[go: up one dir, main page]

CN113795970A - Batteries & Drones - Google Patents

Batteries & Drones Download PDF

Info

Publication number
CN113795970A
CN113795970A CN202080030882.XA CN202080030882A CN113795970A CN 113795970 A CN113795970 A CN 113795970A CN 202080030882 A CN202080030882 A CN 202080030882A CN 113795970 A CN113795970 A CN 113795970A
Authority
CN
China
Prior art keywords
battery
air
channel
casing
air duct
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.)
Pending
Application number
CN202080030882.XA
Other languages
Chinese (zh)
Inventor
张瑞强
黄彦鑫
李日照
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.)
SZ DJI Technology Co Ltd
Original Assignee
SZ DJI Technology 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 SZ DJI Technology Co Ltd filed Critical SZ DJI Technology Co Ltd
Publication of CN113795970A publication Critical patent/CN113795970A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
    • H01M50/249—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders specially adapted for aircraft or vehicles, e.g. cars or trains
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B64C27/14—Direct drive between power plant and rotor hub
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00—Secondary cells; Manufacture thereof
    • H01M10/42—Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
    • H01M10/48—Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00—Secondary cells; Manufacture thereof
    • H01M10/42—Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
    • H01M10/48—Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
    • H01M10/486—Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte for measuring temperature
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00—Secondary cells; Manufacture thereof
    • H01M10/60—Heating or cooling; Temperature control
    • H01M10/61—Types of temperature control
    • H01M10/613—Cooling or keeping cold
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00—Secondary cells; Manufacture thereof
    • H01M10/60—Heating or cooling; Temperature control
    • H01M10/62—Heating or cooling; Temperature control specially adapted for specific applications
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00—Secondary cells; Manufacture thereof
    • H01M10/60—Heating or cooling; Temperature control
    • H01M10/65—Means for temperature control structurally associated with the cells
    • H01M10/655—Solid structures for heat exchange or heat conduction
    • H01M10/6556—Solid parts with flow channel passages or pipes for heat exchange
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00—Secondary cells; Manufacture thereof
    • H01M10/60—Heating or cooling; Temperature control
    • H01M10/65—Means for temperature control structurally associated with the cells
    • H01M10/656—Means for temperature control structurally associated with the cells characterised by the type of heat-exchange fluid
    • H01M10/6561—Gases
    • H01M10/6563—Gases with forced flow, e.g. by blowers
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00—Secondary cells; Manufacture thereof
    • H01M10/60—Heating or cooling; Temperature control
    • H01M10/65—Means for temperature control structurally associated with the cells
    • H01M10/656—Means for temperature control structurally associated with the cells characterised by the type of heat-exchange fluid
    • H01M10/6561—Gases
    • H01M10/6566—Means within the gas flow to guide the flow around one or more cells, e.g. manifolds, baffles or other barriers
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/10—Primary casings; Jackets or wrappings
    • H01M50/147—Lids or covers
    • H01M50/148—Lids or covers characterised by their shape
    • H01M50/152—Lids or covers characterised by their shape for cells having curved cross-section, e.g. round or elliptic
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
    • H01M50/204—Racks, modules or packs for multiple batteries or multiple cells
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
    • H01M50/233—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by physical properties of casings or racks, e.g. dimensions
    • H01M50/24—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by physical properties of casings or racks, e.g. dimensions adapted for protecting batteries from their environment, e.g. from corrosion
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
    • H01M50/289—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by spacing elements or positioning means within frames, racks or packs
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/30—Arrangements for facilitating escape of gases
    • H01M50/35—Gas exhaust passages comprising elongated, tortuous or labyrinth-shaped exhaust passages
    • H01M50/367—Internal gas exhaust passages forming part of the battery cover or case; Double cover vent systems
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10—Energy storage using batteries
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Battery Mounting, Suspending (AREA)
  • Secondary Cells (AREA)

Abstract

一种电池及无人机，该电池包括壳体(1)、电芯(2)、以及盖体(3)，电芯(2)与壳体(1)之间形成有散热风道(11)，盖体(3)上设有与散热风道(11)连通的入风口(31)和出风口(32)；盖体(3)内设有第一气流通道(33)，第一气流通道(33)弯曲设置并连通入风口(31)和散热风道(11)；和/或，所述盖体(3)内设有第二气流通道(35)，所述第二气流通道(35)弯曲设置并连通所述出风口(32)和所述散热风道(11)。电池内形成与外界连通的散热风道，可以降低电池的工作温度，提高电池的工作效率，提高电池的性能及寿命。此外，通过第一气流通道和第二气流通道弯曲设置还可以为电池起到防水的作用。

Figure 202080030882

A battery and an unmanned aerial vehicle, the battery comprises a casing (1), an electric core (2), and a cover (3), and a cooling air duct (11) is formed between the electric core (2) and the casing (1). ), the cover body (3) is provided with an air inlet (31) and an air outlet (32) communicating with the cooling air duct (11); The channel (33) is bent and connected to the air inlet (31) and the cooling air duct (11); and/or, the cover body (3) is provided with a second airflow channel (35), and the second airflow channel ( 35) The air outlet (32) and the cooling air duct (11) are bent and connected to each other. A heat dissipation air duct connected to the outside is formed in the battery, which can reduce the working temperature of the battery, improve the working efficiency of the battery, and improve the performance and life of the battery. In addition, the curved arrangement of the first airflow channel and the second airflow channel can also play a waterproof role for the battery.

