CN114791749B - Isolation airtight capsule cabin for simulating and experiencing local weather conditions - Google Patents

Isolation airtight capsule cabin for simulating and experiencing local weather conditions Download PDF

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Publication number
CN114791749B
CN114791749B CN202111615501.7A CN202111615501A CN114791749B CN 114791749 B CN114791749 B CN 114791749B CN 202111615501 A CN202111615501 A CN 202111615501A CN 114791749 B CN114791749 B CN 114791749B
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cabin
capsule
air
shell
weather
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CN114791749A (en
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彭聪
王鑫
张驰
周拓阳
李思
梁晋
张良
余阳
廖镇
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China Institute Of Marine Technology & Economy
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China Institute Of Marine Technology & Economy
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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D27/00Simultaneous control of variables covered by two or more of main groups G05D1/00 - G05D25/00
    • G05D27/02Simultaneous control of variables covered by two or more of main groups G05D1/00 - G05D25/00 characterised by the use of electric means

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Abstract

The invention provides an isolated closed capsule cabin for simulating experience of local weather conditions, which comprises the following components: the capsule cabin body 100, the destination weather forecast value formatting input module 200, the cabin temperature automatic control module 300, the cabin humidity automatic control module 400, the cabin air pressure automatic control module 500, the cabin wind speed and direction control module 600, the human body multiple physiological parameter monitoring module 700 and the capsule cabin door forbidden module 800. According to the technical scheme, the tactile experience environment of the local weather information of the destination can be provided, real-time objective measurement and evaluation are provided for physiological response of the user in the weather condition experience process, and personalized prevention and adaptation measures for the weather condition change of the destination are provided.

Description

Isolation airtight capsule cabin for simulating and experiencing local weather conditions
Technical Field
The invention belongs to the technical field of human-machine environment system engineering, and particularly relates to an isolated closed capsule cabin for simulating experience of local weather conditions.
Background
In deep open sea navigation, after personnel adapt to the stable indoor living environment of a cabin which is isolated and sealed for a long time, when a ship arrives at a destination and goes out of the cabin, the human body is immediately exposed to the natural weather environment outside the cabin of the destination which has great difference with the stable indoor environment, and the inadaptation of physical functions is easily caused.
The hysteresis of the human body adapting to the new environment causes the unfavorable conditions of subhealth and even sudden diseases and the like caused by the inadequate taking of water and soil and the mutation of body metabolism stress, so that the working capacity of the personnel is reduced and even absent, and the method brings important hidden trouble for the continuous operation of professional teams. Although the current information communication technology is developed, people can extract and acquire the local weather environment of a destination through network communication, the existing weather forecast and the local weather environment are presented to a user in the form of numerical text or view information. It is still difficult for the user to accurately perceive the weather conditions such as air temperature and humidity, air pressure, wind direction and wind speed, etc. only through visual text or image information, because such weather information is perceived and evaluated directly by the touch of the body surface skin in essence. Therefore, destination weather information prediction for the long-distance personnel should be given more direct tactile experience environments so that users can make accurate health risk assessment in advance according to direct experience of the users. However, health risks associated with abrupt changes in weather conditions such as air temperature and humidity, air pressure, wind direction and wind speed are severely dependent on previous experience. The device resides in an isolated closed cabin with stable cabin environment for a long time, and operators just lack experience of coping with weather condition changes, so that the device is unfavorable for making relatively accurate subjective assessment on self tolerance.
Therefore, how to provide an isolated closed capsule cabin for simulating and experiencing local weather conditions, provide a tactile experience environment for local weather information of a destination, provide real-time objective measurement and evaluation for physiological reactions of users in the weather condition experience process, and provide personalized preventive and adaptive measures for coping with the change of the weather conditions of the destination has become a technical problem to be solved urgently.
Disclosure of Invention
The embodiment of the invention provides an isolated closed capsule cabin for simulating local weather conditions, which can provide a tactile experience environment of local weather information of a destination, provide real-time objective measurement and evaluation for physiological response of a user in the weather condition experience process, and provide personalized prevention and adaptation measures for the change of the weather conditions of the destination.
In an embodiment of the present invention, an isolated and sealed capsule for simulating experience of local weather conditions includes: the capsule cabin body 100, the destination weather forecast value formatting input module 200, the cabin temperature automatic control module 300, the cabin humidity automatic control module 400, the cabin air pressure automatic control module 500, the cabin wind speed and direction control module 600, the human body multiple physiological parameter monitoring module 700 and the capsule cabin door forbidden module 800.
Capsule body 100, comprising: the capsule cabin outer layer fixing shell 1, the condenser annular air outlet 2, the condensate overflow hole 3, the annular lighting lamp belt 4, the heating filter screen 5, the upper air inlet and outlet 6 of the inner cabin shell, the refrigerant evaporator 7, the interlayer movable cabin shell 8, the inner layer fixing cabin shell 9, the air booster pump 10, the pneumatic electromagnetic valve 11, the lower air inlet and outlet 12 of the interlayer movable cabin shell, the lower air inlet and outlet 13 of the inner cabin shell, the cabin standing bottom plate 14, the cabin supporting base 15, the hydraulic lifting table 16, the hydraulic lifting table base 17, the cabin top maintenance inlet end cover 18, the gear motor lifting sleeve 19, the output transmission shaft 20, the cabin air inner circulation driving motor 21, the inner circulation driving motor output shaft 22, the fan blades 23, the condenser lifting sleeve 24, the condenser 25, the air ventilation blower 26, the air ventilation electromagnetic valve 27, the cabin humidifying water mist input hole 28 and the ultrasonic atomization sheet 29.
The destination weather forecast values formatting input module 200 includes: the capsule cabin is externally and centrally controlled by an upper computer 30, a destination weather inquiry terminal 31, a weather forecast value formatting interaction terminal 32, a VR scene database server 33 of weather conditions in all places and an audio-visual integrated VR helmet display 34; the outdoor central control upper computer 30 searches the forecast information of environmental noise, weather, air temperature, humidity, air pressure, visibility, wind power and wind direction of the local weather of the simulated subject destination by using the destination weather inquiry terminal 31, and fills and confirms the parameter format requirements of the formatted interactive terminal 32 for representing the weather conditions of the subject destination according to the weather forecast values; the formatted interactive terminal 32 of the weather forecast value sends the position of the destination and the corresponding weather condition information data packet to the VR scene database server 33 of the weather conditions of each place; after the capsule cabin is authorized by the user, the off-cabin central control upper computer 30 presents a VR scene experience to the user that best matches the destination weather conditions through the audiovisual integrated VR head-mounted display 34.
The in-cabin temperature automatic control module 300 includes: an in-capsule lower computer 35, a temperature sensor 36, a heating unit 37 and a refrigerating unit 38; the lower computer 35 in the capsule cabin sets a temperature fluctuation threshold limit in the capsule cabin, and the actual temperature value in the capsule cabin is monitored and fed back in real time through the temperature sensor 36, and the heating unit 37 and the refrigerating unit 38 are respectively used for heating or refrigerating when the actual air temperature in the capsule cabin is lower than the lower error limit of the forecast air temperature or higher than the upper error limit of the forecast air temperature.
The cabin humidity automatic control module 400 includes: a humidity sensor 39 and a humidification unit 40; the humidity sensor 39 monitors and feeds back the actual humidity value in the capsule cabin in real time, and the humidifying unit 40 is used for starting a humidifying function when the actual humidity in the capsule cabin is lower than the error lower limit of the forecast humidity;
the cabin air pressure automatic control module 500 includes: an air pressure sensor 41, a two-way electric control pneumatic valve 42, an air adding pump 43, a buzzer 44 and a warning lamp 45; the actual air pressure in the capsule cabin is lower than the error lower limit of the forecast air pressure, and the two-way electric control pneumatic valve 42 and the air increasing pump 43 are opened; the buzzer 44 and warning light 45 are used to alert the user when the actual air pressure in the cabin is above or below the safety threshold value due to an unexpected failure.
