CN114228436A - Cockpit temperature control system, control method and equipment thereof - Google Patents
Cockpit temperature control system, control method and equipment thereof Download PDFInfo
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- CN114228436A CN114228436A CN202111438928.4A CN202111438928A CN114228436A CN 114228436 A CN114228436 A CN 114228436A CN 202111438928 A CN202111438928 A CN 202111438928A CN 114228436 A CN114228436 A CN 114228436A
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- 238000000034 method Methods 0.000 title claims abstract description 41
- 238000010438 heat treatment Methods 0.000 claims abstract description 68
- 238000009423 ventilation Methods 0.000 claims description 21
- 238000004590 computer program Methods 0.000 claims description 20
- 238000001816 cooling Methods 0.000 claims description 11
- 238000005286 illumination Methods 0.000 claims description 5
- 230000007613 environmental effect Effects 0.000 abstract description 10
- 230000008878 coupling Effects 0.000 abstract description 7
- 238000010168 coupling process Methods 0.000 abstract description 7
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- 230000008569 process Effects 0.000 description 5
- 230000005540 biological transmission Effects 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000011217 control strategy Methods 0.000 description 3
- 230000007935 neutral effect Effects 0.000 description 3
- 230000003287 optical effect Effects 0.000 description 3
- 238000005057 refrigeration Methods 0.000 description 3
- 230000006399 behavior Effects 0.000 description 2
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60H—ARRANGEMENTS OF HEATING, COOLING, VENTILATING OR OTHER AIR-TREATING DEVICES SPECIALLY ADAPTED FOR PASSENGER OR GOODS SPACES OF VEHICLES
- B60H1/00—Heating, cooling or ventilating [HVAC] devices
- B60H1/00642—Control systems or circuits; Control members or indication devices for heating, cooling or ventilating devices
- B60H1/00735—Control systems or circuits characterised by their input, i.e. by the detection, measurement or calculation of particular conditions, e.g. signal treatment, dynamic models
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60H—ARRANGEMENTS OF HEATING, COOLING, VENTILATING OR OTHER AIR-TREATING DEVICES SPECIALLY ADAPTED FOR PASSENGER OR GOODS SPACES OF VEHICLES
- B60H1/00—Heating, cooling or ventilating [HVAC] devices
- B60H1/00271—HVAC devices specially adapted for particular vehicle parts or components and being connected to the vehicle HVAC unit
- B60H1/00285—HVAC devices specially adapted for particular vehicle parts or components and being connected to the vehicle HVAC unit for vehicle seats
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60H—ARRANGEMENTS OF HEATING, COOLING, VENTILATING OR OTHER AIR-TREATING DEVICES SPECIALLY ADAPTED FOR PASSENGER OR GOODS SPACES OF VEHICLES
- B60H1/00—Heating, cooling or ventilating [HVAC] devices
- B60H1/00642—Control systems or circuits; Control members or indication devices for heating, cooling or ventilating devices
- B60H1/00735—Control systems or circuits characterised by their input, i.e. by the detection, measurement or calculation of particular conditions, e.g. signal treatment, dynamic models
- B60H1/0075—Control systems or circuits characterised by their input, i.e. by the detection, measurement or calculation of particular conditions, e.g. signal treatment, dynamic models the input being solar radiation
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60J—WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILAR DEVICES FOR VEHICLES; REMOVABLE EXTERNAL PROTECTIVE COVERINGS SPECIALLY ADAPTED FOR VEHICLES
- B60J1/00—Windows; Windscreens; Accessories therefor
- B60J1/20—Accessories, e.g. wind deflectors, blinds
- B60J1/2011—Blinds; curtains or screens reducing heat or light intensity
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- Power Engineering (AREA)
- Air-Conditioning For Vehicles (AREA)
Abstract
The invention discloses a control system, a control method and equipment for the temperature of a cockpit. The system comprises: a sensor layer and a control layer. The sensor layer comprises an acquisition unit and an execution unit, wherein the acquisition unit comprises an internal temperature sensor, an external temperature sensor and a sunlight sensor, and the execution unit is used for executing corresponding operation according to a control instruction generated by the environmental information; the control layer comprises a control unit and an interface unit, the control unit is used for generating a control instruction according to the environment information, and the interface unit is used for connecting the actuator and the collector. The services in the system interact in a uniform and general way, so as to achieve the purposes of loose coupling, resource sharing and reuse. The temperature control system sets a temperature control scheme through the internal temperature, the external temperature and the sunlight intensity, not only can achieve the aim of accurately controlling the temperature, but also can reduce the energy consumed by a heating device and a refrigerating device and reduce the noise generated during working.
