CN106621385B - External power supply power supply remotely-piloted vehicle systems approach and device - Google Patents

Abstract

External power supply power supply remotely-piloted vehicle system, including aircraft, external power supply and remote controler, the power transmission line using connection external power supply and aircraft make external power supply continually supply aircraft.Fixed point or small range are only being needed in use, external power supply remotely-piloted vehicle of the present invention can save battery weight by means of external power supply facility and possess empty flight performance stagnant for a long time.The sphere of action of aircraft can be defined using power transmission line, thus facilitate the negative effect for reducing it as modern weapon.

Description

External power supply power supply remotely-piloted vehicle systems approach and device

Technical field

The present invention relates to the method and devices of external power supply power supply remotely-piloted vehicle system.

Background technique

Existing electric remote control aircraft includes fixed-wing and rotary wind type, and wherein rotary wind type can be divided into single rotor and more rotations again The wing, they drive by battery, being capable of the free flight within the scope of certain space.But its hang time is limited by battery capacity System.

Summary of the invention

The invention aims to provide the method and device of hang time longer remotely-piloted vehicle.

External power supply power supply remotely-piloted vehicle systems approach of the present invention: one external power supply power supply remotely-piloted vehicle system of manufacture System, including aircraft, external power supply and remote controler；Aircraft includes fixed-wing and rotary wind type two major classes；Aircraft include fuselage, Electronic rotor, state of flight computer control system, radio signal reception processing launch facility and aircraft load, flight shape State computer control system includes satellite positioning-terminal, accelerometer, magnetometer, pressure sensor and gyroscope, using one group with The power transmission line in the power load of external power supply and aircraft composition circuit；External power supply continually supplies aircraft；

A power supply unsteady flow module is manufactured, realizes that by the high voltage-small current electric energy morphological transformation of power line transmission be described fly The electric energy form that row device needs, power supply unsteady flow module include transformer, inverter and the circuit powered to direct current generator；Or

An automatic connector is concatenated between power transmission line and the aircraft, automatic connector includes that an electric wire connecting junction is inserted Seat and an electric wire connecting junction plug；Electric wire connecting junction plug is connect with power transmission line；And contain a power transmission line automatic locking device part；Electric wire connecting junction Socket and power transmission line automatic locking device part are set on fuselage；Power transmission line automatic locking device part is controlled as state of flight computer The execution unit of system；Power transmission line automatic locking device part includes an electronic pressure tongue, and electronic pressure tongue includes electromagnetism pressure tongue；Electronic pressure Tongue is normally closed to push down power transmission line, when the state of electronic pressure tongue from it is normally closed become opening when, electric wire connecting junction plug is in itself and power transmission line weight The lower disengaging fuselage of power effect is fallen: or

Aircraft contains an automatic wire winding device, the power transmission line being located below for folding and unfolding；Or

The electric line carrier communication mould being connect on board the aircraft and at external power supply containing one with powerline signal Block realizes that wire signal transmits using power line carrier；To the control of aircraft flight state include use the prior art and with Lower technology:

The motor of each electronic rotor is direct current generator, and the correspondence winding of each motor is using being connected in series, to described each At least one winding difference multifunction module in parallel of motor, changes control institute by changing the state of multifunction module State the state of each motor；Or

The motor of each electronic rotor is AC induction motor and directly utilizes the work of external three-phase alternating voltage, each electricity The three-phase windings of machine using three branches are connected in series to form, at least one winding to each motor or winding A part of parallel connection multifunction module, and each phase power supply is evenly distributed with multifunction module；Changed by changing the state of multifunction module Become the state for controlling each motor；Or

Work after the motor of each electronic rotor is AC induction motor and is depressured external three-phase alternating voltage using transformer Make, the three-phase windings of each motor using three branches are connected in series to form, at least one winding to each motor or A part of one winding of person or a part of multifunction module in parallel with the transformer of the winding parallel, pass through change The state of multifunction module controls the state of each motor to change；

It further include using the general linkage interface of more than one functional component, or contain more than one functional component,

It further include using the aircraft more than two framves, the power load of two frame the above aircraft passes through same group Power transmission line is concatenated into a circuit loop；Power transmission line contains one group of automatic branching electric wire connecting junction close to intermediate position, and automatic branching connects Line device contains the interface circuit connecting with state of flight computer control system wireless signal；The shape of automatic branching electric wire connecting junction State changes according to the state of state of flight computer control system and is changed；Or

More than two rotor crafts are electrically connected by one group of power transmission line and external power supply；The rotor craft and same One embedded connection of aircraft load, the aircraft load include rigid and nonrigid；In the rotor craft Directly or indirectly signal is connect at least two aircraft and its state is according to the remote controler with the same remote controler The change of state and change.Further include setting track, and enables the trolley travelling for loading external power supply on track；Further, also Including setting and the power main of parallel track or integrated production；

The present invention realizes one of the technical solution of its purpose according to the method described above: one external power supply of manufacture flies for electrical remote control Row device system, including aircraft, external power supply and remote controler, aircraft include fixed-wing and rotary wind type two major classes；Aircraft packet Include fuselage, electric propeller or electronic rotor, state of flight computer control system, radio signal reception processing transmitting set Apply with aircraft load, state of flight computer control system includes satellite positioning-terminal, accelerometer, magnetometer, pressure sensing Device and gyroscope, using one group and the power transmission line in the power load of external power supply and aircraft composition circuit.

The power transmission line can be connect from any orientation with aircraft.The power transmission line is using a piece-root grafting or all institutes It is earth-free to state power transmission line.

One end of distributor electrical connection in power transmission line and fuselage is known as proximal end, and power transmission line and external power supply are electrically connected One end be known as distal end；External power supply persistently supplies the aircraft electrical energy by power transmission line.

Aircraft load includes emitting received facility for wireless telecommunications, for example wifi.Related content can be with reference to both There is technology.

A power supply unsteady flow module can also be used, the high voltage-small current electric energy morphological transformation of power line transmission is by realization The electric energy form that the aircraft needs, power supply unsteady flow module include transformer, inverter and the direct current powered to direct current generator Step-up/step-down circuit；Or

An automatic connector is concatenated between power transmission line and the aircraft, automatic connector includes that an electric wire connecting junction is inserted Seat and an electric wire connecting junction plug；Electric wire connecting junction plug is connect with power transmission line；And use a power transmission line automatic locking device part；Electric wire connecting junction Socket and power transmission line automatic locking device part are set on fuselage；Power transmission line automatic locking device part is controlled as state of flight computer The execution unit of system.Power transmission line automatic locking device part includes an electronic pressure tongue.Electronic pressure tongue includes electromagnetism pressure tongue, electronic pressure Tongue is normally closed to push down power transmission line；When the state of electronic pressure tongue from it is normally closed become opening when, electric wire connecting junction plug is in itself and power transmission line weight The lower disengaging fuselage of power effect is fallen.Related technology can also refer to existing relay and Solenoid Valve Technology.

Aircraft can also be enabled to contain an automatic wire winding device, the power transmission line being located below for folding and unfolding；Or

It is respectively provided with the electric line carrier communication mould connecting with powerline signal on board the aircraft and at external power supply Block realizes that wire signal transmits using power line carrier.

Electric wire connecting junction plug and/or fuselage can also be enabled to connect a parachute, and set: is de- when being issued to electric wire connecting junction plug It disembarks after the instruction of body 0.2 second, parachute starts to open.In this way, providing the means of an aircraft security, can also make to connect Speed when line device plug and power transmission line are fallen down is unlikely to too fast, it is ensured that power transmission line is stowed away.

