Concrete meaning in invention.
The present invention is described in further detail below through specific implementation examples and in conjunction with the accompanying drawings.
Specific structure is as Figure 1-Figure 4.
A kind of wireless communication detection system provided in this embodiment, comprising: multiple groups flight instruments 100 and multiple groups are for drawing
The traction device 300 of flight instruments 100；By combining cable 200 between each group flight instruments 100 and each group traction device 300
Connection；Multiple groups flight instruments 100 can form honeycomb system in high-altitude；It is provided on flight instruments 100 and hangs storehouse, and hung on storehouse
Be provided with signal equipment 400, and the signal equipment 400 on each group flight instruments 100 can on the flight instruments 100 of surrounding
It is carried out wireless communication between signal equipment 400.
Specifically, the signal equipment 400 on multiple groups flight instruments 100 is capable of forming cellular wireless network system, in this way
One, centered on any group of signal equipment 400, around be distributed with multi-unit message equipment 400, as a result, be located at center
Information can mutually be sent between the signal equipment 400 at place and multi-unit message equipment 400 around being located at, such as location information or
Other detection data information etc., finally realize communication function.
Wireless communication detection system provided in this embodiment includes multiple groups flight instruments 100, and each group flight instruments 100 are distinguished
It is connect by combination cable 200 with marine traction device 300, each group flight instruments 100 is flown in a certain range
Row；At sea hundred meters of height are aerial, and multiple groups flight instruments 100 are capable of forming honeycomb system, at this point, on multiple groups flight instruments 100
Signal equipment 400 be capable of forming cellular cordless communication network system, thus, realize the large area covering of marine network,
Nautical signal transmission speed and quality are substantially increased, and then is advantageously implemented overocean communications.
Wireless communication detection system provided in this embodiment communicates compared to traditional marine mast, eliminates construction sea
The trouble of bottom spud pile reduces enforcement difficulty and cost, and not will receive the influence of marine complex environment such as wave, to drop
The low enforcement difficulty of overocean communications；In addition, avoiding compared to satellite transmission signal using bandwidth caused by satellite communication
The problem that narrow, signal difference, time delay are high and communications cost is high；In addition to this, additionally it is possible to effectively solve submarine optical fiber cable communication only
The problem of being adapted to the communication of both ends land, in turn, solves the problems, such as overocean communications.
In the optional technical solution of the present embodiment, signal equipment 400 includes multiple groups radar 410 and multi-unit message antenna 420；
Multiple groups radar 410 is arranged in a ring on flight instruments 100；Communication antenna 420 is arranged in a ring on flight instruments 100.
In the optional technical solution of the present embodiment, 100 bottom of flight instruments is provided with holder 430；Multiple groups radar 410 is uniform
It is arranged on holder 430；Multi-unit message antenna 420 is uniformly arranged on holder 430.
In the optional technical solution of the present embodiment, radar 410 is set as six groups, and between every two groups of adjacent radars 410
Angle be 60 °；Communication antenna 420 is set as six groups, and the angle between every two groups of adjacent communication antennas 420 is 60 °.
In the optional technical solution of the present embodiment, centered on wherein one group of flight instruments 100, this group of flight instruments 100
Around be distributed six groups of flight instruments 100, and six groups of flight instruments 100 of surrounding surround hexagon；With wherein one group of flight dress
Centered on setting the signal equipment 400 on 100, it is distributed six groups of signal equipments 400 around this group of signal equipment 400, and surrounding
Six groups of signal equipments 400 surround hexagon；It can be mutually located between two adjacent groups signal equipment 400 and signal and data
Transmitting.
In the optional technical solution of the present embodiment, coarse positioning is carried out by radio between two adjacent groups signal equipment 400,
And point-to-point communication is carried out by laser or millimeter wave.
Specifically, the signal equipment 400 includes multiple groups radar 410 and multi-unit message antenna 420, and in order to by radar 410
It is mounted on flight instruments 100 with communication antenna 420, is provided with holder 430 in the bottom of flight instruments 100 in the present embodiment,
Multiple groups radar 410 and multi-unit message antenna 420 are arranged at intervals on the side wall around holder 430, in order to be able to logical to this
It is detected around letter equipment 400.It should be noted that above-mentioned storehouse of hanging can be regarded as holder 430 herein.
Preferably, six groups of radars 410 are set in the present embodiment, and are evenly arranged on the side wall of holder 430, specifically,
It is separated by 60 ° between two adjacent groups radar 410, so, six groups of radars 410 are arranged in a ring on the side wall of holder 430, from
And other flight instruments 100 around the flight instruments 100 can be detected by six groups of radars 410.
