CN212106082U - Engine ground orbit satellite internet of things monitoring system - Google Patents
Engine ground orbit satellite internet of things monitoring system Download PDFInfo
- Publication number
- CN212106082U CN212106082U CN202020778484.3U CN202020778484U CN212106082U CN 212106082 U CN212106082 U CN 212106082U CN 202020778484 U CN202020778484 U CN 202020778484U CN 212106082 U CN212106082 U CN 212106082U
- Authority
- CN
- China
- Prior art keywords
- engine
- pipe
- air inlet
- orbit satellite
- earth orbit
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Landscapes
- Arrangements For Transmission Of Measured Signals (AREA)
Abstract
The utility model discloses an engine ground orbit satellite internet of things monitoring system, which comprises a frame and an engine, wherein the engine is arranged on the frame, one side of the frame is provided with a controller, the air inlet end of the engine is connected with an air inlet assembly, the air inlet assembly comprises an air inlet pipe and a branch pipe, the output end of the air inlet pipe is provided with the branch pipe, the output end of the branch pipe is provided with a voltage stabilizer, one end of the voltage stabilizer is communicated with an adjusting pipe, the adjusting pipe is provided with a plurality of groups, and the output end of the adjusting pipe is provided with a gas collecting box; the utility model discloses an air input of flowmeter real time monitoring engine controls opening and close and the degree of opening and shutting of multiunit control tube through the solenoid valve comes the control flow, the management and control air input of being convenient for, and the temperature through temperature sensor real-time induction engine, comes for the engine cooling through heat-conducting plate and heat radiation fins to the cooperation force (forcing) pump carries out water-cooling with the water course of the leading-in heat-conducting plate of water in the water tank, the management and control temperature of being convenient for.
Description
Technical Field
The utility model relates to an engine monitoring technology field especially relates to an engine earth orbit satellite thing networking monitored control system.
Background
In recent years, with the rapid development of automation equipment, the technology of an engine is steadily improved, and the engine is a machine capable of converting other forms of energy into mechanical energy, including an internal combustion engine, an external combustion engine, an electric motor and the like, for example, the internal combustion engine usually converts chemical energy into mechanical energy. The engine is suitable for automation equipment and also applied to automobiles;
engine in use, it is very important to some large-scale automation equipment specially, to the engine control, the key management and control temperature, management and control air input that needs, and among the prior art, the information of engine is hardly given control terminal for fast transmission, and ageing is good inadequately, and this just causes the information lag, and is unfavorable to the control of engine, influences the normal operating of equipment even, consequently, the utility model provides an engine earth orbit satellite thing networking monitored control system is in order to solve the problem that exists among the prior art.
SUMMERY OF THE UTILITY MODEL
To the problem, the utility model aims to provide an engine ground rail satellite thing networking monitored control system, this engine ground rail satellite thing networking monitored control system be convenient for the management and control air input, the management and control temperature of being convenient for, and ground rail satellite communication, transmission delay is short, and path loss is little, and frequency reuse is more effective, has guaranteed the ageing, provides the guarantee for equipment normal operating.
For realizing the purpose of the utility model, the utility model discloses a following technical scheme realizes: the utility model provides an engine earth orbit satellite thing networking monitored control system, includes frame and engine, be equipped with the engine on the frame, and one side on the frame is equipped with the controller, the inlet end of engine is connected with the subassembly that admits air, and the subassembly that admits air includes intake pipe and bleeder, the output of intake pipe is equipped with the bleeder, and the output of bleeder is equipped with the stabiliser, the one end intercommunication of stabiliser has the regulating tube, and the regulating tube is equipped with the multiunit, multiunit the output of regulating tube is equipped with the gas collection box, the output of gas collection box is equipped with the connecting pipe, and the air inlet intercommunication of connecting pipe and engine, the intercommunication has a section of thick bamboo, multiunit in the intake pipe all the intercommunication has the solenoid valve on the regulating tube, the intercommunication has the flowmeter on the connecting pipe, the both.
The further improvement lies in that: the top of the inside one end of stabiliser and the below of the inside other end all are equipped with the stabiliser board, the top intercommunication of lateral pipe and stabiliser one end, the below intercommunication of regulating tube and the stabiliser other end.
The further improvement lies in that: the cooling assembly comprises a heat-conducting plate and radiating fins, the heat-conducting plate is attached to the engine, the radiating fins are arranged on one side of the heat-conducting plate, and a water channel is arranged in the heat-conducting plate.
