CN206466170U - Multi-stage cascade formula self-balancing is tethered at UAS - Google Patents
Multi-stage cascade formula self-balancing is tethered at UAS Download PDFInfo
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- CN206466170U CN206466170U CN201720024353.4U CN201720024353U CN206466170U CN 206466170 U CN206466170 U CN 206466170U CN 201720024353 U CN201720024353 U CN 201720024353U CN 206466170 U CN206466170 U CN 206466170U
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- tethered
- cable
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- unmanned plane
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Abstract
The utility model provides a kind of multi-stage cascade formula self-balancing and is tethered at UAS, and whole system is made up of Duo Tai " being tethered at unmanned plane ".Every unmanned plane is respectively mounted " upper interface module " and " bottom standard cable module ", it is connected by the bottom standard cable module of wherein one unmanned plane with the upper interface module of an adjacent other unmanned plane, composition serial frame is tethered at unmanned unit, is substantially improved so as to realize and be tethered at unmanned plane core technology index in terms of load, stability, reliability, the lift-off height.
Description
Technical field
The utility model is related to a kind of unmanned plane, and specifically a kind of multi-stage cascade formula self-balancing is tethered at UAS.
Background technology
Be tethered at UAS by multi-rotor unmanned aerial vehicle, be tethered at cable, ground landing platform and constitute, unmanned plane uses ground
Stagnant hovering stops for a long time for power supply, meanwhile, the data such as HD video of airborne equipment collection can be by the light that is tethered at built in cable
Fibre passes back to ground, with the advantage that aerial long working, output transmission are roomy, and whole system free-standing can be installed,
It can be installed with vehicle-mounted, and can the movement of automatic synchronization following vehicle.Suitable for fields such as live telecast, signal transmitting, video monitorings.
It is main using multi-rotor unmanned aerial vehicle or coaxial unmanned plane as body currently " to be tethered at unmanned plane ", lift is produced by rotor, by being
Cable is powered for rotor motor, so that the long-time air-staying platform of the complete set constituted；It is more satisfactory at present to be tethered at unmanned plane
It is long when, top load, high performance-price ratio, air-staying platform easy to operate.
Being tethered at unmanned air vehicle technique field has " lift-off benefit " at present, due to the influence of earth surface curvature, radio
Ripple, the transmission of light are limited and influence by sighting distance；Solving the effective ways of this problem is：Wireless device, photoelectricity are set
Standby lift-off, increases such device height, is formed " lift-off benefit ".The limitation of current common ' lift-off platform '：Fixed-wing flies
Machine, vertical rotor aircraft（Helicopter）, the platform such as dirigible, it is necessary to the self-contained energy, so airborne period is limited, and cost compared with
It is high；The platforms such as captive balloon, bulky, lifting is relatively low compared with slow, load；Common unmanned aerial vehicle platform, is limited by its cells capacity
System, load and cruising time are limited.
Currently being tethered at unmanned plane all uses single cpu mode（I.e. whole system only exists a frame unmanned plane）, so carrying
There is limiting value in terms of the core technology indexs such as lotus, stability, reliability, lift-off height, and because core can only be passed through
Part（Such as motor）Performance boost be tethered at the overall performance of unmanned plane to be lifted, cause the technical difficulty that overall performance is lifted very
Greatly；In addition, current be tethered at the gesture stability that unmanned plane all carries out unmanned plane using single winged control modular manner, there is technology
It is required that it is high, wind resistance is poor, power consumption penalty is big, cost is high, take off slow, the low defect of power utilization rate；Problem above causes to work as
Before be tethered at unmanned plane as air-staying platform, in core technology index（Lift-off height, stability, reliability, load etc.）It is upper to exist
Bottleneck, limits the whole development for being tethered at unmanned plane industry.
The content of the invention
The purpose of this utility model be provide multi-stage cascade formula self-balancing be tethered at UAS, by multi-stage cascade formula without
Man-machine system and self-balancing are tethered at UAS two parts composition, to solve the problems mentioned in the above background technology.
