CN204068303U - A kind of charging system, electric supply installation and aircraft - Google Patents
A kind of charging system, electric supply installation and aircraft Download PDFInfo
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- CN204068303U CN204068303U CN201420314042.8U CN201420314042U CN204068303U CN 204068303 U CN204068303 U CN 204068303U CN 201420314042 U CN201420314042 U CN 201420314042U CN 204068303 U CN204068303 U CN 204068303U
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Abstract
The utility model embodiment provides a kind of charging system, electric supply installation and aircraft, wherein, charging system comprises: described electric supply installation and charging device, described charging device can be configured on described aircraft, and described electric supply installation comprises: power supply and at least two pieces of power supply boards be exposed in external environment condition; Power supply board is connected to power supply, and is connected to the power supply board of positive source and is connected to the power supply board alternately arrangement of power cathode, insulate and be separated by between every two pieces of power supply boards; The charging circuit that charging device comprises at least two charging contact element and is connected with at least two contact element of charging, each charging contact element is connected with the negative pole that charges with the charging positive pole of charging circuit respectively by diode; Charging device is contacted with power supply board by charging contact element to be that the load connected is charged.Adopt the utility model, can low cost, rapidly access charging circuit charge.
Description
Technical field
The utility model relates to electronic technology field, particularly relates to a kind of charging system, electric supply installation and aircraft.
Background technology
Charger can be the power source charges of the equipment such as Electric aircraft, robot by the power supply such as civil power or storage battery.Wherein, the charging completing relevant device is generally realized jointly by the socket be electrically connected with city, the charger that comprises plug and charging circuit.Charger wherein can be an isolated system, also can be the structure of the device interior such as aircraft, robot, and it is inserted in the jack that socket provides by the mode of flexible plug, has coordinated charging.
Existing charging technique comparative maturity, charging process is stable and cost is lower.But, for the automatic charging scene of the equipment such as aircraft, robot, if adopt the mode that existing plug and socket coordinates, the equipment such as aircraft and robot is then needed accurately to identify the position of the position of socket, the position of jack and himself plug, computation requirement is higher improves cost, and algorithm complexity also not easily realizes.
Utility model content
The utility model embodiment provides a kind of charging system, electric supply installation and aircraft, can complete charging quickly and easily under the automatic charging scene of equipment.
The utility model embodiment provides a kind of charging system, comprising: electric supply installation and charging device, wherein:
Described electric supply installation comprises: power supply and at least two pieces of power supply boards be exposed in external environment condition; Described power supply board is connected to described power supply, and is connected to the power supply board of described positive source and is connected to the power supply board alternately arrangement of described power cathode, insulate and be separated by between every two pieces of power supply boards;
The charging circuit that described charging device comprises at least two charging contact element and is connected with described at least two contact element of charging, each charging contact element is connected with the negative pole that charges with the charging positive pole of described charging circuit respectively by diode;
Described charging device is contacted with described power supply board by charging contact element to be that the load connected is charged.
Wherein alternatively, the minimum value insulated between described every two pieces of power supply boards in the standoff distance value of being separated by is initial distance value;
Each charging contact element comprises: be set to the contact site contacted with described power supply board, described contact site is less than described initial distance value for the distance value between any two points in the plane that contacts with described power supply board.
Wherein alternatively, the minimum value insulated between described every two pieces of power supply boards in the standoff distance value of being separated by is initial distance value;
Each charging contact element comprises: be set to the contact site contacted with described power supply board, described contact site is cylinder, and the distance in described contact site cylinder bottom surface between any two points is less than initial distance value.
Wherein alternatively, described charging contact element also comprises fixed part and elastic portion, and one end of described elastic portion is connected with described fixed part, and the other end is connected with described contact site.
Wherein alternatively, described electric supply installation also comprises: controller;
Described controller, for identify described electric supply installation each power supply board in the power supply board that touches by the charging contact element of described charging device, and control described power supply and power to the described power supply board identified.