It is the rotary aircraft of an axis or more, including more than one electronic rotor that the aircraft, which can also be enabled,；

And it is more than two to enable each motor of all electronic rotors of driving be divided into according to two one group of Space Axisymmetric distribution Motor group enables each stator winding of the motor of each motor group be connected in series to form one or more branch, adopts to the branch Mode in series or in parallel is taken to connect with the external power supply；

A part of multifunction module in parallel of at least one winding or a winding to every motor and every Branch described in item at least contains a multifunction module；

Multifunction module includes flight control circuit, controlled rectification or chopper circuit, rechargeable battery, power load and vacation Load；Controlled rectification or chopper circuit adjust its power output by changing the service time of rectifying device；Power load Including filter circuit of pressure-stabilizing, state of flight computer control system, flight control circuit, for detecting each multifunction module electric current With the detection device, radio reception transmit circuit and other all possible electricity consumption devices of voltage；Fictitious load includes can power transformation Resistance also includes fixed resistance device and concatenates with it silicon-controlled, and fictitious load is for consuming electric energy to influence its rotation in parallel The state of wing motor and all rotor motors；Flight control circuit work normally when can also completely from rechargeable battery take electricity without Electricity is taken from controlled rectification or chopper circuit, it means that aircraft power supply capacity increased；Flight control circuit is as winged A part of row state computation machine control system connect and connects with state of flight computer control system host signal and is controlled by it； Change the state for controlling each motor by changing the state of multifunction module, comprising: as needed, when the shape of aircraft State control requires to fly to some direction, can enable in parallel with the rotor motor in the direction is located under the guide of gyroscope Multifunction module consumes some electric currents more, specifically includes the silicon-controlled when opening of the fictitious load branch for enabling related multifunction module Between it is longer；Or enable the resistance value of variable resistance become smaller, therefore the rotor because the by-pass current of motor to increase itself defeated Entering power and reducing lift and also reduces causes lift generation one of the aircraft axial line run-off the straight to aircraft to the side To horizontal component push aircraft mobile to the direction；Silicon-controlled one as flight control circuit concatenated with fictitious load A execution unit, it is ensured that power control of the flight control circuit to each multifunction module；For because the multifunction module increases The problem that adds using energy and may cause aircraft lift deficiency, can solve by other means, including increase external electrical The voltage in source solves；

Each aircraft can also provide the thrust of horizontal direction using special lateral thrust rotor；

The suitable power load of electric attribute can also be in series or in parallel with the branch of all motor forms；

The motor that each electronic rotor can also be enabled includes direct current generator, is connected between the winding of each motor using series connection It connects, to one multifunction module of at least one winding parallel of each motor, by the state for changing the multifunction module To change the state for controlling each motor；Or

It enables the motor of each electronic rotor be AC induction motor and is directly worked using external three-phase alternating voltage, it is described each The three-phase windings of motor use and are connected in series to form three branches, at least one winding or a winding to each motor A part of multifunction module in parallel, and each phase power supply is evenly distributed with multifunction module；By change multifunction module state come Change the state for controlling each motor；Or

The motor for enabling each electronic rotor is AC induction motor and will be after the decompression of external three-phase alternating voltage using transformer Work, the three-phase windings of each motor are using three branches are connected in series to form, at least one winding of each motor Or winding a part or a part of multifunction module in parallel with the transformer of the winding parallel, by changing Become the state of multifunction module to change the state for controlling each motor.

It is the above rotary aircraft of four axis that the aircraft, which can also be enabled, which includes one and rotor Film-form object in same level position；The area of the film-form object is 0.4 square metre or more and weight to the greatest extent may be used It can be light；Film-form object aperture at electronic rotor；Or

It includes blacking or film-form that film-form object, which has high-absorbility characteristic for transparent perhaps tympan body surface face, Object includes film photovoltaic cell；

Film photovoltaic cell can use sunlight and provide electric power.Film-form object can allow sunlight to penetrate and arrive to be transparent Up to the photovoltaic cell on fuselage.Film-form object has high-absorbility characteristic can will too on the barrier effect of air and its surface Sunlight be changed into thermal energy be used to form fire balloon effect help promote the aircraft to save electric power.Film-form object can be with The thermal current risen using lower section, which is lifted, asks the aircraft to reduce power consumption；Just as eagle stretch open wings it is motionless can be The case where spiraling in the air.Film-form object can be also used for umbrella effect, at this moment, airintake wind-tunnel or air inlet thereon Then can not only keep off the rain the hail side of blocking pendant object protection rotor, but also can ensure that rotor works normally.

The general linkage interface of more than one functional component can also be used, or uses more than one functional component,

The functional component further includes a telemechanical flame atomizing device.For national defence and to struggle with mountain fire and prior It burns used in isolation strip.

The functional component further includes projectile weapon and electromagnetism projectile weapon.Pirate's self-defence, fright are tackled for ocean liner Or eliminate terrorist.

The functional component further includes bomb, kinetic energy bomb or glomb and high-pitched speaker, for alerting to vessel Form the sea rover threatened and for antitank on battlefield.

The functional component further includes more physical quantity transducers.Including collect itself by strike position and intensity letter It ceases and sends, the firepower for battlefield is investigated.

The functional component further includes that a tracking powder dispenses device.This tracking powder is invisible but available special It is observed, and can remained in for a long time on the hair and clothes of people with equipment, in the feelings for letting alone target person Cullet are arranged on road to help to seize to destroy the people and other bad persons of tire in setting flag under condition.Related tracking powder The content at end can refer to the prior art.

The functional component further includes airport bird scaring device, including sound scarer.

The functional component further includes explosive dismounting or apparatus to cause bursting；Thunder device and submarine mine device is swept including sweeping the floor.

The functional component further includes laser cutting device, for cutting object to be treated.

The functional component further include hang on flexible cable below rotor craft perhaps cloth be used for building or Photovoltaic battery panel sweeps away snow.

The functional component further includes single load interface, the single load interface include buttocks sling apparatus and One handgrip.Buttocks sling apparatus can lift related personnel.Handgrip can make related personnel that the aircraft be caught to make in short-term Between fly.It is suitble to scene to transport soldier and fireman.

These functional components can be applied in combination, and for example spray and sow simultaneously.It is general using more than one functional component Linkage interface can be dual-use with a tractor serves several purposes, manufacturing products for both peacetime and wartime us by connecting different functional components.

It can also enable containing a revolute pair mechanism between automatic wire winding device and basis, so that the automatic wire winding device Energy pivoting can be prevented in this way because of the winding of power transmission line nocuousness or rotation that the reasons such as the aircraft circuit generate Turn.

Or the interior storehouse for enabling the line storehouse of non-bare wire automatic deploying and retracting line apparatus contain the manufacture of a conductive material, the interior storehouse are protected Hold the high potential being had close to non-bare wire.The operating condition of non-bare wire in cabin can be kept good in this way.

Same group can also be passed through using the aircraft more than two framves, the power load of two frame the above aircraft Power transmission line is concatenated into a circuit loop；Power transmission line contains one group of automatic branching electric wire connecting junction close to intermediate position, and automatic branching connects Line device contains the interface circuit connecting with state of flight computer control system wireless signal；The shape of automatic branching electric wire connecting junction State changes according to the state of state of flight computer control system and is changed；In this way, can use unmanned plane described in a wherein frame The weight or wind-force for bearing part power transmission line, can be improved wind loading rating.

In this way, can also realize the turn at mountainous region, can be tied down to avoid power transmission line by the water surface in water surface flying.

Alternatively, several rotor crafts can also be enabled electrically to connect by one group or a branch of power transmission line with external power supply It connects；Several described rotor crafts and the embedded connection of the same load, the load include rigid and nonrigid；It is described At least two aircraft in several rotor crafts and the same remote controler directly or indirectly signal connect and Its state changes according to the change of the remote controller state.

Speed regulation mentioned herein includes for the state control to aircraft.

Rotor craft includes a column and multiaxis rotor craft, and a column includes single-blade and double-vane.

Surface of two naked steel wire power transmission lines at bifurcated terminals above can also be provided with insulating layer；Or

The monitor being connect containing one with state of flight computer control system host signal on the aircraft；Or Person

It is passed on the aircraft containing an acceleration being connect with state of flight computer control system host signal Sensor.

A spray unit, including two frame rotor crafts spray aircraft, assisting in flying device and logistics can also be formed Vehicle, logistics vehicle are mounted with automatic wire winding device, the automatic retraction device of water delivery pipe, external power supply and pesticide container；Use power transmission line Connect external power supply and power load on aircraft unit, on spray aircraft containing spray port, using a both ends point The delivery pipe not being connected to spray port and pesticide container；Or

Form a sowing unit, including two frame rotor crafts sowing aircraft, assisting in flying device and logistics vehicle, logistics Vehicle be mounted with automatic wire winding device, external power supply, seed transport tube automatic retraction device and seed cabin；It is outer with power transmission line connection Portion's power supply and power load on aircraft unit, on sowing aircraft containing sowing module, using a both ends respectively with broadcast The seed transport tube that kind module is connected to seed cabin.

It can also be using an optical fiber connection aircraft and extraneous realization optical-fibre communications.

The present invention realizes the two of the technical solution of its purpose according to the method described above: one external power supply of manufacture flies for electrical remote control Row device system, including aircraft, external power supply and remote controler, aircraft include fixed-wing and rotary wind type two major classes；Aircraft packet It is negative to include fuselage, electronic rotor, state of flight computer control system, radio signal reception processing launch facility and aircraft Lotus, state of flight computer control system include satellite positioning-terminal, accelerometer, magnetometer, pressure sensor and gyroscope, are adopted With one group and the power transmission line in the power load of external power supply and aircraft composition circuit.

