CN218850419U

CN218850419U - Intelligent flying battery

Info

Publication number: CN218850419U
Application number: CN202221951887.9U
Authority: CN
Inventors: 侯庆
Original assignee: Shenzhen Aoshe Information Technology Co ltd
Current assignee: Shenzhen Aoshe Information Technology Co ltd
Priority date: 2022-07-27
Filing date: 2022-07-27
Publication date: 2023-04-11
Anticipated expiration: 2032-07-27

Abstract

The utility model relates to an intelligence flight battery, including the unmanned aerial vehicle body, battery body, BMS battery management system unit, collection module, BMS battery management system, power module, a control module, a display module, wireless communication module, the group battery inner core, the battery switch unit, load detection module and display screen, a serial communication port, battery body in the unmanned aerial vehicle body is inside including BMS battery management system unit, BMS battery management system unit is including collection module, BMS battery management system, power module and control module, collection module's output is connected to BMS battery management system's input. Has the advantages that: prevent that external load short circuit from arousing that the group battery inner core from damaging, effectively protect the battery, the time display screen calculates battery duration, and power display screen and power indicator are the percentage display window of current residual capacity, can accurately show residual capacity, realize intelligent flight, and simple structure is stable, reasonable in design ingenious, and practical value is high.

Description

Intelligent flying battery

Technical Field

The utility model relates to a battery correlation technique field particularly, relates to an intelligence flight battery.

Background

Smart batteries, also known as Smart Battery Systems (SBS), are a branch and an important component of modern power technology, which utilize internal electronics to measure, calculate and store battery data, which makes the use and management of power more predictable.

The battery of aircraft in the existing market adopts ordinary battery mostly, by the battery, power cord and power plug constitute, the colour that relies on the LED lamp that flies on the accuse when using changes, just know whether have the electricity, and when non-operating condition, can only detect the electric quantity through the electric quantity detector, the electric quantity shows the inaccuracy, the user is also very inconvenient when using, it is unfavorable to the maintenance of battery, and if when the aircraft flies, it can lead to the aircraft to explode to dredge the observation, thereby lead to serious consequence, in addition in the in-service use process, if the control unit still controls intelligent battery for the power supply of external load when external load takes place the short circuit trouble, then can lead to intelligent battery to take place the short circuit, damage intelligent battery, cause the conflagration to propose an intelligent flight battery to above phenomenon even.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an intelligence flight battery to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an intelligence flight battery, includes unmanned aerial vehicle body, battery body, BMS battery management system unit, collection module, BMS battery management system, power module, control module, display module, wireless communication module, group battery inner core, battery switch unit, load detection module and display screen, in the unmanned aerial vehicle body the battery body is inside including BMS battery management system unit, BMS battery management system unit is including collection module, BMS battery management system, power module and control module, collection module's output is connected to BMS battery management system's input, BMS battery management system output is connected to power module with control module, control module's output is connected to the group battery inner core, the group battery inner core passes through battery switch unit is connected to on the input of load detection module, the output of load detection module is connected to on the unmanned aerial vehicle body, there is switch on one side of the top of unmanned aerial vehicle body through screw fixed mounting, lie in on the unmanned aerial vehicle body one side of switch is provided with time display screen.

Further, be located on the unmanned aerial vehicle body top one side of time display screen has the electric quantity display screen through screw fixed mounting, be located on the unmanned aerial vehicle body top one side of electric quantity display screen is provided with the electric quantity pilot lamp.

Furthermore, the output end of the acquisition module is connected to the display module, and the display module is connected with the time display screen, the electric quantity display screen and the electric quantity indicator lamp.

Further, an output terminal of the BMS battery management system is connected to an input terminal of the wireless communication module.

Furthermore, the output end of the power supply module is connected to the load detection module through the battery switch unit, and the battery switch unit is connected to the power switch.

Further, the inside of unmanned aerial vehicle body is including NFC read-write module, data transmission module and flight control module.

Further, the control module is connected to the unmanned aerial vehicle body through the load detection module.

Compared with the prior art, the utility model discloses following beneficial effect has: detect the short circuit state of external load when the start through the unmanned aerial vehicle body, and control intelligent battery and stop supplying power when external load short circuit, thereby prevent that the group battery inner core that external load short circuit arouses from damaging, effectively protect the battery, calculate the duration of a journey time of battery in the ware through the time display screen, and the battery is charged and is full of required time, user's observation more facilitates the use, power display screen and power indicator are the percentage display window of current residual capacity, can accurately show residual capacity, realize intelligent flight, moreover, the steam generator is simple in structure and stable, reasonable in design is ingenious, and high practical value.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.

Fig. 1 is a schematic diagram of a structure of an intelligent flying battery in accordance with an embodiment of the present invention;

fig. 2 is a schematic diagram of a battery body structure of an intelligent flying battery according to the present invention;

reference numerals:

1. an unmanned aerial vehicle body; 2. a battery body; 3. a BMS battery management system unit; 4. an acquisition module; 5. a BMS battery management system; 6. a power supply module; 7. a control module; 8. a display module; 9. a wireless communication module; 10. a battery pack inner core; 11. a battery switch unit; 12. a load detection module; 13. a time display screen; 14. a power switch; 15. an electric quantity display screen; 16. an electric quantity indicator light; 17. an NFC read-write module; 18. a data transmission module; 19. and a flight control module.

Detailed Description

The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, rather than all embodiments, and all other embodiments obtained by a person of ordinary skill in the art without creative work belong to the protection scope of the present invention based on the embodiments of the present invention.