Correspondingly, the utility model embodiment still provides a kind of electric supply installation, comprising: power supply and at least two pieces of power supply boards be exposed in external environment condition; Described power supply board is connected to described power supply, and is connected to the power supply board of described positive source and is connected to the power supply board alternately arrangement of described power cathode, insulate and be separated by between every two pieces of power supply boards;
Wherein alternatively, what described electric supply installation was provided by described power supply board and outside device to be powered is connected, to power for this device to be powered for electric contact unit.
Wherein alternatively, described electric supply installation also comprises: controller;
Described controller, for identify described electric supply installation each power supply board in by the device to be powered of outside provide for electric contact unit the power supply board that touches, and control described power supply and power to the described power supply board identified.
Wherein alternatively, described electric supply installation also comprises: communication module;
Described controller, also for identify only have one piece of power supply board be powered contact element contact or detect without charging current time, send the mobile control signal of consulting with described device to be powered to described communication module;
Described communication module, for described mobile control signal is sent to device to be powered, moves according to the control signal of consulting to control described device to be powered.
Wherein alternatively, described electric supply installation also comprises: cleaning assemblies;
Described cleaning assemblies, for performing clean operation according to the control law preset to described power supply board.
Correspondingly, the utility model embodiment still provides a kind of aircraft, comprise: power module and charging device, the charging circuit that described charging device comprises at least two charging contact element and is connected with described at least two contact element of charging, each charging contact element is connected with the negative pole that charges with the charging positive pole of described charging circuit respectively by diode;
Described charging device is contacted with at least two pieces of power supply boards that external powering device provides by charging contact element to be that the described power module connected charges.
Wherein alternatively, each charging contact element comprises: be set to the contact site contacted with the power supply board of external powering device, described contact site is less than initial distance value for the distance value between any two points in the plane that contacts with the power supply board of external powering device, wherein, described initial distance value is the minimum value of spacer distance values between every two pieces of power supply boards of providing of external powering device.
Wherein alternatively, each charging contact element comprises: be set to the contact site contacted with the power supply board of external powering device, described contact site is cylinder, distance in described contact site cylinder bottom surface between any two points is less than initial distance value, wherein, described initial distance value is the minimum value of spacer distance values between every two pieces of power supply boards of providing of external powering device.
Wherein alternatively, described charging contact element also comprises fixed part and elastic portion, and one end of described elastic portion is connected with described fixed part, and the other end is connected with described contact site.
Wherein alternatively, described aircraft also comprises: sniffer;
Described sniffer, for identifying the position of at least two pieces of power supply boards that external powering device provides, lands to indicate aircraft.
Wherein alternatively, described aircraft also comprises: communication module;
Described communication module, for when receiving the mobile control signal that external powering device sends, instruction aircraft carries out according to described mobile control signal mobile and landing of going around.
Wherein alternatively, described aircraft also comprises: checkout gear;
Described checkout gear, for be accommodated to external powering device at described aircraft power supply board after, if detect, described charging circuit does not produce charging current, then indicate aircraft to go around and land.
The utility model embodiment can at all types of SUAVs, or in the equipment such as Remote Control Vehicle, robot, access charging circuit at lower cost, fast to charge, without the need to accurately locating and accurately moving, greatly reduce control overflow and difficulty.Simultaneously because charging touch panel has good contact with charging electric shock, the requirement of big current quick charge can be met, improve charging operating efficiency.
