CN205150261U - Many rotors captain flight time electrical power generating system that flies - Google Patents

Abstract

The utility model discloses a many rotors captain flight time electrical power generating system that flies, include and use the solar cell power supply to existing many gyroplanes (1) to a design method and system make many gyroplanes (1) realize that long flight time flies that ground solar electric source board, perhaps hybrid power source supplies power for many gyroplanes (1) in the flight is proposed. Wherein, ground power supply's design method and power supply system include many gyroplanes (1) power supply of set point flight, perhaps give many gyroplanes (1) the power supply of removing flight two kinds of forms. The utility model discloses the long flight time flight of many gyroplanes is realized with lower expense. The utility model discloses introduce ripe power supply design method and system to lower economic cost gains the long flight time flight target that prior art is difficult to the breakthrough short time, has enlarged the range of application of current many gyroplanes.

Description

Flight power-supply system when a kind of many rotors captain navigates

Technical field

The utility model relates to a kind of method of designing and system of many cyclogyros applied solar energy Power supply, belongs to new forms of energy and technical field of aerospace.

Background technology

Unmanned plane refers to reusable unmanned vehicle, and it has corresponding avionics system, sensing system, communication system, flight control system etc., and have the function of autonomous flight and a certain task of complete independently, also someone is referred to as air-robot.Relative to piloted vehicle, unmanned plane has cheap, is applicable to Various Complex task environment, can reduces the advantages such as personal casualty.Britain has just succeeded in developing first unmanned plane in the world as far back as 1917, to about the eighties in 20th century, the development of unmanned plane is paid attention to gradually, and at present, a lot of country all expands research and the manufacture of unmanned plane in the world.

Rotary wind type unmanned plane is a classification of unmanned plane, relies on one or more rotor to provide lift and the power of body.Along with the deep development of unmanned plane in every field, rotary wind type unmanned plane obtains increasing favor with the hovering ability of its uniqueness, the low-altitude low-speed characteristic more excellent compared with fixed-wing formula unmanned plane, the low requirement to landing site, splendid maneuverability and high reliability, is widely used in the army and the people's industry-by-industry.

The application impact of continuation of the journey on unmanned plane of unmanned plane is very large, unmanned plane directly can be subject to illumination awing, solar power is eco-friendly power source, unmanned plane awing charges by solar power, at present by increasing for unmanned plane field, and the continued power ability that the electronic multiaxis cyclogyro (being called for short many cyclogyros) that the common combination by three and multiple electric propeller lift controls flight now exists battery on using is weak, flight cruise duration shorter shortcoming, the demand only realizing the flight continuation of the journey of many cyclogyros long period by solution battery technology is more difficult in recent years to make progress.

It is a globoid in the middle part of the usual body of rotary wind type unmanned plane; can consider globoid surface is arranged solar energy collecting plate thus utilizes solar power to power; but because the daylighting area of sphere is restricted; and be not easy that thus expanding area principle is adopted can be limited very large; and the solar cell woof silicon chip overwhelming majority is planar materials, should not promoting of special sphere.In addition, the flying speed of many cyclogyros is slow, insensitive to solar panels enlarged areas, utilizes the larger plane lighting panel of its low speed feature erection space to have more practicality.

Therefore, fly when how to realize the long boat of many rotor wing unmanned aerial vehicles is the important technological problems needing at present to solve.

Utility model content

The purpose of this utility model is the power-supply system providing a kind of many cyclogyros applied solar energy Power supply, to solve the problem of many rotor wing unmanned aerial vehicles long period flight continuation of the journey.

The technical solution of the utility model is as follows:

First, to the utility model proposes when a kind of many rotors captain navigates the method for designing of flight, which comprises at least one of following A, B, C tri-kinds of schemes or the combination of A scheme and B scheme or the combination of A scheme and C scheme:

A scheme: flight when being navigated with the length realizing many cyclogyros to the battery charge on many cyclogyros by the solar panel that many cyclogyros carry;

B scheme: during many cyclogyro fixed point flight, that many cyclogyros adopts supply cable and ground or solar cell on automobile, automobile current generator, or the power-supply management system introducing civil power composition connects to realize powering to many cyclogyros, power-supply management system carries out charging by earthbound solar energy power panel or civil power to its storage battery and is connected to supply cable;

C scheme: when many cyclogyros move flight, many cyclogyros adopt supply cable to be connected to realize powering to many cyclogyros with the power-supply management system on the automobile on ground, power-supply management system can configure storage battery, carries out charging be connected to supply cable by Vehicular solar power supply to its storage battery.