In the description of the present invention, it should be noted that the terms "top", "bottom", "one side", "the other side", "front", "back", "middle part", "inside", "top", "bottom", etc. indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, which is only for the convenience of description and simplification of the description, but does not indicate or imply that the device or element referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance; furthermore, unless expressly stated or limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, as they may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Please refer to fig. 1-2, according to the utility model discloses an intelligent flight battery, including unmanned aerial vehicle body 1, battery body 2, BMS battery management system unit 3, collection module 4, BMS battery management system 5, power module 6, control module 7, display module 8, wireless communication module 9, group battery inner core 10, battery switch unit 11, load detection module 12 and time display screen 13, battery body 2 in unmanned aerial vehicle body 1 is inside including BMS battery management system 5 unit 3, BMS battery management system 5 unit 3 is including collection module 4, BMS battery management system 5, power module 6 and control module 7, collection module 4's output is connected to BMS battery management system 5's input, BMS battery management system 5 output is connected to power module 6 and control module 7, control module 7's output is connected to group battery inner core 10, group battery inner core 10 is connected to the input of load detection module 12 through battery switch unit 11, the output of load detection module 12 is connected to unmanned aerial vehicle body 1, there is a switch 14 top one side of unmanned aerial vehicle body 1 through screw fixed mounting, one side of group battery inner core 10 is provided with unmanned aerial vehicle switch 13 and shows that the time display screen.

Wherein, there is power display screen 15 at the top one side that lies in time display screen 13 on unmanned aerial vehicle body 1 through screw fixed mounting, and the top one side that lies in power display screen 15 on unmanned aerial vehicle body 1 is provided with power indicator 16, realizes the demonstration to unmanned aerial vehicle body 1.

Wherein, collection module 4's output is connected to display module 8 on, and display module 8 is connected with time display screen 13, electric quantity display screen 15 and electric quantity pilot lamp 16, realizes the demonstration to battery body 2.

Wherein, the output end of the BMS battery management system 5 is connected to the input end of the wireless communication module 9, realizing remote control.

The output end of the power supply module 6 is connected to the load detection module 12 through the battery switch unit 11, and the battery switch unit 11 is connected to the power switch 14, so as to implement operation control.

Wherein, the inside of unmanned aerial vehicle body 1 is including NFC read-write module 17, data transmission module 18 and flight control module 19, realizes unmanned aerial vehicle body 1's steady operation.

Wherein, control module 7 is connected to unmanned aerial vehicle body 1, stable in structure through load detection module 12.

Principle of operation

Through the above technical scheme of the utility model, an intelligence flight battery detects external load's short-circuit condition when the start through the unmanned aerial vehicle body when using, and control intelligent battery stop power supply when external load short circuit, thereby prevent that the group battery inner core that the external load short circuit arouses from damaging, effectively protect the battery, calculate the time of endurance of battery in the line ware through time display screen, and battery charging is full of required time, more person of facilitating the use's observation, battery indicator screen and quantity indicator are current residual capacity's percentage display window, can accurate display residual capacity, realize intelligent flight, moreover, the steam generator is simple in structure and stable, and reasonable in design is ingenious, and high practical value.

It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.

Claims

1. An intelligent flying battery, comprising an unmanned aerial vehicle body (1), a battery body (2), a BMS battery management system unit (3), a collection module (4), a BMS battery management system (5), a power supply module (6), a control module (7), a display module (8), a wireless communication module (9), a battery pack inner core (10), a battery switch unit (11), a load detection module (12) and a time display screen (13), characterized in that the BMS battery management system (5) unit (3) is included inside the battery body (2) in the unmanned aerial vehicle body (1), the BMS battery management system (5) unit (3) includes a collection module (4), a BMS battery management system (5), a power supply module (6) and a control module (7), the output end of the collection module (4) is connected to the input end of the BMS battery management system (5), the output end of the BMS battery management system (5) is connected to the power supply module (6) and the control module (7), the output end of the control module (7) is connected to the battery pack inner core (10), the battery pack inner core (10) is connected to the input end of the battery pack inner core (11) through the battery switch unit (12), the output of load detection module (12) is connected to on the unmanned aerial vehicle body (1), there is switch (14) top one side of unmanned aerial vehicle body (1) through screw fixed mounting, lie in on the unmanned aerial vehicle body (1) one side of switch (14) is provided with time display screen (13).

2. The intelligent flying battery of claim 1, wherein the unmanned aerial vehicle body (1) is provided with a power display screen (15) at one side of the top of the time display screen (13) through a screw, and the unmanned aerial vehicle body (1) is provided with a power indicator (16) at one side of the top of the power display screen (15).

3. An intelligent flight battery as claimed in claim 1, wherein the output end of the acquisition module (4) is connected to the display module (8), and the display module (8) is connected to the time display screen (13), the electric quantity display screen (15) and the electric quantity indicator lamp (16).

4. An intelligent flying battery as defined in claim 1, wherein the output of the BMS battery management system (5) is connected to the input of the wireless communication module (9).

5. An intelligent flying battery as claimed in claim 1, wherein the output of the power supply module (6) is connected to the load detection module (12) through the battery switch unit (11), and the battery switch unit (11) is connected to the power switch (14).

6. The intelligent flying battery of claim 1, wherein the inside of the unmanned aerial vehicle body (1) comprises an NFC read-write module (17), a data transmission module (18) and a flying control module (19).

7. A smart flight battery as claimed in claim 1, wherein the control module (7) is connected to the drone body (1) by the load detection module (12).