Accompanying drawing explanation
Fig. 1 is the structural representation of the charging system of the utility model embodiment;
Fig. 2 is the structural representation of power supply board in electric supply installation;
Fig. 3 is the circuit connection diagram of the charging contact element of the charging device of the utility model embodiment;
Fig. 4 is wherein a kind of structural representation of the charging contact element of the utility model embodiment;
Fig. 5 is the wherein another kind of structural representation of the charging contact element of the utility model embodiment;
Fig. 6 is wherein another structural representation of the charging contact element of the utility model embodiment;
Fig. 7 is the structural representation of a kind of electric supply installation of the utility model embodiment;
Fig. 8 is the structural representation of a kind of aircraft of the utility model embodiment.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
In the utility model embodiment, electric supply installation can be arranged on ground as a supply station, and the power supply board be exposed in external environment condition can be connected with power supplys such as civil power, Large Copacity storage battery, and power supply board can level or the mode such as vertical be placed.As UAV (Unmanned Aerial Vehicle, unmanned plane) etc. aircraft, Remote Control Vehicle, robot etc. can by the charging device with two or more charging contact element quickly and easily with expose power supply board in the environment and contact, complete charging.
Specifically refer to Fig. 1, it is the structural representation of the charging system of the utility model embodiment, the described charging system of the utility model embodiment comprises: electric supply installation 20 and charging device 10, described electric supply installation 20 can be arranged in a surface power supply station, be specifically as follows landing and the automatic charging platform of an aircraft, or be the charging pile etc. of the equipment such as ground remote control vehicle, robot.
Described electric supply installation 20 comprises: power supply 201 and at least two pieces of power supply boards 202 be exposed in external environment condition; Described power supply board 202 is connected to described power supply 201, and is connected to the power supply board of described power supply 201 positive pole and is connected to the power supply board alternately arrangement of described power supply 201 negative pole, insulate and be separated by between every two pieces of power supply boards;
The charging circuit 101 that described charging device 10 comprises at least two charging contact element 102 and is connected with described at least two contact element 102 of charging, each charging contact element 102 is connected with the negative pole that charges with the charging positive pole of described charging circuit 101 respectively by diode;
Described charging device 10 is contacted with described power supply board 202 by charging contact element 102 to be that the load connected is charged.
Described power supply 201 can for civil power, also can be a jumbo storage battery, can be accordingly as equipment charges such as aircraft, Remote Control Vehicle, robots.Described power supply board 202 is specifically as follows copper coin or also can is ask the detachable conductive plate etc. manually adding width and length as required, and the power supply board 202 that can configure large-size contacts with the charging contact element 102 of charging device 10 to facilitate.
In the utility model embodiment, as shown in Figure 2, the power supply board 202 in electric supply installation 20 can be the copper sheet of strip, can arrange the substrate of an insulation, it cover the copper sheet as power supply board 202 of not mutual conduction.Take width as L, the cuboid power supply board 202 that length and thickness can be arranged as required is described for example, in other embodiments, shape, the size of power supply board 202 can be arranged arbitrarily as required, be separated by as long as ensureing insulate between every two pieces of power supply boards 202, and be connected to the power supply board of described power supply 201 positive pole and be connected to the power supply board alternately arrangement of described power supply 201 negative pole, such as, power supply board 202 can be the polygon copper coin of the various sizes such as triangle, pentagon size.
The quantity of power supply board 202 can carry out choosing configuration as required, can configure the region that a large amount of power supply boards 202 forms larger area, so that power to multiple stage equipment to be powered simultaneously.
Fig. 3 shows the circuit connection diagram of the charging contact element 102 of charging device 10 in the utility model embodiment, as seen from Figure 3, if the power supply board 202 that charging contact element 102 touches is positive pole power supply board, the then diode current flow of access charging positive pole, if and the power supply board 202 that charging contact element 102 touches is negative pole power supply board, the then diode current flow of access charging negative pole, when having at least one power supply board touching positive pole in three of the charging device 10 shown in Fig. 4 charging contact element 102 and at least one touches the power supply board of negative pole, the load charging of charging device 10 can be embodied as.When the number of contact element 102 of charging is more, the probability simultaneously having positive and negative power supply board to be touched is also larger.
Concrete, in order to ensure that charging contact element 102 better, more stably contacts with positive and negative charging contact element 102, and avoiding the generation of short circuit accident, correspondence can be carried out to the size of insulation gap between contact element 102, power supply board 202 and power supply board 202 of charging and arranging.