Wherein, in A scheme, the solar panel that many cyclogyros carry and supporting construction thereof are arranged on the electrical motor armshaft extending structure of many cyclogyros, can dismantle, the design of solar panel makes the prop-blast of many cyclogyros circulate smoothly downwards, the mechanism of the reduction windage of solar panel design structure changes, and the mechanism of regulating plate face version.

In B scheme and C scheme, automobile in the process of moving, allow many cyclogyros of mobile flight obtain the real time position of automobiles by navigation information, to guide and moving vehicle followed by many cyclogyros of controlling mobile flight, keep mutual position and distance thus obtain the power supply continued.Supply cable realizes the adjustment of cable length by the cable reel installation be arranged on automobile, the control of twisted and released of the cable length is adopted to two kinds of modes of electronic and manual combination; Manual mode can be used on power-off or other extraordinary circumstances; Motorized adjustment patten's design is the relaxed state that "on" position is in unwrapping wire, and cable reel installation records unwrapping wire length automatically, and cable reel installation is according to its automatic measured data or the control being combined take-up and the unwrapping wire realized unwrapping wire length with navigation information.

In above each scheme, in parallelly with information transmission link with the remote measuring and controlling usually configure on many cyclogyros can also install 4G/LTE(additional and contain LTE-A) communication apparatus, the data of mission payload or acquisition sensor are recorded on machine or under pass to the reception facilities of specifying, the reception facilities on the ground of specifying or mobile platform multiple stage can receive down the information passed simultaneously.

Based on said method, when a kind of many rotors captain of the present utility model navigates, flight control system is such: it comprises the many cyclogyros being provided with storage battery and charger, and this many cyclogyro is provided with solar electric power supply system; Described solar electric power supply system be below any one:

The first is: solar electric power supply system comprises the solar panel be arranged on many cyclogyros, and this solar panel is to the battery charge on many cyclogyros;

The second is: solar electric power supply system comprises the power-supply management system be arranged on the automobile of ground, power-supply management system is by earthbound solar energy power panel, automobile current generator or civil power are powered, power-supply management system is by the battery charge of supply cable to many cyclogyros, or the consumer directly connecting many cyclogyros is powered; It is mainly used in the situation of many cyclogyros fixed point flight;

The third is: solar electric power supply system comprises the power-supply management system be arranged on the automobile of ground, power-supply management system is powered by Vehicular solar power supply or automobile current generator, power-supply management system is by the battery charge of supply cable to many cyclogyros, or the consumer directly connecting many cyclogyros is powered; It is mainly used in the situation that many cyclogyros move flight.

Wherein, solar panel is arranged on the electrical motor armshaft extending structure of many cyclogyros, can dismantle, and solar panel is donut platy structure.That is, solar cell and supporting construction thereof can be dismantled from many cyclogyros, the design in solar panel face, can ensure that the prop-blast of many cyclogyros circulates smoothly downwards, the mechanism of reduction windage that is that sectional type gap length can be designed in solar panel face or structure changes, and the mechanism of regulating plate face version.Therefore, preferred solar panel face shape is donut.Because general many cyclogyros structure all adopts composite material, therefore, solar panel and supporting framework thereof also adopt composite material and lightweight structural material.

The power-supply management system be arranged on ground or automobile comprises storage battery, charger and power supervisor.Supply cable should arrange the fastening design of failure-free at the two ends exported and hang, and the intensity of supply cable can require to select according to wind resistance.

Vehicular solar power supply is arranged on automobile collapsibly, the power supply of Vehicular solar power supply can be carried out AC-battery power source with other ground power supplies and power, managed by power supervisor, and powered to the storage battery on many cyclogyros through supply cable by vehicle-mounted charger, wherein, the generator powered of vehicle, and Portable storage battery to power be movable power source than being easier to obtain, and hybrid power supply can be formed with vehicle-mounted solar cell.Power supervisor can with charger integrated design.

The supply cable being connected to many cyclogyros consumer designs two attachment points, the anatomical connectivity of the consumer on an attachment point and many cyclogyros, attachment point then should design on many cyclogyros landing support or on custom-designed fixed mount according to the scantling of structure of many cyclogyros by another attachment point, keep with the suitable distance of The Cloud Terrace motion structure and make the moment of the center of gravity of many cyclogyros as far as possible little, this attachment point is as the load fastening point of bearing wind-force or tractive force, The Cloud Terrace work about 180 degree or 360 degree left-right rotaries of observation load can be allowed to transfer be not powered cable winding or block, avoided even if block also suitably to be rotated by the course of many cyclogyros oneself.