Preferably, six groups of communication antennas 420 are set in the present embodiment, and are evenly arranged on the side wall of holder 430, specifically
, 60 ° are separated by between two adjacent groups communication antenna 420, likewise, six groups of communication antennas 420 are arranged in holder 430 in a ring
On side wall, and every group of communication antenna 420 is responsible for respectively ± 30 ° of region, thus, it can be with week by six groups of communication antennas 420
Enclose the transmitting that signal and data are carried out between other communication antennas 420.
In the present embodiment, by taking any group is located at the flight instruments 100 and signal equipment 400 thereon of center as an example,
Herein it should be noted that when wirelessly communicating detection system includes unlimited number of flight instruments, each flight instruments 100
To regard as positioned at center or be located at peripheral location, specific communication process is as follows:
It is located at around 410 pairs of six groups of radars in the signal equipment 400 of center by the group and is detected, when scanning is arrived
Around other signal equipments 400 when being respectively positioned in 410 scanning range of radar, by six groups of communication antennas 420 carry out coarse positionings (with
Low frequency is found), so, the signal equipment 400 positioned at center just receives other flight instruments 100 of surrounding and communication
The approximate location of equipment 400；After approximate location to be confirmed, then with laser or millimeter wave progress point-to-point communication, to transmit signal
And data, and then realize communication process.
Since multi-unit message equipment 400 is distributed in cellular wireless network, so that each signal equipment 400 can be made
It (since cellular wireless network system is limited, is removed really positioned at the logical of edge for the signal equipment 400 in center
400) letter is equipped, thus, the signal equipment 400 positioned at center can be equipped between 400 with other multi-unit messages around it
Realize communication process, and other multi-unit messages of surrounding equipment 400 can be regarded as positioned at center, then again respectively with week
Realize communication process between the signal equipment 400 enclosed, and so on, formed cellular wireless network system, and can by signal,
Data transmitting, finally realizes communication process.
Preferably, every group of 100 surrounding of flight instruments for being located at center is distributed six groups of flight instruments 100, and six groups fly
Luggage sets 100 and surrounds regular hexagon, correspondingly, six groups of signal equipments 400 of surrounding distribution equally surround regular hexagon, as a result,
Centered on wherein one group of signal equipment 400, wireless communication connection is formed between six groups of signal equipments 400 around, and with position
In six groups of signal equipments 400 of surrounding be center position, then with this six groups in six groups of communications around each group signal equipment 400 fill
Wireless communication connection is formed between standby 400, and so on, ultimately form the honeycomb plane being made of multiple planar regular hexagonals
The network system, it is final to realize signal and data transmitting, to realize communication process.
Herein it should be noted that in position fixing process, the scanning result of radar 410 can be transmitted by combination cable 200
Into the control unit 500 of each flight instruments 100, also, the coarse positioning result of communication antenna 420 equally can be by group zygonema
Cable 200 is sent to corresponding control unit 500.By taking any group of 100 surrounding of flight instruments is distributed six groups of flight instruments 100 as an example,
When being located at the scanning of the radar 410 of flight instruments 100 of center and arriving six groups of flight instruments 100 of surrounding, show around six
Group flight instruments 100 are respectively positioned within preset range, then do not need the position for greatly moving each group flight instruments 100 around
It sets；When the scanning of flight instruments 100 for being located at center lacks flight instruments 100 to surrounding, then scanning result can be sent
To corresponding control unit 500, and further, feedback arrives control room, and the flight instruments of scanning range are finally exceeded by manually adjusting
100 position, to make it into scanning range.The control principle of the control unit 500 can refer to the prior art, not do in detail
It is thin to illustrate, in addition, the adjusting about 100 position of flight instruments, it can be by manually controlling flight instruments through control unit 500
100 state of flight, so that 100 change of flight position of flight instruments, can refer to unmanned plane during flying principle, do not do and explain in detail herein
It states.
Further, the radar 410 on the flight instruments 100 that the flight instruments of surrounding 100 are respectively positioned on center is swept
When retouching in range, coarse positioning is carried out by the radio of communication antenna 420.Specifically, being located at the flight instruments 100 of center
On six groups of communication antennas 420 be sent out radio (RI radio intelligence include through respective location information, which can be by
Self poisoning element obtains), that is, every group of communication antenna 420 is responsible for respectively ± 30 ° of regions, is located at the flight of center as a result,
Device 100 and the approximate location for then capableing of mutual perception other side between the flight instruments 100 of surrounding, then again with laser or
Millimeter wave carries out point-to-point communication, and then realizes overocean communications.Herein it should be noted that about radio coarse positioning and laser
Or the point-to-point communication principle of millimeter wave can refer to the prior art, be not set forth in detail herein.