Wherein, the minimum value insulated between described every two pieces of power supply boards 202 in the standoff distance value of being separated by is initial distance value;
Each charging contact element 102 comprises: be set to the contact site contacted with described power supply board 202, described contact site is less than described initial distance value for the distance value between any two points in the plane that contacts with described power supply board 202.
The width of power supply board 202 can be shown in Fig. 2 in L, the distance of insulation gap is d, and now d is initial distance value.Then described contact site needs to be less than d for the distance value between two points of furthest apart in the plane that contacts with described power supply board 202, such as, when contact site is cylinder, the diameter of the bottom surface that cylindrical charging contact element 102 contacts with power supply board 202 is infinitely close to d, but be not d, so can guarantee that a charging contact element 102 can not touch positive and negative power supply board simultaneously, guarantee the accident that can not be short-circuited.And further, distance between every two charging contact element 102 then can be got and is more than or equal to L to the number be less than in 2L, can ensure that the equipment such as aircraft, Remote Control Vehicle, robot are when needs charging contacts with power supply board 202, can touch positive and negative power supply board to greater probability simultaneously preferably with this.
Further, described charging contact element 102 can be the foot rest of unmanned plane, also can be mounted in the extensible probe etc. on the equipment such as Remote Control Vehicle, robot.Charging contact element 102 can be the cylinder such as cylinder, various prisms, and between described every two pieces of power supply boards 202, the minimum value insulated in the standoff distance value of being separated by is initial distance value; Each charging contact element 102 comprises: be set to the contact site contacted with described power supply board 202, described contact site is cylinder, and the distance in described contact site cylinder bottom surface between any two points is less than described initial distance value.The number of charging contact element 102 also can be more than or equal to 3, and becomes regular polygon arrangement, and concrete size can with reference to the size shown in figure 2, Fig. 4 to Fig. 6.
Further alternatively, described charging contact element 102 also comprises fixed part and elastic portion, and one end of described elastic portion is connected with described fixed part, and the other end is connected with described contact site.Elastic portion can be spring or other damping devices, aircraft not only can be made to land for this kind of design or Remote Control Vehicle, robotic contact is to can damping during power supply board 202, reduce the damage to power supply board 202 and aircraft, Remote Control Vehicle or robot, the good contact of all contact element and power supply board 202 can also be ensured preferably.
Further alternatively, described electric supply installation 20 also comprises: controller;
Described controller, for identify described electric supply installation 20 each power supply board 202 in the power supply board 202 that touches by the charging contact element 102 of described charging device 10, and control described power supply 201 and power to the described power supply board 202 identified.
Whether the pressure that described controller can produce based on each power supply board 202 of detection, each power supply board 202 produce the modes such as charging current to determine the power supply board 202 be accessed.
Detect simultaneously the power supply board 202 of at least one piece of positive pole and the power supply board 202 of at least one piece of negative pole all produces deformation there is force value time, two pieces of such as adjacent power supply boards 202 produce deformation when having a force value, and just control is powered to these power supply boards 202.
Or, described electric supply installation 20 controls power supply 201 and powers to each power supply board 202, when there being charging contact element 102 to touch the power supply board of the power supply board of certain block positive pole and negative pole, form loop, the circuit of these two pieces of power supply board 202 correspondences can produce normal current, now only maintain power supply 201 to the power supply of these two pieces of power supply boards 202, and disconnect the power supply to other power supply boards 202.Wherein, described electric supply installation 20 can be after receiving the request power supply signal that described device such as charging device 10 grade sends, and controls power supply 201 and powers, so that sensed current signal to each power supply board 202; Or described electric supply installation 20 according to the power supplies regulation preset, as periodically brief power supplies regulation, can control power supply 201 and briefly powers, so that sensed current signal to each power supply board 202.
By above-mentioned controller, can realize only having powered to the power supply of the equipment such as aircraft, Remote Control Vehicle or robot to the power supply board 202 be touched, reduce the quantity of the power supply board 202 of energising, effectively can reduce the risk of accidental short circuit.