The further improvement lies in that: one end on the frame is equipped with the water tank, and the output of water tank is equipped with the force (forcing) pump, the output of force (forcing) pump passes through the input intercommunication of water pipe and water course, the export of water course leads to pipe and water tank intercommunication.
The further improvement lies in that: the inside of controller is equipped with treater, earth orbit satellite communication module and signal receiver, the signal output part of temperature sensor and flowmeter all passes through wire and treater electric connection, the output and the earth orbit satellite communication module electric connection of treater, earth orbit satellite communication module and earth orbit satellite wireless communication transmit for control terminal, signal receiver receives control terminal's instruction and gives the treater with the instruction transmission, and the control end of treater with solenoid valve and force (forcing) pump electric connection.
The utility model has the advantages that: the utility model monitors the air input of the engine in real time by the flowmeter, controls the opening and closing degree of a plurality of groups of regulating tubes by the electromagnetic valve to control the flow, is convenient for controlling the air input, senses the temperature of the engine in real time by the temperature sensor, cools the engine by the heat conducting plate and the radiating fins, and guides the water in the water tank into the water channel of the heat conducting plate by matching with the pressure pump to carry out water cooling, is convenient for controlling the temperature, simultaneously, the data measured in real time by the temperature sensor and the flowmeter are wirelessly communicated with the earth orbit satellite by the earth orbit satellite communication module and are transmitted to the control terminal, then the signal receiver receives the instruction of the control terminal and controls the electromagnetic valve by the processor to adjust the air input, the pressure pump is controlled to adjust the water cold flow to adjust the temperature, the earth orbit satellite communication is short in transmission delay, the path, and the normal operation of the equipment is guaranteed.
Drawings
Fig. 1 is a front view of the present invention;
FIG. 2 is a schematic diagram of the structure of the voltage stabilizer of the present invention;
fig. 3 is a schematic diagram of the electrical connection of the controller of the present invention.
Wherein: 1. a machine base; 2. an engine; 3. a controller; 4. an air inlet pipe; 5. a branch pipe; 6. a voltage regulator; 7. an adjusting tube; 8. a gas collection box; 9. a connecting pipe; 10. a filter cartridge; 11. an electromagnetic valve; 12. a flow meter; 13. a temperature sensor; 14. a pressure stabilizing plate; 15. a heat conducting plate; 16. heat dissipation fins; 17. a water tank; 18. a pressure pump; 19. a processor; 20. a ground-orbit satellite communication module; 21. a signal receiver.
Detailed Description
In order to deepen the understanding of the present invention, the following embodiments will be combined to make the present invention do further details, and the present embodiment is only used for explaining the present invention, and does not constitute the limitation of the protection scope of the present invention.
According to fig. 1, 2 and 3, the embodiment provides an engine ground orbit satellite internet of things monitoring system, which comprises a base 1 and an engine 2, wherein the engine 2 is arranged on the base 1, a controller 3 is arranged on one side of the base 1, an air inlet component is connected to an air inlet end of the engine 2, the air inlet component comprises an air inlet pipe 4 and a branch pipe 5, the output end of the air inlet pipe 4 is provided with the branch pipe 5, the output end of the branch pipe 5 is provided with a voltage stabilizer 6, one end of the voltage stabilizer 6 is communicated with an adjusting pipe 7, the adjusting pipe 7 is provided with a plurality of groups, the output end of the adjusting pipe 7 is provided with a gas collecting box 8, the output end of the gas collecting box 8 is provided with a connecting pipe 9, the connecting pipe 9 is communicated with an air inlet of the engine 2, the air inlet pipe 4 is communicated with a filter cartridge 10, the adjusting pipes 7 are communicated, the flowmeter 12 is in a model of ZJS9-CQ-25, a cooling assembly and a temperature sensor 13 are arranged on two sides of the engine 2, and the temperature sensor 13 is in a model of CWDZ 11. During the use, the air gets into bleeder 5 from intake pipe 4 and shunts into the stranded, and rethread regulator 6 steady voltage back gets into regulating tube 7, and leading-in gas collection box 8 merges back entering connecting pipe 9 to get into engine 2, at this in-process, through flowmeter 12 real time monitoring engine 2's air input, control the opening and shutting of multiunit regulating tube 7 and the degree of opening and shutting through solenoid valve 11 and control the air flow.
The top of the inside one end of stabiliser 6 and the below of the inside other end all are equipped with stabiliser board 14, the top intercommunication of lateral pipe 5 and stabiliser 6 one end, the below intercommunication of the regulating tube 7 and stabiliser 6 other end. The air current gets into stabiliser 6 from the top of stabiliser 6 one end, through the gap between two sets of stabiliser boards 14, after the steady pressure, goes out the admission control pipe 7 from the below of the stabiliser 6 other end.