And external power supply is enabled to be installed on a vehicle.Visitor directly is transported to from express delivery vehicle for use in by courier packages On the balcony of family.Or external power supply is enabled to be installed on a naval vessel.Or external power supply is enabled to be installed on a submarine.Or External power supply is enabled to be installed on another aircraft.Or external power supply is enabled to be installed on aerial ladder.Or enable external power supply It is installed in other machines or robot；Or external power supply wearing is cared on the body of people and animal.It is trained For example dog can load external power supply and the aircraft is followed to move on sandy beach animal.This conveniently takes photo by plane；Or

Track, including aerial conveyor are set；Aerial conveyor include several stubs and connect by stub with ground one Two rail of group；Aerial conveyor further include using one group two mutual electric insulations and respectively with two electrode electricity of power supply The rail of gas connection；Rail doubles as power main, is formed together circuit with power supply and power load；Track further includes using two The form of closed conduct, the pipeline are used for trandfer fluid, and fluid includes water, liquid pesticidal and fertilizer；Or

Using independent Transmission main line, independent Transmission main line be arranged with parallel track and with power supply, load and the earth together shape At a circuit；Typical independent Transmission main line includes the power main above electric railway；

The place of track setting includes but is not limited to our side of ground, forest zone and boundary line,

Traveling loads the logistics vehicle of external power supply in orbit；Logistics vehicle includes the chassis with electric wheel set and logistics vehicle Computer control system, logistics vehicle load external power supply, and external power supply is powered by power transmission line to aircraft；

The vehicle travelled in orbit further includes freight trolley and by electric trolley；

Freight trolley includes the chassis with electric wheel set and freight trolley computer control system, and purposes includes loading agriculture Woods herds product and feed fertilizer and pesticide；

Included the chassis with electric wheel set, current collector part and by electric trolley computer control system by electric trolley, and passed through Power transmission line is powered to aircraft；

Current collector part is used to be electrically connected with the track or independent power main；Typical current collector part is electrical Change the pantograph of railway locomotive；

Electric wheel set includes idler wheel and the sliding block with track cooperation, and sliding block and track cooperation are able to take upward and side Pulling force is without departing from track；Sliding block is a kind of universal component being cooperatively connected with track；Stub is a kind of commonly using for aerial conveyor Component, simple pier stud include the steel pipe with concrete pipe base；The particular content of sliding block and stub can refer to the prior art；

Logistics vehicle and freight trolley further include current collector part；

A video monitor is configured on the aircraft, on site including the video monitoring near national boundary；

Or an early warning radar is configured on the aircraft, for completing the work of early warning plane and early warning can be formed Band.Possessing for the unmanned early warning plane of external power supply is low with use cost, can each naval vessel one frame of configuration or multi rack；Or A wireless network communication local area network antenna facility on the aircraft provides Communications service to outlying district.

A computer control system is also configured on ground.

Beneficial effects of the present invention: when only needing fixed point or a small range using related aircraft, the present invention When the remotely-piloted vehicle of external power supply power supply can save the weight of many batteries and possess long by means of external power supply facility Between stagnant empty flight ability.Can make inercant ships pool that there is the protection capability for dealing with a plurality of sea rover attack --- it is self-dependent Pre-alerting ability finds the suspicious boat other than 10 kms, once suspicious boat leans on too for example 60 meters nearly, sets out the nothing immediately Man-machine carrying gasoline or combustion gas.The strike of shock wave that oil gas fires can make pirates that dare not go again to invade or open easily Fire.Due to power supply freedom, unmanned plane described in a frame can be in 1 minute by three pieces of electromagnetism shooting burnings of power transmission Bullet.Into before harbour, if the case where reporting all unmanned planes to maritime sector and by firebomb oil gas take out, that is, recognize For in no longer holding any automatic weapon state.

May be implemented to still maintain regular flight condition in satellite positioning signal poor quality using pressure sensor and It is unlikely to direct aircraft bombing.Secrecy is more advantageous to using power line transmission signal.

The present invention can also be used to that puppet role, background and performer be arranged in the sky, and it includes aerial for carrying out performance in the sky The bullfight of machine ox is obtained than by being carried out synthesizing better visual effect to picture with software.The present invention can also use In in water surface setting screen broadcasting film or video program.Amateur photographers also can use aircraft of the invention and clap Take the photograph acquisition and using shooting effect in midair similar in large-scale photography facility.The present invention can also be by pulling electricity over long distances in the sky The mode of the line of force is used to provide driving power for the agricultural machinery on terraced fields.

Aircraft of the invention includes various unmanned flight's devices, using power transmission line can sphere of action to aircraft into Row limits, thus facilitates the negative effect for reducing it as modern weapon.

Detailed description of the invention

Fig. 1 is that an external power supply power supply fixed-wing remotely-piloted vehicle is connected with external power source structural schematic diagram.

Fig. 2 is that the aerial marshalling of an external power supply power supply rotor remotely-piloted vehicle is connected with external power source structural representation Figure.

Fig. 3 and Fig. 4 is the double plug in automatic connectors in three ends respectively to be inserted into singly slotting states and changes structural schematic diagrams from double, Its amplification that can be regarded as the double plug in automatic connectors in three ends in Fig. 2 embodiment.

Fig. 5 is one and utilizes the structural schematic diagram that following aircraft is that aircraft above shares transmission of electricity specific electric load.

Fig. 6 is a power transmission line surface setting tooth and engages the structural representation for realizing transmission connection with synchronous pulley Figure.

Fig. 7 is a power transmission line azimuthal structural schematic diagram of 270 degree of winding or more on driving idler wheel.

Fig. 8 is the circuit block diagram of the 4 asynchronous motors concatenation of a 4 axis rotor crafts.

Fig. 9 is the upper view structural schematic diagram of an external power supply 4 axis rotor remotely-piloted vehicles of power supply.

Figure 10 is the functional block diagram of a multifunction module.

Figure 11 is an autocoupling type three-phase transformer circuit diagram.

Figure 12 is one 4 electronic rotor direct current generator series connection and motor and the block diagram for connecing multifunction module.

Figure 13 is the top view of a quadrotor external power supply power supply remotely-piloted vehicle system with separation layer.

Figure 14 is the front view of a quadrotor external power supply power supply remotely-piloted vehicle system with separation layer.

Figure 15 is the schematic diagram that wire signal transmission is carried out using power transmission line.

Figure 16 is the working principle diagram of an agricultural chemical spraying flight unit.

Figure 17 is the working principle diagram of an agricultural sowing flight unit.

Figure 18 is the structural schematic diagram of several rotor crafts one load of embedded connection.

Figure 19 is the work on the spot schematic diagram of a shared external power supply remotely-piloted vehicle ultrahigh speed cleaning device.

The work powered by electric trolley to aircraft on mono- aerial conveyor operated in as power main of Figure 20 is former Reason figure；Figure 21 is in Figure 20 circle of dotted line by the enlarged drawing of electric trolley.

1. aircraft in figure；2. fuselage；3. electric propeller；4. remote controler；5. external power supply；6. power transmission line；7. automatic Coiling apparatus；8. wheel group；9. chassis；10. Plane Rotation vice mechanism；11. line storehouse；12. line door；13. double insert in three ends connects automatically Line device；14. unmanned ship；15. the water surface；16. socket；17. plug；18. Auto-plug lock；19. electronic rotor；21. Spring；22. support block；23. electronic pressure tongue；24. electric reel；25. pedestal；26. bifurcated terminals；27. monitor；28. accelerating Spend sensor；29. automatic wire winding device；31. tooth；32. synchronous pulley；33. limiting pressure roller；34. closed bin；35. aluminium sheet Inner cylinder；36. absorb heat coil pipe；37. blower；38. lineation wheel group；41. idler wheel；42,43,44,45. electronic rotor；42.1,43.1, 44.1,45.1 motor；46. parachute；47. variable resistance；48-51. multifunction module；52. direct current generator；53. controlled rectification Or chopper circuit；54. rechargeable battery；55. power load；56. fictitious load；57. transformer；58. winding；59. early warning thunder It reaches；60. separation layer；61. flange；62. lightweight retaining frame；63. axis stream air passage；64. high-pressure area；65. area of low pressure；66. aerial Video camera；67. PLC communication module；68. spray aircraft；69. assisting in flying device；70. rise and fall platform；71. pesticide Tank；72. logistics vehicle；73. spray port；74. delivery pipe；75. sowing aircraft；76. seed cabin；77. sowing module；78. kind Sub- delivery pipe；79. load；80. flexible cable cloth；81. photovoltaic battery panel；82. mountain forest；83. stub；84. rail；85. power supply； 86. electric wheel set；87. current collector part；88. terraced fields；89. agricultural machinery.

Specific embodiment

Fig. 1 provides embodiment 1.