Figure 202080030882

Description

Battery and unmanned aerial vehicle
Technical Field
The application relates to a battery and an unmanned aerial vehicle.
Background
With the shortage of traditional fossil energy, new energy vehicles and other mobile devices represented by electric energy are increasingly favored due to their energy-saving and environmental-friendly properties. The battery is used as one of the core components of the new energy mobile device and provides power energy for the mobile device. The operating state of the battery directly affects the operating conditions of the mobile device. Among them, an important factor affecting the operational performance of the battery is the temperature of the battery. During operation of the battery, the battery generates a large amount of heat during high-rate discharge, which leads to rapid temperature rise of the battery itself and the surrounding environment. The high temperature environment will reduce battery work efficiency, influence battery power output even burn out the battery.
Disclosure of Invention
The application discloses battery and unmanned aerial vehicle to solve the high technical problem who influences battery working property of battery temperature.
According to an aspect of an embodiment of the present application, there is provided a battery, including a casing, a battery cell accommodated in the casing, and a cover covering the casing, wherein a heat dissipation air duct is formed between the battery cell and the casing, and an air inlet and an air outlet communicated with the heat dissipation air duct are provided on the cover;
a first air flow channel is arranged in the cover body, and the first air flow channel is arranged in a bent mode and is communicated with the air inlet and the heat dissipation air channel; and/or the presence of a gas in the gas,
and a second air flow channel is arranged in the cover body, and the second air flow channel is arranged in a bent manner and is communicated with the air outlet and the heat dissipation air duct.
According to two aspects of this application embodiment, this application provides an unmanned aerial vehicle, includes:
a frame including a central body and a plurality of arms coupled to the central body;
a plurality of rotor devices respectively mounted on the plurality of horn; each rotor wing device comprises a motor and a propeller arranged on the motor; and
the battery is arranged on the central body and comprises a shell, an electric core accommodated in the shell and a cover body covering the shell, a heat dissipation air channel is formed between the electric core and the shell, and an air inlet and an air outlet which are communicated with the heat dissipation air channel are formed in the cover body;
a first air flow channel is arranged in the cover body, and the first air flow channel is arranged in a bent mode and is communicated with the air inlet and the heat dissipation air channel; and/or the presence of a gas in the gas,
a second air flow channel is arranged in the cover body, and the second air flow channel is arranged in a bent mode and is communicated with the air outlet and the heat dissipation air duct;
the battery is located in the middle of a surrounding area of the rotor wing devices, and airflow generated by the rotor wing devices can enter from an air inlet of the battery and flow out from an air outlet of the battery.
The technical scheme provided by the embodiment of the application can have the following beneficial effects:
a heat dissipation air channel is formed between the battery core and the shell of the battery, a first air channel and a second air channel are arranged in the cover body, the first air channel is arranged in a bent mode and communicated with the air port and the heat dissipation air channel, the second air channel is arranged in a bent mode and communicated with the air outlet and the heat dissipation air channel, so that the heat dissipation air channel communicated with the outside is formed in the battery, heat in the battery is taken away through the battery core flowing through air flow, the working temperature of the battery is reduced, the working efficiency of the battery is improved, and the performance and the service life of the battery are improved. In addition, the first air flow channel and the second air flow channel are bent to play a role of water resistance for the battery.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings needed to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present application, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without inventive labor.
FIG. 1 is a schematic diagram illustrating an angular configuration of a battery according to an exemplary embodiment of the present application;
FIG. 2 is a schematic view of another angular configuration of a battery shown in an exemplary embodiment of the present application;
FIG. 3 is an exploded view of a battery shown in an exemplary embodiment of the present application;
FIG. 4 is a schematic cross-sectional view of a battery shown in an exemplary embodiment of the present application;
FIG. 5 is an angular cross-sectional schematic view of a battery shown in an exemplary embodiment of the present application;
FIG. 6 is a schematic top cross-sectional view of a battery shown in an exemplary embodiment of the present application;
fig. 7 is a cross-sectional schematic view of a housing and cell portion of a battery shown in an exemplary embodiment of the present application;
FIG. 8 is a schematic diagram of a housing of a battery according to an exemplary embodiment of the present application;
fig. 9 is a schematic structural diagram of a drone according to an exemplary embodiment of the present application;
fig. 10 is a top view of a drone according to an exemplary embodiment of the present application.
Detailed Description
The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only a part of the embodiments of the present application, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.
The present application will be described in detail below with reference to the accompanying drawings. The features of the following examples and embodiments may be combined with each other without conflict.
Referring to fig. 1 to 4, fig. 1 is a schematic view illustrating an angular structure of a battery according to an exemplary embodiment of the present disclosure; FIG. 2 is a schematic view of another angular configuration of a battery shown in an exemplary embodiment of the present application; FIG. 3 is an exploded view of a battery shown in an exemplary embodiment of the present application; fig. 4 is an angular cross-sectional schematic view of a battery shown in an exemplary embodiment of the present application. The battery 10 of the embodiment of the present application includes a case 1, a battery cell 2 accommodated in the case 1, and a cover 3 covering the case 1.
A heat dissipation air duct 11 is formed between the battery cell 2 and the casing 1, and the cover 3 is provided with an air inlet 31 and an air outlet 32 which are communicated with the heat dissipation air duct 11, so that air flows into the battery 10 from the air inlet 31 and flows to the air outlet 32 through the heat dissipation air duct 11, and heat in the battery 10 is taken out, thereby achieving heat dissipation of the battery 10. In addition, because the heat dissipation air duct 11 can dissipate heat for the battery 10 during use, the battery 10 can be charged after the battery 10 is stopped, and the battery 10 does not need to be cooled to the charge cutoff temperature.
In some embodiments, a first air flow channel 33 is formed in the cover 3, and the first air flow channel 33 is bent and connected to the air inlet 31 and the heat dissipation air duct 11. In other embodiments, a second air flow channel 35 is disposed in the cover 3, and the second air flow channel 35 is disposed in a bent manner and communicates with the air outlet 32 and the heat dissipation air duct 11. In the embodiment of the present application, the first air flow channel 33 is disposed in a bent manner and communicates with the air inlet 31 and the heat dissipation air duct 11, and the second air flow channel 35 is disposed in a bent manner and communicates with the air outlet 32 and the heat dissipation air duct 11, so that the first air flow channel 33 and the second air flow channel 35 are both disposed in a bent manner, thereby effectively preventing water from entering the battery 10.