Of the present utility modelly realize flying when many rotors captain navigates power-supply system, technology maturation, the cost of realization is lower, is applicable to improving also connected applications with existing many cyclogyros.Fly when can realize the long boat of three kinds of modes in principle, that is: many cyclogyros can be realized and continue flight of fixing a point round the clock, many cyclogyros and land vehicle can be realized work in coordination with, to power compared with the movement of low velocity and to carry out the flight of long period, the many cyclogyros of little wind weather can also be realized and carry the flight of solar cell long period.

Generally only have compared with the ability within 1 hour with current many cyclogyros flight time, during the utility model attainable long boat the flight time by bring up to fixed point round the clock long boat time flight, carry the capability improving that solar cell sunlight sky can reach flight in 6 hours daytime.As for the supply cable anti-wind problems that surface power supply mode relates to, annual more than 3/4 most of weather can stabilized flight, minority weather has impact, and one is the restriction that low power many cyclogyros are subject to the use of strong wind sky, and two is restrictions that high-performance many cyclogyros can not use by strong wind sky.Therefore, for many cyclogyros of flight when needing to continue long boat, many cyclogyros of relatively high power can be selected to solve anti-wind problems, meet the demand that strong wind sky uses.Particularly the AC-battery power source scheme of powering, can ensure that complicated weather and night power to many cyclogyros, meets the demand of flight during long boat round the clock.

When length of powering to many cyclogyros of the present utility model is navigated, Flight Design method and system, are based on the method for designing of many cyclogyros system and system, and the power-supply service of increase can not bring new technical barrier and principle to change.

For the purposes of flight during long boat, some citings can be provided.According to application, comprise the fields such as civilian, military, as city and express traffic, rally or travel surge district, news interview or movies-making, border port and strategic point are on duty, accident rescue is on-the-spot, forest fire observation, round the clock hidden lasting reconnaissance and surveillance (quietness of many cyclogyros), the observation on duty of critical point at night, low speed with car with ship detection, to scout or interference is fought, disaster area Continued communication relaying with mobile.According to application department, comprise agriculture and forestry, traffic police, People's Armed Police and special force.Particularly there is 4G/LTE(containing LTE-A) area of communication signal, many cyclogyros install additional 4G/LTE mobile phone wireless electrical transmission equipment, can the passage of recording unit on increase machine or breath of delivering a letter under increasing, the information of acquisition sensor is passed to the reception facilities of ground or movement, the reception facilities of Gong specifying receives, and receives for multiple stage reception facilities even simultaneously.

The same with common many cyclogyros, increase many cyclogyros of solar cell for supplying power, use remains low flyer.Installation anticollision induction device can be increased, in public spatial domain, perform some particular tasks.Flying when realizing long boat is the value of service that the utility model provides.

Compared with prior art, existing many cyclogyros due to load-carrying ability limited, the flight time that the capacity of its airborne storage battery can be supported is shorter, is generally 1 hours, therefore time that can only be limited in limited spatial domain performs limited task, limits the application widely of many cyclogyros.The utility model adopts mature technology to increase electric energy supply to many cyclogyros, significantly can increase the follow-on mission time of many cyclogyros, therefore expand the field of application of many cyclogyros, can for meeting the need of market and improving the condition that economic gain provides more favourable.

Accompanying drawing explanation

Fig. 1: illustrate the many cyclogyros of typical four axle;

Fig. 2: signal solar cell is arranged on the electrical motor armshaft extending structure of many cyclogyros, and solar-electricity pool area is about 1m ²;

Fig. 3: signal solar cell is arranged on the top of many cyclogyros, and solar-electricity pool area is identical with accompanying drawing 2;

Fig. 4: many cyclogyros that ground power supply is flown by cable set point are powered, and wherein ground power supply can include but not limited to solar cell, automobile current generator, storage battery, and civil power;

Fig. 5: signal ground power supply powers to mobile aloft many cyclogyros by cable, and wherein ground power supply is installed on the vehicle of movement, and vehicle power can include but not limited to solar cell, automobile current generator, storage battery, and diesel engine.