Description
Technical Field
The present disclosure relates to the field of cockpit temperature control, and more particularly, to a cockpit temperature control system, a control method, and an apparatus thereof.
Background
In an existing cockpit temperature control system, a user manually adjusts a set temperature, a deviation between the set temperature and an actual temperature is obtained through a temperature sensor in a vehicle, a control instruction is generated based on the deviation, an air conditioner compressor or a heating device is controlled to work, and air is cooled or heated.
The conventional temperature control system is controlled based on a single control source of the temperature in the vehicle, and when the vehicle is irradiated by strong light, although the temperature in the vehicle may be lower than a set temperature, the sensible temperature is high, and the driver may feel that the temperature is too high and discomfort is caused to the driver by heating again. The sensor and the executive component of the current cockpit temperature control system are packaged as a system, and if the sensor or the executive component with the same model can only be replaced during maintenance, the inconvenience is brought to the maintenance and the function upgrade.
Disclosure of Invention
In this summary, concepts in a simplified form are introduced that are further described in the detailed description. This summary of the invention is not intended to identify key features or essential features of the claimed subject matter, nor is it intended to be used as an aid in determining the scope of the claimed subject matter.
In order to at least partially solve the problems of reasonably controlling the temperature in the vehicle and the complexity of upgrading and maintaining the vehicle, the invention provides a cockpit temperature control system in a first aspect, which comprises:
a sensor layer and a control layer;
the sensor layer comprises an acquisition unit and an execution unit, wherein the acquisition unit comprises an internal temperature sensor, an external temperature sensor and a sunlight sensor, the acquisition unit is used for acquiring internal and external environment information of the vehicle, the execution unit comprises a heating device and a refrigerating device, and the execution unit is used for executing corresponding operation according to a control instruction generated by the environment information;
the control layer includes a control unit and an interface unit, wherein the control unit is configured to generate the control instruction according to the environment information, and the interface unit is configured to connect the actuator and the collector.
Optionally, the system further includes a coordination layer, the coordination layer includes a temperature linkage unit, and the temperature linkage unit controls the operating states of the systems other than the cockpit temperature control system according to the operating state of the cockpit temperature control system.
Optionally, the other systems include a sun shade system.
Optionally, the other systems described above include a seat ventilation/heating system.
In a second aspect, the present invention further provides a method for controlling a temperature of a cabin, which is applied to any one of the cabin temperature control systems of the first aspect, and includes:
acquiring the internal temperature, the external temperature and the sunlight illumination intensity of the vehicle;
controlling the operating state of the heating device and/or the cooling device based on the internal temperature, the external temperature, and the solar light intensity.
Optionally, the method further includes:
and controlling the working state of the sun-shading system according to the working state of the heating device and/or the refrigerating device.
Optionally, the method further includes:
and controlling the working state of the seat ventilation/heating system according to the working state of the heating device and/or the refrigerating device.
In a third aspect, the present invention further provides a cockpit temperature control device, including:
an acquisition unit for acquiring an inside temperature, an outside temperature, and a sunlight intensity of the vehicle;
and a control unit for controlling the operating state of the heating device and/or the cooling device based on the internal temperature, the external temperature, and the solar light intensity.
In a fourth aspect, the present invention further provides an electronic device, including: a memory, a processor and a computer program stored in the memory and executable on the processor, wherein the processor is configured to implement the steps of the cabin temperature control method according to any one of the second aspect when the computer program stored in the memory is executed.
In a fifth aspect, the present invention further provides a computer-readable storage medium, on which a computer program is stored, which, when being executed by a processor, carries out the steps of the cabin temperature control method of any one of the above aspects of the second aspect.
