CN111076845A - Feedback type unmanned aerial vehicle running temperature measuring device - Google Patents
Feedback type unmanned aerial vehicle running temperature measuring device Download PDFInfo
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- CN111076845A CN111076845A CN202010207835.XA CN202010207835A CN111076845A CN 111076845 A CN111076845 A CN 111076845A CN 202010207835 A CN202010207835 A CN 202010207835A CN 111076845 A CN111076845 A CN 111076845A
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K13/00—Thermometers specially adapted for specific purposes
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M3/00—Investigating fluid-tightness of structures
- G01M3/02—Investigating fluid-tightness of structures by using fluid or vacuum
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- 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
- H01M10/4228—Leak testing of cells or batteries
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- 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
- H01M10/4285—Testing apparatus
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- 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
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- 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
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- 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
- H01M10/63—Control systems
- H01M10/635—Control systems based on ambient temperature
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- 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
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- 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
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- 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
- H01M10/6567—Liquids
- H01M10/6568—Liquids characterised by flow circuits, e.g. loops, located externally to the cells or cell casings
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- 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
- H01M10/6569—Fluids undergoing a liquid-gas phase change or transition, e.g. evaporation or condensation
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- 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
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- 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
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- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Secondary Cells (AREA)
Abstract
The invention relates to the technical field of unmanned aerial vehicles, and discloses a feedback type unmanned aerial vehicle running temperature measuring device which comprises an unmanned aerial vehicle body, wherein a battery box is arranged on the inner wall of the unmanned aerial vehicle body, a protective shell is arranged on the inner wall of the battery box, a battery pack is arranged on the inner wall of the protective shell, a battery cover plate is arranged at the top of the battery box, a cavity is formed between the protective shell and the battery box, a winding pipe wound on the surface of the protective shell is arranged on the inner wall of the cavity, a coiled pipe located below the protective shell is communicated with one end of the winding pipe, a micro condenser located on one side of the battery box is arranged on the inner wall of the unmanned aerial vehicle body, and the other end of the winding pipe is communicated with. The invention solves the problem that the service life of the unmanned aerial vehicle is seriously influenced because the unmanned aerial vehicle lacks an operation temperature measuring device and the battery of the unmanned aerial vehicle is easily burnt out even the phenomenon of electric leakage or liquid leakage occurs once the internal temperature of the unmanned aerial vehicle is overhigh.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a feedback type unmanned aerial vehicle operation temperature measuring device.
Background
Unmanned aerial vehicles are unmanned aerial vehicles operated by radio remote control equipment and self-contained program control devices, and are widely applied to military and civil fields. Many rotor unmanned aerial vehicle have control simple, the reliability is high to need the runway alright in order to VTOL, can hover advantages such as in the air after taking off, consequently all obtained wide application in each field.
In the unmanned aerial vehicle use, the battery discharges and provides the electric energy for unmanned aerial vehicle, makes unmanned aerial vehicle can normal operating, but in the use of reality, because unmanned aerial vehicle lacks operating temperature measuring device, in case unmanned aerial vehicle inside high temperature, lead to unmanned aerial vehicle's battery to burn out very easily, appear the phenomenon of electric leakage or weeping even, seriously influence unmanned aerial vehicle's life.
Disclosure of Invention
The invention aims to solve the defects in the prior art, such as: because unmanned aerial vehicle lacks operating temperature measuring device, in case unmanned aerial vehicle inside high temperature leads to unmanned aerial vehicle's battery to burn out very easily, appears electric leakage or the phenomenon of weeping even, seriously influences unmanned aerial vehicle's life, and the feedback type unmanned aerial vehicle operating temperature measuring device who provides.