Further alternatively, electric supply installation 20 can also comprise cleaning assemblies, the control law that described cleaning assemblies is used for according to presetting performs clean operation to described power supply board 202.Cleaning assemblies can comprise the parts such as motor, brush, has carried out the cleaning work to each power supply board 202 by driven by motor brush, and after effectively can preventing long-time use, dirt causes the situation of loose contact too much.
Further alternatively, described electric supply installation 20 can also arrange communication module;
Described controller, also for identify only have one piece of power supply board 202 or with the power supply board 202 of electrode be powered contact element contact or detect without charging current time, send the mobile control signal of consulting with described device to be powered to described communication module;
Described communication module, for described mobile control signal is sent to device to be powered, moves according to the control signal of consulting to control described device to be powered.
One piece of power supply board 202 is only had when described controller detects, only there is the power supply board 202 of two pieces or polylith positive pole, the pressure only having two pieces or polylith to be all on the power supply board 202 of negative pole is larger, or when detecting that power supply board 202 is touched contact but does not all have electric current to produce in each power supply board 202, mobile control signal can be sent to described communication module, described communication module forwards mobile control signal to the aircraft of coupling, the equipment such as Remote Control Vehicle or robot, go around land again to control aircraft, control Remote Control Vehicle or robot move and contact, to guarantee that charging contact element touches positive and negative power supply board simultaneously.
Known by the description of the utility model embodiment, at all types of SUAVs, or in the equipment such as Remote Control Vehicle, robot, can be at lower cost, quick access charging circuit charges, without the need to accurately locating and accurately moving, greatly reduce control overflow and difficulty.Simultaneously because charging touch panel has good contact with charging electric shock, the requirement of big current quick charge can be met, improve charging operating efficiency.
Refer to Fig. 7 again, it is the structural representation of the electric supply installation 20 of the utility model embodiment, the described electric supply installation 20 of the utility model embodiment can be arranged in a surface power supply station, be specifically as follows landing and the automatic charging platform of an aircraft, or be the charging pile etc. of the equipment such as ground remote control vehicle, robot.
Described electric supply installation 20 comprises: power supply 201 and at least two pieces of power supply boards 202 be exposed in external environment condition; Described power supply board 202 is connected to described power supply 201, and is connected to the power supply board of described power supply 201 positive pole and is connected to the power supply board alternately arrangement of described power supply 201 negative pole, insulate and be separated by between every two pieces of power supply boards 202;
Wherein, what described electric supply installation 20 was provided by described power supply board 202 and outside device to be powered is connected, to power for this device to be powered for electric contact unit.
Described power supply 201 can for civil power, also can be a jumbo storage battery, can be accordingly as equipment charges such as aircraft, Remote Control Vehicle, robots.Described power supply board 202 is specifically as follows copper coin or also can is ask the detachable conductive plate etc. manually adding width and length as required, and the power supply board 202 that can configure large-size contacts for the charging contact element of charging with device to be powered to facilitate.
The specific descriptions of the power supply board 202 of described electric supply installation 20 refer to above-mentioned about the description corresponding to Fig. 2, Fig. 4 to Fig. 6.
Further alternatively, described electric supply installation 20 can also comprise: controller 203;
Described controller 203, for identify described electric supply installation 20 each power supply board 202 in by the device to be powered of outside provide for electric contact unit the power supply board 202 that touches, and control described power supply 201 and power to the described power supply board 202 identified.
Described controller 203 can based on detect the pressure that each power supply board 202 produces, each power supply board 202 whether the mode such as generation current determine the power supply board 202 that is accessed.
Detect the power supply board of the power supply board of at least one piece of positive pole and at least one piece of negative pole produce deformation there is force value time, two pieces of such as adjacent power supply boards 202 produce deformation when having a force value, and just control is powered to these power supply boards 202.