As shown in fig. 1 to 6, the cover 3 is a box structure and is mounted on the top of the housing 1. The battery 10 of the present application further includes a control circuit board 363 disposed in the cover 3, where the control circuit board 363 is configured to manage and control the battery cell 2 of the battery 10 to perform charging and discharging. In some embodiments, the battery cell 2 is pre-assembled in the casing 1, and the control circuit board 363 is electrically connected to the battery cell 2 when the cover 3 covers the casing 1. In other embodiments, the battery cell 2 may also be pre-assembled on the cover 3 and electrically connected to the control circuit board 363, and then assembled in the housing 1.
Wherein, the cover 3 is provided with an air inlet 31 and an air outlet 32 towards one side of the casing 1. Since the cover 3 is installed on the top of the casing 1, and the air inlet 31 and the air outlet 32 are disposed on one side of the cover 3 facing the casing 1, that is, one side of the cover 3 facing the casing 1 is the lower side of the cover 3, both the air inlet 31 and the air outlet 32 face downward, so that water is not easy to flow into the cover 3. In the embodiment of the present application, the air inlet 31 and the air outlet 32 are disposed on one side of the cover 3 facing the housing 1, and the first airflow channel 33 and the second airflow channel 35 are disposed in a curved manner, so as to satisfy the condition that the battery 10 has a heat dissipation channel, and further play a role in waterproofing, thereby preventing water from entering the heat dissipation channel of the battery 10.
In some embodiments, as shown in fig. 3 to 8, the housing 1 has an opening, and a side of the cover 3 facing the housing 1 includes a covering surface 361 and a non-covering surface 362. The covering surface 361 covers the opening, and the air inlet 31 and the air outlet 32 are disposed on the non-covering surface 362. In this embodiment, the non-covering surface 362 is located at the periphery of the covering surface 361, and the air inlet 31 and the air outlet 32 are respectively disposed at two opposite sides of the housing 1. The air inlet 31 is a long strip-shaped opening in the longitudinal direction of the housing 1.
In some embodiments, as shown in fig. 3 and 4, the cover 3 includes an upper cover portion 37 and a lower cover portion 36 disposed opposite the upper cover portion 37. The control circuit board 363 is located in the accommodating space formed by the upper cover portion 37 and the lower cover portion 36, and the air inlet 31 and the air outlet 32 are opened in the lower cover portion 36. The upper cover portion 37 is provided with operation keys for controlling the battery 10, and functions of the operation keys include at least one of: the power switch controls and displays the residual capacity and the current temperature of the battery 10.
Further, as shown in fig. 3 to 6, a holding portion 34 is disposed on the cover 3, and the holding portion 34 is used for assisting a user to insert and remove the battery 10. In some embodiments, the gripping portion 34 is a gripping handle disposed on the cover 3, and the gripping handle is located on the non-covering surface 362 of the cover 3. The holding handle extends outward from one side of the cover 3 in the longitudinal direction, and the holding portion 34 includes a holding hole 341, and the holding hole 341 penetrates through the upper cover portion 37 and the lower cover portion 36 of the cover 3.
In this embodiment, the number of the air inlets 31 is two, and the two air inlets 31 are respectively disposed on two sides of the holding portion 34 in the length direction of the housing 1, that is, the two air inlets 31 are disposed on two sides of the holding hole 341. Two air inlets 31 are arranged on the cover body 3, so that the air inlet amount can be increased, and the heat dissipation efficiency is improved. In addition, the air inlets 31 are arranged on both sides of the holding portion 34 in the longitudinal direction of the housing 1, so that the space on the cover 3 can be effectively utilized by arranging the air inlets 31, and additional occupied space is not needed. Of course, in other embodiments, the air outlet 32 may be disposed beside the holding portion 34.
As shown in fig. 1 to 8, the first air flow channel 33 includes a first channel 331 and at least one second channel 332. The second passage 332 is communicated between the air inlet 31 and the first passage 331, and the first passage 331 is communicated with the heat dissipation air duct 11. The second channel 332 is used for guiding the airflow from the air inlet 31 to the first channel 331 and flowing from the first channel 331 to the heat dissipation duct 11. Wherein, the extending direction of the first channel 331 is parallel to the length direction of the housing 1. In this embodiment, the air inlet 31 and the air outlet 32 are respectively disposed on two opposite sides of the casing 1 in the width direction, so that the heat dissipation air duct 11 can cover the region of the battery cell 2 in the length direction of the casing 1, the overall size of the heat dissipation air duct 11 is increased, and the heat dissipation efficiency of the battery 10 can be improved.
In some embodiments, the second passages 332 include at least two, and at least two of the second passages 332 extend divergently toward the first passage 331. The second passage 332 includes a guide cavity having a trumpet shape, and the guide cavity communicates with the first passage 331 to guide the airflow flowing in from the air inlet 31 into the first passage 331. In the illustration of the application, the number of the second channels 332 is two, and the two second channels 332 extend in a trumpet shape to the first channel 331, so that the airflow can dispersedly flow into the first channel 331, and thus the airflow flowing into the first channel 331 can be relatively uniformly distributed, and further the airflow relatively uniformly flows into the heat dissipation air duct 11, which is beneficial to performing overall heat dissipation on the battery cell 2. In other embodiments, the second passage 332 may be plural, and the plural second passages 332 may be dispersed uniformly and extend toward the first passage 331.
The cross section of the first air flow channel 33 in the air flow direction is n-shaped, and the structural arrangement can effectively prevent water from entering. When the first air flow path 33 includes at least two second paths 332, each of the second paths 332 and the first path 331 has an n-shaped cross section in the air flow direction.
Referring to fig. 1 to 8 again, the casing 1 of the present application includes a bottom wall 12 and a side wall 13 enclosing a cavity in cooperation with the bottom wall 12, where the cavity is used to accommodate the battery cell 2. The side wall 13 and/or the bottom wall 12 are provided with a first matching portion 14, the battery cell 2 is provided with a second matching portion 21 matched with the first matching portion 14, and the battery cell 2 is mounted in the casing 1 through the assembly of the first matching portion 14 and the second matching portion 21. In some embodiments, the first matching portion 14 is a rib disposed on the casing 1, and the second matching portion 21 is a groove disposed on the battery cell 2. In other embodiments, the first matching portion 14 is a groove disposed on the casing 1, and the second matching portion 21 is a rib disposed on the battery cell 2. In the drawings of the present application, the first matching portion 14 is a rib disposed on the casing 1, and the second matching portion 21 is a groove disposed on the battery cell 2. Wherein the protruding height range of the ribs is 4mm-5 mm.
In some embodiments, at least one pair of opposing side walls 13 and bottom wall 12 are each provided with a first mating portion 14, and the first mating portion 14 on the bottom wall 12 is engaged with the first mating portion 14 on at least one pair of opposing side walls 13. When the battery cell 2 is installed in the casing 1, a gap is formed between the battery cell and the side wall 13 and the bottom wall 12 provided with the first matching portion 14, and the gap forms at least two spaced heat dissipation sub-air channels 110. In this embodiment, after the first matching portions 14 on the opposite side walls 13 and the bottom wall 12 are matched and assembled with the second matching portion 21 of the battery cell 2, the heat dissipation air duct 11 is divided into two spaced heat dissipation sub-air ducts 110.