In embodiment 1, an external power supply power supply fixed-wing remotely-piloted vehicle 1, including fuselage 2, electric propeller are manufactured 3, state of flight computer control system, radio signal reception processing launch facility, aircraft load and remote controler 4, use One group two form the power transmission line 6 in circuit with external power supply 5 and aircraft power load.

6 one end proximal end of power transmission line and aircraft 1 are electrically connected, and other end distal end and an automatic winding for power transmission line 6 fills 7 transmission connections are set, and are electrically connected by automatic wire winding device 7 and external power supply 5；External power supply 5 is persistently supplied by power transmission line 6 Answer 1 electric energy of aircraft.

Automatic wire winding device 7 includes chassis 9, Plane Rotation vice mechanism 10 and the electronic reel of belt wheel group 8.Automatic winding The distance that flies away from of the device 7 with aircraft 1, automatic deploying and retracting power transmission line 6.The chassis 9 of belt wheel group 8 fills automatic winding Setting 7 can move freely.Plane Rotation vice mechanism 10 is for 7 pivoting of automatic wire winding device above chassis 9.Automatic winding Device 7 can not also include chassis 9 and the plane revolute pair mechanism 10 of belt wheel group 8.

A line storehouse 11 is also provided with inside fuselage 2, line storehouse 11 has a line door 12, inside setting The power transmission line of winding；When line door 12 is opened, the power transmission line inside line storehouse is orderly pulled out.It is just beaten in Fig. 1 for line door 12 The situation opened.Line storehouse 11 can be the hollow cage constituted using several parallel shafts.

Line storehouse 11 is mainly used for the relatively low situation of flight path last stages of aircraft 1, including enemy position is gone to hold At this moment row task requires patch ground flying as far as possible to keep hidden, just very suitable using the orderly unwrapping wire in line storehouse 11.

Fig. 2 provides embodiment 2.

In embodiment 2, an aerial marshalling is formed with two frame rotor remotely-piloted vehicles 1.Aircraft 1 includes fuselage 2, electronic Rotor 19, state of flight computer control system, radio signal reception processing launch facility, aircraft load and remote controler 4. Two frame aircraft 1 share the automatic winding on one group of power transmission line 6 and unmanned ship 14 by a multichannel automatic socket device 13 Device 7 connects and takes electricity from external power supply 5.

It is used to share the weight of part power transmission line, referred to as assisting in flying device using the frame in two frame aircraft 1, takes on Task include pull-up power transmission line 6 to avoid the other farther away aircraft of frame flying distance --- main carry-on power transmission line 6 readily access the unfavorable operating condition of the water surface 15.

Naval searching is carried out, originally with one 100 tonnes of the scale of construction of manned ship, 10 meters of detector height.Now it is changed to 10 tonnes, the unmanned ship of configuration external power supply power supply remotely-piloted vehicle system, the flying height of the aircraft detect Device height is increased to 50 meters, and search efficiency improves 1000 times.It enables the carry-on picture signal be transferred to backstage and realizes people Work auxiliary search, and visited using external power supply power supply remotely-piloted vehicle system is configured at left and right sides of unmanned ship 10 Survey search.Search efficiency can achieve unprecedented height.Searching ship cost is reduced to original 1/10th.

Compared with the aircraft for fully relying on the self-contained power supply of aircraft, the power supply remote control distributor of 2 external power supply of embodiment The continuous hang time of device system extends to dozens of days from dozens of minutes.

Unmanned ship 14 in embodiment 2 can also be changed to unmanned submarines.Concealment is more preferable in this way.

Main aircraft in embodiment 2 can be newly defined as wired cruise missile.End flight land mine, end flight water Thunder or fish, and related hot weapons are configured, it is used for battlefield.

External power supply power supply remotely-piloted vehicle system itself configures a small amount of power electric battery for returning under the state of emergency Boat.Since the battery of carrying is few, even if calculating the weight into power transmission line, the lift-off weight of external power supply power supply remotely-piloted vehicle system It measures still lower.The aircraft of same load, power of motor are smaller.

Fig. 3 and Fig. 4 provides embodiment 3.

In embodiment 3, the double plug in automatic connectors in three ends include two sockets, 16, two plugs 17 and two Auto-plug locks Determine device 18.Plug 17 is concentric double structure and is electrically connected with power transmission line 6.Concentric double structure particular content can be with reference to existing Having technology includes handset earphone plug.21 sliding fiting sleeve of spring is on power transmission line 6.Auto-plug lock 18 includes support block 22 With electronic pressure tongue 23, and it connect or is electrically connected using signal with state of flight computer control system.Auto-plug locking Device 18 is that normally closed i.e. electronic pressure tongue 23 is protruding and plug 17 is pressed in support block 22 to locking plug 17；At this moment spring 21 In compressive state.Socket 17 is also electrically connected with power transmission line 6.

Once Auto-plug lock 18 instructs to obtain electric opening according to state of flight computer control system host, then electric Dynamic pressure tongue 23 retracts, and plug 17 pops up under the promotion of spring 21, realizes the automatic extraction of plug 17, and power transmission line 6 and aircraft are de- From.

The double plug in automatic connectors 13 in three ends of embodiment 3 remove one group of socket and plug, and picture be rotated up and down after will be remaining Under socket 16 connect with the fuselage of aircraft, just constitute both ends singly plug in automatic connector.It can be used for aircraft and outer The electrical connection of portion's power supply, and power transmission line can be in case of emergency got rid of automatically.Unmanned plane after getting rid of power transmission line can be according to Electric energy by battery makes a return voyage.

Spring in the various automatic connectors of the present invention can also not have to.At this moment it can realize that automatic extract is inserted by gravity Head.Technology in relation to these plugs can refer to the prior art.Usually require that the contact engaging and separating forces of these plugs close to zero.Delivery fire In the electric connector using zero insertion force on arrow.Fig. 5 provides embodiment 4.

In embodiment 4, two frame external power supplies power rotor remotely-piloted vehicle 1 by sharing one group of concatenation of power transmission line 6 and ground The automatic wire winding device 7 in face connects and takes electricity from external power supply 5.Automatic wire winding device 7 includes an electric reel 24 and two The pedestal 25 being connect with electric reel 24.And inside aircraft 1 above, it is also equipped with an automatic wire winding device 29, Including an electric reel 24.But unlike the automatic wire winding device 7 for being set to ground, 29 folding and unfolding position of automatic wire winding device Automatic wire winding device 7 in the related content ginseng embodiment 1 of following power transmission line 6(automatic wire winding device 29).This concatenation Mode and power transmission line arrangement undertake the weight of a big chunk power transmission line due to following aircraft, be conducive to above fly Row device flies get Geng Gao, freer.

Single rack aircraft use automatic wire winding device 29, be suitble to nap of the earth flight without draw power transmission line, can to avoid or Person mitigates the abrasion and yoke of power transmission line significantly, and can pack up power transmission line and realize recycling.

In embodiment 4, below aircraft using three naked steel wires be used as power transmission line, and one bifurcated wiring of use Three power transmission lines 6 are drawn at end 26, and every power transmission line respectively uses an automatic wire winding device individually to be stored.Naked steel wire does not have to Insulating layer is conducive to that heat dissipation, component is light, does not have the problem of wearout.

Insulating layer can also be set to surface of three naked steel wire power transmission lines at bifurcated terminals 26 above, because one Winding upper part, which occurs, for three power transmission lines of denier first to collide.

One prison connecting with state of flight computer control system host signal can also be set on the aircraft Device 27 is controlled, when recognizing that three power transmission lines are in the hole, monitor 27 is reported to state of flight computer control system, Accident is avoided to cut off the power in time.

Can also be arranged on the aircraft one connect with state of flight computer control system host signal plus Velocity sensor 28 makes three transmissions of electricity more than 100 degree including rotating horizontally when the state for recognizing the aircraft goes wrong When line is possible to winding, is reported to state of flight computer control system, avoid accident to cut off the power in time.

Automatic wire winding device can also include folding and unfolding line control circuit and retractable cable execution unit.Retractable cable execution unit contains There is the interface circuit connecting with folding and unfolding line control circuit signal, the state of automatic wire winding device is according to the control circuit state Change and changes；The control circuit and state of flight computer control system are networked.

In embodiment 4, the heat absorption coil pipe heat transfer of the inner surface and a compressor refrigerating plant of electric reel 24 is enabled to connect, The temperature for two layers of power transmission line for being close to 24 inner surface of electric reel is greatly lowered, to keep good operating condition.Work as major part When power transmission line remains in electric reel surface, the power transmission line of aircraft load is few, its load is light, the electric current of power transmission line is also smaller.

It is 1 meter one long, the power transmission line that two layers of diameter is 2 millimeters is wound on 0.67 meter of outer diameter of electric reel, then transmit electricity The length of line is up to 2 kms.