In summary, the cockpit temperature control system proposed in this application includes: a sensor layer and a control layer; the sensor layer comprises an acquisition unit and an execution unit, wherein the acquisition unit comprises an internal temperature sensor, an external temperature sensor and a sunlight sensor, the acquisition unit is used for acquiring internal and external environment information of the vehicle, the execution unit comprises a heating device and a refrigerating device, and the execution unit is used for executing corresponding operation according to a control instruction generated by the environment information; the control layer comprises a control unit and an interface unit, wherein the control unit is used for generating a control instruction according to the environment information, and the interface unit is used for connecting the actuator and the collector. The cockpit temperature control system provided by this embodiment is divided into a sensor layer and a control layer, the sensor layer is only responsible for collecting environmental information and executing actions according to control instructions, the control layer includes control programs corresponding to corresponding functions, the control programs generate the control instructions according to the environmental information, the sensor layer and the control layer are linked through a good interface and contract, and the interface is defined in a neutral manner and is independent of a hardware platform, an operating system and a programming language for realizing services. The service in the system can be interacted in a uniform and universal mode, and the data in the cockpit temperature control system can be used for other systems to execute other functions, so that the purposes of loose coupling and resource sharing and reusing are achieved. The temperature control system sets a temperature control scheme through the internal temperature, the external temperature and the sunlight intensity, not only can achieve the aim of accurately controlling the temperature, but also can reduce the energy consumed by a heating device and a refrigerating device and reduce the noise generated during working.
The proposed cockpit temperature control system of the present invention, and other advantages, objects, and features of the present invention will be set forth in part in the description which follows and in part will become apparent to those having ordinary skill in the art upon examination of the following or may be learned from practice of the invention.
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Various other advantages and benefits will become apparent to those of ordinary skill in the art upon reading the following detailed description of the preferred embodiments. The drawings are only for purposes of illustrating the preferred embodiments and are not to be construed as limiting the specification. Also, like reference numerals are used to refer to like parts throughout the drawings. In the drawings:
fig. 1 is a schematic structural diagram of a cockpit temperature control system according to an embodiment of the present application;
FIG. 2 is a schematic flow chart of a method for controlling a temperature of a cockpit according to an embodiment of the present disclosure;
FIG. 3 is a schematic structural diagram of a cockpit temperature control device according to an embodiment of the present disclosure;
fig. 4 is a schematic structural diagram of an electronic device according to an embodiment of the present application.
Detailed Description
The embodiment of the application provides a control system, a control method and equipment for the temperature of a cockpit. The cockpit temperature control system provided by this embodiment is divided into a sensor layer and a control layer, the sensor layer is only responsible for collecting environmental information and executing actions according to control instructions, the control layer includes control programs corresponding to corresponding functions, the control programs generate the control instructions according to the environmental information, the sensor layer and the control layer are linked through a good interface and contract, and the interface is defined in a neutral manner and is independent of a hardware platform, an operating system and a programming language for realizing services. The service in the system can be interacted in a uniform and universal mode, and the data in the cockpit temperature control system can be used for other systems to execute other functions, so that the purposes of loose coupling and resource sharing and reusing are achieved. The temperature control system sets a temperature control scheme through the internal temperature, the external temperature and the sunlight intensity, not only can achieve the aim of accurately controlling the temperature, but also can reduce the energy consumed by a heating device and a refrigerating device and reduce the noise generated during working.
The terms "first," "second," "third," "fourth," and the like in the description and in the claims of the present application and in the drawings described above, if any, are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It will be appreciated that the data so used may be interchanged under appropriate circumstances such that the embodiments described herein may be practiced otherwise than as specifically illustrated or described herein. Furthermore, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed, but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus. 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.
In a first aspect, the present disclosure is directed to a cockpit temperature control system.
Referring to fig. 1, fig. 1 is a view illustrating a temperature control system for a cockpit according to an embodiment of the present disclosure.
In some examples, a cockpit temperature control system is presented, comprising:
a sensor layer and a control layer;
the sensor layer comprises an acquisition unit and an execution unit, wherein the acquisition unit comprises an internal temperature sensor, an external temperature sensor and a sunlight sensor, the acquisition unit is used for acquiring internal and external environment information of the vehicle, the execution unit comprises a heating device and a refrigerating device, and the execution unit is used for executing corresponding operation according to a control instruction generated by the environment information;
specifically, the collection unit includes inside temperature sensor, outside temperature sensor and solar sensor, can record the inside and outside temperature of vehicle according to inside temperature sensor and outside temperature sensor, can measure the intensity of sunshine according to solar sensor, according to inside and outside temperature and sunshine intensity, formulates temperature control scheme, control heating device and refrigerating plant's operating condition. The inlet flow of natural wind can be adjusted according to ideal temperature by measuring the internal and external temperatures; the influence of the sunlight intensity on the temperature is determined by a method of checking historical data, and the working states of the heating device and the refrigerating device are controlled according to the influence. The temperature control strategy can not only achieve the aim of accurately controlling the temperature, but also reduce the energy consumed by a heating device and a refrigerating device and reduce the noise generated during the operation.