Or, described electric supply installation 20 controls power supply 201 and powers to each power supply board 202, when have touch the power supply board of the power supply board of certain block positive pole and negative pole for electric contact unit simultaneously time, form loop, the circuit of these two pieces of power supply board 202 correspondences can produce normal current, now described controller 203 controls power supply 201 and only maintains power supply to these two pieces of power supply boards 202, and disconnects the power supply to other power supply boards 202.Wherein, can be that described controller 203 controls power supply 201 and powers, so that sensed current signal to each power supply board 202 after receiving the power supply signal that described device such as charging device 10 grade sends; Or can according to the power supplies regulation preset, as periodically brief power supplies regulation, described controller 203 controls power supply 201 and briefly powers, so that sensed current signal to each power supply board 202.
By above-mentioned controller 203, can realize only having powered to the power supply of the equipment such as aircraft, Remote Control Vehicle or robot to the power supply board 202 be touched, reduce the quantity of the power supply board 202 of energising, effectively can reduce the risk of accidental short circuit.
Described controller 203 can for relevant process chip.
Further alternatively, described electric supply installation 20 can also comprise: communication module 204;
Described controller 203, also for identify only have one piece of power supply board 202 or with the power supply board 202 of electrode be powered contact element contact or detect without charging current time, send the mobile control signal of consulting with described device to be powered to described communication module;
Described communication module 204, for described mobile control signal is sent to device to be powered, moves according to the control signal of consulting to control described device to be powered.
Described communication module 204 can realize communication based on bluetooth, communication mode that the is infrared or form such as mobile communication, wifi.
One piece of power supply board 202 is only had when described controller 203 detects, only there is the power supply board 202 of two pieces or polylith positive pole, the pressure only having two pieces or polylith to be all on the power supply board 202 of negative pole is larger, or when detecting that power supply board 202 is contacted by the confession electric contact unit of outside but do not have electric current to produce in each power supply board 202, mobile control signal can be sent to described communication module, described communication module can send mobile control signal to the aircraft of coupling, the equipment such as Remote Control Vehicle or robot, go around land again to control aircraft, control Remote Control Vehicle or robot move and contact, to guarantee that charging contact element touches positive and negative power supply board 202.
Further alternatively, described electric supply installation 20 can also comprise: cleaning assemblies 205;
Described cleaning assemblies 205, for performing clean operation according to the control law preset to described power supply board 202.Described cleaning assemblies 205 can comprise the parts such as motor, brush, has carried out the cleaning work to each power supply board 202 by driven by motor brush, and after effectively can preventing long-time use, dirt causes the situation of loose contact too much.
Known by the description of the utility model embodiment, the power supply board provided can be at lower cost, quick access charging circuit is that the equipment such as corresponding unmanned plane, Remote Control Vehicle and robot charge, without the need to accurately locating and accurately moving, greatly reduce control overflow and difficulty, improve charging operating efficiency.
Refer to Fig. 8 again, it is the structural representation of a kind of aircraft of the utility model embodiment, this aircraft comprises existing agent structure, Power Component, and navigation module, the existing functional module such as motion sensor, in the utility model embodiment, described aircraft also comprises: power module 100 and charging device 10, the charging circuit 101 that described charging device 10 comprises at least two charging contact element 102 and is connected with described at least two contact element 102 of charging, and each charging contact element 102 is connected with the negative pole that charges with the charging positive pole of described charging circuit 101 respectively by diode,
Described charging device 10 is contacted with at least two pieces of power supply boards that external powering device provides by charging contact element 102 to be that the described power module 100 connected charges.Charging contact element 102 can be arranged on the foot rest of aircraft, also can be set to one group of telescopic probe.
Outside electric supply installation is specifically as follows the corresponding structure described in embodiment of Fig. 7.The shape of described charging device 10 and correspond to the size of outside electric supply installation, can with reference to content corresponding to Fig. 2, Fig. 4 to Fig. 6 in foregoing description.