In embodiment 4, the automatic wire winding device including an electric reel and two pedestals can also be reduced to one it is defeated Electric wire wire storehouse is used only for storage power transmission line.And the line storehouse can also be with the absorbing heat disk of a compressor refrigerating plant Pipe heat transfer connection, for cooling down.

Fig. 6 provides embodiment 5.

In embodiment 5, power transmission line 6 is using integrated flat type two-wire or trigram formula；6 one side surface of power transmission line is evenly equipped with tooth Shape object 31 constitutes a synchronous belt, and is connected by meshing transmission with a synchronous pulley 32 and realizes folding and unfolding.Synchronizing belt gear 32 also with One cooperation of limiting pressure roller 33 prevents power transmission line 6 from falling off.And power transmission line is provided to the suitable tension of automatic wire winding device.

There is a closed bin 34 using the manufacture of high thermal resistance material below synchronous pulley 32, power transmission line 6 is from closed bin 34 The hole of top is pierced into closed bin 34 and is wound on the aluminium sheet inner cylinder 35 of electric reel 24.Aluminium sheet inner cylinder 35 and a compressor freeze The heat absorption coil pipe 36 of device, which conducts heat, to be connected, and the line temperature being close on aluminium sheet inner cylinder 35 is greatly lowered.In closed bin 34 It also sets up fan-coil device and keeps good operating condition for carrying out forced air cooling to closed bin inside.Fan-coil device includes wind Another heat absorption coil pipe 36 of machine 37 and the Cempression engine refrigerating apparatus being placed in front of blower 37.

The synchronous belt power line transmission mode of embodiment 6 has tractive force big, and power transmission line folding and unfolding length controllable precise can be surveyed The advantages that.

Naked steel wire lesser for coefficient of friction, then can by increase its be wrapped in the azimuth on idler wheel increase rolling The tractive force of wheel.

Fig. 7 provides embodiment 6.

In embodiment 6, enabling naked steel wire power transmission line 6 first pass through lineation wheel group 38 and formed to subsequent object includes automatic winding dress The suitable tension set keeps not falling off.Then it is more than 290 degree that power transmission line 6 winds azimuth on idler wheel 41, to increase idler wheel 41 To the tractive force of the lesser power transmission line of coefficient of friction --- cable shape object is more in the circle number that column is wound around, and column is to cable shape The tractive force of object is bigger.

Fig. 8 to 10 provides embodiment 7.

In embodiment 7, external power supply 4 axis rotor crafts 1 of power supply include fuselage 2, by 4 ACasynchronous motor drives Electronic rotor 42,43,44,45 and parachute 46.Using automatic connector.The threephase stator coil of the motor is gone here and there two-by-two respectively It connects to form three branches, the head end of three branches is by naked steel wire power transmission line 6, automatic wire winding device 7 and variable resistance 47 and outside The controllable three-phase alternating-current supply connection in portion.Three branch ends simultaneously connect, since all motors correspond to the voltage and electricity of phase winding Flow equal, the state of motor is also equal, but requires their direction of rotation two just two anti-.

4 motors are divided into two groups, enable every group described in motor be arranged symmetrically in space with the axial line of aircraft, rotate The contrary rotating reactive force with cancel out each other rotor and rotor.From Fig. 9 plane right-angle coordinate: electronic Rotor 42,43,44,45 is respectively at the 1st, 2,3,4, four quadrants.

By 42.1,43.1,44.1,45.1 tapping of motor to 4 electronic rotors 42,43,44,45, in tap Place and related winding overhang are connected in parallel 4 multifunction modules 48,49,50,51 in total.Tapping to the motor be for The lower voltage of acquisition comes and light current load matched.

Multifunction module 48,49,50,51 includes flight control circuit, controlled rectification or chopper circuit 53, rechargeable battery 54, power load 55 and fictitious load 56.Controlled rectification or chopper circuit 53 are adjusted by changing the service time of rectifying device Save its power output.Power load 55 include filter circuit of pressure-stabilizing, state of flight computer control system, flight control circuit, Radio reception transmit circuit and other all possible electricity consumption devices；Fictitious load 56 includes resistance device and concatenates one controllably Silicon.Rechargeable battery 54 also has voltage regulation filtering effect；All its dump energy is detected and filled after each aerial mission Be discharged to setting range for example Full Charge Capacity 62% to 65%.The function of flight control circuit includes the control to the motor.Fly Line control circuit can take electricity without taking electricity from controlled rectification or chopper circuit from rechargeable battery 54 completely when working normally.Fly The a part and state of flight computer control system host signal of line control circuit as state of flight computer control system It connects and connects and be controlled by it.As needed, when the state control of aircraft requires to enable and some direction to the flight of some direction The multifunction module of rotor motor parallel connection consume some electric currents more, specifically include the fictitious load branch for enabling related multifunction module Silicon-controlled service time it is longer, therefore the rotor because motor by-pass current increase itself input power reduce lift Also reducing causes the run-off the straight of aircraft axial line to push away to which the lift of aircraft generates one to the horizontal component in the direction Dynamic aircraft is mobile to the direction.The silicon-controlled execution unit as flight control circuit concatenated with fictitious load, really Flight control circuit is protected to the power control of each multifunction module.

When flowing through the electric current of multifunction module 48,49,50,51 from zero to maximum, asynchronous machine 42.1,43.1,44.1, 45.1 power is from being up to minimum.

The status controlling packet of aircraft includes:

It is adjusted by voltage to external controllable three-phase alternating-current supply and/or frequency, and adjusts each variable resistance 52, it can be achieved that the motor power control and/or revolving speed control to realize to the status controlling packet of aircraft 1 include rising, Aerial static, decline and stopping.

It can be sketched using the principle that multifunction module 48,49,50,51 adjusts state of flight are as follows: be in hovering in aircraft 1 It is described a certain to change by one or several power being adjusted in synchronism in multifunction module 48,49,50,51 when state The state of platform or several motors, to realize the control to flight state.For example:

Enable in the 1st, the machine winding of two electronic rotors 42,45 of 4 quadrants and the multifunction module 48,51 that connects Electrical power is greater than the electrical power with other two multifunction module 49,50, this will reduce the function of electronic rotor 45,42 associated motors Rate increases the power of electronic rotor 43,44 associated motors simultaneously, and the spatial altitude of electronic rotor 45,42 is caused to be slightly less than electricity The spatial altitude of dynamic rotor 43,44, this state start aircraft 1 to the direct north flight in other words of Y-axis arrow direction. At this point, passing through the electrical power of 4 multifunction modules of synchronous balance 48,49,50,51, the power of electronic rotor 45,42 will be restored, And electronic rotor 42,43,44,45 is caused to be in sustained height, aircraft restores to be in aerial stationary state.

As a same reason, the power for reducing two, the right side, two, quadrant electronic rotor associated motors in 4 quadrants, will lead to winged Row device flies to positive east direction.... also, because the mechanism of this change of flight device flight can be superimposed, so as to reality Existing aircraft can fly to any direction.Several measure voltage & current facilities can also be configured when needing and facilitate control.Control The technology of flight state processed reference may also be made to utilize existing technology.

From the winding centre tap of the motor but electricity directly can not certainly be taken from the both ends of the machine winding Related multifunction module is supplied, and the mode of 1 state of flight of change of flight device recited above is still set up.

Even if three multifunction modules are all in full power and charged state, because the input of external power supply can be increased, Aircraft still can be with normal flight.

When external power supply 5 is unable to normal power supply, power transmission line 6 is extracted by automatic connector and opens each parachute 46, Aircraft 1 is declined under the action of parachute 46 with speed slow enough；Each power transmission line 6 also under the action of parachute 46 with compared with Slow speed declines so as to the normal take-up of automatic wire winding device 7.

The beneficial effect of embodiment 7 includes: to utilize to load on carry-on about 1520 volts controllable three-phase alternating-current supplies drives The AC induction motor for the electronic rotor that dynamic 4 operating voltages are 380 volts, due to supply voltage height, the electric current of power transmission line is corresponding Reduce, thermal losses in square substantially reduces with electric current, facilitates using thinner lighter power transmission line；By to external controllable The supply voltage of three-phase alternating-current supply, which is adjusted, realizes that flight power control is very convenient including adjusting using adjustable transformer.

Although being increased using AC power source risk, than four unsteady flows using the motor power supply to 4 electronic rotors Module is more reasonable.Although high voltage power supply increases to the insulating requirements of motor, electric current is decreased to a quarter, it is believed that value ?.

When using other motors, the associated winding string of this motor grouping to electronic rotor, each motor can also be used Connect the design to use high voltage.

Figure 11 provides embodiment 8.