To achieve the above object, the utility model provides following technical scheme：
Specifically, multi-stage cascade formula self-balancing described in the utility model is tethered at UAS, and whole system is by more
Platform " being tethered at unmanned plane " is constituted（Unmanned plane main body can from multi-rotor unmanned aerial vehicle, coaxial anti-rotor wing unmanned aerial vehicle etc. it is a variety of nobody
Machine scheme, and it is not limited to the unmanned plane of these above-mentioned species）.Every unmanned plane is respectively mounted " upper interface module " and " bottom
Standard cable module ", bottom standard cable module and the top of an adjacent other unmanned plane by wherein one unmanned plane
Interface module is connected, and composition serial frame is tethered at unmanned unit, thus realize be tethered at unmanned plane load, stability, can
It is substantially improved by core technology index in terms of property, lift-off height.
Further, multi-stage cascade formula self-balancing described in the utility model is tethered at UAS, each unmanned plane
Separately installed upper interface module and bottom standard cable module；Wherein, upper interface module includes Fastening tenon structure and is tethered at
Cable interface；Bottom standard cable module includes being tethered at cable box and is tethered at cable, upper interface module and bottom standard cable
By being tethered at cable connection between module, bottom standard cable module be tethered at cable and upper interface module be tethered at cable interface
Connection.
Further, the end for being tethered at cable of the bottom standard cable module, which is provided with, is used for and upper interface module
Be tethered at cable interface connection connector.
Further, the connector is provided with attaching nut.
Further, the cable that is tethered at includes outer layer elastic protecting sleeve, signal shielding network, Kev drawing successively from outside to inside
Material cable and inner core waterproof insulating layer, the center of inner core waterproof insulating layer are that some electricity are provided with around signal wire, signal wire
Source line, the outer wall of power line is outer insulation.
Further, it is tethered at unmanned plane bottom and " balancing pole suspension member module " is installed（Using weight self-balancing principle）, pass through
This module realizes the function of the partially stabilized sexual function for being tethered at unmanned plane and suspension various functions gondola；Self-balancing is tethered at unmanned plane
It is more convenient that system implements the core technology index " stability " for being tethered at unmanned plane；Make to be tethered at the takeoff speed of unmanned plane more
It hurry up；And can be used cooperatively with other various winged control devices, lifting is tethered at unmanned plane general safety coefficient.
Further, the balancing pole suspension member module is made up of self-balancing bar and hard disk two parts, makes it in nothing
Man-machine bottom reaches the effect of weight self-balancing, so as to lift the stability of unmanned plane.
Further, multi-stage cascade formula self-balancing described in the utility model is tethered at UAS, in addition to ground is put down
Platform, ground surface platform includes the cable control system and dynamical system interconnected, is tethered at cable and is connected with cable control system.