The many cyclogyros of description of reference numerals: 1-, 2-screw propeller, 3-electrical motor armshaft extending structure, 4-spheroid fuselage, 5-solar panel, 6-earthbound solar energy power panel, 7-cable reel installation, 8-power-supply management system, 9-civil power, 10-automobile current generator, 11-supply cable, 12-automobile, 13-Vehicular solar power supply.

Detailed description of the invention

Below in conjunction with drawings and Examples, the utility model is described in further detail.

Typical four axle many cyclogyros structures, as shown in Figure 1, based on this, the utility model proposes following three kinds of embodiments and make improvements.A kind of is that solar cell is connected on solar cell panel structure that many cyclogyros are installed, power to the current consumer on many cyclogyros by supply cable, or the needs of the using electricity system according to provided many cyclogyros, are powered by increase charger accumulators and resupply using electricity system.Another kind is that solar cell is connected on ground or car, and can with automobile generating electromechanical source, Portable storage battery power supply, and mains supply etc. forms AC-battery power source, conversion and management is concentrated, by charger and the aloft many cyclogyros continued power of supply cable set point, wherein by the power supervisor on ground or car, current consumer directly to many cyclogyros is powered, or gives the storage battery power supply of many cyclogyros.Another is that solar cell connects onboard, and can with automobile generating electromechanical source, Portable storage battery power supplys etc. form AC-battery power source, by the power supervisor centralized management on car, by charger and supply cable set point or aloft many cyclogyros continued power, wherein, the current consumer directly to many cyclogyros is powered, or gives the storage battery power supply of many cyclogyros.Power supervisor or charger have the function of power conversion, can merge the power-supply management system design doing integration.

Embodiment 1:

As shown in Figures 2 and 3, it is install solar panel 5 by supporting structure on the electrical motor armshaft extending structure 3 of many cyclogyros 1 that the utility model is improved one's methods to the first of this many cyclogyro 1, solar panel 5 can be arranged above many cyclogyros 1 or around many cyclogyros 1, solar panel 5 adopts donut structure, as shown in Figure 2, the mechanism cracking to reduce windage of the structure changes that solar panel 5 design takes point section to rotate, and the mechanism tending to sunlight regulating plate face version respectively.

Solar panel 5 is connected with charger by supply cable, and charger is connected with the storage battery be arranged on many cyclogyros 1, is powered by the current consumer of the storage battery on many cyclogyros 1 to many cyclogyros 1.

Solar panel 5 can adopt solar film battery, is combined to form applicable voltage/current to facilitate the electric power system formed many cyclogyros 1 through battery cell.If need the design of solar panel 5 to be connected on many cyclogyros 1, solar energy film can be connected on solar panel 5, and the material structure of honeycomb or other Specific gravity selected by this plate, forms the configuration of certain rigidity, convenient installation on many cyclogyros 1, also can dismantle.Simultaneously, consider when designing its configuration that being conducive to daylighting area maximizes, also consider to be conducive to wind resistance in-flight, as shown in Figures 2 and 3, typical solar panel 5 configuration is designed to the donut of plane, interior circular diameter empties the air flow passage as screw propeller 2 according to motor helical oar 2 circumscribed enveloping diameter of many cyclogyros 1, the outside diameter of donut according to solar cell electric power needed for area design, solar panel aspect is not limited to donut, such as also comprise concentric many annulus, concentration ellipsis, concentric polygon, and plate face does not have/does not have pertusate aforesaid aspect.In addition, solar panel 5 around a kind of parachute-like structure of formation, forms one to many cyclogyros 1 and lifts power, can improve the hang time of many cyclogyros 1, reduce the energy consumption of many cyclogyros 1 above the spheroid fuselage 4 of many cyclogyros 1.

As for the connection mode of solar panel 5 with the structure of many cyclogyros 1, method of designing and system more, principle is not only solid but also make weight cost little, simple method of designing and system stretch out along rotor arm configuration, and in conjunction with the constructional feature of solar panel 5, suitable connection is carried out to the single arm structure extended respectively, with good rigid support solar panel 5.

Such as, when the electric power of solar panel 5 needs 400W, if solar battery thin film photoelectric conversion rate is 30%, then the solar battery thin film area needed is about 1m ².If circumscribed enveloping diameter when many cyclogyros 1 four or six screw propellers 2 rotate is 1.5m, then concentric circles internal diameter is about 1.5m.So the outside diameter of solar panel 5 should be 1.877m, can be designed as 2m.Solar panel 5 can be designed as flat board, or be designed to the taper shape of epirelief, still lower convex taper shape is designed to, even be designed to the structure of piecemeal to regulate it towards the direction of sunlight respectively and to be conducive to wind resistance, for this reason, the areal calculation of solar panel 5 should consider that suitable area margin is to compensate invalid daylighting area.