In embodiment 8, there are four the autocoupling type three-phase transformers 57 of tap for tool, have 9 taps and two terminals.The right side 8 taps constitute four groups of equal outputs with right side terminal；Every group of output includes that an intermediate tap is light current multifunction module The voltage of tens of volts is provided.

With every 0.75 kilowatt meter of motor, three stator winding it is each using 1000 volts of voltage when electric current also with regard to 0.3 ampere. Accordingly it is also possible to using the design in embodiment 7 --- the asynchronous motors of transformer 57 and 4 are concatenated, and from the stator of motor The power supply of tapping offer multifunction module.

Load as early warning radar for 5 kw of power needs one relative to 0.3 amperage, ten kilovolts of voltage A transformer provides high current.Again due to being designed using Switching Power Supply, with greater need for using transformer.Winding 58 is negative for aircraft Lotus provides independent power supply all the way.

The AC induction motor of high reliablity and lighter in weight can be directly used using alternating current, and change can be passed through Voltage and/or frequency control the state of aircraft.

Embodiment 8 realizes low current to adapt to the requirement to power transmission line weight, and because using upper frequency and substantially Degree reduces the volume and weight of transformer.When concatenating using transformer with asynchronous machine, the operating condition of motor was not only guaranteed, but also into one Step cuts down the bulking value of transformer.

It includes being changed to auto-transformer for the first time that each winding of 8 auto-transformer 57 of embodiment, which is also readily modified as independent winding, The coupling transformer of grade isolation.

Early warning radar can be using unmanned submarines as platform, and extreme weather drops to submarine and sinks to the water surface or less.By In may be advanced into other than seashore 200 nautical miles, early warning range is bigger.

Figure 12 provides embodiment 9.

In embodiment 9, the direct current generator 52 that mutually concatenates of direct current power supply that is provided by external power supply.Direct current generator 52 wraps It includes and various is suitble to concatenated motor for example brushless motor.Each direct current generator 52 and connects multifunction module 48,49,50,51 (the related content of ginseng example 7 above).Electricity is controlled by the flight of state of flight computer control system and multifunction module The control to aircraft is realized on road.

Under the conditions of meeting direct current generator and mutually concatenating, what the state control of aircraft can also be provided using the prior art Other methods.

Figure 13 and 14 provides embodiment 10 jointly.

In embodiment 10, quadrotor external power supply with separation layer power supply remotely-piloted vehicle system 1 includes fuselage 2, electronic Rotor 42, state of flight computer control system, radio signal reception handle launch facility, as the early warning of aircraft load Radar 59, bifurcated terminals 26, remote controler, external power supply 7, power transmission line 6 and separation layer 60.

Separation layer 60, including aluminium sheet and plastic sheeting making, is set at electronic 42 place plane of rotor with light laminated； It is seamlessly connected flange 61 up and down in the periphery of separation layer 60；The upper edge hole of flange 61 is connect with a lightweight retaining frame 62； Separation layer 60 aperture and seamless connecting shaft stream air duct 63 at electronic rotor 42.The technology of axis stream air passage can refer to axial flow blower Etc. the prior arts.

Lightweight retaining frame can use carbon fiber material, light, impact resistance.Port below axis stream air passage can be than above Port is larger.

Benefit using separation layer 60 is can be below each electronic 42 place plane of rotor and upper by separation layer 60 Face keeps a high-pressure area 64 and an area of low pressure 65 respectively.When the pressure of high-pressure area 64 is higher by area of low pressure 65 about When 0.003 standard atmospheric pressure, every square metre can generate about 30kg(10000*0.003*1) lift.And the electricity consumed Power is only about 1.5kw, is greatly decreased when than not using separation layer.Flange 61 and axis stream air passage 63 help to enhance high-pressure area Pressure difference between 64 and area of low pressure 65.Axis stream air passage 63 can improve the efficiency of electronic rotor.The altitude range of flange 61 can To take 50 to 600 millimeters；The altitude range of axis stream air passage 63 can take 10 to 65 millimeters.

When embodiment 10 is used as the radar picket in 7 km high-altitudes, using 22kv900 hz AC electricity and transformer is used Decompression, 0.3 ampere of power line current, power about 10kw(1.732*22000*0.3*0.88 ≈ 10.059).

Using the copper facing stainless steel multiply bare wire of 3 sectional area 0.15mm2, consider that the resistance of temperature rise is total up to 15400 Ω (3*0.11/0.15*7000), line loss are total up to 1.386kw, are rounded 1.4kw；Copper-plated effect has made weight constant resistance Reduce, is suitble to 900 hz AC electricity and reply hydrogen embrittlement.3 copper facing stainless steel multi cord gross weight 24kg.

It includes: power transmission line 24kg(0.15*0.01*100* that the load of quadrotor 1 with separation layer, which amounts to 50kg, 7.6*7*3=23.94), early warning radar 10kg, unmanned plane itself 16kg include that the total 4kg of the electronic rotor of 4 axis, fuselage include parachute 4kg, communication control and other 1kg, transformer 7kg.

In terms of the every kilowatt of rotor motor load 20kg of aircraft 1, electric efficiency 0.95, the power consumption 9.6kw in total of embodiment 7, Include: 4 electronic 2.7 kw(50/20/0.95 ≈ 2.64 of rotor power consumption), 1.9 kw of power transmission line and transformer loss, unmanned plane 0.4 kw of other parts electricity consumption, 5 kw of early warning radar.

The allowable stress of steel wire: 24/(0.15*3) ≈ 53.3.Pass through.

Revolving speed is slightly below 5400 revs/min when motor uses 20 pole.Aircraft in embodiment 10 is when taking off, power transmission line 6 Load is light, at this moment uses lower voltage and lower frequency；Increase later as aircraft rises transmission of electricity specific electric load by voltage and frequency Rate also improves.Finally reach the full power state of ceiling voltage and frequency when opening all loads.

Early warning radar in embodiment 10 can also be changed to wireless network communication local area network antenna facility, including wifi transmitting Reception device, for a wide range of interior offer related service.

Figure 15 provides embodiment 11.

In embodiment 11, external power supply power supply remotely-piloted vehicle system 1 includes aerocamera 66, passes through 6 He of power transmission line Automatic wire winding device 7 is connect with external power supply 5；Communication contact with aircraft 1 is realized using remote controler 4.In embodiment 11, also The PLC communication module 67 connecting with 6 signal of power transmission line is respectively provided on aircraft 1 and at external power supply 5, It realizes that wire signal transmits using power transmission line 6, is communicated.Content in relation to electric line carrier communication can refer to existing electricity Line of force Internet technology.

Figure 16 provides embodiment 12.

Embodiment 12, spray unit include two frame rotor crafts spray aircraft 68, assisting in flying device 69 and logistics vehicle 72, logistics vehicle 72 is mounted with automatic wire winding device 7, the automatic retraction device of water delivery pipe 74, external power supply 5, landing platform 70 With pesticide container 71.The power load on external power supply 5 and aircraft unit is connected with power transmission line 6, contains spray on spray aircraft Medicine port 73, the delivery pipe 74 being connected to respectively with spray port 73 and pesticide container 71 using a both ends.Pesticide container 71 is configured with Medical fluid promotes facility, including booster pump.Logistics vehicle 72 automatically tracks assisting in flying device 69.Spray port 73 be one it is horizontal, its Side is provided with the tube of round, and the related content such as spray port 73 can refer to the prior art.

The brief introduction of work principle of embodiment 13 are as follows: system boot self-test includes that assisting in flying device 69 and spray aircraft 68 are first Rise hovering from landing platform 70 afterwards to stop；Then logistics vehicle 72 follows spray unit to reach scene, and pesticide container 71 starts medical fluid and mentions It rises facility and implements spray drug operation.And using resupply vehicle in due course to pesticide container dosing.In operation process, automatic wire winding device 7 and water The automatic retraction device automatic deploying and retracting power transmission line 6 and water delivery pipe 74 of delivery pipe 74.Operation is completed, and enables medical fluid promote facility reversed Medical fluid is sucked back to pesticide container 71.Then two frame aircraft drop on landing platform 70, recall storehouse.

Due to that can work continuously for a long time, the present invention is than existing several minutes of the spray aircraft working efficiency of can only working High 3 times, the employee without configuring replacement battery.Again since spray drug operation is not interrupted, neither drain spray is also seldom sprayed.It is high-efficient to go back Mean to kill locust within a few hours without allowing it to escape.The wind of gyroplane facilitates the back that medicament reaches plant leaf Face, this is original advantage.

Assisting in flying device 69 has shared the weight of water delivery pipe 74 and power transmission line 6, realizes spray aircraft 68 from its fuselage Connection power transmission line 6 increases the freedom degree of spray above；The support of assisting in flying device 69 can also increase spray aircraft 68 and make The distance and area of industry.