The cabin wind speed and direction control module 600 includes: a swivel drive motor 46, a rotational angle displacement sensor 47, an in-cabin circulation fan 48, and a wind speed sensor 49; when the rotary driving motor 46 is arranged at the top of the capsule cabin and the two pairs of air inlets and air outlets on the interlayer movable cabin shell 8 are opposite to the air inlets and the air outlets on the fixed cabin shell 9 at the inner layer of the capsule cabin and the direction of the weather forecast wind is consistent, the angular displacement sensor 47 monitors that the angular displacement of the movable cabin shell 8 at the interlayer of the capsule cabin reaches a specified angle value, the rotary driving motor 46 is turned off, the in-cabin circulating fan 48 is started, the rotating speed of the in-cabin circulating fan 48 continuously increases until the wind speed of the longitudinal section of the cabin monitored by the wind speed sensor 49 at the air inlet on the fixed cabin shell 9 at the inner layer of the capsule cabin reaches the allowable range of the wind speed value in the weather forecast, and the in-cabin lower computer 35 of the capsule cabin maintains the current rotating speed of the in-cabin circulating fan 48.
A human multi-physiological parameter monitoring module 700, comprising: the device comprises a blood oxygen heart rate body temperature detection module 50, an electrocardiograph electrode 51, a physiological signal noise reduction processing module 52, a human physiological state detection control unit 53, a physiological state warning and feedback module 54 and a vibration motor 55; the blood oxygen heart rate body temperature detection module 50 and the electrocardiograph electrode 51 respectively collect blood oxygen, heart rate, body temperature and electrocardiograph signals of a user when experiencing an immersive destination weather condition VR scene, and the physiological signal noise reduction processing module 52 respectively carries out filtering and signal noise removal processing on the blood oxygen, heart rate, body temperature and electrocardiograph signals; the human physiological state detection control unit 53 performs classification synchronous display monitoring on the blood oxygen, heart rate, body temperature and electrocardiosignals subjected to signal processing, and compares the physiological parameters in weather of the destination of the cabin body test of the user with blood oxygen, heart rate, body temperature and heart rate variability indexes of the user before the user enters the cabin; the physiological condition alert and feedback module 54 color marks physiological response indices and time periods greater than a set threshold and maps the magnitude of the abnormal amplitude linearly to the vibration frequency of the vibration motor 55 integrated with the wristband of the blood oxygen heart rate body temperature detection module 50.
Capsule door disable module 800, comprising: the hydraulic lifting platform 16, an infrared remote controller 56, an infrared receiver module 57, a travel switch 58, an electric hatch locking assembly 59, a touch switch 60, a smoke sensor 61 and a hatch emergency switch 62; the infrared remote controller 56 sends an instruction to the infrared receiver module 57, the infrared receiver module 57 transmits the received instruction to the lower cabin computer 35 of the capsule cabin, and the lower cabin computer 35 of the capsule cabin starts the hydraulic lifting table 16 to lift a user into the cabin; when the capsule cabin bottom cabin cover is lifted and is attached to the cabin wall of the capsule cabin, the travel switch 58 is triggered, the travel switch 58 activates the electric cabin cover locking assembly 59 after triggering, the bottom cabin cover is locked and sealed, and a cabin door closing signal is fed back to the out-of-cabin central control upper computer 30 of the capsule cabin.
Further, the in-cabin lower computer 35 drives the temperature sensor 36 to monitor and feed back the actual temperature value in the capsule cabin in real time through a communication command, when the temperature in the capsule cabin is required to be kept at the air temperature level of weather forecast in a certain period of time, the actual air temperature in the capsule cabin is lower than the error lower limit of the forecast air temperature, and the in-cabin lower computer 35 automatically starts the heating function of the heating unit 37; the lower computer 35 in the capsule cabin automatically shuts down the heating of the heating unit 37 and starts the refrigerating function of the refrigerating unit 38 until the actual air temperature in the capsule cabin is stabilized within the allowable range of the air temperature value in the weather forecast, and automatically shuts down the refrigerating of the refrigerating unit 38.
Further, the heating unit 37 heats, including:
the cabin air internal circulation driving motor 21 is started, the cabin air internal circulation driving motor 21 drives the fan blades 23 to rotate through the internal circulation driving motor output shaft 22, the cabin air is pumped upwards, the cabin air is sent into a cavity between the capsule cabin outer layer fixing shell 1 and the interlayer movable cabin shell 8 through the condenser annular air outlet 2, the sent air is heated through the electric heating filter screen 5, a pair of upper air inlet and outlet 6 of the inner cabin shell opposite to the interlayer movable cabin shell and the inner cabin shell and a lower air inlet and outlet 13 of the inner cabin shell opposite to the lower air inlet and outlet 12 of the interlayer movable cabin shell are sent back to the cabin in a circulating mode.
Further, the refrigeration unit 38 refrigerates, including: starting an in-cabin air internal circulation driving motor 21, and driving the fan blades 23 to rotate by the air internal circulation driving motor 21 through an output shaft 22 of the internal circulation driving motor to pump out the in-cabin air upwards; air in the capsule is sent into a cavity between the capsule cabin outer layer fixed shell 1 and the interlayer movable cabin shell 8 through the condenser annular air outlet 2, the sent air is subjected to heat absorption and temperature reduction through the refrigerant evaporator 7, and finally cooled cabin air is sent back into the cabin in a circulating and reciprocating mode through a pair of upper air inlets and outlets 6 of the inner cabin shell opposite to the interlayer movable cabin shell and the inner cabin shell and a lower air inlet and outlet 13 of the inner cabin shell opposite to a lower air inlet and outlet 12 of the interlayer movable cabin shell.
Further, the lower computer 35 in the capsule cabin drives the humidity sensor 39 to monitor and feed back the actual humidity value in the capsule cabin in real time through serial communication instructions; the actual humidity in the capsule cabin is lower than the error lower limit of the forecast humidity, and the cabin lower computer 35 automatically starts the humidifying function of the humidifying unit 40; the lower computer 35 in the capsule cabin automatically shuts down the humidification of the humidification unit 40 and automatically starts the refrigeration and dehumidification functions of the refrigeration unit 38 until the actual humidity in the capsule cabin is stabilized within the allowable range of the humidity value in the weather forecast, and automatically shuts down the refrigeration and dehumidification of the refrigeration unit 38.
Further, the in-cabin lower computer 35 of the capsule cabin sends a communication command to drive the air pressure sensor 41 to monitor and feed back the actual air pressure value in the capsule cabin in real time, when the air pressure in the capsule cabin is required to be kept at the air pressure level of weather forecast in a certain period of time, the actual air pressure in the capsule cabin is lower than the error lower limit of the forecast air pressure, the in-cabin lower computer 35 of the capsule cabin automatically opens the bidirectional electric control pneumatic valve 42 and the air increasing pump 43 to pressurize the cabin, the actual air pressure in the capsule cabin is higher than the error upper limit of the forecast air pressure, and the in-cabin lower computer 35 of the capsule cabin automatically shuts down the pressurizing functions of the bidirectional electric control pneumatic valve 42 and the air increasing pump 43.
Further, when the off-board central control upper computer 30 of the capsule cabin requires the start and stop of the direct control two-way electric control pneumatic valve 42 and the air increasing pump 43 to actively raise or lower the air pressure in the cabin, the automatic air pressure regulation of the off-board lower computer 35 of the capsule cabin is interrupted until the off-board central control upper computer 30 of the capsule cabin finishes the direct control of the two-way electric control pneumatic valve 42 and the air increasing pump 43, and the automatic air pressure regulation of the off-board lower computer 35 of the capsule cabin can continue to operate; when the actual pressure in the capsule cabin is higher than or lower than the safety threshold value due to unexpected faults, the lower computer 35 in the capsule cabin automatically turns on the buzzer 44 and the warning lamp 45 to warn the user to immediately take out of the capsule cabin.