It will be appreciated that the refrigeration unit includes an electrically powered compressor and its associated piping and valves. Accordingly, the heating means comprises an electric heater and associated piping and valves, which may include: one or more of a three-way proportional valve, an electronic expansion valve, a four-way control valve and the like.
The sensor layer is mainly responsible for data transmission with the sensor, determining a transmission mode and a matching protocol (such as PWM and LIN) so as to acquire complete raw data of the sensor and establish a uniform interface for outputting or calling the raw data of the sensor to the outside. Meanwhile, the hardware platform supports LIN and PWM transmission mode sensor/actuator connection, when iteration is carried out or the platform is switched to need to replace the sensor/actuator, the sensor layer software component can be adapted to acquire the replaced complete sensor original data only by updating a sensor data transmission protocol.
The control layer includes a control unit and an interface unit, wherein the control unit is configured to generate the control instruction according to the environment information, and the interface unit is configured to connect the actuator and the collector.
Specifically, the interface unit may include a cockpit temperature sensor interface and an actuator interface, and the corresponding interface and its corresponding collector and actuator are connected by a generalized service interface to form a cockpit temperature control hardware system. The control unit is stored with control programs with corresponding functions, and calls the corresponding control programs to generate corresponding control instructions according to the environmental information collected by the collector, so as to control the working states of the corresponding heating devices and/or refrigerating devices.
It is understood that the interface unit may not be limited to the above-mentioned interfaces, and other interfaces may be reserved for use in upgrading the vehicle cabin temperature control system.
In summary, the cockpit temperature control system provided in this embodiment is divided into a sensor layer and a control layer, the sensor layer is only responsible for collecting environmental information and executing actions according to a control instruction, the control layer includes a control program corresponding to a corresponding function, the control program generates the control instruction according to the environmental information, the sensor layer and the control layer are linked through a good interface and a contract, and the interface is defined in a neutral manner and is independent of a hardware platform, an operating system, and a programming language for implementing services. The service in the system can be interacted in a uniform and universal mode, and the data in the cockpit temperature control system can be used for other systems to execute other functions, so that the purposes of loose coupling and resource sharing and reusing are achieved. The temperature control system sets a temperature control scheme through the internal temperature, the external temperature and the sunlight intensity, not only can achieve the aim of accurately controlling the temperature, but also can reduce the energy consumed by a heating device and a refrigerating device and reduce the noise generated during working.
In some examples, the system further comprises a coordination layer, wherein the coordination layer comprises a temperature linkage unit, and the temperature linkage unit controls the working states of other systems except the cockpit temperature control system according to the working state of the cockpit temperature control system.
Specifically, the system can further comprise a coordination layer, the coordination layer comprises a temperature linkage unit, the temperature linkage unit controls the working states of other systems except the cockpit temperature control system according to the working state of the cockpit temperature control system, multi-system linkage is achieved, and the temperature control of the vehicle cockpit is more intelligent.
In conclusion, through the temperature linkage unit of the coordination layer, other systems can be controlled to work according to the working state of the temperature system of the cockpit, so that a more specific and comfortable temperature control strategy is provided for a user.
In some examples, the other systems described above include a sun shade system.
Specifically, other systems linked to the cockpit temperature control system may include a sunshade system that controls the intensity of light emitted into the cockpit by changing the open and closed states of the blinds. The temperature linkage unit is according to heating device and/or refrigerating plant's operating condition among the cockpit temperature control system, need cool down or heat when acquireing the vehicle this moment to and the intensity of the sunshine that the demand of the degree and the heating of cooling and sunshine sensor acquireed, thereby the state of opening and shutting of control sunshade screen. For example: when the sunlight sensor measures that the illumination intensity of sunlight is very strong and the temperature in the vehicle is higher than the comfortable temperature, the temperature linkage unit controls the refrigerating device of the cockpit to work and controls the sunshade curtain to be completely unfolded. The sunlight emitted into the cockpit is reduced while cold air is conveyed to the cockpit, so that the cockpit is rapidly cooled. When the temperature is reduced to the temperature close to the comfortable temperature, the refrigerating device is controlled to reduce the power, and the temperature of the vehicle is reduced by means of the residual heat of the refrigerating device.