The cooling assembly comprises a heat conduction plate 15 and radiating fins 16, the heat conduction plate 15 is attached to the engine 2, the radiating fins 16 are arranged on one side of the heat conduction plate 15 and conduct heat exchange with air to dissipate heat, and a water channel is arranged inside the heat conduction plate 15.
One end on the frame 1 is equipped with water tank 17, and the output of water tank 17 is equipped with force (forcing) pump 18, the output of force (forcing) pump 18 passes through the input intercommunication of water pipe and water course, the export of water course leads to pipe and water tank 17 intercommunication. The pressure pump 18 guides the water in the water tank 17 into the water passage of the heat conducting plate 15 to cool the water.
The utility model discloses a controller 3, controller 3's inside is equipped with treater 19, earth orbit satellite communication module 20 and signal receiver 21, treater 19 is baseband and CPU, earth orbit satellite communication module 20 adopts cellular communication, multiple access, spot beam, frequency multiplex realization and earth orbit satellite wireless communication, signal receiver 21's model is zigBee, temperature sensor 13 and flowmeter 12's signal output part all pass through wire and treater 19 electric connection, treater 19's output and earth orbit satellite communication module 20 electric connection, earth orbit satellite communication module 20 and earth orbit satellite wireless communication transmit for control terminal, signal receiver 21 receives control terminal's instruction and transmits the instruction for treater 19, and the 19 control end of treater with solenoid valve 11 and force (forcing) pump 18 electric connection. The data measured by the temperature sensor 13 and the flowmeter 12 in real time are wirelessly communicated with an earth orbit satellite through the earth orbit satellite communication module 20 and transmitted to the control terminal, then the instructions of the control terminal are received through the signal receiver 21, the electromagnetic valve 11 is controlled by the processor 19 to adjust the air inflow, and the pressure pump 18 is controlled to adjust the water and cold flow to adjust the temperature, so that the earth orbit satellite communication is short in transmission delay, small in path loss and more effective in frequency reuse.
The engine earth orbit satellite internet of things monitoring system monitors the air input of an engine 2 in real time through a flow meter 12, controls the opening and closing and opening degrees of a plurality of groups of adjusting pipes 7 through an electromagnetic valve 11 to control the flow, is convenient for controlling the air input, senses the temperature of the engine 2 in real time through a temperature sensor 13, cools the engine 2 through a heat conducting plate 15 and a radiating fin 16, guides water in a water tank 17 into a water channel of the heat conducting plate 15 to carry out water cooling and cooling by matching with a pressure pump 18, is convenient for controlling the temperature, simultaneously, data measured in real time by the temperature sensor 13 and the flow meter 12 are wirelessly communicated with an earth orbit satellite through a earth orbit satellite communication module 20 and are transmitted to a control terminal, then a signal receiver 21 receives an instruction of the control terminal and a processor 19 is used for controlling the electromagnetic valve 11 to adjust the air input, and a pressure pump 18, the transmission delay is short, the path loss is small, the frequency reuse is more effective, the timeliness is ensured, and the normal operation of equipment is guaranteed.
The foregoing illustrates and describes the principles, general features, and advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (5)
1. The utility model provides an engine earth orbit satellite thing networking monitored control system, includes frame (1) and engine (2), its characterized in that: an engine (2) is arranged on the base (1), a controller (3) is arranged on one side of the base (1), an air inlet end of the engine (2) is connected with an air inlet assembly, the air inlet assembly comprises an air inlet pipe (4) and branch pipes (5), the output end of the air inlet pipe (4) is provided with the branch pipes (5), the output end of the branch pipes (5) is provided with a pressure stabilizer (6), one end of the pressure stabilizer (6) is communicated with an adjusting pipe (7), the adjusting pipe (7) is provided with a plurality of groups, the output end of the adjusting pipe (7) is provided with a gas collecting box (8), the output end of the gas collecting box (8) is provided with a connecting pipe (9), the connecting pipe (9) is communicated with an air inlet of the engine (2), the air inlet pipe (4) is communicated with a filter cylinder (10), the adjusting pipes (7) are all communicated with a plurality of groups, the connecting pipe (11, and both sides of the engine (2) are provided with a cooling assembly and a temperature sensor (13).
