CN209290712U - A kind of Modularized unmanned machine system - Google Patents

A kind of Modularized unmanned machine system Download PDF

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Publication number
CN209290712U
CN209290712U CN201822059435.XU CN201822059435U CN209290712U CN 209290712 U CN209290712 U CN 209290712U CN 201822059435 U CN201822059435 U CN 201822059435U CN 209290712 U CN209290712 U CN 209290712U
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CN
China
Prior art keywords
connect
amu
output end
input terminal
unmanned plane
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201822059435.XU
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Chinese (zh)
Inventor
金岭
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Guangdong Kaiyi Zhinong Technology Co ltd
Original Assignee
Foshan Open A Robot Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Foshan Open A Robot Co Ltd filed Critical Foshan Open A Robot Co Ltd
Priority to CN201822059435.XU priority Critical patent/CN209290712U/en
Application granted granted Critical
Publication of CN209290712U publication Critical patent/CN209290712U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of Modularized unmanned machine systems, it is related to unmanned plane technical field of aerospace, the Modularized unmanned machine system, the Modularized unmanned machine system includes: unmanned plane main body, power-supply system, dynamical system, control system and operating system, and the control system includes AMU, IMU, GPS and main controller;The dynamical system includes the mechanical, electrical tune of electricity, drive shaft and rotor;The unmanned plane main body is connect with the power-supply system, and the unmanned plane main body is connect with the operating system.The Modularized unmanned machine system of the utility model uses modular combination, and detachably installation combination between module is easy to use;In addition when any one module is damaged, the module of damage can be only dismantled, the use of other modules is not influenced, thus save the cost;In addition, mode can be switched in main controller, user can be according to different mode, the corresponding operating system with commutation.

Description

A kind of Modularized unmanned machine system
Technical field
The utility model relates to unmanned plane technical field of aerospace, specifically a kind of Modularized unmanned machine system.
Background technique
The varied but current unmanned plane of unmanned plane type on existing market can only be suitble to a kind of operation, drop significantly Low the practicality;In addition existing unmanned plane, mostly integrated setting, user are mostly inconvenience when carrying, and are not easy to make With;When unmanned plane breaks down, entire unmanned plane can only be sent to maintenance by user, be influenced using more seriously, entirely Unmanned plane is scrapped with regard to this, cannot be used completely, and use cost is increased.
Utility model content
The purpose of this utility model is to provide a kind of Modularized unmanned machine system, makes it that combination to be detachably installed, be convenient for Use and be suitble to several work.
To achieve the above object, the utility model provides the following technical solutions: a kind of Modularized unmanned machine system, the mould Block UAV system includes: unmanned plane main body, power-supply system, dynamical system, control system and operating system, the control system System includes AMU, IMU, GPS and main controller;The dynamical system includes the mechanical, electrical tune of electricity, drive shaft and rotor;The unmanned owner Body is connect with the power-supply system, and the unmanned plane main body is connect with the operating system, the unmanned plane main body and the AMU Connection, the AMU are connect with the GPS, and the AMU is connect with the IMU, and the AMU is connect with the main controller, the nothing Man-machine main body is connect with the motor, the power-supply system be electric machine with energy, the motor supply power to drive shaft from And rotor is driven, the motor is adjusted and is connected by described its revolving speed of electric tune section, the main controller and the electricity.
The output end of the power-supply system connects the input terminal of the motor, and the output end connection electricity of the motor is adjusted Input terminal, the output end that the electricity is adjusted connects the input terminal of the drive shaft, and the output end of the drive shaft connects the rotation The input terminal of the wing.
The output end of the AMU connects the input terminal of the GPS, and the output end of the AMU connects the input of the IMU End, the output end of the AMU connect the input terminal of the main controller, and the output end of the IMU connects the input of the main controller End, the output end of the main controller connect the input terminal that the electricity is adjusted.
The power-supply system includes power battery, super capacitor.
The power-supply system, dynamical system, control system and operating system are each as a further improvement of the utility model, From for separate modular, four modules are mountable in unmanned plane main body, detachably installation combination between module, any one disassembly Other uses are not influenced.
Compared with prior art, the utility model has the beneficial effects that the Modularized unmanned machine system uses modularization group It closes, detachably installation combination, is easy to use between module;In addition it when any one module is damaged, can only dismantle The module of damage does not influence the use of other modules, thus save the cost;In addition, mode, user can be switched in main controller Can be according to different mode, the corresponding operating system with commutation.
Detailed description of the invention
Fig. 1 is a kind of structural block diagram of embodiment of the Modularized unmanned machine system of the utility model.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work Every other embodiment obtained, fall within the protection scope of the utility model.
Modularized unmanned machine system described in the utility model includes: unmanned plane main body, power-supply system, dynamical system, control System and operating system, the control system include AMU, IMU, GPS and main controller, the dynamical system include electricity it is mechanical, electrical adjust, Drive shaft and rotor, the unmanned plane main body are connect with the power-supply system, and the unmanned plane main body and the operating system connect It connects, the unmanned plane main body is connect with the AMU, and the AMU is connect with the GPS, and the AMU is connect with the IMU, described AMU is connect with the main controller, and the unmanned plane main body is connect with the motor, and the power-supply system is electric machine with energy, The motor supplies power to drive shaft to drive rotor, and the motor passes through described its revolving speed of electric tune section, the master control Device and the electricity are adjusted and are connected.
Embodiment 1
As shown in Figure 1, the Modularized unmanned machine system includes: unmanned plane main body, power-supply system, dynamical system, control System and operating system, the control system include AMU, IMU, GPS and main controller;The dynamical system include electricity it is mechanical, electrical adjust, Drive shaft and rotor;The unmanned plane main body is connect with the power-supply system, and the unmanned plane main body and the operating system connect It connects, the unmanned plane main body is connect with the AMU, and the AMU is connect with the GPS, and the model of the GPS can be G21, described AMU is connect with the IMU, and the AMU is connect with the main controller, and the unmanned plane main body is connect with the motor, the electricity Source system is electric machine with energy, and the motor supplies power to drive shaft to drive rotor, and the motor passes through the electricity Its revolving speed of tune section, the main controller and the electricity are adjusted and are connected, and the model of the motor can be Y90S-2, and the model which adjusts can be 3S/160A.The output end of the power-supply system connects the input terminal of the motor, and the output end connection electricity of the motor is adjusted Input terminal, the output end that the electricity is adjusted connects the input terminal of the drive shaft, and the output end of the drive shaft connects the rotation The input terminal of the wing, the power-supply system include power battery, super capacitor, and the output end of the AMU connects the input of the GPS End, the output end of the AMU connect the input terminal of the IMU, and the output end of the AMU connects the input terminal of the main controller, The output end of the IMU connects the input terminal of the main controller, and the output end of the main controller connects the input terminal that the electricity is adjusted, The information of acquisition is transferred to main controller by IMU, and main controller is analyzed, and then the information of analysis is transferred to electric tune by main controller, Electricity is adjusted and is transferred to motor later, and motor is executed;The power-supply system, power as a further improvement of the utility model, System, control system and operating system are respectively separate modular, and four modules are mountable in unmanned plane main body, can between module Disassembly installation combination, any one disassembly do not influence other uses, and mode can be switched in main controller, and user can be according to different moulds Formula, the corresponding operating system with commutation.
Compared with prior art, the utility model has the beneficial effects that the Modularized unmanned machine system uses modularization group It closes, detachably installation combination, is easy to use between module;In addition it when any one module is damaged, can only dismantle The module of damage does not influence the use of other modules, thus save the cost;In addition, mode, user can be switched in main controller Can be according to different mode, the corresponding operating system with commutation.
It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in other specific forms Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing for the equivalent requirements of the claims will be fallen in All changes in justice and range are embraced therein.It should not treat any reference in the claims as limiting Related claim.