In order to achieve the purpose, the invention adopts the following technical scheme:
a feedback type unmanned aerial vehicle running temperature measuring device comprises an unmanned aerial vehicle body, wherein a battery box is arranged on the inner wall of the unmanned aerial vehicle body, a protective shell is arranged on the inner wall of the battery box, a battery pack is arranged on the inner wall of the protective shell, a battery cover plate is arranged at the top of the battery box, a cavity is formed between the protective shell and the battery box, a winding pipe wound on the surface of the protective shell is arranged on the inner wall of the cavity, one end of the winding pipe is communicated with a coiled pipe located below the protective shell, a micro condenser located on one side of the battery box is arranged on the inner wall of the unmanned aerial vehicle body, the other end of the winding pipe is communicated with the inlet of the micro condenser, the outlet of the micro condenser is communicated with a micro water pump, and the water outlet of; the unmanned aerial vehicle body inner wall still is provided with control module, control module's input electric connection has operating temperature monitoring module, operating temperature monitoring module's output electric connection has feedback module, feedback module's output and control module electric connection, miniature condenser and miniature pump's input all with control module's output electric connection, control module's output electric connection has signal receiver, signal receiver is located the top of unmanned aerial vehicle body, and control module has mobile terminal through signal receiver signal connection.
Preferably, the protective shell is a heat-conducting silica gel material member, and heat-conducting holes are formed in the surface of the protective shell and are distributed at equal intervals.
Preferably, the clamping groove has all been seted up to the inner wall front and the inner wall back of protecting crust, the inner wall joint of clamping groove has the anti-collision baffle.
Preferably, a cavity is formed inside the anti-collision partition plate, a cooling box with cooling liquid pre-installed inside is arranged inside the cavity, and a detachable sealing cover is arranged at the top of the anti-collision partition plate.
Preferably, through holes are formed in both sides of the anti-collision partition plate.
Preferably, the bottom of the battery cover plate is respectively provided with a leakage detection circuit and a leakage detection circuit which are matched with the battery pack, and the output ends of the leakage detection circuit and the leakage detection circuit are electrically connected with the control module.
Preferably, the micro condenser is a self-contained water tank type condenser, and the water tank, the coil pipe and the coiled pipe are filled with cooling liquid.
Preferably, the control module comprises a central processing unit, a ROM preset module, a data comparator and an a/D converter, the central processing unit is electrically connected with the ROM preset module in a bidirectional manner, an output end of the ROM preset module is electrically connected with an output end of the data comparator, the data comparator is electrically connected with the central processing unit in a bidirectional manner, and an output end of the operating temperature monitoring module is electrically connected with the central processing unit through the a/D converter.
Preferably, the operation temperature monitoring module is including embedded CPU, battery temperature sensor, the inside temperature sensor of organism and organism surface temperature sensor's output all with embedded CPU electric connection, and battery temperature sensor installs in the inner wall of protecting crust, and battery temperature sensor and group battery laminating, the inside temperature sensor of organism sets up in the inside of unmanned aerial vehicle body, organism surface temperature sensor sets up in the top of unmanned aerial vehicle body.
Preferably, the mobile terminal is a mobile device with a communication function, and the mobile terminal is a mobile phone or a tablet computer of a user.
Compared with the prior art, the invention has the following advantages:
1. by arranging the operation temperature monitoring module, the body temperature, the internal temperature and the surface temperature of the battery of the unmanned aerial vehicle in the operation process can be monitored in real time, the operation processing is carried out by the control module, if the surface temperature of the battery pack is overhigh, the control module controls the micro water pump and the micro condenser to operate, so that the cooling liquid flows in the coiled pipe and the coiled pipe, and the cooling liquid is always kept at a lower temperature after being cooled by the micro condenser, thereby absorbing the heat generated by the battery, playing a role in reducing the surface temperature of the battery, avoiding the battery from being burnt out due to overhigh temperature, and simultaneously when the temperatures monitored by the operation temperature monitoring module are recovered to normal levels, the feedback module feeds back signals to the control module to enable the control module to control the micro condenser and the micro water pump to stop operating so as to achieve the real-time operation process of the unmanned aerial vehicle, the real-time monitoring of the operation temperature reduces the possibility of the unmanned aerial vehicle burning due to overhigh temperature;
2. when the control module receives temperature data detected by the operation temperature monitoring module, if abnormal conditions are temporarily not relieved or the battery pack has liquid leakage or electric leakage, the control module sends the abnormal conditions to a mobile phone or a flat plate of a user in an information mode through the signal receiver, so that the user can control the unmanned aerial vehicle to return in time, long-time abnormal operation of the unmanned aerial vehicle is avoided, and the possibility of damage of the unmanned aerial vehicle is reduced;
3. through seting up the heat conduction hole on the protecting crust surface, help the thermal scattering and disappearing of group battery, set up simultaneously in the protecting crust is inside to prevent bumping the baffle, can avoid colliding between the group battery and set up the cooling box in the cavity is inside, the heat conduction of cooperation through-hole has certain cooling effect to the group battery in to the spaced between the group battery, has reduced the possibility that the group battery burns out.
