Desert Space Rescue Integrated Life-saving Cabin

Abstract

The present invention discloses an integrated life-saving cabin for desert aerospace rescue, which relates to the field of aircraft technology, and includes five functional modules, namely, a medical rescue function module, an auxiliary function module, a flight function module, a communication function module, and a background planning function module: the medical rescue function module is mainly divided into two parts, namely, a monitoring function and a treatment function. The present invention communicates with the wounded in the desert through the communication function module, locates the wounded in the desert using the communication function module and the background planning module, deploys the position of the life-saving cabin using the flight function module, and after the wounded are found, monitors and treats the wounded's body using the medical rescue function module, diagnoses the wounded's condition through the auxiliary function module, and remotely connects to experts for diagnosis through the communication function module, guides the on-site medical staff to treat, and meets the needs of desert aviation rescue.

Description

Technical Field

[0001] The invention relates to the technical field of aircraft, in particular to an integrated life-saving cabin for desert aerospace rescue. Background Art

[0002] A life-saving cabin is a specially designed medical device or system, usually used for emergency medical treatment and rapid patient transfer. It can be used for emergency treatment, intensive care or occasions with specific medical needs. The life-saving cabin can carry medical equipment such as monitors, ventilators, medicines, etc. to provide necessary life support and medical treatment.

[0003] Desert areas often bring huge challenges to rescue work due to their harsh natural environment and complex geographical conditions. Especially in desert manned space return rescue missions, an integrated life-saving cabin that adapts to the desert environment is of vital importance. Summary of the invention

[0004] The purpose of the present invention is to provide an integrated life-saving cabin for desert aerospace rescue to solve the problems raised by the above-mentioned background technology.

[0005] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: a desert aerospace rescue integrated life-saving cabin, including five functional modules: a medical rescue function module, an auxiliary function module, a flight function module, a communication function module and a background planning function module:

[0006] The medical rescue function module is mainly divided into two parts: monitoring function and treatment function. Among them, the monitoring function is realized by equipping the treatment cabin with monitoring equipment, which is used to grasp the physical condition and rescue information of the injured; among them, the treatment function is realized by the built-in first aid device in the treatment cabin, which is used to carry out treatment work in harsh environments and emergency situations;

[0007] The auxiliary function module is mainly divided into three parts: AI diagnosis function, temperature control function and sealing and ventilation function. Among them, the AI ​​diagnosis function transmits and processes monitoring information through Bluetooth 5.4, and the monitoring information is generated by the inference engine in the main body, and finally the inference engine analyzes and obtains AI diagnosis. Among them, the automatic air-conditioning system uses the compressor for heating and cooling to realize the temperature control function. Among them, the treatment cabin adopts a sealed design, and the fan assists the automatic air-conditioning system to adjust the ventilation volume to realize the sealing and ventilation functions.

[0008] The flight function module mainly includes the helicopter deployment function and the autonomous flight function. The helicopter deployment function is realized by cooperating with the hook on the top of the rescue cabin and the helicopter hook delivery system to quickly deploy and withdraw the rescue cabin. The autonomous flight function includes the power redundancy system, unmanned operating system, control redundancy system, background planning system, intelligent obstacle avoidance function, and intelligent self-checking function.

[0009] The communication function module is mainly divided into communication ad hoc network, satellite communication, cellular network communication, and internal communication; the communication ad hoc network is used for the IoT signal connection of the rescue cabin; satellite communication is used to maintain a stable signal connection between the rescue cabin and the outside world; cellular network communication is used to establish a signal connection with a remote hospital; and internal communication is used for near-field anti-interference signal connection;

[0010] In the background planning function module, the control center is responsible for receiving, processing and analyzing data through the control console, the tablet device is responsible for personnel monitoring and management of the command post members, and the server software is responsible for the integration of data displayed in different modes.

[0011] Preferably, the monitoring equipment includes an electrocardiogram monitor, a cuff-type blood pressure monitor, a blood oxygen saturation meter, an ear thermometer, a respiration monitor, a handheld ultrasound and a stethoscope.

[0012] Preferably, the first aid equipment includes a defibrillator, an aspirator, a ventilator, an oxygen concentrator, a video laryngoscope, and cardiopulmonary resuscitation equipment, and the rescue function also includes configuring first aid medicines and consumables in the rescue cabin.