In other embodiments, at least one pair of opposite side walls 13 and bottom wall 12 are respectively provided with a plurality of spaced first matching portions 14, and the battery cell 2 is provided with second matching portions 21 corresponding to the first matching portions 14 one to one. A plurality of first matching parts 14 are respectively arranged on the opposite side wall 13 and the bottom wall 12, and the first matching parts 14 are respectively matched and assembled with the second matching part 21 on the electric core 2 to divide the heat dissipation air duct 11 in the casing 1 into a plurality of heat dissipation sub-air ducts 110 with smaller size. Through setting up a plurality of heat dissipation sub-wind channels 110, can effectively guide the air current to flow along heat dissipation sub-wind channel 110 fast, avoid leading to the air current to cross talk because of heat dissipation wind channel 11 is too big to influence the outflow speed of air current.
In the embodiments, the heat-dissipating sub-air duct 110 is "U" -shaped, that is, the heat-dissipating sub-air duct 110 is divided into a plurality of smaller heat-dissipating sub-air ducts 110. Each of the sub-air channels 110 is respectively connected to the first air channel 33 and the second air channel 35, so that each of the sub-air channels 11 can independently dissipate heat.
Further, in order to accelerate the heat dissipation efficiency of the electrical core 2, heat dissipation fins are disposed on the electrical core 2 and located in the heat dissipation air duct 11. In addition, in order to further ensure the safety of the battery 10, the surface of the battery cell 2 is provided with a waterproof layer, thereby further improving the waterproof property of the battery 10.
In some embodiments, the heat dissipation air duct 11 includes a first air duct 111 and a second air duct 112 respectively formed between the two opposite side walls 13 and the battery cells 2, and a third air duct 113 formed between the bottom wall 12 and the battery cells 2. The first air duct 111 and the second air duct 112 are respectively communicated with the third air duct 113, the first air flow passage 33 is communicated with the first air duct 111, and the second air flow passage 35 is communicated with the second air duct 112. The whole radiating air duct is in a U shape, and the three air ducts can radiate heat for three sides of the battery 10. The first air duct 111 and the second air duct 112 are located on two sides of the electric core 2 in the length direction of the casing 1, and the third air duct 113 is located on the bottom surface of the electric core 2 in the length direction of the casing 1, so that the total area of the heat dissipation air duct 11 is maximized, which is beneficial to dissipating heat for the electric core 2 and improving the heat dissipation efficiency of the battery 10.
With reference to the above embodiment, when the first matching portions 14 and the second matching portions 21 on the electric core 2 are respectively matched and assembled to separate the heat dissipation air duct 11 in the casing 1 into a plurality of heat dissipation sub-air ducts 110 with small sizes, a plurality of first air ducts 111 and a plurality of second air ducts 112 are respectively formed between the two opposite side walls 13 and the electric core 2, and a plurality of third air ducts 113 are formed between the bottom wall 12 and the electric core 2, so as to divide the U-shaped heat dissipation air duct 11 into a plurality of heat dissipation sub-air ducts 110 arranged side by side.
In the opposite direction of the side wall 13 and the battery cell 2, the distance between the first air ducts 111 is 30mm to 40 mm. The distance between the second air ducts 112 in the opposite direction of the bottom wall 12 and the battery cell 2 is 30mm to 40 mm.
The heat dissipation air duct 11 is formed between the electric core 2 of the battery 10 and the shell 1 in the embodiment of the application, the first air flow channel 33 and the second air flow channel 35 are arranged in the cover body 3, the first air flow channel 33 is arranged in a bent mode and communicated with the air inlet 31 and the heat dissipation air duct 11, the second air flow channel 35 is arranged in a bent mode and communicated with the air outlet 32 and the heat dissipation air duct 11, so that the heat dissipation air duct 11 communicated with the outside is formed in the battery 10, heat in the battery 10 is taken away through the electric core 2 flowing through the air flow, the working temperature of the battery 10 is reduced, the working efficiency of the battery 10 is improved, and the performance and the service life of the battery 10 are improved. In addition, the bent arrangement of the first air flow channel 33 and the second air flow channel 35 also serves to prevent water from being applied to the battery 10.
As shown in fig. 9 and 10 in conjunction with fig. 1-8, in yet another aspect of an embodiment of the present application, there is also provided a drone 100, the drone 100 including a frame 20, a plurality of rotor devices 30, and a battery 10. This unmanned aerial vehicle 100 can be agricultural plant protection machine. The specific structure of the battery 10 is shown in the above embodiments, and will not be described herein. Of course, in other embodiments, the battery 10 may be applied to a new energy vehicle, a robot, and other mobile devices.
The rack 20 includes a hub 201 and a plurality of arms 202 coupled to the hub 201. The plurality of rotor apparatuses 30 are mounted on the plurality of horn 202, respectively. Each rotor apparatus 30 includes a motor 301 and a propeller 302 mounted on the motor 301. The cell 10 is mounted on the central body 201.
At present, agricultural plant protection machines generally have large loading capacity, so when working, the working current is very large, and because the battery has certain internal resistance, the agricultural plant protection machines can generate very high heat when working under the working condition of large current. When the battery temperature is high, the performance of the battery itself is degraded, and the battery life is affected by operating at a high temperature for a long time. And in actual operation, if the battery temperature is higher, the charger can not charge the battery.
Based on the above background, the heat dissipation air duct 11 is provided in the battery 10 of the present application, and the air inlet 31 and the air outlet 32 of the battery 10 are disposed downward, and the air flow generated by the plurality of rotor devices 30 can enter from the air inlet 31 of the battery 10 and flow out from the air outlet 32 of the battery 10, so as to dissipate heat for the battery 10. Meanwhile, the arrangement of the air inlet 31 and the air outlet 32 of the battery 10 facing downwards is beneficial to the waterproof arrangement of the battery 10. Furthermore, a first air flow channel 33 and a second air flow channel 35 are arranged in the cover 3, the first air flow channel 33 is bent and communicated with the air opening 31 and the heat dissipation air duct 11, the second air flow channel 35 is bent and communicated with the air outlet 32 and the heat dissipation air duct 11, and the first air flow channel 33 and the second air flow channel 35 are bent and communicated to achieve a waterproof effect for the battery 10.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. The terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
The method and apparatus provided by the embodiments of the present application are described in detail above, and the principle and the embodiments of the present application are explained herein by applying specific examples, and the description of the embodiments above is only used to help understand the method and the core idea of the present application; meanwhile, for a person skilled in the art, according to the idea of the present application, there may be variations in the specific embodiments and the application scope, and in summary, the content of the present specification should not be construed as a limitation to the present application.