2. The engine earth orbit satellite internet of things monitoring system of claim 1, characterized in that: the top of stabiliser (6) inside one end and the below of the inside other end all are equipped with stabiliser board (14), lateral pipe (5) and the top of stabiliser (6) one end intercommunication, regulating tube (7) and the below intercommunication of stabiliser (6) other end.
3. The engine earth orbit satellite internet of things monitoring system of claim 1, characterized in that: the cooling assembly comprises a heat conduction plate (15) and heat dissipation fins (16), the heat conduction plate (15) is attached to the engine (2), the heat dissipation fins (16) are arranged on one side of the heat conduction plate (15), and a water channel is arranged inside the heat conduction plate (15).
4. The engine earth orbit satellite internet of things monitoring system of claim 3, characterized in that: one end on frame (1) is equipped with water tank (17), and the output of water tank (17) is equipped with force (forcing) pump (18), the output of force (forcing) pump (18) passes through the input intercommunication of water pipe and water course, the export of water course leads to pipe and water tank (17) intercommunication.
5. The engine earth orbit satellite internet of things monitoring system of claim 4, wherein: the inside of controller (3) is equipped with treater (19), earth orbit satellite communication module (20) and signal receiver (21), the signal output part of temperature sensor (13) and flowmeter (12) all passes through wire and treater (19) electric connection, the output and earth orbit satellite communication module (20) electric connection of treater (19), earth orbit satellite communication module (20) and earth orbit satellite wireless communication transmit for control terminal, signal receiver (21) receive control terminal's instruction and with instruction transmission for treater (19), and the control end of treater (19) with solenoid valve (11) and force (forcing) pump (18) electric connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020778484.3U CN212106082U (en) | 2020-05-12 | 2020-05-12 | Engine ground orbit satellite internet of things monitoring system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020778484.3U CN212106082U (en) | 2020-05-12 | 2020-05-12 | Engine ground orbit satellite internet of things monitoring system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212106082U true CN212106082U (en) | 2020-12-08 |
Family
ID=73617150
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020778484.3U Expired - Fee Related CN212106082U (en) | 2020-05-12 | 2020-05-12 | Engine ground orbit satellite internet of things monitoring system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212106082U (en) |
-
2020
- 2020-05-12 CN CN202020778484.3U patent/CN212106082U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111465274B (en) | Single-cabinet modular server liquid cooling system and control method thereof | |
| CN202127079U (en) | Water-cooling system of power battery pack of electric automobile based on thermoelectric cooling | |
| CN103840569A (en) | Stator module and magnetic force generating member thereof | |
| CN107492922A (en) | A kind of charging module and the charger using the charging module | |
| CN113053682B (en) | Air-cooled air pipe, ventilation housing and multipoint cooling device for circuit breaker | |
| CN112421147A (en) | Heat collecting and dissipating integrated power battery pack heat management system device | |
| CN111010846A (en) | Heat exchanger substrate of plate-type frequency converter, heat exchanger, frequency converter and automatic temperature adjusting method of frequency converter | |
| CN212106082U (en) | Engine ground orbit satellite internet of things monitoring system | |
| CN201365188Y (en) | Totally sealed water-cooling type rectifying power supply device for processing metal surface | |
| CN107172854A (en) | Vehicle-mounted integrated controller cooling system based on plate-fin heat pipe radiator | |
| CN210865779U (en) | Transformer cooling device | |
| CN113587997A (en) | Large-scale transformer loss utilization device | |
| CN114039124A (en) | Power battery multistage heat dissipation system based on magnetic refrigeration effect and control method | |
| CN106301008B (en) | A kind of water-cooling frequency converter rectification module structure | |
| CN113540616A (en) | Battery thermal management system based on gravity heat pipe cooling and control method | |
| CN112549994A (en) | Power system with cooling assembly for hydrogen energy fuel cell automobile and control method | |
| CN212411140U (en) | CPU-imitating radiator | |
| CN214625179U (en) | Novel double-water inlet and outlet liquid cooling plate assembly | |
| CN215672423U (en) | Cooling water heat exchange system of emergency diesel generating set | |
| CN220985545U (en) | Water-cooling high-frequency synchronous rectification switching power supply | |
| CN214152999U (en) | Heat collecting and dissipating integrated power battery pack heat management system device | |
| CN219303714U (en) | Fuel cell thermal management system for hydrogen fuel cell passenger car | |
| CN218470932U (en) | Integral type lithium cell partial volume equipment | |
| CN210006863U (en) | liquid cooling device and battery module liquid cooling system | |
| CN210898903U (en) | Device for installing high-low voltage conversion circuit |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201208 |