Further, the lower computer 35 in the capsule cabin sets a wind speed fluctuation threshold of the longitudinal section in the capsule cabin according to the destination wind speed and the wind direction of weather forecast, starts the rotary driving motor 46 at the top of the capsule cabin, drives the movable capsule shell 8 of the capsule cabin interlayer to rotate, and the 8 pairs of air inlets on the fixed capsule shell 9 of the inner capsule cabin correspond to eight azimuth angles of east, south, west, north, southeast, southwest, northwest and northeast respectively; when the two pairs of air inlets and air outlets on the interlayer movable cabin shell 8 are opposite to the air inlets and air outlets on the capsule cabin inner layer fixed cabin shell 9, which are consistent with the weather forecast wind direction, the angular displacement sensor 47 simultaneously monitors that the angular displacement of the capsule cabin interlayer movable cabin shell 8 reaches a specified angular value, the lower cabin computer 35 of the capsule cabin turns off the rotary body driving motor 46, and the cabin circulating fan 48 is started.
Further, the physiological signal noise reduction processing module 52 performs filtering and signal noise removal processing on the blood oxygen, heart rate, body temperature and electrocardiosignals respectively. The human physiological state detection control unit 53 of the off-cabin central control upper computer 30 of the capsule cabin performs classification synchronous display monitoring on the blood oxygen, heart rate, body temperature and electrocardiosignals subjected to signal processing, and compares physiological parameters in the weather of the user who enters the cabin for checking eyes with blood oxygen, heart rate, body temperature and heart rate variability indexes of the user before entering the cabin.
Further, the smoke sensor 61 detects that the smoke concentration in the capsule cabin reaches the fire threshold, the buzzer 44 and the warning lamp 45 of the automatic control module of the air pressure in the capsule cabin are automatically called by the lower computer 35 in the capsule cabin to give out fire alarms to personnel in and out of the capsule cabin, the locking seal of the electric cabin cover locking assembly 59 is immediately released, and the cabin opening door action of the hydraulic lifting platform 16 is lowered for the user to escape. If the lower in-capsule computer 35 fails due to a line fault, the user in the capsule can initiate a door opening action through a hatch emergency switch 62 positioned in the capsule. The personnel outside the cabin can also start the cabin opening action through the cabin central control upper computer 30 or the cabin cover emergency switch 62 arranged outside the cabin.
The beneficial effects brought by the invention are as follows:
according to the scheme, the embodiment of the invention provides an isolated closed capsule cabin for simulating local weather conditions, which comprises the following components: the capsule cabin body 100, the destination weather forecast value formatting input module 200, the cabin temperature automatic control module 300, the cabin humidity automatic control module 400, the cabin air pressure automatic control module 500, the cabin wind speed and direction control module 600, the human body multiple physiological parameter monitoring module 700 and the capsule cabin door forbidden module 800. According to the technical scheme, the tactile experience environment of the local weather information of the destination can be provided, real-time objective measurement and evaluation are provided for physiological response of the user in the weather condition experience process, and personalized prevention and adaptation measures for the weather condition change of the destination are provided.
Drawings
FIG. 1 is a schematic diagram of an isolated capsule compartment for a localized weather simulation experience according to an embodiment of the present invention;
FIG. 2 is a schematic diagram of an isolated capsule compartment structure for a local weather simulation experience according to an embodiment of the present invention;
FIG. 3 shows a control flow diagram of an automatic cabin temperature control module for an isolated closed capsule cabin for a localized weather simulation experience in accordance with an embodiment of the present invention;
FIG. 4 shows a control flow diagram of an automatic cabin humidity control module for an isolated closed capsule cabin for a localized weather simulation experience in accordance with an embodiment of the present invention;
FIG. 5 shows a control flow diagram of a human body multi-physiological parameter monitoring module of an isolated closed capsule for local weather condition simulation experience according to an embodiment of the present invention;
FIG. 6 shows a control flow diagram of an intra-capsule wind speed and direction control module of an isolated closed capsule for a local weather condition simulation experience in accordance with an embodiment of the present invention;
FIG. 7 shows a capsule entrance guard module control flow diagram of an isolated closed capsule for a local weather simulation experience in accordance with an embodiment of the present invention;
in the figure, 100 is a capsule cabin body, 200 is a destination weather forecast numerical value formatting input module, 300 is an in-cabin temperature automatic control module, 400 is an in-cabin humidity automatic control module, 500 is an in-cabin air pressure automatic control module, 600 is an in-cabin air speed and direction control module, 700 is a human body multiple physiological parameter monitoring module, 800 is a capsule cabin door forbidden module, 1 is a capsule cabin outer layer fixed shell, 2 is a condenser annular air outlet, 3 is a condensate water overflow hole, 4 is an annular illuminating lamp belt, 5 is a heating filter screen, 6 is an upper air inlet and outlet of an inner cabin shell, 7 is a refrigerant evaporator, 8 is an interlayer movable cabin shell, 9 is an inner layer fixed cabin shell, 10 is an air booster pump, 11 is a pneumatic electromagnetic valve, 12 is a lower air inlet and outlet of the interlayer movable cabin shell, 13 is a lower air inlet and outlet of the inner cabin shell, 14 is a cabin standing bottom plate, 15 is a cabin body supporting base, 16 is a hydraulic lifting platform, 17 is a hydraulic lifting platform base, 18 is a cabin top maintenance inlet end cover, 19 is a gear motor lifting sleeve, 20 is an output transmission shaft, 21 is an in-cabin air internal circulation driving motor, 22 is an internal circulation driving motor output shaft, 23 is a fan blade, 24 is a condenser lifting sleeve, 25 is a condenser, 26 is a ventilation blower, 27 is a ventilation electromagnetic valve, 28 is an in-cabin humidifying water mist input hole, 29 is an ultrasonic atomizing sheet, 30 is an out-cabin central control upper computer of a capsule cabin, 31 is a destination weather inquiry terminal, 32 is a formatting interactive terminal of weather forecast values, 33 is a VR scene database server of weather conditions in all places, 34 is an audiovisual integrated VR helmet display, 35 is an in-cabin lower computer of the capsule cabin, 36 is a temperature sensor, 37 is a heating unit, 38 is a refrigerating unit, 39 is a humidity sensor, 40 is a humidifying unit, 41 is an air pressure sensor, 42 is a bidirectional electric control pneumatic valve, 43 is an air increasing pump, 44 is a buzzer, 45 is a warning lamp, 46 is a swivel driving motor, 47 is a corner displacement sensor, 48 is an in-cabin circulating fan, 49 is an air speed sensor, 50 is a blood oxygen heart rate body temperature detection module, 51 is an electrocardiograph electrode, 52 is a physiological signal noise reduction processing module, 53 is a human physiological state detection control unit, 54 is a physiological state warning and feedback module, 55 is a vibrating motor, 56 is an infrared remote controller, 57 is an infrared receiver module, 58 is a travel switch, 59 is an electric cabin cover locking assembly, 60 is a touch switch, 61 is a smoke sensor, and 62 is a cabin cover emergency switch.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the present invention more apparent, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is apparent that the described embodiments are some embodiments of the present invention, but not all embodiments of the present invention. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
The capsule cabin is used for providing an isolated and sealed simulation experience capsule cabin for operators residing in the isolated and sealed cabin for a long time to feel natural weather conditions outside the destination cabin in advance. According to the invention, a single isolated closed capsule cabin is designed, and a set of cabin environment regulation and control system capable of simulating weather conditions of a specified destination for a user is designed in the cabin. The system utilizes an immersion VR system to present illumination brightness change along with wind for a user, local cloud layer movement, surrounding vegetation landscape flutter, wind sound, whistle, animal crying and other surrounding environments to be seen and hearing feeling, utilizes an in-cabin environment regulation and control system to present temperature, humidity, air pressure and other touch feeling for the user, and utilizes a wearable physiological parameter measuring unit to monitor physical stress response of the user.
As shown in fig. 1, a schematic diagram of an isolated closed capsule cabin for simulating a local weather condition according to an embodiment of the present invention in fig. 1 is shown.
In fig. 1, an isolated capsule for a local weather simulation experience, comprising: the capsule cabin body 100, the destination weather forecast value formatting input module 200, the cabin temperature automatic control module 300, the cabin humidity automatic control module 400, the cabin air pressure automatic control module 500, the cabin wind speed and direction control module 600, the human body multiple physiological parameter monitoring module 700 and the capsule cabin door forbidden module 800.