In conclusion, the temperature linkage unit controls the working state of the heating device and/or the refrigerating device of the temperature control system and the opening and closing state of the sunshade curtain through the environmental information acquired by the cockpit temperature system, so that the temperature in the vehicle is controlled together, and the energy consumption can be reduced while the temperature is controlled quickly.
In some examples, the other systems described above include a seat ventilation/heating system.
In particular, other systems that are linked to the cabin temperature control system may include a seat ventilation/heating system. And when the temperature control system of the cab detects that the internal environment temperature is lower than the comfortable temperature, the heating device is started to convey heated air into the cab. Meanwhile, the temperature linkage unit judges that the temperature in the cockpit is lower at the moment according to the heating behavior of the cockpit temperature control system, and controls the seat ventilation/heating system to start the seat heating function, so that linkage heating of air and the seat is realized, and a more comfortable environment is provided for a driver.
It will be appreciated that the temperature linkage unit may also activate the seat ventilation function in response to operation of the refrigeration unit when the temperature within the cabin is high.
Further, the seat ventilation/heating system can be controlled to open different ventilation/heating gears by presetting the air temperature output by the cockpit temperature control system, when the heating device works, the higher the power of the heating device is, the higher the seat heating power is, and when the cooling device works, the higher the cooling device is, and the higher the seat ventilation power is.
In conclusion, the temperature linkage unit controls the working state of the seat ventilation/heating system by acquiring the working state of the heating device and/or the refrigerating device of the cockpit temperature control system, so that the linkage of the temperature control system and the seat ventilation/heating system is realized, and a more comfortable driving environment is provided for users.
Referring to fig. 2, fig. 2 is a schematic flow chart of a method for controlling a temperature of a cockpit according to an embodiment of the present application.
In some examples, a cockpit temperature control method is provided, comprising:
s210, acquiring the internal temperature, the external temperature and the sunlight illumination intensity of the vehicle;
specifically, the temperature inside and outside the vehicle can be measured by the internal temperature sensor and the external temperature sensor, and the intensity of sunlight can be measured according to the sunlight sensor.
S220, controlling the operation state of the heating device and/or the cooling device based on the internal temperature, the external temperature, and the solar light intensity.
Specifically, the inlet flow of natural wind can be adjusted according to the ideal temperature by measuring the internal and external temperatures; the influence of the sunlight intensity on the temperature is determined by a method of checking historical data, and the working states of the heating device and the refrigerating device are controlled according to the influence.
In summary, the temperature control strategy can not only achieve the purpose of accurately controlling the temperature, but also reduce the energy consumed by the heating device and the refrigerating device and reduce the noise generated during the operation.
In some examples, the method further comprises:
and controlling the working state of the sun-shading system according to the working state of the heating device and/or the refrigerating device.
Specifically, according to the working state of a heating device and/or a refrigerating device in the cockpit temperature control system, the temperature of the vehicle needs to be reduced or heated at the moment, the temperature reduction degree and the heating requirement are met, and the sunlight intensity obtained by the sunlight sensor is obtained, so that the opening and closing state of the sunshade curtain is controlled. For example: when the sunlight sensor measures that the illumination intensity of sunlight is very strong and the temperature in the vehicle is higher than the comfortable temperature, the temperature linkage unit controls the refrigerating device of the cockpit to work and controls the sunshade curtain to be completely unfolded. The sunlight emitted into the cockpit is reduced while cold air is conveyed to the cockpit, so that the cockpit is rapidly cooled. When the temperature is reduced to the temperature close to the comfortable temperature, the refrigerating device is controlled to reduce the power, and the temperature of the vehicle is reduced by means of the residual heat of the refrigerating device.
In conclusion, the working state of the heating device and/or the refrigerating device of the temperature control system and the opening and closing state of the sunshade curtain are controlled through the environmental information acquired by the cockpit temperature system, the temperature in the vehicle is controlled together, and the energy consumption can be reduced while the temperature is controlled rapidly.
In some examples, the method further comprises:
and controlling the working state of the seat ventilation/heating system according to the working state of the heating device and/or the refrigerating device.