Embodiment 2:

As shown in Figure 4, the situation of many cyclogyros 1 fixed point flight is mainly used in.

In that case, solar cell is earthbound solar energy power panel 6, many cyclogyros 1 control supply cable 11 by the cable reel installation 7 on automobile 12 and control as kiteflying, and automobile 12 is arranged power-supply management system 8, power-supply management system 8 comprises charger and storage battery.

In this case, the design of solar cell is mounted on ground or car, i.e. earthbound solar energy power panel 6 and Vehicular solar power supply 13, and the weight of solar cell is no longer responsive, can solar battery thin film be selected, or the solar cell of other materials.The design of solar panel can be more traditional, and the structure design being particularly arranged on the solar panel on automobile 12 more can consider the rigidity of its structure and the convenience of installation, even can consider the foldable structure of solar panel.In order to the ability of powering round the clock can be provided, the power supply introducing automobile current generator 10 can be considered, Portable storage battery power supply, and civil power 9 power supply etc. forms AC-battery power source together with earthbound solar energy power panel 6, the power supply different to these power quality, the automatic distribution management that can carry out conversion process with the power supervisor in power-supply management system 8 and concentrate, powers to many cyclogyros 1 by charger and supply cable 11.In power-supply management system 8, the function that power supervisor and charger can merge power conversion does integrated design.Because consider that fixed point flight just done by many cyclogyros 1, therefore, the AC-battery power source on method of designing and system upper ground surface or car be also can not highlight removable.

Embodiment 3:

As shown in Figure 3, the situation that many cyclogyros 1 move flight is mainly used in.

On the basis of embodiment 2, if consider that many cyclogyros 1 are mobile flight, then ground AC-battery power source also should be applicable to the mobile needs used, typical method of designing and system are by solar battery power, portable battery feed, and automobile current generator 10 power supply all carries out vehicle-mounted design, form Vehicular solar power supply 13.Particularly the design of supply cable 11 needs emphasis to consider the feature of mobile power supply.Some design measure can be selected, one is and the connection method of designing of many cyclogyros 1 and system, prevent from being wound around and blocking, for preventing supply cable 11, observation load movable on many cyclogyros 1 is wound around, the supply cable 11 being connected to the consumer on many cyclogyros 1 can design two attachment points, the anatomical connectivity of the consumer on an attachment point and many cyclogyros 1, another attachment point is then according to the scantling of structure of many cyclogyros 1, by second of supply cable 11 attachment point design on many cyclogyro 1 landing supports or on custom-designed fixed mount, keep with the suitable distance of The Cloud Terrace motion structure and make the moment of the center of gravity to many cyclogyros 1 as far as possible little, this attachment point is as the load fastening point of bearing wind-force or tractive force, The Cloud Terrace work about 180 degree or 360 degree left-right rotaries of observation load can be allowed to transfer not to be powered cable 11 be wound around or block, also can control suitably to rotate the course of many cyclogyros 1 oneself to be avoided by ground even if block.Two is adopt navigation information to keeping safety and rational positional distance between many cyclogyros 1 and the power supply being arranged on moving vehicle, the appropriate length of maintenance supply cable 11, prevents cable to mop floor wearing and tearing, also alleviates the active area of wind-force to supply cable 11.Three is consider to design a kind of cable reel installation 7 onboard, carries out Electronic control folding and unfolding or hand-turning folding and unfolding to the length of supply cable 11, avoid artificial carelessness make mobile in the unnecessary cable length of traction to be damaged fault.

Because the common flying speed of many cyclogyros 1 is comparatively slow, in vehicle-mounted mobile, air-flow is to the interference of cable and wind-force to compared with the interference of cable, and the interference of wind-force is stronger.Supply cable 11 is under wind-force effect, the pulling force that there is a downward also lateral deviation acts on many cyclogyros 1, for ensureing the rated wind velocity performance of many cyclogyros 1, design can adopt Several Measures, one is the many cyclogyros 1 selecting lift capability larger, by the rich lift of many cyclogyros 1, improve the performance of the windage pulling force that carrying supply cable 11 exists.Two is Joint strenghts supply cable 11 being connected to ground and many cyclogyros 1 two ends, selects the cable type specification with applicable intensity.Three is that when there is larger wind-force weather, namely the flying height reducing many cyclogyros 1 shortens cable length of wind, or allows many cyclogyros 1 land wind sheltering in time.