Drawings
FIG. 1 is a perspective view of the present invention;
FIG. 2 is a schematic structural view of the present invention;
FIG. 3 is a system flow diagram of the present invention;
FIG. 4 is a schematic structural view of a battery case according to the present invention;
FIG. 5 is a schematic structural view of a coiled tubing of the present invention;
FIG. 6 is a schematic view of the structure of the anti-collision partition according to the present invention;
FIG. 7 is a circuit diagram of a leakage detection circuit according to the present invention;
fig. 8 is a circuit diagram of the leakage detecting circuit according to the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. a battery box; 3. a protective shell; 4. a heat conduction hole; 5. a cavity; 6. a coiled tube; 7. a serpentine tube; 8. a micro condenser; 9. a micro water pump; 10. a battery pack; 11. a collision-proof partition plate; 12. a cooling box; 13. a control module; 131. a central processing unit; 132. a ROM preset module; 133. a data comparator; 14. an operating temperature monitoring module; 141. an embedded CPU; 142. a battery temperature sensor; 143. a temperature sensor inside the body; 144. a body surface temperature sensor; 15. a feedback module; 16. a signal receiver; 17. a mobile terminal; 18. a battery cover plate; 19. a liquid leakage detection circuit; 20. a leakage detection circuit; 21. a detachable cover; 22. and a through hole.
Detailed Description
The technical solutions 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 a part of the embodiments of the present invention, and not all of the embodiments.
Referring to fig. 1-8, a feedback type unmanned aerial vehicle operating temperature measuring device comprises an unmanned aerial vehicle body 1, a battery box 2 is arranged on the inner wall of the unmanned aerial vehicle body 1, a protective shell 3 is arranged on the inner wall of the battery box 2, a battery pack 10 is arranged on the inner wall of the protective shell 3, a battery cover plate 18 is arranged at the top of the battery box 2, a cavity 5 is formed between the protective shell 3 and the battery box 2, a winding pipe 6 wound on the surface of the protective shell 3 is arranged on the inner wall of the cavity 5, one end of the winding pipe 6 is communicated with a coiled pipe 7 positioned below the protective shell 3, a micro condenser 8 positioned on one side of the battery box 2 is arranged on the inner wall of the unmanned aerial vehicle body 1, the other end of the winding pipe 6 is communicated with an inlet of the micro condenser 8, an outlet of the micro pump 9 is communicated with the; the inner wall of unmanned aerial vehicle body 1 still is provided with control module 13, control module 13's input electric connection has operating temperature monitoring module 14, operating temperature monitoring module 14's output electric connection has feedback module 15, feedback module 15's output and control module 13 electric connection, miniature condenser 8 and miniature pump 9's input all with control module 13's output electric connection, control module 13's output electric connection has signal receiver 16, signal receiver 16 is located unmanned aerial vehicle body 1's top, and control module 13 has mobile terminal 17 through signal receiver 16 signal connection.
Specifically, protective housing 3 is heat conduction silica gel material component, and protective housing 3's surface sets up the heat conduction hole 4 that the equidistance distributes, and heat conduction silica gel material not only has good heat conduction effect, and the texture is softer, can carry out good protection effect to group battery 10, and the heat conduction hole 4 can accelerate thermal flow, helps the cooling of group battery 10.
Specifically, the draw-in groove has all been seted up at the inner wall front and the inner wall back of protecting crust 3, and the inner wall joint of draw-in groove has the baffle 11 of preventing bumping, and the draw-in groove makes the inner wall that prevents bumping baffle 11 and can follow protecting crust 3 take out, has made things convenient for the dismouting of preventing bumping baffle 11.
Specifically, the inside of preventing bumping baffle 11 is formed with the cavity, and the inside of cavity is provided with inside cooling box 12 of preassembleing the coolant liquid, and prevents bumping baffle 11's top and be provided with removable closing cap 21, and removable closing cap 21 makes cooling box 12 can follow the cavity inside and takes out, conveniently changes inside coolant liquid, uses convenient more reliable.