Specifically, when the cabin temperature control system detects that the internal environment temperature is lower than the comfortable temperature, the heating device is started to convey heated air into the cabin. Meanwhile, the temperature linkage unit judges that the temperature in the cockpit is lower at the moment according to the heating behavior of the cockpit temperature control system, and controls the seat ventilation/heating system to start the seat heating function, so that linkage heating of air and the seat is realized, and a more comfortable environment is provided for a driver.
It will be appreciated that the temperature linkage unit may also activate the seat ventilation function in response to operation of the refrigeration unit when the temperature within the cabin is high.
Further, the seat ventilation/heating system can be controlled to open different ventilation/heating gears by presetting the air temperature output by the cockpit temperature control system, when the heating device works, the higher the power of the heating device is, the higher the seat heating power is, and when the cooling device works, the higher the cooling device is, and the higher the seat ventilation power is.
In conclusion, the working state of the heating device and/or the refrigerating device of the cockpit temperature control system is obtained, and the working state of the seat ventilation/heating system is controlled, so that linkage of the temperature control system and the seat ventilation/heating system is realized, and a more comfortable driving environment is provided for a user.
In a third aspect, the invention further provides a cockpit temperature control device.
Referring to fig. 2, an embodiment of a cockpit temperature control device in an embodiment of the present application may include:
an acquisition unit 21 configured to acquire an internal temperature, an external temperature, and a sunlight intensity of the vehicle;
a control unit 22 for controlling the operation state of the heating device and/or the cooling device based on the internal temperature, the external temperature and the solar light intensity.
As shown in fig. 3, the embodiment of the present application further provides an electronic device 300, which includes a memory 310, a processor 320 and a computer program 311 stored on the memory 320 and executable on the processor, wherein when the processor 320 executes the computer program 311, the steps of any one of the methods for controlling the temperature of the cockpit are implemented.
Since the electronic device described in this embodiment is a device used for implementing a high-speed navigation control apparatus in this embodiment, based on the method described in this embodiment, a person skilled in the art can understand a specific implementation manner of the electronic device of this embodiment and various variations thereof, so that how to implement the method in this embodiment by the electronic device is not described in detail herein, and as long as the person skilled in the art implements the device used for implementing the method in this embodiment, the device falls within the scope of protection intended by this application.
In a specific implementation, the computer program 311 may implement any of the embodiments corresponding to fig. 3 when executed by a processor.
It should be noted that, in the foregoing embodiments, the descriptions of the respective embodiments have respective emphasis, and reference may be made to relevant descriptions of other embodiments for parts that are not described in detail in a certain embodiment.
As will be appreciated by one skilled in the art, embodiments of the present application may be provided as a method, system, or computer program product. Accordingly, the present application may take the form of an entirely hardware embodiment, an entirely software embodiment or an embodiment combining software and hardware aspects. Furthermore, the present application may take the form of a computer program product embodied on one or more computer-usable storage media (including, but not limited to, disk storage, CD-ROM, optical storage, and the like) having computer-usable program code embodied therein.
The present application is described with reference to flowchart illustrations and/or block diagrams of methods, apparatus (systems), and computer program products according to embodiments of the application. It will be understood that each flow and/or block of the flow diagrams and/or block diagrams, and combinations of flows and/or blocks in the flow diagrams and/or block diagrams, can be implemented by computer program instructions. These computer program instructions may be provided to a processor of a general purpose computer, special purpose computer, embedded computer, or other programmable data processing apparatus to produce a machine, such that the instructions, which execute via the processor of the computer or other programmable data processing apparatus, create means for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be stored in a computer-readable memory that can direct a computer or other programmable data processing apparatus to function in a particular manner, such that the instructions stored in the computer-readable memory produce an article of manufacture including instruction means which implement the function specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be loaded onto a computer or other programmable data processing apparatus to cause a series of operational steps to be performed on the computer or other programmable apparatus to produce a computer implemented process such that the instructions which execute on the computer or other programmable apparatus provide steps for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
Embodiments of the present application further provide a computer program product, where the computer program product includes computer software instructions, and when the computer software instructions are run on a processing device, the processing device is caused to execute the procedure in the cockpit temperature control method in the embodiment corresponding to fig. 2.