Multi-stage cascade formula self-balancing described in the utility model is tethered at UAS, has the following advantages that：
1st, multi-stage cascade formula self-balancing, which is tethered at unmanned plane, realizes the cascade of unmanned plane, stack design so that be tethered at nobody
Linear expansion is realized in terms of the dynamic property of machine, reliability, the reliability of core component；Tradition is tethered at unmanned plane without this side
Design in face；
2nd, self-balancing is tethered at that UAS is simple in construction, realizes the core technology index stability for being tethered at unmanned plane
Come more convenient；And can be used cooperatively with a variety of winged control devices, lifting is tethered at unmanned plane safety coefficient；Make to be tethered at unmanned plane simultaneously
Takeoff speed faster；Tradition is tethered at unmanned plane and not designed in this respect；
3rd, multi-stage cascade formula system realizes the cascade of unmanned plane, stack design so that be tethered at the power performance of unmanned plane
It can linearly expand, that is, the lift-off for being tethered at unmanned plane total system highly be got a promotion；
4th, multi-stage cascade formula system realizes the cascade ＆ stack designs of unmanned plane so that be tethered at unmanned plane total system
Reliability gets a promotion；
5th, because multi-stage cascade formula system realizes the linear expansion of unmanned plane, to single motor（Single unmanned plane）'s
Performance requirement is reduced；
6th, multi-stage cascade formula system suitability is strong, no matter multi-rotor unmanned aerial vehicle, coaxial anti-rotor wing unmanned aerial vehicle or it is other nobody
Machine can be used；
7th, self-balancing is tethered at that UAS is simple in construction, realizes the core technology index stability for being tethered at unmanned plane
Come more convenient；And can be used cooperatively with a variety of winged control devices, lifting is tethered at unmanned plane safety coefficient；
8th, self-balancing, which is tethered at UAS, makes to be tethered at the takeoff speed of unmanned plane faster；In a word, multi-stage cascade formula is certainly flat
To be tethered at unmanned plane be a kind of initiative invention to weighing apparatus, make to be tethered at unmanned plane lift-off height, reliability, stability, security,
Rapidly all many-side such as degree are broken through, method that can be by linearly expanding, realize be tethered at unmanned plane acquisition it is higher, longer when
Between, more stable, safer property, the benefit of more ease of Use.
Brief description of the drawings
Fig. 1 is the overall structure diagram of the utility model embodiment；
Fig. 2 is tethered at cable connection diagram for the utility model embodiment；
Fig. 3 is schematic diagram after being connected in Fig. 2；
Fig. 4 is the diagrammatic cross-section of AA ' lines in Fig. 2；
Fig. 5 is the schematic diagram of the utility model embodiment balancing pole suspension member module；
In figure：1 it is unmanned plane, 11 be upper interface module, 12 is that bottom standard cable module, 110 are connect to be tethered at cable
Mouthful, 2 for be tethered at cable, 20 be connector, 200 be attaching nut, 21 be outer layer elastic protecting sleeve, 22 be signal shielding network, 23
For Kev draw material cable, 24 be inner core waterproof insulating layer, 25 be power line, 26 be outer insulation, 27 be signal wire, 3 be
Ground surface platform, 31 be cable control system, 32 be dynamical system, 41 be self-balancing bar, 42 be hard disk.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belongs to the scope of the utility model protection.
Referring to Fig. 1, multi-stage cascade formula self-balancing described in the utility model is tethered at UAS, whole system is by more
Platform " being tethered at unmanned plane " is constituted, and every unmanned plane 1 is respectively mounted upper interface module 11 and bottom standard cable module 12, by the
The bottom standard cable module 12 of one unmanned plane is connected with the upper interface module 11 of second unmanned plane, constitutes serial frame
Structure is tethered at unmanned unit, in addition to ground surface platform 3, and ground surface platform 3 includes cable control system 31 and the power interconnected
System 32, is tethered at cable 2 and is connected with cable control system 31.Upper interface module 11 includes Fastening tenon structure and is tethered at cable interface
110；Bottom standard cable module 12 includes being tethered at cable box and is tethered at cable 2, upper interface module 11 and bottom standard cable
Connected between module 12 by being tethered at cable 2, bottom standard cable module 12 is tethered at being tethered at for cable 2 and upper interface module 11
Cable interface 110 is connected；The end for being tethered at cable 2 of the bottom standard cable module 12, which is provided with, to be used for and upper interface module
The connector 20 for being tethered at cable interface connection, the connection, 20 provided with attaching nut 200, after connection as Figure 2-3.