As shown in fig. 2, fig. 2 is a schematic structural diagram of an isolated and sealed capsule cabin for simulating a local weather condition according to an embodiment of the present invention.
Capsule body 100, comprising: the capsule cabin outer layer fixing shell 1, the condenser annular air outlet 2, the condensate overflow hole 3, the annular lighting lamp belt 4, the heating filter screen 5, the upper air inlet and outlet 6 of the inner cabin shell, the refrigerant evaporator 7, the interlayer movable cabin shell 8, the inner layer fixing cabin shell 9, the air booster pump 10, the pneumatic electromagnetic valve 11, the lower air inlet and outlet 12 of the interlayer movable cabin shell, the lower air inlet and outlet 13 of the inner cabin shell, the cabin standing bottom plate 14, the cabin supporting base 15, the hydraulic lifting table 16, the hydraulic lifting table base 17, the cabin top maintenance inlet end cover 18, the gear motor lifting sleeve 19, the output transmission shaft 20, the cabin air inner circulation driving motor 21, the inner circulation driving motor output shaft 22, the fan blades 23, the condenser lifting sleeve 24, the condenser 25, the air ventilation blower 26, the air ventilation electromagnetic valve 27, the cabin humidifying water mist input hole 28 and the ultrasonic atomization sheet 29.
The destination weather forecast values formatting input module 200 includes: the capsule cabin is externally and centrally controlled by an upper computer 30, a destination weather inquiry terminal 31, a weather forecast value formatting interaction terminal 32, a VR scene database server 33 of weather conditions in all places and an audio-visual integrated VR helmet display 34; the outdoor central control upper computer 30 searches the forecast information of environmental noise, weather, air temperature, humidity, air pressure, visibility, wind power and wind direction of the local weather of the simulated subject destination by using the destination weather inquiry terminal 31, and fills and confirms the parameter format requirements of the formatted interactive terminal 32 for representing the weather conditions of the subject destination according to the weather forecast values; the formatted interactive terminal 32 of the weather forecast value sends the position of the destination and the corresponding weather condition information data packet to the VR scene database server 33 of the weather conditions of each place; after the capsule cabin is authorized by the user, the off-cabin central control upper computer 30 presents a VR scene experience to the user that best matches the destination weather conditions through the audiovisual integrated VR head-mounted display 34.
The in-cabin temperature automatic control module 300 includes: an in-capsule lower computer 35, a temperature sensor 36, a heating unit 37 and a refrigerating unit 38; the lower computer 35 in the capsule cabin sets a temperature fluctuation threshold limit in the capsule cabin, and the actual temperature value in the capsule cabin is monitored and fed back in real time through the temperature sensor 36, and the heating unit 37 and the refrigerating unit 38 are respectively used for heating or refrigerating when the actual air temperature in the capsule cabin is lower than the lower error limit of the forecast air temperature or higher than the upper error limit of the forecast air temperature.
As shown in fig. 3, fig. 3 is a control flow chart of an automatic cabin temperature control module of an isolated closed capsule cabin for simulating experience of local weather conditions in an embodiment of the invention.
In the embodiment of the present invention, after the off-board central control upper computer 30 of the capsule cabin designates the destination temperature value to be experienced, the on-board lower computer 35 of the capsule cabin sets the temperature fluctuation threshold in the capsule cabin according to the destination temperature range of weather forecast. In order to regulate the temperature of the air in the capsule cabin, the cabin lower computer 35 drives the temperature sensor 36 to monitor and feed back the actual temperature value in the capsule cabin in real time through a communication command, when the temperature in the capsule cabin is required to be kept at the air temperature level of weather forecast in a certain period of time, the actual air temperature in the capsule cabin is lower than the error lower limit of the forecast air temperature, and the heating function of the heating unit 37 is automatically started by the cabin lower computer 35; the lower computer 35 in the capsule cabin automatically shuts down the heating of the heating unit 37 and starts the refrigerating function of the refrigerating unit 38 until the actual air temperature in the capsule cabin is stabilized within the allowable range of the air temperature value in the weather forecast, and automatically shuts down the refrigerating of the refrigerating unit 38.
In the embodiment of the present invention, when the external central control upper computer 30 of the capsule cabin requires to directly control the start and stop of the heat and refrigeration functions so as to realize active heating or cooling, the automatic temperature control of the internal lower computer 35 of the capsule cabin is interrupted until the external central control upper computer 30 of the capsule cabin finishes directly controlling the heating unit 37 and the refrigeration unit 38, and the automatic temperature control method of the internal lower computer 35 of the capsule cabin can continue to operate.
In one implementation of the embodiment of the present invention, the heating unit 37 heats, including:
the cabin air internal circulation driving motor 21 is started, the cabin air internal circulation driving motor 21 drives the fan blades 23 to rotate through the internal circulation driving motor output shaft 22, the cabin air is pumped upwards, the cabin air is sent into a cavity between the capsule cabin outer layer fixing shell 1 and the interlayer movable cabin shell 8 through the condenser annular air outlet 2, the sent air is heated through the electric heating filter screen 5, a pair of upper air inlet and outlet 6 of the inner cabin shell opposite to the interlayer movable cabin shell and the inner cabin shell and a lower air inlet and outlet 13 of the inner cabin shell opposite to the lower air inlet and outlet 12 of the interlayer movable cabin shell are sent back to the cabin in a circulating mode.
In one implementation of the present embodiment, the refrigeration unit 38 is configured to cool, including: starting an in-cabin air internal circulation driving motor 21, and driving the fan blades 23 to rotate by the air internal circulation driving motor 21 through an output shaft 22 of the internal circulation driving motor to pump out the in-cabin air upwards; air in the capsule is sent into a cavity between the capsule cabin outer layer fixed shell 1 and the interlayer movable cabin shell 8 through the condenser annular air outlet 2, the sent air is subjected to heat absorption and temperature reduction through the refrigerant evaporator 7, and finally cooled cabin air is sent back into the cabin in a circulating and reciprocating mode through a pair of upper air inlets and outlets 6 of the inner cabin shell opposite to the interlayer movable cabin shell and the inner cabin shell and a lower air inlet and outlet 13 of the inner cabin shell opposite to a lower air inlet and outlet 12 of the interlayer movable cabin shell.
The cabin humidity automatic control module 400 includes: a humidity sensor 39 and a humidification unit 40; the humidity sensor 39 monitors and feeds back in real time the actual humidity value in the capsule compartment, and the humidifying unit 40 is used for starting the humidifying function when the actual humidity in the capsule compartment is lower than the error lower limit of the forecast humidity.
As shown in fig. 4, fig. 4 is a control flow chart of an automatic cabin humidity control module of an isolated closed capsule cabin for simulating a local weather condition according to an embodiment of the present invention.
In the embodiment of the invention, the lower computer 35 in the capsule cabin drives the humidity sensor 39 to monitor and feed back the actual humidity value in the capsule cabin in real time through serial communication instructions; the actual humidity in the capsule cabin is lower than the error lower limit of the forecast humidity, and the cabin lower computer 35 automatically starts the humidifying function of the humidifying unit 40; the lower computer 35 in the capsule cabin automatically shuts down the humidification of the humidification unit 40 and automatically starts the refrigeration and dehumidification functions of the refrigeration unit 38 until the actual humidity in the capsule cabin is stabilized within the allowable range of the humidity value in the weather forecast, and automatically shuts down the refrigeration and dehumidification of the refrigeration unit 38.
In the embodiment of the present invention, after the off-board central control upper computer 30 of the capsule cabin designates the destination humidity value to be experienced, the on-board lower computer 35 of the capsule cabin sets the humidity fluctuation threshold in the capsule cabin according to the destination humidity range of the weather forecast. In order to regulate the humidity of the air in the capsule cabin, the cabin lower computer 35 of the capsule cabin drives the humidity sensor 39 to monitor and feed back the actual humidity value in the capsule cabin in real time through serial communication instructions. When it is required that the humidity inside the capsule compartment is maintained at the humidity level of the weather forecast for a certain period of time, the lower-level computer 35 inside the capsule compartment automatically starts the humidifying function of the humidifying unit 40 once the actual humidity inside the capsule compartment is lower than the error lower limit of the forecast humidity. When the off-board central control upper computer 30 of the capsule cabin requires the start and stop of the direct control humidification and refrigeration dehumidification functions to realize the active lifting or lowering of the air humidity in the cabin, the automatic humidity control of the on-board lower computer 35 of the capsule cabin is interrupted until the off-board central control upper computer 30 of the capsule cabin finishes the direct control of the humidification unit and the refrigeration unit, and the automatic humidity control method of the on-board lower computer 35 of the capsule cabin can continue to operate.