The computer program product includes one or more computer instructions. The procedures or functions according to the embodiments of the present application are all or partially generated when the computer program instructions are loaded and executed on a computer. The computer may be a general purpose computer, a special purpose computer, a network of computers, or other programmable device. The computer instructions may be stored on a computer readable storage medium or transmitted from one computer readable storage medium to another computer readable storage medium, for example, the computer instructions may be transmitted from one website, computer, server, or data center to another website, computer, server, or data center via wire (e.g., coaxial cable, fiber optic, Digital Subscriber Line (DSL)) or wireless (e.g., infrared, wireless, microwave, etc.). A computer-readable storage medium may be any available medium that a computer can store or a data storage device, such as a server, a data center, etc., that is integrated with one or more available media. The usable medium may be a magnetic medium (e.g., floppy disk, hard disk, magnetic tape), an optical medium (e.g., DVD), or a semiconductor medium (e.g., Solid State Disk (SSD)), among others.
It is clear to those skilled in the art that, for convenience and brevity of description, the specific working processes of the above-described systems, apparatuses and units may refer to the corresponding processes in the foregoing method embodiments, and are not described herein again.
In the several embodiments provided in the present application, it should be understood that the disclosed system, apparatus and method may be implemented in other manners. For example, the above-described apparatus embodiments are merely illustrative, and for example, a division of a unit is merely a logical division, and an actual implementation may have another division, for example, a plurality of units or components may be combined or integrated into another system, or some features may be omitted, or not executed. In addition, the shown or discussed mutual coupling or direct coupling or communication connection may be an indirect coupling or communication connection through some interfaces, devices or units, and may be in an electrical, mechanical or other form.
Units described as separate parts may or may not be physically separate, and parts displayed as units may or may not be physical units, may be located in one place, or may be distributed on a plurality of network units. Some or all of the units can be selected according to actual needs to achieve the purpose of the solution of the embodiment.
In addition, functional units in the embodiments of the present application may be integrated into one processing unit, or each unit may exist alone physically, or two or more units are integrated into one unit. The integrated unit can be realized in a form of hardware, and can also be realized in a form of a software functional unit.
The integrated unit, if implemented in the form of a software functional unit and sold or used as a stand-alone product, may be stored in a computer readable storage medium. Based on such understanding, the technical solution of the present application may be substantially implemented or contributed to by the prior art, or all or part of the technical solution may be embodied in a software product, which is stored in a storage medium and includes instructions for causing a computer device (which may be a personal computer, a server, or a network device) to execute all or part of the steps of the method of the embodiments of the present application. And the aforementioned storage medium includes: various media capable of storing program codes, such as a usb disk, a removable hard disk, a Read-Only Memory (ROM), a Random Access Memory (RAM), a magnetic disk, or an optical disk.
The above embodiments are only used to illustrate the technical solutions of the present application, and not to limit the same; although the present application has been described in detail with reference to the foregoing embodiments, it should be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions in the embodiments of the present application.
Claims (10)
1. A cockpit temperature control system for a vehicle, comprising:
a sensor layer and a control layer;
the sensor layer comprises an acquisition unit and an execution unit, wherein the acquisition unit comprises an internal temperature sensor, an external temperature sensor and a sunlight sensor, the acquisition unit is used for acquiring internal and external environment information of the vehicle, the execution unit comprises a heating device and a refrigerating device, and the execution unit is used for executing corresponding operation according to a control instruction generated by the environment information;
the control layer comprises a control unit and an interface unit, wherein the control unit is used for generating the control instruction according to the environment information, and the interface unit is used for connecting the actuator and the collector.
2. The system of claim 1, further comprising a coordination layer comprising a temperature linkage unit that controls the operating state of systems other than the cockpit temperature control system according to the operating state of the cockpit temperature control system.
3. The system of claim 2, wherein the other system comprises a sun shade system.
4. The system of claim 2, wherein the other system comprises a seat ventilation/heating system.
5. A cabin temperature control method for use in the cabin temperature control system according to any one of claims 1 to 4, comprising:
acquiring the internal temperature, the external temperature and the sunlight illumination intensity of the vehicle;
controlling an operating state of the heating device and/or the cooling device based on the interior temperature, the exterior temperature, and the solar irradiance.
6. The method of claim 5, further comprising:
and controlling the working state of the sun shading system according to the working state of the heating device and/or the refrigerating device.
7. The method of claim 5, further comprising:
controlling the working state of the seat ventilation/heating system according to the working state of the heating device and/or the refrigerating device.