In the optional technical solution of the present embodiment, flight instruments 100 include body 110, multiple groups wing 120 and multiple groups spiral
The wing 130；Multiple groups wing 120 is symmetricly set on the left and right sides of body 110；Screw wing 130 is arranged on body 110, and multiple groups
Screw wing 130 is symmetricly set on the left and right sides of body 110.
In the optional technical solution of the present embodiment, wing 120 is set as two groups, and two groups of wings 120 and the formation of body 110
Scholar's character form structure；Screw wing 130 is set as four groups, and every two groups of screw wings 130 are symmetricly set on the machine of 110 left and right sides of body
On the wing 120.
In the optional technical solution of the present embodiment, the tail portion of body 110 is provided with the wind direction for stabilized flight device 100
Rudder 140.
In the optional technical solution of the present embodiment, flight instruments 100 are whole to use carbon fibre materials.
Flight instruments 100 in the present embodiment include body 110, multiple groups wing 120 and multiple groups screw wing 130, specifically,
With reference to Fig. 2-4, two groups of 120 time intervals of wing settings, respectively to extending at left and right sides of body 110, and wing 120 is used
Streamline similar with the passenger plane wing, and two groups of wings 120 and body 110 form " scholar " character form structure, and 110 tail portion of body also
Provided with wind direction rudder 140.As a result, when flight instruments 100 reach hundred meters of high-altitudes, under sufficiently large wind-force effect, pass through machine
The wing 120 and wind direction rudder 140 can guarantee that flight instruments 100 will not fall in the air in hundred meters of height, also, wind direction rudder 140 has surely
The effect of 100 heading of flight instruments is determined, so that flight instruments 100 be made to be constantly in state windward.In addition, in body 110
Cable 200 is combined in upper connection, draw is played to flight instruments 100 by combining cable 200, to prevent flight instruments 100
Beyond flight range.
Further, screw wing 130 is respectively set in the left and right sides of two groups of wings 120, that is, every group of flight instruments 100
Four groups of screw wings 130 of upper setting, and four groups of screw wings 130 are individually controlled by the control unit 500 of each group flight instruments 100
System controls the working condition of each group screw wing 130 by control unit 500 when marine hundred meters of high-altitude wind speed are unstable, and
And each group screw wing 130 is used cooperatively with wing 120, to guarantee that flight instruments 100 can fly in hundred meters of high-altitude held stationaries
Row.In addition, providing power by screw wing 130, that is, when taking off, by for Denso when flight instruments 100 take off or land
600 supply electric energy are set, the working condition of screw wing 130 are controlled by control unit 500, so that flight instruments 100 can steadily rise
Fly；When landing, when flight instruments 100 decline to a certain extent, sea wind intensity reduces, and flight instruments 100 is insufficient to allow to continue
Flight, at this point, 100 rapid decrease of flight instruments, before landing, screw wing 130 starts, and provides centainly for flight instruments 100
Lift impact the landing of flight instruments 100 to reduce the downward acceleration of flight instruments 100 and speed and reduce, thus slow
The problem of solution landing of flight instruments 100 is impacted and is damaged.
Specifically, being provided with driving motor in wing 120 in the present embodiment, driving motor passes through the dynamic member of some biographies
Part transfers power on screw wing 130, and driving screw wing 130 rotates, in order to fly.Herein it should be noted that spiral
The self structure and driving principle of the wing 130 can refer to helicopter, and details are not described herein again.
In addition, combination cable 200 includes rope 230, fiber optic cable 210 and cable 220, wherein the connection of 230 upper end of rope flies
Luggage sets 100 body 110, and lower end is connect with traction device 300, plays draw by rope 230, with limitation flight dress
Set 100 flight range；210 upper end of fiber optic cable is connect with the driving motor of flight instruments 100 and other electrical components, such as high
Sensor, air velocity transducer etc. are spent, lower end is connect with control unit 500, can receive come from by control unit 500 as a result,
The signal of flight instruments 100, and the working condition of screw wing 130 can be controlled, in order to maintain the high-altitude of flight instruments 100
Smooth flight；The upper end of cable 220 is connect with driving motor, and lower end is connect with power supply unit 600 (battery pack or other power supplys),
It is powered by the starting that power supply unit 600 is screw wing 130, so that flight instruments 100 can take off or steadily land.It is preferred that
Ground, rope 230 use aramid fiber rope or supra polymer cordage.