Figure 17 provides embodiment 13.

Embodiment 13, sowing unit include two frame rotor crafts sowing aircraft 75, assisting in flying device 69 and logistics vehicle 72, logistics vehicle 72 is mounted with automatic wire winding device 7, external power supply 5, the automatic retraction device of seed transport tube 78, landing platform 70 and seed cabin 76.The power load on external power supply 5 and aircraft unit is connected with power transmission line 6, is contained on sowing aircraft 75 The seed transport tube 78 for having sowing module 77, being connected to respectively with sowing module 77 and seed cabin 76 using a both ends.Seed cabin 76 promote the automatic retraction device of facility and seed transport tube 78, including air-flow conveying facility configured with seed, can specifically join Examine related art.Logistics vehicle 72 automatically tracks assisting in flying device 69.Module 77 is sowed to be designed according to different seeds, it is related Content can refer to the prior art.

The brief introduction of work principle of embodiment 13 are as follows: system boot self-test includes that assisting in flying device 69 and sowing aircraft 75 are first Lift-off hovering afterwards；Then logistics vehicle 72 follows sowing unit to reach scene, and seed cabin 76 starts seed promotion facility and implements sowing Operation.And seed cabin 76 is fed in due course using resupply vehicle.In operation process, automatic wire winding device 7 and seed transport tube 78 automatic retraction device automatic deploying and retracting power transmission line 6 and seed transport tube 78.Operation is completed, and is enabled seed promote facility and is reversely sucked back Seed is to seed cabin 76.Then storehouse is recalled.

Due to that can work continuously for a long time, the present invention sows flight unit, and work efficiency is high.

Assisting in flying device 69 has shared the weight of seed transport tube 78 and power transmission line 6, and the support of assisting in flying device 69 may be used also To increase the operation distance and area of sowing aircraft 75.

In embodiment 12 in the automatic retraction device of water delivery pipe 74 and embodiment 13 seed transport tube 78 automatic deploying and retracting The related content of device please join automatic wire winding device 7 and the prior art in embodiment 1.

Figure 18 provides embodiment 14.

Embodiment 14, several rotor crafts 1 are electrically connected by one group or a branch of power transmission line 6 and external power supply 5； Several described rotor crafts 1 and the embedded connection of the same nonrigid load 79.Two in several rotor crafts 1 Directly or indirectly signal is connect and its state changing according to 4 state of remote controler for a above aircraft and the same remote controler 4 Become and changes.

Load in embodiment 14 is also possible to rigid load.And the element of traditional culture, magic can also be added Element.Various stories are played and described in the sky to embodiment 14, can satisfy the demand of the aesthetic of people and amusement.

Figure 19 provides embodiment 15.

Embodiment 15 manufactures a remotely-piloted vehicle ultrahigh speed cleaning device, including rotor craft 1 and flexible cable cloth 80；Rotor craft 1 includes fuselage 2, several electronic rotor 45, state of flight computer control system and remote controlers；Flexible cable Cloth 80 hangs on 1 lower section of aircraft；Flexible cable includes nylon rope；Cloth includes canvas.External electrical is connected using a power transmission line 6 Source 5 and aircraft 1, and continually electric energy is provided to aircraft 1.Embodiment 15 shares an outside using two frame aircraft 1 Power supply 5.External power supply 5 is loaded on a logistics vehicle 72；Channel of the logistics vehicle 72 between the photovoltaic battery panel 81 not yet to sweep away snow Automatically it crosses.

When sweeping away snow, shake is hit plus the pumping of flexible cable cloth 80 in the powerful bottom blowing air current of the electronic rotor 45 of rotor craft 1 Under double action, the accumulated snow on photovoltaic battery panel 81 as described in Figure 19 dashed middle line is slipped to ground.

Figure 20 and Figure 21 provides embodiment 16.

Embodiment 16, is arranged aerial conveyor in mountain forest 82, and aerial conveyor includes several stubs 83 and by stub 83 One group of two rail 84 being connect with ground, between two rail 84 mutually electric insulation and respectively with two electrodes of power supply 85 Electrical connection；Rail 84 doubles as power main, is formed together circuit with power supply 85 and power load.Rail 84 uses detour shape Formula, it is insensitive to the variation of length caused by expanding with heat and contract with cold.

Traveling is by electric trolley on aerial conveyor；It is included the chassis 9 with electric wheel set 86,87 and of current collector part by electric trolley It is included communication module by electric trolley computer control system by electric trolley computer control system；Passed through power transmission line 5 by electric trolley It powers to aircraft 1；Current collector part 87 is a pantograph with pantograph arm；

Current collector part 87 is used to cooperate with rail 84 and rolls or be slidably connected and realize electrical connection；Electric wheel set 86 is wrapped Idler wheel, electric roller and the sliding block cooperated with rail 84 are included, the sliding block cooperated with rail 84 is able to take upwardly and laterally to draw Power is without departing from rail 84；

The logistics vehicle and freight trolley for loading external power supply can also be travelled above aerial conveyor in embodiment 10；Logistics Vehicle and freight trolley can be electrically connected from charged pool or using current collector part and rail for powering to aircraft.

In embodiment 16, power transmission line 5 from aerial conveyor by electric trolley, pass through that assisting in flying device above The distance of horizontal direction is extended after pulling significantly, and is simultaneously that agricultural machinery 89 in terraced fields 88 provides electric energy, is 88 top of terraced fields Agricultural main aircraft electric energy is provided；These both contribute to solve the problems, such as that who comes and how to cultivate terraced fields from now on.

The logistics vehicle that traveling loads battery on aerial conveyor can use the pine forests spray in Yushan Hill；Goods is travelled on aerial conveyor Trolley is transported, the moso bamboo in mountain is cut down and is hoisted on freight trolley using unmanned plane moso bamboo harvesting robotic and transports a distance It reaches highway to be transported outward with truck again, may be implemented to be replaced manually with machine part.

Claims (10)

1. The remotely-piloted vehicle systems approach 1. external power supply is powered: one external power supply power supply remotely-piloted vehicle system of manufacture, including Aircraft, external power supply and remote controler；Aircraft includes fuselage, electronic rotor, state of flight computer control system, radio Signal receiving area transmission facility and aircraft load are formed using one group with the power load of external power supply and the aircraft The power transmission line in circuit；External power supply continually supplies aircraft；

   A power supply unsteady flow module is manufactured, realizes that by the high voltage-small current electric energy morphological transformation of power line transmission be the aircraft The electric energy form needed, power supply unsteady flow module include transformer, inverter and the circuit powered to direct current generator；Or

   Concatenate an automatic connector between power transmission line and the aircraft, automatic connector include a connector jack and One electric wire connecting junction plug；Electric wire connecting junction plug is connect with power transmission line；And contain a power transmission line automatic locking device part；Connector jack It is set on fuselage with power transmission line automatic locking device part；Power transmission line automatic locking device part is as state of flight computer control system Execution unit；Power transmission line automatic locking device part includes an electronic pressure tongue, and electronic pressure tongue includes electromagnetism pressure tongue；Electronic pressure tongue is normal Close and push down power transmission line, when the state of electronic pressure tongue from it is normally closed become opening when, electric wire connecting junction plug is made in itself and power transmission line gravity It is fallen with lower disengaging fuselage；Or

   Aircraft contains an automatic wire winding device, the power transmission line being located below for folding and unfolding；Or

   The PLC communication module being connect on board the aircraft and at external power supply containing one with powerline signal, benefit Wire signal transmission is realized with power line carrier；

   The motor of each electronic rotor is direct current generator, and the correspondence winding of each motor is using being connected in series, to each motor At least one winding multifunction module in parallel respectively, it is described each to change control by changing the state of multifunction module The state of motor；Or

   The motor of each electronic rotor is worked for AC induction motor and directly using external three-phase alternating voltage, each motor Three-phase windings use and are connected in series to form three branches, and one of at least one winding or a winding to each motor Divide multifunction module in parallel, and each phase power supply is evenly distributed with multifunction module；Change control by changing the state of multifunction module Make the state of each motor；Or

   The motor of each electronic rotor will be worked for AC induction motor and using transformer after the decompression of external three-phase alternating voltage, institute The three-phase windings of each motor are stated using being connected in series to form three branches, at least one winding to each motor or one A part of winding or a part of multifunction module in parallel with the transformer of the winding parallel, it is multi-functional by changing The state of module controls the state of each motor to change；

   It further include using the general linkage interface of more than one functional component, or contain more than one functional component,