In the embodiment above, in the method for designing implementing to fly when many cyclogyros 1 are long to navigate and system, the consideration of economy is necessary, can carry out cutting to aforesaid method of designing and system.One is the material of solar cell for surface power supply, can select the hull cell that conversion ratio is very high, the every square meter of the material price of 2015 of this up-to-date technology about 150,000 yuan or more expensive.Select the material of conversion ratio about 20%, increase area and just can meet electrical power requirements, and price can reduce a lot.Two is in the method for designing and system of AC-battery power source and power-supply management system 8, and the various power supplys in AC-battery power source can independent utility, only very low with the power supply cost of automobile current generator 10, round-the-clockly can apply, and saves the cost of solar cell.Power supervisor in the utility model in order to carry out automatic management design to AC-battery power source, can substitute with artificial conversion for common use, such as during vehicle-mounted mobile electric power thus supplied, one people drives the conversion of another people's managing electrical power, because by storage battery power supply on many cyclogyros 1, the time of carrying out Power convert on ground is not long, can ensure the continued power to flight, saves the expense of configuration power supervisor.The another kind of method of designing saved power supervisor and charger is merged to do integrated design as power-supply management system 8.Three is the designs for cable reel installation 7, be cut to lengthen for improving cable and realize Electronic control or rocking arm rotates folding and unfolding, and can be completed by manually free-hand in common use, even if the situation that vehicle-mounted mobile uses, one people drives another people can free-hand folding and unfolding cable length, saves the expense of configuration cable reel installation 7.Equally, the object of employing navigation information is the relative distance of the vehicle power controlling many cyclogyros 1 and ground moving, realize the automatic control to cable length, this design also can be substituted by the manual operation on car, and the technology that reducing increases navigation information is applied and increases cost.Therefore, the utility model is implemented to many cyclogyros 1, by the cutting of design above and in apolegamy, the popularization of the larger field of application of many cyclogyros 1 can be realized at lower cost, improve economic gain.

In above embodiment, described many cyclogyros 1 are existing products, or provide improved products.Solar cell is can by the amorphous of maturation/polycrystalline solar cell film, or other materials solar cell makes.Multiple power sources is formed AC-battery power source or power supervisor is all proven technique or combines with matured product, though power supervisor and merging into a single whole of charger are designed as power-supply management system 8 be also mature technology.Supply cable 11 also has the description of plurality of optional.

Certainly, more than just embody rule example of the present utility model, the technical scheme that the utility model also has other embodiment, all employings to be equal to replacement or equivalent transformation to be formed, all drops within the protection domain required by the utility model.

Claims (4)

1. the flight power-supply system when captain of rotor more than navigates, it is characterized in that: it comprises the many cyclogyros (1) being provided with storage battery, this many cyclogyro (1) is provided with solar electric power supply system; Described solar electric power supply system be below any one:

Be arranged on the power-supply management system (8) on ground or automobile (12), power-supply management system (8) is powered by earthbound solar energy power panel (6), and power-supply management system (8) is powered by the consumer of supply cable (11) to many cyclogyros (1) or charged a battery;

Be arranged on the power-supply management system (8) on ground automobile (12), power-supply management system (8) is powered by Vehicular solar power supply (13), and power-supply management system (8) is by the battery charge of supply cable (11) to many cyclogyros (1).

2. flight power-supply system when many rotors captain according to claim 1 navigates, it is characterized in that: solar panel (5) is removably mounted on the electrical motor armshaft extending structure (3) of many cyclogyros (1), the platy structure that solar panel (5) is donut.

3. when many rotors captain according to claim 1 navigates fly power-supply system, it is characterized in that: described in the power-supply management system (8) be arranged on ground automobile (12) comprise storage battery, charger.

4. flight power-supply system when many rotors captain according to claim 1 navigates, it is characterized in that: supply cable (11) design two attachment points being connected to many cyclogyros (1) consumer, the anatomical connectivity of the consumer on an attachment point and many cyclogyros (1), another attachment point is used to an attachment point of clamping supply cable (11), and another attachment point described is designed on many cyclogyros (1) landing support or on fixed mount according to the scantling of structure of many cyclogyros (1).