Wherein, the realization of humidification function of humidification unit includes: after the humidifying unit 40 is started, water in the bilge cavity below the bilge standing bottom plate 14 passes through the ultrasonic atomizing sheet 29 to generate water mist, and then the water mist enters the cabin through the cabin humidifying water mist input hole 28 to increase the humidity of air in the cabin.
The realization of the refrigeration dehumidification function of the refrigeration unit comprises the following steps: the cabin air internal circulation driving motor 21 is started, the cabin air internal circulation driving motor 21 drives the fan blades 23 to rotate through the internal circulation driving motor output shaft 22, cabin air is pumped upwards after being condensed and liquefied through the condenser 25, then the cabin air is sent into a cavity between the capsule cabin outer layer fixed shell 1 and the interlayer movable cabin shell 8 through the condenser annular air outlet 2, finally, the cabin air subjected to condensation dehumidification is sent back to the cabin in a circulating mode through the upper air inlet and outlet 6 of the inner cabin shell opposite to the interlayer movable cabin shell and the lower air inlet and outlet 13 of the inner cabin shell opposite to the lower air inlet and outlet 12 of the interlayer movable cabin shell, and the humidity of the cabin air is reduced. The water produced by the condensation and liquefaction of the condenser 25 drips around the ceiling in the cabin through the condensed water overflow hole 3, flows back to the bilge cavity below the cabin standing bottom plate 14 through the cabin humidifying water mist input hole 28 to be stored as a humidifying water source.
The cabin air pressure automatic control module 500 includes: an air pressure sensor 41, a two-way electric control pneumatic valve 42, an air adding pump 43, a buzzer 44 and a warning lamp 45; the actual air pressure in the capsule cabin is lower than the error lower limit of the forecast air pressure, and the two-way electric control pneumatic valve 42 and the air increasing pump 43 are opened; the buzzer 44 and warning light 45 are used to alert the user when the actual air pressure in the cabin is above or below the safety threshold value due to an unexpected failure.
As shown in fig. 5, fig. 5 is a control flow chart of a human body multi-physiological-parameter monitoring module of an isolated closed capsule cabin for local weather condition simulation experience according to an embodiment of the invention.
In the embodiment of the present invention, when the external central control upper computer 30 of the capsule cabin requires the direct control of the two-way electric control pneumatic valve 42 and the air increasing pump 43 to start and stop and actively raise or lower the air pressure in the cabin, the automatic regulation and control of the air pressure of the internal lower computer 35 of the capsule cabin will be interrupted until the external central control upper computer 30 of the capsule cabin ends the direct control of the two-way electric control pneumatic valve 42 and the air increasing pump 43, and the automatic regulation and control of the air pressure of the internal lower computer 35 of the capsule cabin can continue to operate; when the actual pressure in the capsule cabin is higher than or lower than the safety threshold value due to unexpected faults, the lower computer 35 in the capsule cabin automatically turns on the buzzer 44 and the warning lamp 45 to warn the user to immediately take out of the capsule cabin.
After the off-board central control upper computer 30 of the capsule designates the destination air pressure value to be experienced, the on-board lower computer 35 of the capsule sets the air pressure fluctuation threshold in the capsule according to the destination air pressure range of weather forecast. In order to regulate the air pressure of the air in the capsule cabin, the lower cabin computer 35 in the capsule cabin sends a communication command to drive the air pressure sensor 41 to monitor and feed back the actual air pressure value in the capsule cabin in real time. When it is required that the air pressure in the capsule compartment is maintained at the weather forecast air pressure level for a certain period of time, the lower computer 35 in the capsule compartment automatically opens the two-way electric control pneumatic valve 42 and the air increasing pump 43 to pressurize the compartment once the actual air pressure in the compartment is below the error lower limit of the forecast air pressure. The on-board lower computer 35 of the capsule pod automatically shuts down the pressurization functions of the bi-directional electro-pneumatic valve 42 and the air augmentation pump 43 once the on-board actual air pressure is above the upper error limit for the predicted air pressure.
The cabin wind speed and direction control module 600 includes: a swivel drive motor 46, a rotational angle displacement sensor 47, an in-cabin circulation fan 48, and a wind speed sensor 49; when the rotary driving motor 46 is arranged at the top of the capsule cabin and the two pairs of air inlets and air outlets on the interlayer movable cabin shell 8 are opposite to the air inlets and the air outlets on the fixed cabin shell 9 at the inner layer of the capsule cabin and the direction of the weather forecast wind is consistent, the angular displacement sensor 47 monitors that the angular displacement of the movable cabin shell 8 at the interlayer of the capsule cabin reaches a specified angle value, the rotary driving motor 46 is turned off, the in-cabin circulating fan 48 is started, the rotating speed of the in-cabin circulating fan 48 continuously increases until the wind speed of the longitudinal section of the cabin monitored by the wind speed sensor 49 at the air inlet on the fixed cabin shell 9 at the inner layer of the capsule cabin reaches the allowable range of the wind speed value in the weather forecast, and the in-cabin lower computer 35 of the capsule cabin maintains the current rotating speed of the in-cabin circulating fan 48.
In the embodiment of the invention, the off-board central control upper computer 30 of the capsule cabin designates the destination wind speed and the wind back to be experienced, the in-cabin lower computer 35 of the capsule cabin sets the wind speed fluctuation threshold of the longitudinal section in the capsule cabin according to the destination wind speed and the wind direction of weather forecast, and starts the rotary driving motor 46 at the top of the capsule cabin to drive the movable capsule shell 8 of the capsule cabin interlayer to rotate, and the 8 pairs of air inlets on the fixed capsule shell 9 of the inner layer of the capsule cabin correspond to eight azimuth angles of east, south, west, north, southeast, southwest, northwest and northeast respectively. According to the technical scheme, the wind direction and wind speed experience of the destination weather forecast can be provided for the user.
A human multi-physiological parameter monitoring module 700, comprising: the device comprises a blood oxygen heart rate body temperature detection module 50, an electrocardiograph electrode 51, a physiological signal noise reduction processing module 52, a human physiological state detection control unit 53, a physiological state warning and feedback module 54 and a vibration motor 55; the blood oxygen heart rate body temperature detection module 50 and the electrocardiograph electrode 51 respectively collect blood oxygen, heart rate, body temperature and electrocardiograph signals of a user when experiencing an immersive destination weather condition VR scene, and the physiological signal noise reduction processing module 52 respectively carries out filtering and signal noise removal processing on the blood oxygen, heart rate, body temperature and electrocardiograph signals; the human physiological state detection control unit 53 performs classification synchronous display monitoring on the blood oxygen, heart rate, body temperature and electrocardiosignals subjected to signal processing, and compares the physiological parameters in weather of the destination of the cabin body test of the user with blood oxygen, heart rate, body temperature and heart rate variability indexes of the user before the user enters the cabin; the physiological condition alert and feedback module 54 color marks physiological response indices and time periods greater than a set threshold and maps the magnitude of the abnormal amplitude linearly to the vibration frequency of the vibration motor 55 integrated with the wristband of the blood oxygen heart rate body temperature detection module 50.
As shown in fig. 6, fig. 6 is a control flow chart of an intra-cabin wind speed and direction control module of an isolated closed capsule cabin for local weather condition simulation experience according to an embodiment of the invention.