Claims (5)

1. a kind of Modularized unmanned machine system, which is characterized in that the Modularized unmanned machine system includes: unmanned plane main body, electricity Source system, dynamical system, control system and operating system, the control system include AMU, IMU, GPS and main controller;It is described dynamic Force system includes the mechanical, electrical tune of electricity, drive shaft and rotor;The unmanned plane main body is connect with the power-supply system, the unmanned plane Main body is connect with the operating system, and the unmanned plane main body is connect with the AMU, and the AMU is connect with the GPS, described AMU is connect with the IMU, and the AMU is connect with the main controller, and the unmanned plane main body is connect with the motor, the electricity Source system is electric machine with energy, and the motor supplies power to drive shaft to drive rotor, and the motor passes through the electricity Its revolving speed of tune section, the main controller and the electricity are adjusted and are connected.
2. a kind of Modularized unmanned machine system according to claim 1, it is characterised in that: the power-supply system, dynamical system System, control system and operating system are respectively separate modular, and four modules are mountable in unmanned plane main body, removable between module Installation combination is unloaded, any one disassembly does not influence other uses.
3. a kind of Modularized unmanned machine system according to claim 1, it is characterised in that: the output end of the power-supply system The input terminal of the motor is connected, the output end of the motor connects the input terminal that the electricity is adjusted, and the output end that the electricity is adjusted connects The input terminal of the drive shaft is connect, the output end of the drive shaft connects the input terminal of the rotor.
4. a kind of Modularized unmanned machine system according to claim 1, it is characterised in that: the output end of the AMU connects The input terminal of the GPS, the output end of the AMU connect the input terminal of the IMU, and the output end of the AMU connects the master The input terminal of device is controlled, the output end of the IMU connects the input terminal of the main controller, described in the output end connection of the main controller The input terminal that electricity is adjusted.
5. a kind of Modularized unmanned machine system according to claim 1, it is characterised in that: the power-supply system includes power Battery, super capacitor.
CN201822059435.XU 2018-12-10 2018-12-10 A kind of Modularized unmanned machine system Expired - Fee Related CN209290712U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201822059435.XU CN209290712U (en) 2018-12-10 2018-12-10 A kind of Modularized unmanned machine system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201822059435.XU CN209290712U (en) 2018-12-10 2018-12-10 A kind of Modularized unmanned machine system

Publications (1)

Publication Number Publication Date
CN209290712U true CN209290712U (en) 2019-08-23

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022120796A1 (en) * 2020-12-11 2022-06-16 深圳市大疆创新科技有限公司 Modular unmanned aerial vehicle and operation method therefor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022120796A1 (en) * 2020-12-11 2022-06-16 深圳市大疆创新科技有限公司 Modular unmanned aerial vehicle and operation method therefor

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GR01 Patent grant
GR01 Patent grant
CP01 Change in the name or title of a patent holder

Address after: 528300 Chihua Community Resident Committee, Chencun Town, Shunde District, Foshan City, Guangdong Province

Patentee after: Guangdong Kaiyi Zhinong Technology Co.,Ltd.

Address before: 528300 Chihua Community Resident Committee, Chencun Town, Shunde District, Foshan City, Guangdong Province

Patentee before: KAYI ROBOTICS Ltd.

CP01 Change in the name or title of a patent holder
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190823

Termination date: 20211210

CF01 Termination of patent right due to non-payment of annual fee