CN203982395U - Electric drive unmanned plane is stopped maintenance system - Google Patents

Electric drive unmanned plane is stopped maintenance system Download PDF

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Publication number
CN203982395U
CN203982395U CN201420409289.8U CN201420409289U CN203982395U CN 203982395 U CN203982395 U CN 203982395U CN 201420409289 U CN201420409289 U CN 201420409289U CN 203982395 U CN203982395 U CN 203982395U
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China
Prior art keywords
unmanned plane
electric drive
power supply
drive unmanned
module
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Expired - Fee Related
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CN201420409289.8U
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Chinese (zh)
Inventor
潘若愚
褚伟
杨善林
曹龙涛
李荣灿
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潘若愚
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Priority to CN201420409289.8U priority Critical patent/CN203982395U/en
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Abstract

The utility model discloses a kind of electric drive unmanned plane and stop maintenance system, comprise electric drive unmanned plane and stop maintenance site; Described electric drive unmanned plane comprises charging cell module and electronic tag, and described charging cell module comprises the secondary coil of accumulator and the described accumulator of electrical connection; Described stop maintenance site comprises charge power supply module and for identifying the radio frequency identification module of described electronic tag, described charge power supply module comprises power supply, is electrically connected the charge coil of described power supply and controls described power supply the controller that is electrically connected break-make with described charge coil, described charge coil can be launched the electromagnetic wave with described secondary coil coupling, and described controller is connected with described radio frequency identification module signal.Electric drive unmanned plane stop maintenance system described in the utility model, has realized small electrical and has driven the orderly management of unmanned plane and long distance to cruise, and has reduced the hand labor amount of electric drive unmanned plane in the time that stop maintenance site is carried out upkeep operation.