Claims (44)

1.一种电池，其特征在于，包括壳体、收容于所述壳体内的电芯、以及盖于所述壳体的盖体，所述电芯与所述壳体之间形成有散热风道，所述盖体上设有与所述散热风道连通的入风口和出风口；1. A battery, characterized in that it comprises a casing, an electric core accommodated in the casing, and a cover body covering the casing, and a cooling air is formed between the electric core and the casing The cover body is provided with an air inlet and an air outlet communicating with the cooling air duct; 所述盖体内设有第一气流通道，所述第一气流通道弯曲设置并连通所述入风口和所述散热风道；和/或，The cover body is provided with a first air flow channel, the first air flow channel is bent and connected to the air inlet and the heat dissipation air channel; and/or, 所述盖体内设有第二气流通道，所述第二气流通道弯曲设置并连通所述出风口和所述散热风道。The cover body is provided with a second air flow channel, and the second air flow channel is bent and connected to the air outlet and the heat dissipation air channel. 2.根据权利要求1所述的电池，其特征在于，所述盖体朝所述壳体的一侧面设置所述入风口和所述出风口。2 . The battery according to claim 1 , wherein the cover body is provided with the air inlet and the air outlet on a side surface of the casing. 3 . 3.根据权利要求2所述的电池，其特征在于，所述壳体具有开口，所述盖体朝向所述壳体的一侧包括遮盖面和非遮盖面，所述遮盖面遮盖所述开口，所述入风口和所述出风口设置在所述非遮盖面。3 . The battery according to claim 2 , wherein the casing has an opening, a side of the cover facing the casing includes a covering surface and a non-covering surface, and the covering surface covers the opening. 4 . , the air inlet and the air outlet are arranged on the non-covered surface. 4.根据权利要求2所述的电池，其特征在于，所述盖体包括上盖部以及与所述上盖部相对设置的下盖部，所述入风口和所述出风口开设在所述下盖部，所述上盖部设有用于控制所述电池的操作按键，所述操作按键的功能包括如下至少一种：电源开关、控制显示剩余电量、控制显示当前电池温度。4 . The battery according to claim 2 , wherein the cover body comprises an upper cover part and a lower cover part opposite to the upper cover part, and the air inlet and the air outlet are opened in the The lower cover is provided with operation buttons for controlling the battery, and the functions of the operation buttons include at least one of the following: power switch, control and display of remaining power, and control and display of current battery temperature. 5.根据权利要求1所述的电池，其特征在于，所述盖体为盒体结构，且安装在所述壳体的顶部；所述电池还包括设置于所述盖体内的控制电路板，所述控制电路板用于管理和控制所述电池的电芯进行充放电。5 . The battery according to claim 1 , wherein the cover is a box structure and is installed on the top of the casing; the battery further comprises a control circuit board arranged in the cover, 6 . The control circuit board is used to manage and control the charging and discharging of the cells of the battery. 6.根据权利要求1所述的电池，其特征在于，所述第一气流通道包括第一通道、以及至少一个第二通道；其中，所述第二通道连通在所述入风口与所述第一通道之间，所述第一通道与所述散热风道连通。6 . The battery according to claim 1 , wherein the first airflow channel comprises a first channel and at least one second channel; wherein the second channel communicates with the air inlet and the first channel. 7 . Between a channel, the first channel communicates with the cooling air duct. 7.根据权利要求6所述的电池，其特征在于，所述第一通道的延伸方向平行于所述壳体的长度方向。7 . The battery of claim 6 , wherein the extending direction of the first channel is parallel to the length direction of the casing. 8 . 8.根据权利要求6所述的电池，其特征在于，所述第二通道包括至少两个，至少两个所述第二通道分散延伸向所述第一通道。8 . The battery of claim 6 , wherein the second channel comprises at least two, and at least two of the second channels are dispersed and extend toward the first channel. 9 . 9.根据权利要求6所述的电池，其特征在于，所述第二通道包括喇叭状的导向腔，所述导向腔连通所述第一通道，以将从所述入风口流入的气流导入所述第一通道。9 . The battery according to claim 6 , wherein the second channel comprises a trumpet-shaped guide cavity, and the guide cavity communicates with the first channel, so as to guide the air flow from the air inlet into the air inlet. 10 . the first channel. 10.根据权利要求1所述的电池，其特征在于，所述第一气流通道在气流方向上的截面呈n型。10 . The battery according to claim 1 , wherein the cross section of the first airflow channel in the airflow direction is n-type. 11 . 11.根据权利要求1所述的电池，其特征在于，所述盖体上设有握持部，所述入风口包括两个，两个所述入风口分设于所述握持部在所述壳体长度方向上的两侧。11 . The battery according to claim 1 , wherein a gripping portion is provided on the cover body, the air inlets include two, and the two air inlets are respectively arranged on the gripping portion at the side of the gripping portion. 12 . Both sides in the length direction of the shell. 12.根据权利要求1所述的电池，其特征在于，所述壳体包括底壁以及与所述底壁配合围合成腔体的侧壁，所述腔体用以收容所述电芯，所述侧壁和/或所述底壁设有第一配合部，所述电芯上设有与所述第一配合部适配的第二配合部，通过所述第一配合部与所述第二配合部的装配，以使所述电芯安装于所述壳体内。12 . The battery according to claim 1 , wherein the casing comprises a bottom wall and a side wall that cooperates with the bottom wall to form a cavity, and the cavity is used for accommodating the battery cells. 12 . The side wall and/or the bottom wall is provided with a first matching portion, and the battery core is provided with a second matching portion adapted to the first matching portion. The two mating parts are assembled, so that the electric core is installed in the casing. 13.根据权利要求12所述的电池，其特征在于，至少一对相对的所述侧壁和所述底壁分别设有所述第一配合部，位于所述底壁上的所述第一配合部与位于至少一对相对的所述侧壁上的第一配合部衔接。13 . The battery according to claim 12 , wherein at least one pair of the opposite side walls and the bottom wall are respectively provided with the first matching parts, and the first matching portion located on the bottom wall is 13 . The mating portion engages with the first mating portion located on at least one pair of opposite side walls. 14.根据权利要求13所述的电池，其特征在于，所述电芯安装在所述壳体内时，与设置有所述第一配合部的侧壁、底壁之间具有间隙，所述间隙形成至少两个间隔的散热子风道。14 . The battery according to claim 13 , wherein, when the battery cell is installed in the housing, there is a gap between the battery cell and the side wall and the bottom wall on which the first matching portion is provided, and the gap is 14 . At least two spaced apart heat sink air ducts are formed. 15.根据权利要求14所述的电池，其特征在于，至少一对相对的所述侧壁、所述底壁上分别设有多个间隔的所述第一配合部，所述电芯上设有与所述第一配合部一一对应的第二配合部。15 . The battery according to claim 14 , wherein at least one pair of opposite side walls and the bottom wall are respectively provided with a plurality of spaced first matching portions, and the battery core is provided with a plurality of first matching portions. 