Specifically, through-holes 22 have all been seted up to the both sides of anti-collision partition plate 11, and through-holes 22 help the heat dissipation of group battery 10, have played certain radiating effect of accelerating.
Specifically, the bottom of battery apron 18 is provided with respectively and uses with group battery 10 cooperation weeping detection circuitry 19 and electric leakage detection circuitry 20, and weeping detection circuitry 19 and electric leakage detection circuitry 20's output all with control module 13 electric connection, electric leakage detection circuitry 20 can detect the electric leakage condition of group battery 10, and weeping detection circuitry 19 then can detect out whether the weeping condition appears in group battery 10, thereby can be at the operation in-process, carry out good control to the group battery 10 of unmanned aerial vehicle body 1, reduce the possibility that abnormal operation leads to the damage.
Specifically, the micro condenser 8 is a self-contained water tank type condenser, the inside of the water tank, the coil pipe 6 and the coil pipe 7 are filled with cooling liquid, and the cooling liquid circularly flows in the micro condenser 8, the coil pipe 6 and the coil pipe 7, so that the inside of the coil pipe 6 and the coil pipe 7 is kept at a low temperature.
Specifically, the control module 13 includes a central processing unit 131, a ROM preset module 132, a data comparator 133 and an a/D converter, the central processing unit 131 is electrically connected with the ROM preset module 132 in both directions, an output end of the ROM preset module 132 is electrically connected with an output end of the data comparator 133, the data comparator 133 is electrically connected with the central processing unit 131 in both directions, an output end of the operating temperature monitoring module 14 is electrically connected with the central processing unit 131 through the a/D converter, during the flight of the unmanned aerial vehicle, the operating temperature monitoring module 14 transmits the detected temperature data to the central processing unit 131 through the a/D converter, and the data comparator 133 compares the real-time temperature condition with a normal temperature range preset by the ROM preset module 132, if the temperature condition is abnormal, the central processing unit 131 controls the micro water pump 9 and the micro condenser 8 to operate, the coolant can be circulated, so that the temperature can be kept low.
Specifically, the operation temperature monitoring module 14 includes an embedded CPU 141, a battery temperature sensor 142, an internal body temperature sensor 143, and an internal body surface temperature sensor 144, the output ends of the battery temperature sensor 142, the internal body temperature sensor 143, and the internal body surface temperature sensor 144 are electrically connected to the embedded CPU 141, the battery temperature sensor 142 is mounted on the inner wall of the protective shell 3, the battery temperature sensor 142 is attached to the battery pack 10, the internal body temperature sensor 143 is disposed inside the unmanned aerial vehicle body 1, the internal body surface temperature sensor 144 is disposed on the top of the unmanned aerial vehicle body 1, the battery temperature sensor 142 is used for detecting the surface temperature of the battery pack 10, the internal body surface temperature sensor 144 is used for measuring the surface temperature of the unmanned aerial vehicle for determining the temperature condition of the external environment, the internal body temperature sensor 143 is used for detecting the internal body temperature, so as to judge whether the temperature inside the machine body is too high or not and reduce the influence of high temperature on internal components.
Specifically, the mobile terminal 17 is a mobile device with a communication function, the mobile terminal 17 is a mobile phone or a tablet personal computer of a user, and communication devices such as mobile phones are devices which are used in daily life of people and are mature, and most of the devices are carried about, so that information can be received timely, and a response can be made timely.