In the embodiment of the present invention, the physiological signal noise reduction processing module 52 performs filtering and signal noise removal processing on the blood oxygen, the heart rate, the body temperature and the electrocardiosignal, respectively. The human physiological state detection control unit 53 of the off-cabin central control upper computer 30 of the capsule cabin performs classification synchronous display monitoring on the blood oxygen, heart rate, body temperature and electrocardiosignals subjected to signal processing, and compares physiological parameters in the weather of the user who enters the cabin for checking eyes with blood oxygen, heart rate, body temperature and heart rate variability indexes of the user before entering the cabin.
In one implementation of the embodiment of the invention, before experiencing the destination weather condition, the user wears the blood oxygen heart rate body temperature detection module 50 tightened by the wristband and the electrocardiographic electrodes 51 attached to the chest of the user collect blood oxygen, heart rate, body temperature and electrocardiographic signals respectively when the user experiences the immersive destination weather condition VR scene. The human physiological state detection control unit 53 stores various physiological response indexes of the user in the weather of the experience destination in real time, when the abnormal physiological response indexes are detected, the abnormal physiological response indexes and the abnormal physiological response time intervals are marked by utilizing the physiological state warning and feedback module 54, the abnormal amplitude is linearly mapped to the vibration frequency of the vibration motor 55 integrated on the wrist strap of the blood oxygen heart rate body temperature detection module 50, wrist vibration tactile feedback is provided for the user, the current physiological response state of the user is reminded, potential health risks are noted, and the user is considered to actively exit the experience in time.
Capsule door disable module 800, comprising: the hydraulic lifting platform 16, an infrared remote controller 56, an infrared receiver module 57, a travel switch 58, an electric hatch locking assembly 59, a touch switch 60, a smoke sensor 61 and a hatch emergency switch 62; the infrared remote controller 56 sends an instruction to the infrared receiver module 57, the infrared receiver module 57 transmits the received instruction to the lower cabin computer 35 of the capsule cabin, and the lower cabin computer 35 of the capsule cabin starts the hydraulic lifting table 16 to lift a user into the cabin; when the capsule cabin bottom cabin cover is lifted and is attached to the cabin wall of the capsule cabin, the travel switch 58 is triggered, the travel switch 58 activates the electric cabin cover locking assembly 59 after triggering, the bottom cabin cover is locked and sealed, and a cabin door closing signal is fed back to the out-of-cabin central control upper computer 30 of the capsule cabin.
As shown in fig. 7, fig. 7 is a control flow chart of a capsule entrance guard module of an isolated closed capsule for simulating a local weather condition according to an embodiment of the present invention.
In the embodiment of the invention, the smoke sensor 61 monitors that the smoke concentration in the capsule cabin reaches a fire alarm threshold, and the cabin lower computer 35 in the capsule cabin automatically calls the buzzer 44 and the warning lamp 45 of the cabin air pressure automatic control module to send out a fire alarm to personnel outside the cabin, and immediately releases the locking seal of the electric cabin cover locking assembly 59, and lowers the cabin opening door action of the hydraulic lifting platform 16 for a user to escape. If the lower in-capsule computer 35 fails due to a line fault, the user in the capsule can initiate a door opening action through a hatch emergency switch 62 positioned in the capsule. The personnel outside the cabin can also start the cabin opening action through the cabin central control upper computer 30 or the cabin cover emergency switch 62 arranged outside the cabin.
In one implementation of the embodiment of the invention, the user stands on the hydraulic lifting platform 16 supporting the capsule bottom cover to prepare for entering the capsule, then presses the portable infrared remote controller 56, sends a command for lifting the hydraulic lifting platform 16 to the infrared receiver module 57, the infrared receiver module 57 transmits the received command to the lower cabin computer 35 of the capsule, and the lower cabin computer 35 of the capsule starts the hydraulic lifting platform 16 to lift the user into the capsule. When the capsule bottom hatch is raised and engages the capsule wall, the travel switch 58 is triggered. The lower cabin computer 35 in the capsule cabin activates the electric cabin cover locking assembly 59 after detecting that the travel switch 58 is triggered, locks and seals the bottom cabin cover, and feeds back a cabin door closed signal to the upper cabin control computer 30 outside the capsule cabin. After the user wears the audio-visual integrated VR head-mounted display 34, the blood oxygen heart rate body temperature detection module 50 and the electrocardiograph electrode 51 independently, the user touches the touch switch 60 integrated on the wrist strap of the blood oxygen heart rate body temperature detection module 50 to authorize the external central control upper computer 30 of the capsule cabin to start the weather simulation program in the capsule cabin. Then, the lower cabin computer 35 in the capsule cabin starts audio-visual initialization of the destination VR scene according to the destination weather conditions specified by the upper cabin central control computer 30, and corresponding wind direction, wind speed, temperature and humidity and air pressure touch simulation are performed. If the smoke sensor 61 monitors that the smoke concentration in the capsule cabin reaches the fire threshold value in the experience process, the buzzer 44 and the warning lamp 45 of the automatic cabin air pressure control module are automatically called by the lower cabin computer 35 of the capsule cabin to give out fire alarm to personnel in the cabin and outside the cabin, the locking seal of the electric cabin cover locking assembly 59 is immediately released, and the cabin opening door action of the hydraulic lifting platform 16 is lowered for the user to escape. If the lower in-capsule computer 35 fails due to a line fault, the user in the capsule can initiate a door opening action through a hatch emergency switch 62 positioned in the capsule. The personnel outside the cabin can also start the cabin opening door action through an outside central control upper computer 60 or a cabin cover emergency switch 62 arranged outside the cabin.
According to the technical scheme, the isolated closed capsule cabin for a single person is provided, and is provided with a test cabin of an air temperature, humidity, smoke, air pressure, wind direction and air speed and fire alarm and fire control monitoring system, and in addition, a multi-physiological-parameter monitoring unit for monitoring central electricity, body temperature, heart rate and blood oxygen content in the process of a user experience destination weather environment is integrated. The existing cabin environment intelligent regulation and control system is mainly oriented to air component guarantee of a nursing ward or an underwater closed cabin, growth environment simulation of greenhouse or farm cultivation and constant temperature and humidity regulation and control of a high-precision equipment room. A few personalized cabin environment control methods and systems based on multiple physiological parameters dynamically adjust the cabin environment of a single person operation or living according to the average physical characteristics of a user, aiming at ensuring the real-time adaptation of the cabin air environment to the user. The invention focuses on the simulation experience of adapting to the natural weather environment outside the destination cabin in advance for the user according to the weather forecast information, so that the user adapts to the upcoming weather condition in advance, and objective evaluation is provided for the potential of body adaptation by monitoring multiple physiological parameters. The invention has foreseeable technical transformation and product application prospects, namely, the invention is used as a technical platform for supporting harmonious man-machine-environment research and application.
The foregoing is a preferred embodiment of the present invention and it should be noted that modifications and adaptations to those skilled in the art may be made without departing from the principles of the present invention and are intended to be comprehended within the scope of the present invention.