Description

Electric drive unmanned plane is stopped maintenance system
Technical field
The utility model relates to a kind of electric drive unmanned plane and stops maintenance system, belongs to identification stop and the battery boosting technology field thereof of electric drive unmanned plane.
Background technology
Small-sized electric drive unmanned plane is because the power fan-out capability of power system is limited, the battery volume and weight that therefore can carry is limited, thereby cause small electrical drive unmanned plane flying power a little less than, the flight operating radius that has determined thus small-sized electric drive unmanned plane is limited, can effectively overcome the limited problem of flight operating radius of small-sized electric drive unmanned plane by electric drive unmanned plane stop maintenance system is set in predetermined area.But in the prior art, the stop maintenance system of not developing for small-sized electric drive unmanned plane specially.
Utility model content
The needs that the utility model exists based on prior art just, provide a kind of electric drive unmanned plane to stop maintenance system, meet actual operation requirements.
For addressing the above problem, technical solution adopted in the utility model is as follows:
A kind of electric drive unmanned plane is stopped maintenance system, comprising: electric drive unmanned plane and stop maintenance site; Described electric drive unmanned plane comprises charging cell module and electronic tag, and described charging cell module comprises the secondary coil of accumulator and the described accumulator of electrical connection; Described stop maintenance site comprises charge power supply module and for identifying the radio frequency identification module of described electronic tag, described charge power supply module comprises power supply, is electrically connected the charge coil of described power supply and controls described power supply the controller that is electrically connected break-make with described charge coil, described charge coil can be launched the electromagnetic wave with described secondary coil coupling, and described controller is connected with described radio frequency identification module signal.
As the improvement of technique scheme, described charge power supply module also comprises the load cell for detection of described charge coil load signal, and described load cell is connected with described controller signals.
As the improvement of technique scheme, described electric drive unmanned plane also comprises battery detecting module and wireless communication module, described battery detecting module comprises voltage sensor, described voltage sensor is connected with described storage battery, and described voltage sensor is connected with described radio communication mold block signal, and described wireless communication module is connected with described controller signals.Described wireless communication module is connected with described controller signals and does not should be understood to described wireless communication module and be only connected with described controller signals, described wireless communication module is except being connected with described controller signals, can also be connected with the personnel operating side signal of controlling electric drive unmanned plane during flying, so that operating personnel understand the voltage condition of described accumulator in real time, thereby before will exhausting, sends in time described accumulator electric energy the remote signal of stopping charging.
As the improvement of technique scheme, described stop maintenance site also comprises the ceiling that is fixedly installed and enclosure wall that can switch, or described stop maintenance site also comprises the enclosure wall that is fixedly installed and ceiling that can switch.
Compared with prior art, implementation result of the present utility model is as follows for the utility model:
Electric drive unmanned plane described in the utility model is stopped maintenance system, stop maintenance site and identify electric drive unmanned plane by REID, then the power supply of stopping maintenance site carries out wireless charging to the accumulator of electric drive unmanned plane, drive the orderly management of unmanned plane and long distance to cruise thereby realized small electrical, reduced the hand labor amount of electric drive unmanned plane in the time that stop maintenance site is carried out upkeep operation.
Brief description of the drawings
Fig. 1 is that electric drive unmanned plane described in the utility model is stopped maintenance system structural representation.
Embodiment
Content of the present utility model is described below in conjunction with specific embodiments.
As shown in Figure 1, for electric drive unmanned plane described in the utility model is stopped maintenance system structural representation.Electric drive unmanned plane described in the utility model is stopped maintenance system, comprising: electric drive unmanned plane and stop maintenance site; Described electric drive unmanned plane comprises charging cell module 1 and electronic tag 2, and described charging cell module 1 comprises the secondary coil 12 of accumulator 11 and the described accumulator 11 of electrical connection; Described stop maintenance site comprises charge power supply module 3 and for identifying the radio frequency identification module 4 of described electronic tag 2, described charge power supply module 3 comprises power supply 31, is electrically connected the charge coil 32 of described power supply 31 and controls described power supply 31 controller 33 that is electrically connected break-make with described charge coil 32, described charge coil 32 can be launched the electromagnetic wave being coupled with described secondary coil 12, and described controller 33 is connected with described radio frequency identification module 4 signals.Further with improvement, described charge power supply module 3 also comprises the load cell 34 for detection of described charge coil 32 load signals, and described load cell 34 is connected with described controller 33 signals.Further with improvement, described electric drive unmanned plane also comprises battery detecting module 5 and wireless communication module 6, described battery detecting module 5 comprises voltage sensor 51, described voltage sensor 51 is electrically connected with described accumulator 11, and described voltage sensor 51 is connected with described wireless communication module 6 signals, described wireless communication module 6 is connected with described controller 33 signals.
Obtain the voltage condition of described accumulator 11 by voltage sensor 51, in the time of the brownout of described accumulator 11, the information of voltage of the described accumulator 11 that described wireless communication module 6 obtains described voltage sensor 51 is sent to personnel operating side, and operating personnel send the remote signal of stopping charging to electric drive unmanned plane.Electric drive unmanned plane is accommodated to be stopped after maintenance site, described radio frequency identification module 4 identifies described electronic tag 2 by REID, thereby sending signal makes described controller 33 connect being electrically connected between described power supply 31 and described charge coil 32, the electromagnetic wave that described charge coil 32 transmittings and described secondary coil 12 are coupled, the electromagnetic wave that described secondary coil 12 is accepted to be coupled with it also generates induced potential and charges to described accumulator 11, in the time that described accumulator 11 voltages reach predetermined value, described voltage sensor 51 sends signal to described controller 33, described controller 33 disconnects being electrically connected between described power supply 31 and described charge coil 32, thereby stop described accumulator 11 to charge.In addition, when electric drive unmanned plane flies away from stop maintenance site in the time charging, described load cell 34 is experienced on described charge coil 32 does not have load, sends signal to described controller 33, and described controller 33 disconnects being electrically connected between described power supply 31 and described charge coil 32.
Further with improvement, described stop maintenance site also comprises the ceiling that is fixedly installed and enclosure wall that can switch, or described stop maintenance site also comprises the enclosure wall that is fixedly installed and ceiling that can switch.Safety and upkeep operation in order to ensure electric drive unmanned plane are interference-free, stop maintenance site and should be provided with physical protection device, should there be the ceiling that is fixedly installed and enclosure wall that can switch for outdoor stop maintenance site, should have the enclosure wall that is fixedly installed and ceiling that can switch for the stop maintenance site of warehouse-type; These can complete by motor and mechanical linkage.
Above content is the detailed description of in conjunction with specific embodiments the utility model being done, and can not assert that the concrete enforcement of the utility model only limits to these explanations.For the utility model person of ordinary skill in the field, without departing from the concept of the premise utility, can also make some simple deduction or replace, all should be considered as belonging to the scope of the utility model protection.