The working process and the beneficial effects of the invention are as follows: by arranging the operation temperature monitoring module 14, the temperature of the body 1 of the unmanned aerial vehicle in the operation process, the temperature in the unmanned aerial vehicle and the temperature on the surface of the battery can be monitored in real time, and the operation processing is carried out through the control module 13, if the surface temperature of the battery pack 10 is overhigh, the control module 13 controls the micro water pump 9 and the micro condenser 8 to operate, so that cooling liquid flows in the coil pipe 7 and the coil pipe 6, and the cooling liquid is always kept at a lower temperature after being cooled by the micro condenser 8, thereby absorbing the heat generated by the battery, achieving the effect of reducing the surface temperature of the battery, avoiding the overhigh temperature of the battery from being burnt, and when the temperatures monitored by the operation temperature monitoring module 14 are recovered to normal levels, the feedback module 15 feeds back signals to the control module 13, so that the control module 13 controls the micro condenser 8 and the micro water pump 9 to stop operation, so as to reach real-time to the unmanned aerial vehicle operation in-process, operating temperature's real time monitoring, reduce the too high possibility of burning out of unmanned aerial vehicle temperature, in addition, when control module 13 received the temperature data that operating temperature monitoring module 14 detected, when the condition that appears unusually can't be relieved temporarily, or during the condition of weeping or electric leakage appears in group battery 10, control module 13 can be through signal receiver 16 with the abnormal conditions with the form of information send to user's cell-phone or dull and stereotyped on, so that the user can be timely control unmanned aerial vehicle return, avoid the long-time unusual operation of unmanned aerial vehicle, reduce the possibility of unmanned aerial vehicle damage.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be able to cover the technical scope of the present invention and the equivalent alternatives or modifications according to the technical solution and the inventive concept of the present invention within the technical scope of the present invention.
Claims (10)
1. The utility model provides a reaction type unmanned aerial vehicle operating temperature measuring device, includes unmanned aerial vehicle body (1), its characterized in that, the inner wall of unmanned aerial vehicle body (1) is provided with battery box (2), the inner wall of battery box (2) is provided with protecting crust (3), the inner wall of protecting crust (3) is provided with group battery (10), and the top of battery box (2) is provided with battery apron (18), form cavity (5) between protecting crust (3) and battery box (2), the inner wall of cavity (5) is provided with coils pipe (6) of coiling on protecting crust (3) surface, the one end intercommunication of coils pipe (6) has coiled pipe (7) that is located protecting crust (3) below, the inner wall of unmanned aerial vehicle body (1) is provided with miniature condenser (8) that is located battery box (2) one side, the other end and the import of miniature condenser (8) of coils pipe (6) communicate, the outlet of the micro condenser (8) is communicated with a micro water pump (9), and the water outlet of the micro water pump (9) is communicated with the coiled pipe (7); unmanned aerial vehicle body (1) inner wall still is provided with control module (13), the input electric connection of control module (13) has operating temperature monitoring module (14), the output electric connection of operating temperature monitoring module (14) has feedback module (15), the output and the control module (13) electric connection of feedback module (15), the input of miniature condenser (8) and miniature pump (9) all with the output electric connection of control module (13), the output electric connection of control module (13) has signal receiver (16), signal receiver (16) are located the top of unmanned aerial vehicle body (1), and control module (13) have mobile terminal (17) through signal receiver (16) signal connection.
2. The device for measuring the operating temperature of the feedback type unmanned aerial vehicle according to claim 1, wherein the protective shell (3) is a heat-conducting silica gel material member, and heat-conducting holes (4) are formed in the surface of the protective shell (3) and are distributed at equal intervals.
3. The device for measuring the operating temperature of the feedback type unmanned aerial vehicle according to claim 1, wherein the front surface and the back surface of the inner wall of the protective shell (3) are provided with clamping grooves, and the inner wall of each clamping groove is clamped with a collision-proof partition plate (11).
4. The device for measuring the operating temperature of the feedback unmanned aerial vehicle according to claim 3, wherein a cavity is formed inside the anti-collision partition plate (11), a cooling box (12) with a coolant liquid pre-installed inside is arranged inside the cavity, and a detachable sealing cover (21) is arranged at the top of the anti-collision partition plate (11).
5. The device for measuring the operating temperature of the feedback type unmanned aerial vehicle according to claim 3, wherein through holes (22) are formed in both sides of the anti-collision partition plate (11).
6. The device for measuring the operating temperature of the feedback type unmanned aerial vehicle according to claim 1, wherein a leakage detection circuit (19) and a leakage detection circuit (20) are respectively arranged at the bottom of the battery cover plate (18) and used in cooperation with the battery pack (10), and output ends of the leakage detection circuit (19) and the leakage detection circuit (20) are electrically connected with the control module (13).
7. A feedback drone operating temperature measuring device according to claim 1, characterised by that the micro-condenser (8) is a self-contained water tank condenser and the inside of the water tank, the coil (6) and the coil (7) are filled with cooling liquid.