Claims (10)

1. An isolated capsule for local weather simulation experience, comprising: the capsule cabin comprises a capsule cabin body (100), a destination weather forecast numerical value formatting input module (200), an intra-cabin temperature automatic control module (300), an intra-cabin humidity automatic control module (400), an intra-cabin air pressure automatic control module (500), an intra-cabin wind speed and direction control module (600), a human body multi-physiological parameter monitoring module (700) and a capsule cabin door forbidden module (800);
the capsule body (100) comprises: the capsule cabin comprises a capsule cabin outer layer fixed shell (1), a condenser annular air outlet (2), a condensate overflow hole (3), an annular lighting lamp belt (4), a heating filter screen (5), an upper air inlet and outlet (6) of an inner cabin shell, a refrigerant evaporator (7), an interlayer movable cabin shell (8), an inner layer fixed cabin shell (9), an air booster pump (10), a pneumatic electromagnetic valve (11), a lower air inlet and outlet (12) of the interlayer movable cabin shell, a lower air inlet and outlet (13) of the inner cabin shell, a cabin standing bottom plate (14), a cabin body supporting base (15), a hydraulic lifting table (16), a hydraulic lifting table base (17), a cabin top maintenance inlet end cover (18), a gear motor lifting sleeve (19), an output transmission shaft (20), a cabin air inner circulation driving motor (21), an inner circulation driving motor output shaft (22), a fan blade (23), a condenser lifting sleeve (24), a condenser (25), a ventilation blower (26), a ventilation electromagnetic valve (27), a cabin inner humidification water mist input hole (28) and an ultrasonic atomization sheet (29);
The destination weather forecast values formatting input module (200) includes: the system comprises an off-board central control upper computer (30) of a capsule cabin, a destination weather inquiry terminal (31), a weather forecast value formatting interaction terminal (32), a VR scene database server (33) of weather conditions in each place and an audio-visual integrated VR helmet display (34); the outdoor central control upper computer (30) searches environmental noise, cloudiness, air temperature, humidity, air pressure, visibility, wind power and wind direction forecast information of local weather of the simulated subject destination by utilizing the destination weather inquiry terminal (31), and fills and confirms the parameter format requirements of the formatted interactive terminal (32) for representing the weather condition of the subject destination according to weather forecast values; the formatting interactive terminal (32) of the weather forecast value sends the position of the destination and the corresponding weather condition information data packet to the VR scene database server (33) of the weather conditions of each place; after the outside central control upper computer (30) of the capsule cabin obtains the authorization of the user, the VR scene experience with the best matched destination weather condition is presented to the user through the audio-visual integrated VR helmet display (34);
the cabin interior temperature automatic control module (300) includes: an in-capsule lower computer (35), a temperature sensor (36), a heating unit (37) and a refrigerating unit (38); an in-capsule lower computer (35) of the capsule cabin sets a temperature fluctuation threshold in the capsule cabin, real-time monitors and feeds back actual temperature values in the capsule cabin through a temperature sensor (36), and a heating unit (37) and a refrigerating unit (38) are respectively used for heating or refrigerating when the actual air temperature in the capsule cabin is lower than the lower error limit of the forecast air temperature or higher than the upper error limit of the forecast air temperature;
The cabin humidity automatic control module (400) comprises: a humidity sensor (39) and a humidifying unit (40); the humidity sensor (39) monitors and feeds back the actual humidity value in the capsule cabin in real time, and the humidifying unit (40) is used for starting a humidifying function when the actual humidity in the capsule cabin is lower than the error lower limit of the forecast humidity;
the cabin air pressure automatic control module (500) comprises: an air pressure sensor (41), a two-way electric control pneumatic valve (42), an air adding pump (43), a buzzer (44) and an alarm lamp (45); the actual air pressure in the capsule cabin is lower than the error lower limit of the forecast air pressure, and the bidirectional electric control pneumatic valve (42) and the air increasing pump (43) are opened; the buzzer (44) and the warning lamp (45) are used for warning a user when the actual air pressure in the cabin is higher than or lower than a safety threshold value due to unexpected faults;
the cabin wind speed and direction control module (600) comprises: a rotor driving motor (46), a rotation angle displacement sensor (47), an in-cabin circulating fan (48) and a wind speed sensor (49); when the rotary driving motor (46) is arranged at the top of the capsule cabin, two pairs of air inlets and air outlets on the interlayer movable cabin shell (8) are opposite to the air inlets and the air outlets which are arranged on the fixed cabin shell (9) at the inner layer of the capsule cabin and have the same direction as the weather forecast wind direction, the angular displacement sensor (47) monitors that the angular displacement of the movable cabin shell (8) at the interlayer of the capsule cabin reaches a specified angle value, the rotary driving motor (46) is turned off, the circulating fan (48) at the inner layer of the capsule cabin is started, the rotating speed of the circulating fan (48) at the inner layer of the capsule cabin is continuously increased until the wind speed of the longitudinal section of the capsule cabin monitored by the wind speed sensor (49) at the air inlet on the fixed cabin shell (9) at the inner layer of the capsule cabin reaches the allowable range of the wind speed value in the weather forecast, and the lower computer (35) at the capsule cabin maintains the current rotating speed of the circulating fan (48) at the inner layer of the capsule cabin;
The human multi-physiological parameter monitoring module (700) includes: the device comprises a blood oxygen heart rate body temperature detection module (50), an electrocardiograph electrode (51), a physiological signal noise reduction processing module (52), a human physiological state detection control unit (53), a physiological state warning and feedback module (54) and a vibration motor (55); the blood oxygen heart rate body temperature detection module (50) and the electrocardiograph electrode (51) respectively collect blood oxygen, heart rate, body temperature and electrocardiograph signals of a user when experiencing an immersive destination weather condition VR scene, and the physiological signal noise reduction processing module (52) respectively carries out filtering and signal noise removal processing on the blood oxygen, heart rate, body temperature and electrocardiograph signals; the human physiological state detection control unit (53) carries out classification synchronous display monitoring on the blood oxygen, heart rate, body temperature and electrocardiosignals which are subjected to signal processing, and compares the physiological parameters of a user in the weather of the experimental destination of the cabin body with blood oxygen, heart rate, body temperature and heart rate variability indexes of the user before the user enters the cabin; the physiological state warning and feedback module (54) marks the physiological response index and the time period which are larger than the set threshold value, and linearly maps the magnitude of the abnormal amplitude to the vibration frequency of a vibration motor (55) integrated on a wrist strap of the blood oxygen heart rate body temperature detection module (50);
The capsule access control module (800) comprises: the hydraulic lifting platform (16), the infrared remote controller (56), the infrared receiver module (57), the travel switch (58), the electric hatch locking assembly (59), the touch switch (60), the smoke sensor (61) and the hatch emergency switch (62); the infrared remote controller (56) sends an instruction to the infrared receiver module (57), the infrared receiver module (57) transmits the received instruction to the lower cabin computer (35) of the capsule cabin, and the lower cabin computer (35) of the capsule cabin starts the hydraulic lifting table (16) to lift a user into the cabin; when the capsule cabin bottom cabin cover is lifted and is attached to the cabin wall of the capsule cabin, a travel switch (58) is triggered, an electric cabin cover locking assembly (59) is activated after the travel switch (58) is triggered, the bottom cabin cover is locked and sealed, and a cabin door closed signal is fed back to an out-of-cabin central control upper computer (30) of the capsule cabin.
2. An isolated closed capsule for simulating a local weather condition according to claim 1, wherein said capsule lower computer (35) drives said temperature sensor (36) to monitor and feed back the actual temperature value in the capsule in real time by communication command, when the temperature in the capsule is required to be maintained at the predicted air temperature level for a certain period of time, said actual air temperature in the capsule is lower than the error lower limit of the predicted air temperature, said capsule lower computer (35) automatically starts the heating function of the heating unit (37); the actual air temperature in the capsule cabin is higher than the error upper limit of the forecast air temperature, the lower computer (35) in the capsule cabin automatically stops heating of the heating unit (37), and the refrigerating function of the refrigerating unit (38) is started until the actual air temperature in the capsule cabin is stabilized within the allowable range of the air temperature value in the weather forecast, and the refrigerating of the refrigerating unit (38) is automatically stopped.
3. An isolated capsule for a localized weather simulation experience according to claim 2, wherein the heating unit (37) heats, comprising:
the method comprises the steps of starting an in-cabin air internal circulation driving motor (21), driving a fan blade (23) to rotate through an output shaft (22) of the internal circulation driving motor by the in-cabin air internal circulation driving motor (21), pumping in-cabin air upwards, sending in-cabin air into a cavity between a capsule cabin outer layer fixing shell (1) and an interlayer movable cabin shell (8) through a condenser annular air outlet (2), heating the sent in-cabin air through an electric heating filter screen (5), and sending back the heated in-cabin air into a cabin in a circulating way through a pair of upper air inlets and outlets (6) of the inner cabin shell opposite to the interlayer movable cabin shell and a lower air inlet and outlet (13) of the inner cabin shell opposite to a lower air inlet and outlet (12) of the interlayer movable cabin shell.