Concrete, each charging contact element 102 comprises: be set to the contact site contacted with the power supply board of external powering device, described contact site is less than initial distance value for the distance value between any two points in the plane that contacts with the power supply board of external powering device, wherein, this initial distance value is the minimum value of spacer distance values between every two pieces of power supply boards of providing of external powering device.
Further, charging contact element 102 can be the foot rest of unmanned plane, also can be mounted in the extensible probe etc. on the equipment such as Remote Control Vehicle, robot.Charging contact element 102 can be the cylinder such as cylinder, various prisms, each charging contact element 102 comprises: be set to the contact site contacted with the power supply board of external powering device, described contact site is cylinder, and the distance in described contact site cylinder bottom surface between any two points is less than initial distance value.
Further alternatively, described charging contact element 102 also comprises fixed part and elastic portion, and one end of described elastic portion is connected with described fixed part, and the other end is connected with described contact site.Elastic portion can be spring or other damping devices, aircraft not only can be made to land for this kind of design or Remote Control Vehicle, robotic contact is to can damping during power supply board, reduce the damage to power supply board and aircraft, Remote Control Vehicle or robot, the good contact of all contact element and power supply board can also be ensured preferably.
Further alternatively, described charging device 10 can also comprise: sniffer 103;
Described sniffer 103, for identifying the position of at least two pieces of power supply boards that external powering device provides, lands to indicate aircraft.
Described sniffer 103 specifically comprises any one or more in the modules such as camera, infrared locator, laser locator, carry out simple pattern identification based on the first-class picture collected of shooting can comparatively accurately drop on the both positive and negative polarity power supply board of external powering device, and based on infrared ray, the laser launched or receive, also can comparatively accurately drop on the both positive and negative polarity power supply board of external powering device.
Further alternatively, described aircraft can also comprise: communication module 104;
Described communication module 104, for when receiving the mobile control signal that external powering device sends, instruction aircraft carries out according to described mobile control signal mobile and landing of going around.
External powering device can detect that all charging contact element 102 only touch one piece of power supply board, or on power supply board during the situation such as no current, sends the mobile control signal of negotiation.The communication module 104 of aircraft is after receiving the mobile control signal of this negotiation, specifically can forward this to the flight controller of aircraft and move control signal, moved control signal by flight controller complete going around of aircraft and landing operation again, to guarantee that the charging contact element 102 of flying at least can contact the power supply board of two pieces of opposed polarities simultaneously based on this.
Further alternatively, described aircraft can also comprise: checkout gear 105;
Described checkout gear 105, for be accommodated to external powering device at described aircraft power supply board after, if detect, described charging circuit 101 does not produce charging current, then indicate aircraft to go around and land.
Known by the description of the utility model embodiment, at all types of SUAVs, or in the equipment such as Remote Control Vehicle, robot, can be at lower cost, quick access charging circuit charges, without the need to accurately locating and accurately moving, greatly reduce control overflow and difficulty.Simultaneously because charging touch panel has good contact with charging electric shock, the requirement of big current quick charge can be met, improve charging operating efficiency.
The foregoing is only embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every utilize the utility model specification and accompanying drawing content to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present utility model.
Claims (16)
1. a charging system, is characterized in that, comprising: electric supply installation and charging device, wherein:
Described electric supply installation comprises: power supply and at least two pieces of power supply boards be exposed in external environment condition; Described power supply board is connected to described power supply, and is connected to the power supply board of described positive source and is connected to the power supply board alternately arrangement of described power cathode, insulate and be separated by between every two pieces of power supply boards;
The charging circuit that described charging device comprises at least two charging contact element and is connected with described at least two contact element of charging;
Described charging device is contacted with described power supply board by charging contact element to be that the load connected is charged.
2. the system as claimed in claim 1, is characterized in that,
Between described every two pieces of power supply boards, the minimum value insulated in the standoff distance value of being separated by is initial distance value;
Each charging contact element comprises: be set to the contact site contacted with described power supply board, described contact site is less than described initial distance value for the distance value between any two points in the plane that contacts with described power supply board.