16 . There are second matching portions corresponding to the first matching portions one-to-one. 16.根据权利要求12所述的电池，其特征在于，所述第一配合部为设置于所述壳体上的筋条，所述第二配合部为设置于电芯上的凹槽；或者，16 . The battery according to claim 12 , wherein the first matching portion is a rib provided on the casing, and the second matching portion is a groove provided on the cell; or , 所述第一配合部为设置于所述壳体上的凹槽，所述第二配合部为设置于所述电芯上的筋条。The first matching portion is a groove arranged on the casing, and the second matching portion is a rib arranged on the battery core. 17.根据权利要求16所述的电池，其特征在于，所述筋条的凸起高度范围为4mm-5mm。17 . The battery according to claim 16 , wherein the height of the protrusion of the ribs ranges from 4 mm to 5 mm. 18 . 18.根据权利要求15所述的电池，其特征在于，所述散热子风道呈“U”型，每一个所述散热子风道分别与所述第一气流通道、所述第二气流通道连通。18 . The battery according to claim 15 , wherein the cooling sub-air ducts are in a “U” shape, and each of the cooling sub-air ducts is connected to the first airflow channel and the second airflow channel respectively. 19 . Connected. 19.根据权利要求1所述的电池，其特征在于，所述电芯上设有散热翅片。19. The battery according to claim 1, wherein heat dissipation fins are provided on the battery core. 20.根据权利要求12所述的电池，其特征在于，所述散热风道包括相对的两个侧壁与所述电芯之间分别构成的第一风道和第二风道、以及所述底壁与所述电芯之间构成的第三风道，所述第一风道和所述第二风道分别与所述第三风道连通，所述第一气流通道与所述第一风道连通，所述第二气流通道与所述第二风道连通。20 . The battery according to claim 12 , wherein the cooling air duct comprises a first air duct and a second air duct respectively formed between two opposite side walls and the battery cell, and the a third air duct formed between the bottom wall and the battery core, the first air duct and the second air duct are respectively communicated with the third air duct, and the first air duct is connected with the first air duct The air passage is in communication, and the second air passage is in communication with the second air passage. 21.根据权利要求20所述的电池，其特征在于，在侧壁与所述电芯的相对方向上，所述第一风道的间距为30mm-40mm；在所述底壁与所述电芯的相对方向上，所述第二风道的间距为30mm-40mm。21. The battery according to claim 20, characterized in that, in the opposite direction of the side wall and the battery core, the distance of the first air duct is 30mm-40mm; In the opposite direction of the core, the spacing of the second air ducts is 30mm-40mm. 22.根据权利要求1所述的电池，其特征在于，所述电芯的表面设有防水层。22. The battery according to claim 1, wherein a waterproof layer is provided on the surface of the battery core. 23.一种无人机，其特征在于，包括：23. An unmanned aerial vehicle, characterized in that, comprising: 机架，包括中心体以及与所述中心体连接的多个机臂；a frame, including a center body and a plurality of arms connected to the center body; 多个旋翼装置，分别安装在多个所述机臂上；每个所述旋翼装置包括电机以及安装在所述电机上的螺旋桨；以及a plurality of rotor devices, respectively mounted on a plurality of the arms; each of the rotor devices includes a motor and a propeller mounted on the motor; and 电池，安装于所述中心体上，所述电池包括壳体、收容于所述壳体内的电芯、以及盖于所述壳体的盖体，所述电芯与所述壳体之间形成有散热风道，所述盖体上设有与所述散热风道连通的入风口和出风口；a battery, mounted on the central body, the battery includes a casing, a battery cell accommodated in the casing, and a cover body covering the casing, and a battery is formed between the battery core and the casing There is a cooling air duct, and the cover body is provided with an air inlet and an air outlet communicating with the cooling air duct; 所述盖体内设有第一气流通道，所述第一气流通道弯曲设置并连通所述入风口和所述散热风道；和/或，The cover body is provided with a first airflow channel, and the first airflow channel is bent and connected to the air inlet and the cooling air channel; and/or, 所述盖体内设有第二气流通道，所述第二气流通道弯曲设置并连通所述出风口和所述散热风道；The cover body is provided with a second air flow channel, and the second air flow channel is bent and connected to the air outlet and the cooling air channel; 其中，所述电池位于多个所述旋翼装置围绕区域的中部，多个所述旋翼装置产生的气流能够从所述电池的入风口进入，从所述电池的出风口流出。Wherein, the battery is located in the middle of the area surrounded by the plurality of rotor devices, and the airflow generated by the plurality of rotor devices can enter from the air inlet of the battery and flow out from the air outlet of the battery. 24.根据权利要求23所述的无人机，其特征在于，所述盖体朝所述壳体的一侧面设置所述入风口和所述出风口。24. The drone according to claim 23, wherein the cover body is provided with the air inlet and the air outlet toward one side of the casing. 25.根据权利要求24所述的无人机，其特征在于，所述壳体具有开口，所述盖体朝向所述壳体的一侧包括遮盖面和非遮盖面，所述遮盖面遮盖所述开口，所述非遮盖面围合于所述遮盖面的外围，所述入风口和所述出风口设置在所述非遮盖面。25. The drone according to claim 24, wherein the casing has an opening, the side of the cover facing the casing comprises a covering surface and a non-covering surface, and the covering surface covers the The opening is formed, the non-covering surface is enclosed on the periphery of the covering surface, and the air inlet and the air outlet are arranged on the non-covering surface. 26.根据权利要求24所述的无人机，其特征在于，所述盖体包括上盖部以及与所述上盖部相对设置的下盖部，所述入风口和所述出风口开设在所述下盖部，所述上盖部设有用于控制所述电池的操作按键，所述操作按键的功能包括如下至少一种：电源开关、控制显示剩余电量、控制显示当前电池温度。26. The drone according to claim 24, wherein the cover body comprises an upper cover part and a lower cover part opposite to the upper cover part, and the air inlet and the air outlet are opened at The lower cover part and the upper cover part are provided with operation buttons for controlling the battery, and the functions of the operation buttons include at least one of the following: power switch, control and display of remaining power, and control and display of current battery temperature. 27.根据权利要求23所述的无人机，其特征在于，所述盖体为盒体结构，且安装在所述壳体的顶部；所述电池还包括设置于所述盖体内的控制电路板，所述控制电路板用于管理和控制所述电池的电芯进行充放电。27. The drone according to claim 23, wherein the cover is a box structure and is mounted on the top of the casing; the battery further comprises a control circuit arranged in the cover The control circuit board is used to manage and control the electric cells of the battery to charge and discharge. 28.根据权利要求23所述的无人机，其特征在于，所述第一气流通道包括第一通道、以及至少一个第二通道；其中，所述第二通道连通在所述入风口与所述第一通道之间，所述第一通道与所述散热风道连通。