Further, traction device 300 includes floating dish 310 and mass 320, and floating dish 310 is swum on sea level, and is controlled
Unit 500 processed and power supply unit 600 are arranged on floating dish 310, to guarantee that floating dish 310 will not be taken away by flight instruments 100, are matched
For seabed mass 320, and connected between floating dish 310 and mass 320 by rope 230, thus, come from flight instruments
100 tractive force is mainly undertaken by mass 320, to guarantee that flight instruments 100 will not be blown away by sea wind.
The overall structure of flight instruments 100 in the present embodiment uses light material, in order to which flight instruments 100 can be more
Add and easily soar high into the air, and maintains hundred meters of high-altitude flights under the action of the wind.Preferably, using carbon fiber, certainly, may be used also
It is unrestricted herein to be other light materials.
Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the present invention., rather than its limitations；To the greatest extent
Pipe present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that: its according to
So be possible to modify the technical solutions described in the foregoing embodiments, or to some or all of the technical features into
Row equivalent replacement；And these are modified or replaceed, various embodiments of the present invention technology that it does not separate the essence of the corresponding technical solution
The range of scheme.
Claims (10)
1. a kind of wireless communication detection system characterized by comprising multiple groups flight instruments and multiple groups are for drawing flight instruments
Traction device；
By combining cable connection between flight instruments and traction device described in each group described in each group；
Flight instruments described in multiple groups can form honeycomb system in high-altitude；
The storehouse of hanging of signal equipment is provided on the flight instruments, and the signal equipment on storehouse is hung described in each group can be with week
It is carried out wireless communication between the signal equipment hung on storehouse enclosed.
2. wireless communication detection system according to claim 1, which is characterized in that the signal equipment includes multiple groups radar
With multi-unit message antenna；
Radar described in multiple groups is arranged in a ring on the flight instruments；
The communication antenna is arranged in a ring on the flight instruments.
3. wireless communication detection system according to claim 2, which is characterized in that the flight instruments bottom is provided with cloud
Platform；
Radar described in multiple groups is uniformly arranged on the holder；
Communication antenna described in multiple groups is uniformly arranged on the holder.
4. wireless communication detection system according to claim 3, which is characterized in that the radar is set as six groups, and every
Angle between radar described in adjacent two groups is 60 °；
The communication antenna is set as six groups, and often the angle between communication antenna described in adjacent two groups is 60 °.
5. wireless communication detection system according to claim 1-4, which is characterized in that with wherein described in one group
Flight instruments described in being distributed six groups centered on flight instruments, around the group flight instruments, and fly described in six groups of surrounding
Luggage, which is set, surrounds hexagon；
Centered on the signal equipment on wherein flight instruments described in one group, six are distributed around the group signal equipment
The group signal equipment, and signal equipment described in six groups of surrounding surrounds hexagon；Energy between signal equipment described in two adjacent groups
Enough be mutually located and signal and data transmitting.
6. wireless communication detection system according to claim 5, which is characterized in that between signal equipment described in two adjacent groups
Coarse positioning is carried out by radio, and point-to-point communication is carried out by laser or millimeter wave.
7. wireless communication detection system according to claim 1, which is characterized in that the flight instruments include body, more
Group wing and multiple groups screw wing；
Wing described in multiple groups is symmetricly set on the left and right sides of the body；
The screw wing is arranged on the body, and screw wing described in multiple groups is symmetricly set on the left and right sides of the body.
8. wireless communication detection system according to claim 7, which is characterized in that the wing is set as two groups, and two
The group wing and the body form scholar's character form structure；
The screw wing is set as four groups, and screw wing described in every two groups is symmetricly set on the machine at left and right sides of the body
On the wing.
9. wireless communication detection system according to claim 7, which is characterized in that the tail portion of the body, which is provided with, to be used for
Stablize the wind direction rudder of the flight instruments.
10. according to the described in any item wireless communication detection systems of claim 7-9, which is characterized in that the flight instruments are whole
Body uses carbon fibre materials.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910297465.0A CN109921845A (en) | 2019-04-12 | 2019-04-12 | Wirelessly communicate detection system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910297465.0A CN109921845A (en) | 2019-04-12 | 2019-04-12 | Wirelessly communicate detection system |
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| CN109921845A true CN109921845A (en) | 2019-06-21 |
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Citations (10)
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