8. A cabin temperature control apparatus for use in the cabin temperature control system according to any one of claims 1 to 4, comprising:
an acquisition unit for acquiring an interior temperature, an exterior temperature, and a sunlight intensity of the vehicle;
a control unit for controlling the working state of the heating device and/or the cooling device based on the internal temperature, the external temperature and the sunlight intensity.
9. An electronic device comprising a memory, a processor, wherein the processor is configured to implement the steps of the cabin temperature control method according to any one of claims 5 to 7 when executing a computer program stored in the memory.
10. A computer-readable storage medium having stored thereon a computer program, characterized in that: the computer program when being executed by a processor realizes the steps of the method for controlling the temperature of a cockpit as claimed in any one of claims 5 to 7.
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| CN202111438928.4A CN114228436A (en) | 2021-11-30 | 2021-11-30 | Cockpit temperature control system, control method and equipment thereof |
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| CN202111438928.4A CN114228436A (en) | 2021-11-30 | 2021-11-30 | Cockpit temperature control system, control method and equipment thereof |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2024125496A3 (en) * | 2022-12-13 | 2024-08-08 | 蔚来移动科技有限公司 | Method for controlling temperature inside driving device, and driving device and medium |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170246930A1 (en) * | 2016-02-25 | 2017-08-31 | Toyota Motor Engineering & Manufacturing North America, Inc. | Vehicle automatic defrost system and method |
| US20180134116A1 (en) * | 2016-11-11 | 2018-05-17 | International Business Machines Corporation | Facilitating personalized vehicle occupant comfort |
| CN207670163U (en) * | 2017-12-12 | 2018-07-31 | 安徽江淮汽车集团股份有限公司 | Environmental control system in the sunshade control system of vehicle, mobile terminal and vehicle |
| CN110696587A (en) * | 2019-09-24 | 2020-01-17 | 中国第一汽车股份有限公司 | Air conditioner control method and system and vehicle |
| US20200132352A1 (en) * | 2018-10-31 | 2020-04-30 | International Business Machines Corporation | Internal climate control system |
| CN111216514A (en) * | 2020-01-19 | 2020-06-02 | 东风小康汽车有限公司重庆分公司 | Method, device and system for automatically adjusting temperature in vehicle |
| CN111376676A (en) * | 2020-03-23 | 2020-07-07 | 长城汽车股份有限公司 | Vehicle air conditioner control method and system |
| CN213441973U (en) * | 2020-10-27 | 2021-06-15 | 东风汽车集团有限公司 | Humiture automatically regulated type vehicle |
| CN113060084A (en) * | 2021-04-28 | 2021-07-02 | 中国第一汽车股份有限公司 | Method, device, server and storage medium for controlling driving environment of vehicle passenger compartment |
-
2021
- 2021-11-30 CN CN202111438928.4A patent/CN114228436A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170246930A1 (en) * | 2016-02-25 | 2017-08-31 | Toyota Motor Engineering & Manufacturing North America, Inc. | Vehicle automatic defrost system and method |
| US20180134116A1 (en) * | 2016-11-11 | 2018-05-17 | International Business Machines Corporation | Facilitating personalized vehicle occupant comfort |
| CN207670163U (en) * | 2017-12-12 | 2018-07-31 | 安徽江淮汽车集团股份有限公司 | Environmental control system in the sunshade control system of vehicle, mobile terminal and vehicle |
| US20200132352A1 (en) * | 2018-10-31 | 2020-04-30 | International Business Machines Corporation | Internal climate control system |
| CN110696587A (en) * | 2019-09-24 | 2020-01-17 | 中国第一汽车股份有限公司 | Air conditioner control method and system and vehicle |
| CN111216514A (en) * | 2020-01-19 | 2020-06-02 | 东风小康汽车有限公司重庆分公司 | Method, device and system for automatically adjusting temperature in vehicle |
| CN111376676A (en) * | 2020-03-23 | 2020-07-07 | 长城汽车股份有限公司 | Vehicle air conditioner control method and system |
| CN213441973U (en) * | 2020-10-27 | 2021-06-15 | 东风汽车集团有限公司 | Humiture automatically regulated type vehicle |
| CN113060084A (en) * | 2021-04-28 | 2021-07-02 | 中国第一汽车股份有限公司 | Method, device, server and storage medium for controlling driving environment of vehicle passenger compartment |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2024125496A3 (en) * | 2022-12-13 | 2024-08-08 | 蔚来移动科技有限公司 | Method for controlling temperature inside driving device, and driving device and medium |
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