8. The device for measuring the operating temperature of the feedback type unmanned aerial vehicle according to claim 1, wherein the control module (13) comprises a central processing unit (131), a ROM preset module (132), a data comparator (133) and an a/D converter, the central processing unit (131) is electrically connected with the ROM preset module (132) in a bidirectional manner, an output end of the ROM preset module (132) is electrically connected with an output end of the data comparator (133), the data comparator (133) is electrically connected with the central processing unit (131) in a bidirectional manner, and an output end of the operating temperature monitoring module (14) is electrically connected with the central processing unit (131) through the a/D converter.
9. The device for measuring the operating temperature of the feedback type unmanned aerial vehicle according to claim 1, wherein the operating temperature monitoring module (14) comprises an embedded CPU (141), a battery temperature sensor (142), an internal body temperature sensor (143) and a surface body temperature sensor (144), the output ends of the battery temperature sensor (142), the internal body temperature sensor (143) and the surface body temperature sensor (144) are electrically connected with the embedded CPU, the battery temperature sensor (142) is installed on the inner wall of the protective shell (3), the battery temperature sensor (142) is attached to the battery pack (10), the internal body temperature sensor (143) is arranged inside the unmanned aerial vehicle body (1), and the surface body temperature sensor (144) is arranged at the top of the unmanned aerial vehicle body (1).
10. The device for measuring the operating temperature of the feedback unmanned aerial vehicle according to claim 1, wherein the mobile terminal (17) is a mobile device with a communication function, and the mobile terminal (17) is a mobile phone or a tablet computer of a user.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010207835.XA CN111076845A (en) | 2020-03-23 | 2020-03-23 | Feedback type unmanned aerial vehicle running temperature measuring device |
| CN202021534873.8U CN213649914U (en) | 2020-03-23 | 2020-07-29 | Feedback type unmanned aerial vehicle running temperature measuring device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010207835.XA CN111076845A (en) | 2020-03-23 | 2020-03-23 | Feedback type unmanned aerial vehicle running temperature measuring device |
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| Publication Number | Publication Date |
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| CN111076845A true CN111076845A (en) | 2020-04-28 |
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| CN202010207835.XA Withdrawn CN111076845A (en) | 2020-03-23 | 2020-03-23 | Feedback type unmanned aerial vehicle running temperature measuring device |
| CN202021534873.8U Active CN213649914U (en) | 2020-03-23 | 2020-07-29 | Feedback type unmanned aerial vehicle running temperature measuring device |
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| CN202021534873.8U Active CN213649914U (en) | 2020-03-23 | 2020-07-29 | Feedback type unmanned aerial vehicle running temperature measuring device |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115064826A (en) * | 2022-06-09 | 2022-09-16 | 深圳市恒创兴电子科技有限公司 | Intelligent household equipment battery protection device based on emergency power supply function |
| CN115483416A (en) * | 2022-06-30 | 2022-12-16 | 华北电力大学 | System and method for testing external temperature field of SOFC (solid oxide Fuel cell) stack |
| JP7550095B2 (en) | 2021-03-29 | 2024-09-12 | 本田技研工業株式会社 | Flying object |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114013671A (en) * | 2021-12-10 | 2022-02-08 | 南京中智腾飞航空科技研究院有限公司 | Carry pipeline nondestructive test device in unmanned aerial vehicle |
| CN115294717B (en) * | 2022-08-03 | 2023-12-22 | 中国民用航空飞行学院 | Unmanned aerial vehicle fire detection method, unmanned aerial vehicle fire detection device and unmanned aerial vehicle fire detection medium |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| JP7550095B2 (en) | 2021-03-29 | 2024-09-12 | 本田技研工業株式会社 | Flying object |
| CN115064826A (en) * | 2022-06-09 | 2022-09-16 | 深圳市恒创兴电子科技有限公司 | Intelligent household equipment battery protection device based on emergency power supply function |
| CN115483416A (en) * | 2022-06-30 | 2022-12-16 | 华北电力大学 | System and method for testing external temperature field of SOFC (solid oxide Fuel cell) stack |
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| CN213649914U (en) | 2021-07-09 |
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