3. the system as claimed in claim 1, is characterized in that,
Between described every two pieces of power supply boards, the minimum value insulated in the standoff distance value of being separated by is initial distance value;
Each charging contact element comprises: be set to the contact site contacted with described power supply board, described contact site is cylinder, and the distance in described contact site cylinder bottom surface between any two points is less than described initial distance value.
4. system as claimed in claim 2 or claim 3, is characterized in that,
Described charging contact element also comprises fixed part and elastic portion, and one end of described elastic portion is connected with described fixed part, and the other end is connected with described contact site.
5. the system as claimed in claim 1, is characterized in that, described electric supply installation also comprises: controller;
Described controller, powers to the power supply board identified for controlling described power supply.
6. an electric supply installation, is characterized in that, comprising: power supply and at least two pieces of power supply boards be exposed in external environment condition; Described power supply board is connected to described power supply, and is connected to the power supply board of described positive source and is connected to the power supply board alternately arrangement of described power cathode, and insulate between every two pieces of power supply boards and be separated by, described power supply comprises mains supply or storage battery;
Wherein, what described electric supply installation was provided by described power supply board and outside device to be powered is connected, to power for this device to be powered for electric contact unit.
7. device as claimed in claim 6, is characterized in that, also comprise: controller;
Described controller, powers to the power supply board identified for controlling described power supply.
8. device as claimed in claim 7, is characterized in that, also comprise: communication module;
Described controller, also for sending the mobile control signal of consulting with described device to be powered to described communication module;
Described communication module, for described mobile control signal being sent to outside device to be powered, moves according to the control signal of consulting to control described device to be powered.
9. device as claimed in claim 7, is characterized in that, also comprise: for performing the cleaning assemblies of clean operation to described power supply board.
10. an aircraft, is characterized in that, comprising: power module and charging device, the charging circuit that described charging device comprises at least two charging contact element and is connected with described at least two contact element of charging;
Described charging device is contacted with at least two pieces of power supply boards that external powering device provides by charging contact element to be that the described power module connected charges.
11. aircraft as claimed in claim 10, it is characterized in that, each charging contact element comprises: be set to the contact site contacted with the power supply board of external powering device, described contact site is less than initial distance value for the distance value between any two points in the plane that contacts with the power supply board of external powering device, wherein, described initial distance value is the minimum value of spacer distance values between every two pieces of power supply boards of providing of external powering device.
12. aircraft as claimed in claim 10, it is characterized in that, each charging contact element comprises: be set to the contact site contacted with the power supply board of external powering device, described contact site is cylinder, distance in described contact site cylinder bottom surface between any two points is less than initial distance value, wherein, described initial distance value is the minimum value of spacer distance values between every two pieces of power supply boards of providing of external powering device.
13. aircraft as described in claim 11 or 12, it is characterized in that, described charging contact element also comprises fixed part and elastic portion, and one end of described elastic portion is connected with described fixed part, and the other end is connected with described contact site.
14. aircraft as claimed in claim 10, is characterized in that, also comprise: sniffer;
Described sniffer, for identifying the position of at least two pieces of power supply boards that external powering device provides, lands to indicate aircraft.
15. aircraft as claimed in claim 10, is characterized in that, also comprise: communication module;
Described communication module, is used to indicate aircraft and carries out according to the mobile control signal received mobile and landing of going around.
16. aircraft as claimed in claim 10, is characterized in that, also comprise: checkout gear;
Described checkout gear, if be accommodated to the power supply board of external powering device for described aircraft but described charging circuit does not produce charging current, then indicate aircraft to go around and lands.
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| CN201420314042.8U CN204068303U (en) | 2014-06-12 | 2014-06-12 | A kind of charging system, electric supply installation and aircraft |
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| CN201420314042.8U CN204068303U (en) | 2014-06-12 | 2014-06-12 | A kind of charging system, electric supply installation and aircraft |
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