28. The unmanned aerial vehicle of claim 23, wherein the first airflow channel comprises a first channel and at least one second channel; wherein the second channel communicates between the air inlet and the air inlet. Between the first passages, the first passage communicates with the cooling air duct. 29.根据权利要求28所述的无人机，其特征在于，所述第一通道的延伸方向平行于所述壳体的长度方向。29. The drone of claim 28, wherein the extending direction of the first channel is parallel to the length direction of the housing. 30.根据权利要求28所述的无人机，其特征在于，所述第二通道包括至少两个，至少两个所述第二通道分散延伸向所述第一通道。30. The unmanned aerial vehicle of claim 28, wherein the second channel comprises at least two, and at least two of the second channels are dispersed and extend toward the first channel. 31.根据权利要求28所述的无人机，其特征在于，所述第二通道包括喇叭状的导向腔，所述导向腔连通所述第一通道，以将从所述入风口流入的气流导入所述第一通道。31. The unmanned aerial vehicle of claim 28, wherein the second passage comprises a horn-shaped guide cavity, and the guide cavity communicates with the first passage for the airflow flowing from the air inlet Import the first channel. 32.根据权利要求23所述的无人机，其特征在于，所述第一气流通道在气流方向上的截面呈n型。32. The unmanned aerial vehicle of claim 23, wherein the cross section of the first airflow channel in the airflow direction is n-shaped. 33.根据权利要求23所述的无人机，其特征在于，所述盖体上设有握持部，所述入风口包括两个，两个所述入风口分设于所述握持部在所述壳体长度方向上的两侧。33. The unmanned aerial vehicle of claim 23, wherein a gripping portion is provided on the cover body, the air inlets comprise two, and the two air inlets are respectively arranged on the gripping portion at both sides in the length direction of the casing. 34.根据权利要求23所述的无人机，其特征在于，所述壳体包括底壁以及与所述底壁配合围合成腔体的侧壁，所述腔体用以收容所述电芯，所述侧壁和/或所述底壁设有第一配合部，所述电芯上设有与所述第一配合部适配的第二配合部，通过所述第一配合部与所述第二配合部的装配，以使所述电芯安装于所述壳体内。34. The drone according to claim 23, wherein the casing comprises a bottom wall and a side wall that cooperates with the bottom wall to form a cavity, and the cavity is used to accommodate the battery cells , the side wall and/or the bottom wall is provided with a first matching portion, the battery core is provided with a second matching portion adapted to the first matching portion, and the first matching portion is connected to the The second matching portion is assembled, so that the battery core is installed in the housing. 35.根据权利要求34所述的无人机，其特征在于，至少一对相对的所述侧壁和所述底壁分别设有所述第一配合部，位于所述底壁上的所述第一配合部与位于至少一对相对的所述侧壁上的第一配合部衔接。35. The unmanned aerial vehicle of claim 34, wherein at least one pair of opposite side walls and the bottom wall are respectively provided with the first matching portion, and the first matching portion is located on the bottom wall. The first matching portion engages with the first matching portion located on at least one pair of the opposite side walls. 36.根据权利要求35所述的无人机，其特征在于，所述电芯安装在所述壳体内时，与设置有所述第一配合部的侧壁、底壁之间具有间隙，所述间隙形成至少两个间隔的散热子风道。36. The unmanned aerial vehicle according to claim 35, wherein when the battery cell is installed in the housing, there is a gap between the side wall and the bottom wall on which the first matching portion is provided, so that the The gaps form at least two spaced heat sink air ducts. 37.根据权利要求36所述的无人机，其特征在于，至少一对相对的所述侧壁、所述底壁上分别设有多个间隔的所述第一配合部，所述电芯上设有与所述第一配合部一一对应的第二配合部。37 . The drone according to claim 36 , wherein at least one pair of the opposite side walls and the bottom wall are respectively provided with a plurality of spaced first matching parts, and the battery cores are 37 . 37 . A second matching portion corresponding to the first matching portion is provided thereon. 38.根据权利要求36所述的无人机，其特征在于，所述第一配合部为设置于所述壳体上的筋条，所述第二配合部为设置于电芯上的凹槽；或者，38. The drone according to claim 36, wherein the first matching portion is a rib provided on the casing, and the second matching portion is a groove provided on the battery core ;or, 所述第一配合部为设置于所述壳体上的凹槽，所述第二配合部为设置于所述电芯上的筋条。The first matching portion is a groove arranged on the casing, and the second matching portion is a rib arranged on the battery core. 39.根据权利要求38所述的无人机，其特征在于，所述筋条的凸起高度范围为4mm-5mm。39. The unmanned aerial vehicle according to claim 38, wherein the height of the protrusion of the ribs ranges from 4mm to 5mm. 40.根据权利要求37所述的无人机，其特征在于，所述散热子风道呈“U”型，每一个所述散热子风道分别与所述第一气流通道、所述第二气流通道连通。40. The unmanned aerial vehicle according to claim 37, wherein the cooling sub-air ducts are in a "U" shape, and each of the cooling sub-air ducts is connected to the first airflow channel, the second Air flow passages communicate. 41.根据权利要求23所述的无人机，其特征在于，所述电芯上设有散热翅片。41. The unmanned aerial vehicle of claim 23, wherein heat dissipation fins are provided on the battery core. 42.根据权利要求36所述的无人机，其特征在于，所述散热风道包括相对的两个侧壁与所述电芯之间分别构成的第一风道和第二风道、以及所述底壁与所述电芯之间构成的第三风道，所述第一风道和所述第二风道分别与所述第三风道连通，所述第一气流通道与所述第一风道连通，所述第二气流通道与所述第二风道连通。42. The drone according to claim 36, wherein the cooling air duct comprises a first air duct and a second air duct respectively formed between two opposite side walls and the battery core, and A third air duct formed between the bottom wall and the battery core, the first air duct and the second air duct are respectively connected to the third air duct, and the first air duct is connected to the third air duct. The first air passage communicates with the second air passage, and the second air passage communicates with the second air passage. 43.根据权利要求42所述的无人机，其特征在于，在侧壁与所述电芯的相对方向上，所述第一风道的间距为30mm-40mm；在所述底壁与所述电芯的相对方向上，所述第二风道的间距为30mm-40mm。43. The unmanned aerial vehicle according to claim 42, characterized in that, in the opposite direction of the side wall and the battery core, the spacing of the first air duct is 30mm-40mm; In the opposite direction of the cells, the spacing of the second air ducts is 30mm-40mm. 44.根据权利要求23所述的无人机，其特征在于，所述电芯的表面设有防水层。44. The drone according to claim 23, wherein a waterproof layer is provided on the surface of the battery core.
CN202080030882.XA 2020-06-10 2020-06-10 Batteries & Drones Pending CN113795970A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2020/095280 WO2021248345A1 (en) 2020-06-10 2020-06-10 Battery and unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN113795970A true CN113795970A (en) 2021-12-14