   It further include using the aircraft more than two framves, the power load of two frame the above aircraft is transmitted electricity by same group Line is concatenated into a circuit loop；Power transmission line contains one group of automatic branching electric wire connecting junction, automatic branching electric wire connecting junction close to intermediate position The interface circuit being connect containing one with state of flight computer control system wireless signal；The state root of automatic branching electric wire connecting junction Change according to the state of state of flight computer control system and changes；Or

   More than two rotor crafts are electrically connected by one group of power transmission line and external power supply；The rotor craft with it is same The embedded connection of aircraft load, the aircraft load include rigid and nonrigid；In the rotor craft at least Directly or indirectly signal is connect more than two aircraft and its state is according to the remote controller state with the same remote controler Change and change；Further include setting track, and enables the trolley travelling for loading external power supply on track；Further, further include Power main with parallel track or integrated production is set.
2. The remotely-piloted vehicle system 2. external power supply is powered, using the external power supply power supply remotely-piloted vehicle system side of claim 1 Method, it is characterized in that including aircraft, external power supply and remote controler；Aircraft includes fuselage, electronic rotor, state of flight computer Control system, radio signal reception processing launch facility and aircraft load, using one group and external power supply and the flight The power transmission line in the power load composition circuit of device；External power supply continually supplies aircraft.
3. 3. external power supply power supply remotely-piloted vehicle system according to claim 2, it is characterized in that containing a power supply unsteady flow Module realizes the electric energy form for needing the high voltage-small current electric energy morphological transformation of power line transmission for the aircraft, power supply Unsteady flow module includes transformer, inverter and the traditional direct current booster circuit powered to direct current generator；Or

   Concatenate an automatic connector between power transmission line and the aircraft, automatic connector include a connector jack and One electric wire connecting junction plug；Electric wire connecting junction plug is connect with power transmission line；And contain a power transmission line automatic locking device part；Connector jack It is set on fuselage with power transmission line automatic locking device part；Power transmission line automatic locking device part is as state of flight computer control system Execution unit；Power transmission line automatic locking device part includes an electronic pressure tongue, and electronic pressure tongue includes electromagnetism pressure tongue；Electronic pressure tongue is normal Close and push down power transmission line, when the state of electronic pressure tongue from it is normally closed become opening when, electric wire connecting junction plug is made in itself and power transmission line gravity It is fallen with lower disengaging fuselage；Or

   Aircraft contains an automatic wire winding device, the power transmission line being located below for folding and unfolding.
4. The remotely-piloted vehicle system 4. external power supply described in accordance with the claim 3 is powered, it is characterized in that electric wire connecting junction plug and/or machine Body connects a parachute, and sets: 0.2 second after issuing the instruction for being detached from fuselage to electric wire connecting junction plug, parachute starts It opens；

   And it enables each motor of all electronic rotors of driving be distributed two one group according to Space Axisymmetric and is divided into more than two motors Group enables each stator winding of each each motor of motor group be connected in series to form a plurality of branch respectively, takes string to the branch Connection or the mode of parallel connection are connect with the external power supply；

   A part of multifunction module in parallel and every institute of at least one winding or a winding to every motor It states branch and at least contains a multifunction module；

   Multifunction module includes that flight control circuit, controlled rectification or chopper circuit, rechargeable battery, power load and vacation are negative It carries；Controlled rectification or chopper circuit adjust its power output by changing the service time of rectifying device；Power load packet Include filter circuit of pressure-stabilizing, state of flight computer control system, flight control circuit, for detect each multifunction module electric current and Detection device, radio reception transmit circuit and other all possible electricity consumption devices of voltage；Fictitious load includes variable resistance, Also include fixed resistance device and concatenated with it silicon-controlled, fictitious load is used to consume electric energy to influence its rotor electricity in parallel The state of machine and all rotor motors；The a part and flight shape of flight control circuit as state of flight computer control system State computer control system host signal, which is connected and connect, to be controlled by it；Change control institute by changing the state of multifunction module State the state of each motor, comprising: as needed, require to fly to some direction when the state of aircraft controls, it can be in gyroscope Guide under, enable and consume some electric currents, therefore the rotor with being located at the rotor motor in direction multifunction module in parallel more Because the by-pass current of motor increase itself input power reduce lift also reduces cause the run-off the straight of aircraft axial line thus The lift of aircraft generates one and pushes aircraft mobile to the direction to the horizontal component in the direction；It is concatenated with fictitious load A silicon-controlled execution unit as flight control circuit, it is ensured that power control of the flight control circuit to each multifunction module System；

   The motor of each electronic rotor includes direct current generator, using being connected in series between the winding of each motor, to each electricity One multifunction module of at least one winding parallel of machine is changed described in control by changing the state of the multifunction module The state of each motor；Or

   The motor of each electronic rotor is worked for AC induction motor and directly using external three-phase alternating voltage, each motor Three-phase windings use and are connected in series to form three branches, and one of at least one winding or a winding to each motor Divide multifunction module in parallel, and each phase power supply is evenly distributed with multifunction module；Change control by changing the state of multifunction module Make the state of each motor；Or

   The motor of each electronic rotor will be worked for AC induction motor and using transformer after the decompression of external three-phase alternating voltage, institute The three-phase windings of each motor are stated using being connected in series to form three branches, at least one winding to each motor or one A part of winding or a part of multifunction module in parallel with the transformer of the winding parallel, it is multi-functional by changing The state of module controls the state of each motor to change.
5. 5. external power supply power supply remotely-piloted vehicle system according to claim 2, it is characterized in that the aircraft is four axis The above rotary aircraft comprising one is in the film-form object of same level position with rotor；The film-form object The aperture at electronic rotor.
6. 6. external power supply power supply remotely-piloted vehicle system according to claim 2, it is characterized in that containing more than one function The general linkage interface of component, or contain more than one functional component,

   The functional component further include telemechanical flame thrower, projectile weapon, bomb, high-pitched speaker, tracking powder dispense device, Explosive is removed or apparatus to cause bursting, hangs on flexible cable or cloth below rotor craft.
7. 7. external power supply power supply remotely-piloted vehicle system according to claim 2, it is characterized in that in two naked steel wires transmissions of electricity Surface of the line at bifurcated terminals above is provided with insulating layer；Or

   The monitor being connect containing one with state of flight computer control system host signal on the aircraft；Or

   The acceleration transducer being connect containing one with state of flight computer control system host signal on the aircraft.
8. 8. external power supply power supply remotely-piloted vehicle system according to claim 2, it is characterized in that one spray unit of composition, Including two frame rotor crafts spray aircraft, assisting in flying device and logistics vehicle, it is defeated that logistics vehicle is mounted with automatic wire winding device, water Send the automatic retraction device, external power supply and pesticide container of pipe；The electricity consumption on external power supply and aircraft unit is connected with power transmission line Contain the port that sprays, the delivery pipe being connected to respectively with spray port and pesticide container using a both ends in load, spray aircraft； Or

   Form a sowing unit, including two frame rotor crafts sowing aircraft, assisting in flying device and logistics vehicle, logistics vehicle dress Be loaded with automatic wire winding device, external power supply, seed transport tube automatic retraction device and seed cabin；External electrical is connected with power transmission line Source and power load on aircraft unit, on sowing aircraft containing sowing module, using a both ends respectively with sowing mould The seed transport tube that block is connected to seed cabin.
9. The remotely-piloted vehicle system 9. external power supply is powered, using the external power supply power supply remotely-piloted vehicle system side of claim 1 Method, it is characterized in that including aircraft, external power supply and remote controler；Aircraft includes fuselage, electronic rotor, state of flight computer Control system, radio signal reception processing launch facility and aircraft load, using one group and external power supply and the flight The power transmission line in the power load composition circuit of device；

   Track, including aerial conveyor are set；Traveling loads the logistics vehicle of external power supply in orbit；Logistics vehicle includes with electronic The chassis of wheel group and logistics vehicle computer control system, logistics vehicle load external power supply, and external power supply passes through power transmission line to flight Device power supply；

   The vehicle travelled in orbit further includes freight trolley and by electric trolley.
10. 10. external power supply power supply remotely-piloted vehicle system according to claim 9, it is characterized in that further including that independent Transmission is dry Line, independent Transmission main line and parallel track are arranged and are formed together a circuit with power supply, load and the earth；It is typical independent defeated Electric main line includes the power main above electric railway；Or

    Freight trolley includes the chassis with electric wheel set and freight trolley computer control system；

    Included the chassis with electric wheel set, current collector part and by electric trolley computer control system by electric trolley, and passes through transmission of electricity Line is powered to aircraft；

    Current collector part is used to be electrically connected with the track or independent power main；

    Electric wheel set includes idler wheel and the sliding block with track cooperation, and sliding block and track cooperation are able to take upward and side pulling force Without departing from track；

    Logistics vehicle and freight trolley further include current collector part.