[0013] Preferably, the handheld ultrasound has two built-in voltage sensors. The scanning mode of the voltage sensor is at least one of using a high-frequency linear sensor for superficial scanning and using a curved sensor for deep scanning. The handheld ultrasound switches between three modes: B-type, M-type, and D-type ultrasound. An ultrasonic image is formed after chip processing and transmitted to the inference machine via Bluetooth 5.4. The inference machine analyzes and obtains an AI diagnosis, and the image and the AI ​​diagnosis result are displayed together.

[0014] Preferably, the diagnostic sound of the stethoscope is transmitted to the inference engine via Bluetooth 5.4, and the inference engine locally processes the auscultation sound to give a classification and diagnosis, which is displayed together with the visualized waveform.

[0015] Preferably, the autonomous flight function is achieved by equipping eight sets of arms outside the rescue cabin, each set of arms being equipped with a set of coaxial twin propellers.

[0016] Preferably, the helicopter deployment function is achieved by designing the arms to be foldable so that the arms can be folded and retracted during deployment and withdrawal, and the cabin of the rescue cabin adopts a streamlined design.

[0017] Preferably, the propeller blades of the coaxial twin propellers are made of carbon fiber T1100, and the coaxial twin propellers are driven to rotate by a brushless DC motor controlled by a sensorless FOC driver.

[0018] Preferably, the power redundancy system uses 12 sets of condensed matter aviation batteries, which are installed at the bottom of the rescue cabin to monitor the battery voltage, current, and temperature status in real time.

[0019] Preferably, the fuselage of the treatment cabin is made of carbon fiber reinforced plastic and aluminum alloy materials using a manufacturing process that combines CNC machining and 3D printing, and the surface of the fuselage is covered with a fluorocarbon coating of polyvinylidene fluoride.

[0020] Compared with the prior art, the present invention has the following beneficial effects:

[0021] 1. In the present invention, the communication function module is used to communicate with the wounded in the desert, the communication function module and the background planning module are used to locate the wounded in the desert, the flight function module is used to deploy the position of the life-saving cabin, and after the wounded are found, the medical rescue function module is used to monitor and treat the body of the wounded, the auxiliary function module is used to diagnose the condition of the wounded, and the communication function module is used to remotely connect with experts for diagnosis and guide the on-site medical staff to treat, thereby meeting the needs of desert aviation rescue.

[0022] 2. In the present invention, multiple communication channels of the life-saving cabin are constructed to meet the different communication needs of the life-saving cabin. A communication self-organizing network is used for wireless communication with high reliability and strong anti-strike and anti-interference capabilities. Satellite communication is used for long-distance and stable external communication. Cellular network communication and video communication are used. Internal communication is used for communication between the sensor monitoring instruments inside the life-saving cabin and the host, so as to provide a safe and reliable network link for the perception of the wounded.

[0023] 3. In the present invention, the power system of the rescue cabin adopts 12 groups of condensed matter aviation batteries, which are installed at the bottom of the rescue cabin by taking advantage of their smaller size, higher safety and long cycle life, thereby reducing the battery weight in the total empty cabin weight of the rescue cabin and increasing the flight range. The 12-group battery system provides a large amount of power redundancy backup to ensure flight safety.

[0024] 4. In the present invention, the treatment cabin adopts carbon fiber reinforced plastic, aluminum alloy and 3D printing technology to ensure structural strength and lightness.

[0025] 5. In the present invention, the rescue cabin has two transfer modes: helicopter deployment and autonomous flight. It can use its own power to transfer the wounded by air. The hook on the top of the rescue cabin is connected to the helicopter's hanging and delivery system, which can be deployed and withdrawn quickly and reliably. BRIEF DESCRIPTION OF THE DRAWINGS

[0026] Figure 1 This is the overall system block diagram of the desert space rescue integrated life-saving cabin of the present invention;

[0027] Figure 2 It is a system block diagram of the medical rescue function module in the desert aerospace rescue integrated life-saving cabin of the present invention;

[0028] Figure 3 It is a system block diagram of the auxiliary function modules in the desert aerospace rescue integrated life-saving cabin of the present invention;

[0029] Figure 4 It is a system block diagram of the flight function module in the desert aerospace rescue integrated life-saving cabin of the present invention;

[0030] Figure 5 It is a system block diagram of the communication function module in the desert aerospace rescue integrated life-saving cabin of the present invention;

[0031] Figure 6 This is a system block diagram of the background planning function module in the desert aerospace rescue integrated life-saving cabin of the present invention. DETAILED DESCRIPTION

[0032] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the implementation regulations described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0033] Embodiment 1: According to Figure 1 - Figure 6 As shown: Desert space rescue integrated life-saving cabin, including medical rescue function module, auxiliary function module, flight function module, communication function module and background planning function module;