As shown in figure 4, be tethered at cable 2 includes outer layer elastic protecting sleeve 21, signal shielding network 22, Kev successively from outside to inside
Material cable 23 and inner core waterproof insulating layer 24 are drawn, the center of inner core waterproof insulating layer 24 is signal wire 27, the week of signal wire 27
Enclose provided with some power lines 25, the outer wall of power line 25 is outer insulation 26.As shown in figure 5, being tethered at the installation of unmanned plane bottom
Balancing pole suspension member module, the balancing pole suspension member module is made up of self-balancing bar 41 and the two parts of hard disk 42, makes it in nothing
Man-machine bottom reaches the effect of weight self-balancing, so as to lift the stability of unmanned plane
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out in the case where not departing from principle of the present utility model and spirit a variety of changes, repaiies
Change, replace and modification, scope of the present utility model is defined by the appended claims and the equivalents thereof.
Claims (9)
1. a kind of multi-stage cascade formula self-balancing is tethered at UAS, it is characterised in that：Including many unmanned planes, every unmanned plane
Upper interface module and bottom standard cable module are respectively mounted, passes through the bottom standard cable module and phase of wherein one unmanned plane
The upper interface module of an adjacent other unmanned plane is connected, and constitute serial frame is tethered at unmanned unit.
2. multi-stage cascade formula self-balancing according to claim 1 is tethered at UAS, it is characterised in that：The unmanned plane
Including multi-rotor unmanned aerial vehicle or coaxial anti-rotor wing unmanned aerial vehicle.
3. multi-stage cascade formula self-balancing according to claim 1 or 2 is tethered at UAS, it is characterised in that：On described
Portion's interface module includes Fastening tenon structure and is tethered at cable interface；Bottom standard cable module includes being tethered at cable box and is tethered at line
Cable, by being tethered at cable connection between upper interface module and bottom standard cable module, bottom standard cable module is tethered at line
Cable is connected with the cable interface that is tethered at of upper interface module.
4. multi-stage cascade formula self-balancing according to claim 3 is tethered at UAS, it is characterised in that：The bottom mark
The end for being tethered at cable of quasi- wiring module, which is provided with, is used for the connector that cable interface is connected that is tethered at upper interface module.
5. multi-stage cascade formula self-balancing according to claim 4 is tethered at UAS, it is characterised in that：The connector
It is provided with attaching nut.
6. multi-stage cascade formula self-balancing according to claim 3 is tethered at UAS, it is characterised in that：It is described to be tethered at line
Cable includes outer layer elastic protecting sleeve, signal shielding network, Kev and draws material cable and inner core waterproof insulating layer successively from outside to inside, interior
The center of core waterproof insulating layer is that some power lines are provided with around signal wire, signal wire, and the outer wall of power line is outer layer insulation
Layer.
7. multi-stage cascade formula self-balancing according to claim 1 or 2 is tethered at UAS, it is characterised in that：The nothing
Man-machine bottom is installed by balancing pole suspension member module.
8. multi-stage cascade formula self-balancing according to claim 7 is tethered at UAS, it is characterised in that：The balancing pole
Suspension member module is made up of self-balancing bar and hard disk two parts.
9. multi-stage cascade formula self-balancing according to claim 1 or 2 is tethered at UAS, it is characterised in that：Also include
Ground surface platform, ground surface platform includes the cable control system and dynamical system interconnected, is tethered at cable and cable control system
Connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720024353.4U CN206466170U (en) | 2017-01-10 | 2017-01-10 | Multi-stage cascade formula self-balancing is tethered at UAS |
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| CN201720024353.4U CN206466170U (en) | 2017-01-10 | 2017-01-10 | Multi-stage cascade formula self-balancing is tethered at UAS |
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| CN206466170U true CN206466170U (en) | 2017-09-05 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106585972A (en) * | 2017-01-10 | 2017-04-26 | 周欣 | Multistage cascaded self-balancing mooring unmanned aerial vehicle system |
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2017
- 2017-01-10 CN CN201720024353.4U patent/CN206466170U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106585972A (en) * | 2017-01-10 | 2017-04-26 | 周欣 | Multistage cascaded self-balancing mooring unmanned aerial vehicle system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170905 Termination date: 20180110 |