Family

ID=78846619

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202080030882.XA Pending CN113795970A (en) 2020-06-10 2020-06-10 Batteries & Drones

Country Status (2)

Country Link
CN (1) CN113795970A (en)
WO (1) WO2021248345A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116435648A (en) * 2023-04-14 2023-07-14 苏州时代华景新能源有限公司 Heat dissipation structure
CN117497953A (en) * 2024-01-03 2024-02-02 孚能科技(赣州)股份有限公司 Airflow dredging piece and power battery
CN117508695A (en) * 2023-11-07 2024-02-06 国网甘肃省电力公司甘南供电公司 Unmanned aerial vehicle carried battery pack

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114914614B (en) * 2022-05-16 2023-09-12 北京科易动力科技有限公司 battery pack
WO2025015552A1 (en) * 2023-07-19 2025-01-23 深圳市大疆创新科技有限公司 Aircraft, aircraft system, battery, movable platform, and movable platform system
CN116826246B (en) * 2023-08-31 2023-12-05 成都沃飞天驭科技有限公司 Battery module and aircraft of adaptation forced air cooling system
CN119898499B (en) * 2025-04-02 2025-06-17 飞客工场科技(北京)有限公司 Unmanned aerial vehicle airborne power module and unmanned aerial vehicle

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1290046A (en) * 1999-09-28 2001-04-04 松下电器产业株式会社 Combined sealed secondary battery
US20010030069A1 (en) * 2000-04-13 2001-10-18 Toyota Jidosha Kabushiki Kaisha Vehicle power source device wherein cooling air is introduced into battery casing through opening formed through vehicle floor
CN105514319A (en) * 2016-02-24 2016-04-20 宁德时代新能源科技股份有限公司 Battery pack cooling system
CN108110179A (en) * 2017-12-25 2018-06-01 湛江正信科技服务有限公司 A kind of power battery pack
CN207558855U (en) * 2017-11-02 2018-06-29 绿驰汽车科技（上海）有限公司 A kind of improved battery case
CN108615835A (en) * 2018-05-04 2018-10-02 安徽上造智能设备科技有限公司 A kind of autonomous heat dissipation battery of new-energy automobile high strength anti-explosion
CN108777337A (en) * 2018-05-30 2018-11-09 安徽工程大学 A kind of new energy car battery case
CN109524582A (en) * 2017-09-19 2019-03-26 郑州宇通客车股份有限公司 The battery case and its battery box body of built-in independent heat dissipation channel
CN210110871U (en) * 2019-06-24 2020-02-21 风帆（扬州）有限责任公司 Heat-resistant plastic shell start-stop battery for automobile

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103413989B (en) * 2013-07-25 2016-11-09 天津市松正电动汽车技术股份有限公司 A kind of battery heat removal system
CN108352472B (en) * 2015-10-28 2021-02-05 株式会社村田制作所 Electronic device case and battery pack provided with same
CN207664199U (en) * 2017-12-07 2018-07-27 珠海格力精密模具有限公司 Air duct structure of battery box and battery box
CN208423109U (en) * 2018-07-12 2019-01-22 珠海格力精密模具有限公司 Battery box and battery box

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1290046A (en) * 1999-09-28 2001-04-04 松下电器产业株式会社 Combined sealed secondary battery
US20010030069A1 (en) * 2000-04-13 2001-10-18 Toyota Jidosha Kabushiki Kaisha Vehicle power source device wherein cooling air is introduced into battery casing through opening formed through vehicle floor
CN105514319A (en) * 2016-02-24 2016-04-20 宁德时代新能源科技股份有限公司 Battery pack cooling system
CN109524582A (en) * 2017-09-19 2019-03-26 郑州宇通客车股份有限公司 The battery case and its battery box body of built-in independent heat dissipation channel
CN207558855U (en) * 2017-11-02 2018-06-29 绿驰汽车科技（上海）有限公司 A kind of improved battery case
CN108110179A (en) * 2017-12-25 2018-06-01 湛江正信科技服务有限公司 A kind of power battery pack
CN108615835A (en) * 2018-05-04 2018-10-02 安徽上造智能设备科技有限公司 A kind of autonomous heat dissipation battery of new-energy automobile high strength anti-explosion
CN108777337A (en) * 2018-05-30 2018-11-09 安徽工程大学 A kind of new energy car battery case
CN210110871U (en) * 2019-06-24 2020-02-21 风帆（扬州）有限责任公司 Heat-resistant plastic shell start-stop battery for automobile

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116435648A (en) * 2023-04-14 2023-07-14 苏州时代华景新能源有限公司 Heat dissipation structure
WO2024212392A1 (en) * 2023-04-14 2024-10-17 苏州时代华景新能源有限公司 Heat dissipation structure
CN117508695A (en) * 2023-11-07 2024-02-06 国网甘肃省电力公司甘南供电公司 Unmanned aerial vehicle carried battery pack
CN117508695B (en) * 2023-11-07 2024-05-31 国网甘肃省电力公司甘南供电公司 Drone battery pack
CN117497953A (en) * 2024-01-03 2024-02-02 孚能科技(赣州)股份有限公司 Airflow dredging piece and power battery
CN117497953B (en) * 2024-01-03 2024-05-07 孚能科技(赣州)股份有限公司 Airflow dredging piece and power battery

Also Published As

Publication number Publication date
WO2021248345A1 (en) 2021-12-16

Similar Documents

Publication Publication Date Title
CN113795970A (en) Batteries & Drones
CN107004919B (en) Battery and have unmanned vehicles of this battery
CN210074100U (en) Battery pack and battery pack heat dissipation structure
CN205488366U (en) Battery and have unmanned vehicles of this battery
CN212874584U (en) Energy storage battery box and energy storage system
CN212257622U (en) Battery and unmanned aerial vehicle
CN113054286A (en) Battery box device and electric automobile with same
CN210669578U (en) Charger and unmanned equipment
CN219873793U (en) battery pack
CN208939115U (en) A lithium battery with uniform heat dissipation in all directions
WO2022228565A1 (en) Battery pack and power consuming device
CN212113796U (en) Module Housings and Modules
CN221574023U (en) Battery Pack
CN215496940U (en) Battery heat radiation structure and aircraft
WO2023040066A1 (en) Household energy storage system
CN222591265U (en) Electric vehicle charger
CN222653994U (en) Battery module and energy storage device
CN215184186U (en) Battery box device and electric automobile with same
CN221728745U (en) Portable electronic equipment accessory
CN222763043U (en) Battery pack and electric equipment
CN213304249U (en) Battery module heat dissipation shell
CN216852938U (en) Industrial computer heat radiation structure and unmanned logistics vehicle
CN222654185U (en) Battery modules and energy storage devices
CN221150191U (en) A kind of power battery with Baogai structure
CN221041252U (en) Battery pack and energy storage power supply

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20211214

WD01 Invention patent application deemed withdrawn after publication