[0034] The medical rescue function module is mainly divided into two parts: monitoring function and treatment function. Among them, the monitoring function is realized by equipping the treatment cabin with monitoring equipment, which is used to grasp the physical condition and rescue information of the injured; among them, the treatment function is realized by the built-in first aid device in the treatment cabin, which is used to carry out treatment work in harsh environments and emergency situations;

[0035] The auxiliary function module is mainly divided into three parts: AI diagnosis function, temperature control function and sealing and ventilation function. Among them, the AI ​​diagnosis function transmits and processes monitoring information through Bluetooth 5.4, and the monitoring information is generated by the inference engine in the main body, and finally the inference engine analyzes and obtains AI diagnosis. Among them, the automatic air-conditioning system uses the compressor for heating and cooling to realize the temperature control function. Among them, the treatment cabin adopts a sealed design, and the fan assists the automatic air-conditioning system to adjust the ventilation volume to realize the sealing and ventilation functions.

[0036] The flight function module mainly includes the helicopter deployment function and the autonomous flight function. The helicopter deployment function is realized by cooperating with the hook on the top of the rescue cabin and the helicopter hook delivery system to quickly deploy and withdraw the rescue cabin. The autonomous flight function includes the power redundancy system, unmanned operating system, control redundancy system, background planning system, intelligent obstacle avoidance function, and intelligent self-checking function.

[0037] The communication function module is mainly divided into communication ad hoc network, satellite communication, cellular network communication, and internal communication; the communication ad hoc network is used for the IoT signal connection of the rescue cabin; satellite communication is used to maintain a stable signal connection between the rescue cabin and the outside world; cellular network communication is used to establish a signal connection with a remote hospital; and internal communication is used for near-field anti-interference signal connection;

[0038] In the background planning function module, the control center is responsible for receiving, processing and analyzing data through the control console, the tablet device is responsible for personnel monitoring and management of the command post members, and the server software is responsible for the integration of data displayed in different modes.

[0039] In this embodiment, the logical operating relationship between the five functional modules of the rescue cabin is as follows: the medical rescue function module utilizes the AI ​​diagnostic function of the auxiliary function module, specifically realizes wireless data transmission through Bluetooth 5.4 technology. The auxiliary function module also involves temperature control function and sealing and ventilation function. The temperature control function creates a stable and comfortable cabin environment in the harsh desert environment and assists in the implementation of the rescue function. The rescue cabin is sealed with tiny textures and protective coatings on the surface to reduce the adhesion and erosion of wind and sand. The doors and windows adopt double-layer sealing, with multi-layer sealing strips and tightly combined components. The outer layer is high-strength polycarbonate with excellent impact resistance. The inner layer is transparent air condensation, which insulates against heat and cold and blocks ultraviolet rays. The frame uses stainless steel with good sealing performance. During the hot desert daytime, after the doors and windows are closed, the internal temperature can be more than 20 degrees Celsius lower than the external temperature. The vents are set at the rear of the cabin and adopt a multi-layer filter structure, including a primary filter, a high-efficiency HEPA filter and an activated carbon adsorption layer, which can remove sand, dust and pathogens in the ambient air; the fan coordinates the air-conditioning system, which can automatically adjust the ventilation volume according to the air quality and the number of people in the cabin. After the dust, the sand and dust in the cabin can be cleared in a short time. The life-saving cabin is combined with the medical rescue function module and the auxiliary function module to realize the rescue in the desert.

[0040] The flight function module realizes the space flight of the life-saving cabin in the desert. The helicopter deployment function and the autonomous flight function realize the space flight of the life-saving cabin from the two aspects of external drive and self-drive respectively. As an aircraft, safety is the first priority. For this reason, the self-service flight module of the life-saving cabin needs to do the following: the power redundancy system is driven by multiple independent engines and propellers to provide sufficient distributed power redundancy to reduce the safety risks caused by partial power failure; the unmanned operating system reduces the risks caused by human operation errors of the pilots and reduces the number of members required to be carried in the life-saving cabin under the premise of ensuring safety; the system redundancy system provides multiple flight control, communication and navigation systems; the background planning system and cluster management ensure safe operation; intelligent obstacle avoidance functions, such as communication self-organizing network, visual positioning, millimeter wave radar, etc.; the intelligent self-check function automatically detects and monitors the safety status of the aircraft before flight. When the autonomous flight function of the life-saving cabin cannot be enabled, it is necessary to realize the space flight function of the life-saving cabin through external drive. The hook on the top of the life-saving cabin is connected to the helicopter's hanging delivery system, which can be deployed and withdrawn quickly and reliably.