4. An isolated capsule for a localized weather simulation experience according to claim 2, wherein the refrigeration unit (38) is refrigerated, comprising: starting an in-cabin air internal circulation driving motor (21), wherein the in-cabin air internal circulation driving motor (21) drives a fan blade (23) to rotate through an output shaft (22) of the in-cabin air internal circulation driving motor, and pumping out the in-cabin air upwards; air in the capsule is sent into a cavity between the capsule cabin outer layer fixed shell (1) and the interlayer movable cabin shell (8) through the condenser annular air outlet (2), the sent air is subjected to heat absorption and temperature reduction through the refrigerant evaporator (7), and finally the cooled cabin air is circularly and reciprocally sent back into the cabin through the upper air inlet and outlet (6) of the inner cabin shell opposite to the interlayer movable cabin shell and the lower air inlet and outlet (13) of the inner cabin shell opposite to the lower air inlet and outlet (12) of the interlayer movable cabin shell.
5. The isolated closed capsule for simulating a local weather condition according to claim 1, wherein the lower computer (35) in the capsule drives the humidity sensor (39) to monitor and feed back the actual humidity value in the capsule in real time through serial communication instructions; the actual humidity in the capsule cabin is lower than the error lower limit of the forecast humidity, and the lower computer (35) in the cabin automatically starts the humidifying function of the humidifying unit (40); the actual humidity in the capsule cabin is higher than the error upper limit of the forecast humidity, the cabin lower computer (35) of the capsule cabin automatically stops the humidification of the humidifying unit (40), and automatically starts the refrigeration and dehumidification functions of the refrigeration unit (38) until the actual humidity in the capsule cabin is stabilized within the allowable range of the humidity value in the weather forecast, and the refrigeration and dehumidification of the refrigeration unit (38) are automatically stopped.
6. The isolated closed capsule for simulating a local weather condition according to claim 1, wherein the lower computer (35) in the capsule sends a communication command to drive the air pressure sensor (41) to monitor and feed back the actual air pressure value in the capsule in real time, when the air pressure in the capsule is required to be kept at the air pressure level of weather forecast in a certain period of time, the actual air pressure in the capsule is lower than the error lower limit of the forecast air pressure, the lower computer (35) in the capsule automatically opens the bidirectional electric control pneumatic valve (42) and the air increasing pump (43) to boost the pressure in the capsule, the actual air pressure in the capsule is higher than the error upper limit of the forecast air pressure, and the lower computer (35) in the capsule automatically shuts down the pressurizing functions of the bidirectional electric control pneumatic valve (42) and the air increasing pump (43).
7. The isolated closed capsule for simulating a local weather condition according to claim 6, wherein the off-board central control upper computer (30) of the capsule requires the start and stop of the direct control two-way electric control pneumatic valve (42) and the air increasing pump (43), and when the air pressure in the capsule is actively raised or lowered, the automatic regulation of the air pressure of the on-board lower computer (35) of the capsule is interrupted until the off-board central control upper computer (30) of the capsule ends the direct control of the two-way electric control pneumatic valve (42) and the air increasing pump (43), and the automatic regulation of the air pressure of the on-board lower computer (35) of the capsule can continue to operate; when the actual pressure in the capsule cabin is higher than or lower than the safety threshold value due to unexpected faults, a lower cabin computer (35) in the capsule cabin automatically turns on a buzzer (44) and an alarm lamp (45) to warn a user to immediately leave the capsule.
8. The isolated closed capsule for simulating a local weather condition according to claim 1, wherein an in-capsule lower computer (35) sets a wind speed fluctuation threshold of a longitudinal section in the capsule according to a destination wind speed and a wind direction of weather forecast, a rotary driving motor (46) at the top of the capsule is started to drive a movable capsule shell (8) of a capsule interlayer to rotate, and 8 pairs of air inlets on a fixed capsule shell (9) of the capsule inner layer correspond to eight azimuth angles of east, south, west, north, southeast, southwest, northwest and northeast respectively; when two pairs of air inlets and air outlets on the interlayer movable cabin shell (8) are opposite to the air inlets and the air outlets which are in the same direction as the weather forecast wind direction on the fixed cabin shell (9) of the inner layer of the capsule cabin, the angular displacement sensor (47) simultaneously monitors that the angular displacement of the interlayer movable cabin shell (8) of the capsule cabin reaches a specified angle value, and the lower computer (35) in the capsule cabin turns off the rotary body driving motor (46) to start the circulating fan (48) in the cabin.
9. The isolated capsule of claim 1, wherein the physiological signal noise reduction processing module (52) filters the blood oxygen, heart rate, body temperature and electrocardiograph signals, respectively, to remove signal noise; the human physiological state detection control unit (53) of the off-board central control upper computer (30) of the capsule cabin carries out classification synchronous display monitoring on the blood oxygen, heart rate, body temperature and electrocardiosignals which are subjected to signal processing, and compares physiological parameters of a user in the weather of the eye examination of the capsule cabin with blood oxygen, heart rate, body temperature and heart rate variability indexes of the user before the user enters the capsule cabin.
10. The isolated closed capsule for simulating the experience of local weather conditions according to claim 1, wherein the smoke sensor (61) monitors that the smoke concentration in the capsule reaches a fire threshold, a buzzer (44) and a warning lamp (45) of an automatic control module of the air pressure in the capsule are automatically called by a lower computer (35) in the capsule to give out fire alarms to personnel in the capsule and outside the capsule, the locking seal of an electric capsule locking assembly (59) is immediately released, the capsule opening action of the hydraulic lifting platform (16) is lowered for a user to escape, and if the lower computer (35) in the capsule fails due to line faults, the capsule opening action can be started by the user in the capsule through a capsule emergency switch (62) arranged in the capsule; the personnel outside the cabin can also start the action of opening the cabin door through an upper computer (30) controlled by the middle of the cabin outside or a cabin cover emergency switch (62) arranged outside the cabin.
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Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113539047A (en) * 2021-08-20 2021-10-22 海南大学 Linkage type parallelization ecological environment simulation device and system

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE9002681L (en) * 1989-09-14 1991-03-15 Shimizu Construction Co Ltd SYSTEM TO CREATE A BEAUTIFUL ENVIRONMENT
GB2254447A (en) * 1991-05-17 1992-10-07 Norm Pacific Automat Corp Interior atmosphere control system.
US6502409B1 (en) * 2000-05-03 2003-01-07 Computer Process Controls, Inc. Wireless method and apparatus for monitoring and controlling food temperature
KR20100086781A (en) * 2009-01-23 2010-08-02 모건에프앤씨(주) The automatic control device for indoor ventilation using weather information and method for driving thereof
CN102945508B (en) * 2012-10-15 2014-01-29 风脉(武汉)可再生能源技术有限责任公司 Model correction based wind power forecasting method
KR20160035886A (en) * 2014-09-24 2016-04-01 한국화학연구원 An add-mounted cooling unit and an additional cooling method for a apparatus for realistic weathering test
CN105788400B (en) * 2016-03-07 2018-11-23 兵器工业卫生研究所 A kind of special vehicle people-machine-environment comprehensive experimental system for simulating
WO2018039433A1 (en) * 2016-08-24 2018-03-01 Delos Living Llc Systems, methods and articles for enhancing wellness associated with habitable environments
CN206558105U (en) * 2017-02-17 2017-10-13 湖南科技大学 Mine operation environment and safe artificial intelligence simulator
CN107122055A (en) * 2017-05-08 2017-09-01 佛山市神风航空科技有限公司 A kind of capsule cabin is gone sightseeing system
CN107462430B (en) * 2017-06-30 2019-06-07 上海建工集团股份有限公司 Climatic environment cabin for thermal performance of building envelope test
US10520213B2 (en) * 2017-10-27 2019-12-31 Haier Us Appliance Solutions, Inc. Air conditioner units and methods of operation
CN110425668B (en) * 2019-08-08 2021-03-16 长沙理工大学 Machine room heat pipe air conditioning system with emergency refrigeration function and control method thereof
CN110780653A (en) * 2019-11-12 2020-02-11 中国人民解放军军事科学院国防工程研究院 Normal-low pressure high-low temperature human body thermal comfort experiment environment cabin
CN113189964A (en) * 2021-04-27 2021-07-30 中国船舶工业集团公司第七0八研究所 Model test platform for fault mode response test of dynamic positioning system

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113539047A (en) * 2021-08-20 2021-10-22 海南大学 Linkage type parallelization ecological environment simulation device and system

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