Claims (4)

1. electric drive unmanned plane is stopped a maintenance system, it is characterized in that, comprising: electric drive unmanned plane and stop maintenance site, described electric drive unmanned plane comprises charging cell module (1) and electronic tag (2), and described charging cell module (1) comprises the secondary coil (12) of accumulator (11) and the described accumulator of electrical connection (11), described stop maintenance site comprises charge power supply module (3) and for identifying the radio frequency identification module (4) of described electronic tag (2), described charge power supply module (3) comprises power supply (31), be electrically connected the charge coil (32) of described power supply (31), and control described power supply (31) and be electrically connected with described charge coil (32) controller (33) of break-make, described charge coil (32) can be launched the electromagnetic wave with described secondary coil (12) coupling, described controller (33) is connected with described radio frequency identification module (4) signal.
2. electric drive unmanned plane as claimed in claim 1 is stopped maintenance system, it is characterized in that, described charge power supply module (3) also comprises the load cell (34) for detection of described charge coil (32) load signal, and described load cell (34) is connected with described controller (33) signal.
3. electric drive unmanned plane as claimed in claim 1 is stopped maintenance system, it is characterized in that, described electric drive unmanned plane also comprises battery detecting module (5) and wireless communication module (6), described battery detecting module (5) comprises voltage sensor (51), described voltage sensor (51) is electrically connected with described accumulator (11), and described voltage sensor (51) is connected with described wireless communication module (6) signal, described wireless communication module (6) is connected with described controller (33) signal.
4. electric drive unmanned plane as claimed in claim 1 is stopped maintenance system, it is characterized in that, described stop maintenance site also comprises the ceiling that is fixedly installed and enclosure wall that can switch, or described stop maintenance site also comprises the enclosure wall that is fixedly installed and ceiling that can switch.
CN201420409289.8U 2014-07-23 2014-07-23 Electric drive unmanned plane is stopped maintenance system Expired - Fee Related CN203982395U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420409289.8U CN203982395U (en) 2014-07-23 2014-07-23 Electric drive unmanned plane is stopped maintenance system

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CN201420409289.8U CN203982395U (en) 2014-07-23 2014-07-23 Electric drive unmanned plane is stopped maintenance system

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104852475A (en) * 2015-04-14 2015-08-19 中电科(德阳广汉)特种飞机系统工程有限公司 Method and system for wirelessly charging unmanned aerial vehicle
CN105226836A (en) * 2015-10-20 2016-01-06 杨珊珊 A kind of can the unmanned plane of automatic charging, unmanned plane charging system and charging method
CN105262187A (en) * 2015-09-22 2016-01-20 张欣 Unmanned plane charging device and charging method
CN105471032A (en) * 2015-12-23 2016-04-06 无锡觅睿恪科技有限公司 Unmanned aerial vehicle wireless charging system
CN107696882A (en) * 2017-07-24 2018-02-16 国网浙江海宁市供电公司 The aerial charging device of unmanned plane

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104852475A (en) * 2015-04-14 2015-08-19 中电科(德阳广汉)特种飞机系统工程有限公司 Method and system for wirelessly charging unmanned aerial vehicle
CN105262187A (en) * 2015-09-22 2016-01-20 张欣 Unmanned plane charging device and charging method
CN105226836A (en) * 2015-10-20 2016-01-06 杨珊珊 A kind of can the unmanned plane of automatic charging, unmanned plane charging system and charging method
CN105471032A (en) * 2015-12-23 2016-04-06 无锡觅睿恪科技有限公司 Unmanned aerial vehicle wireless charging system
CN107696882A (en) * 2017-07-24 2018-02-16 国网浙江海宁市供电公司 The aerial charging device of unmanned plane

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C14 Grant of patent or utility model
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20141203

Termination date: 20200723