[0041] The communication function module is divided into four different communication modes, which meet different signal transmission requirements through different communication modes, and strengthen the information security protection during communication through multi-line transmission;

[0042] In desert environments, due to complex terrain and severe interference, communication, network and processing capabilities often decline, making it difficult to use cloud computing and network architecture to support edge intelligence applications in the Internet of Things. Therefore, self-organizing network communication technology is used to autonomously find the optimal path for data backhaul or relay, and any two modules can communicate. Its communication frequency band is the L band, with five optional bands of 4 / 8 / 10 / 14 / 20MHz. It has the characteristics of self-allocation, self-management, self-repair, no center, no base station, and strong reliability, anti-strike and anti-interference capabilities.

[0043] Satellite communication uses Guangzhou Runxin RF chip RX6003EQK and Huali Chuangtong military communication baseband chip HTD2001. Among them, RX6003EQK supports conventional and emergency life-saving modes, supports FDD / TDD standards, and can realize S-band satellite signal reception and transmission and Beidou B1 / GPS L1 band reception functions, providing satellite direct connection for the rescue capsule; due to the limitation of satellite communication rate, only call and text sending functions can be realized; considering the terminal size and power consumption, a satellite antenna with moderate size, length and gain is adopted to ensure a stable link with the outside world at all times.

[0044] Cellular network communication uses Huawei's Balong 5000 baseband chip, supports 2G / 3G / 4G / 5G network standards, and can establish high-definition video links with remote hospitals under 4G / 5G conditions, general video links under 3G conditions, and voice call links under 2G conditions.

[0045] Internal communications include communication between sensor monitoring instruments and the host, and interconnection and communication between cameras, microphones, smart glasses and display screens. Bluetooth 5.4 is used, which has strong anti-interference capabilities during near-field communication, ensuring flexible, stable, low-latency, and low-power connection between short-range devices, and clearly transmitting sound, images and general data.

[0046] Finally, the background planning function module is the focus and optimization difficulty of the entire system. It needs to have intelligent planning, intelligent grouping, intelligent coordination, and intelligent allocation functions. It can provide a technical basis for the construction and transformation of unmanned intelligent rescue systems through communication with artificial intelligence perception and command systems. The command center is composed of a control console, tablet devices, server software, etc. The server software integrates databases, monitoring and storage data software, APP access interfaces and network servers.

[0047] Embodiment 2: According to Figure 1 and Figure 2 As shown, the monitoring equipment includes an ECG monitor, a blood pressure cuff monitor, a blood oxygen saturation monitor, an ear thermometer, a respiratory monitor, a handheld ultrasound, and a stethoscope;

[0048] The handheld ultrasound has two built-in voltage sensors. The voltage sensors use at least one of the following scanning modes: high-frequency linear sensors for superficial scanning and curved sensors for deep scanning. The handheld ultrasound switches between three modes: B-mode, M-mode, and D-mode ultrasound. The ultrasound image is processed by the chip and transmitted to the inference engine via Bluetooth 5.4. The inference engine analyzes the image and obtains the AI ​​diagnosis. The image and the AI ​​diagnosis result are displayed together.

[0049] The diagnostic sound of the stethoscope is transmitted to the inference engine via Bluetooth 5.4, which processes the sound locally to give a classification and diagnosis of the auscultation sound and displays it together with the visualized waveform.

[0050] In this embodiment, each monitoring device transmits signals via Bluetooth 5.4, transmits auxiliary diagnosis information and collected data to the host, and after being calculated and integrated by the host, is displayed on various display terminals, including the monitor screen and the smart glasses worn by medical personnel. The remote medical system is transmitted in real time through satellite and cellular data networks. Even if the medical personnel are not next to the treatment cabin, they can grasp the physical condition and rescue information of the injured in real time, and issue remote diagnosis and treatment plans. Each monitoring device adopts a wireless signal transmission solution, and no additional wires are required to connect to the host. Each monitoring device has its own battery, which can work continuously for about 8 hours, and supports hot plugging and charging of external power supplies;

[0051] The handheld ultrasound is a portable ultrasound diagnostic device. The B-mode ultrasound mode shows the physical property changes of organs or tissues in grayscale changes from white to gray and then to black. It is a two-dimensional image (black and white gray image) of brightness modulation mode. The D-mode ultrasound mode uses ultrasound to auscultate, measure blood flow and determine the direction of blood flow. On the basis of the two-dimensional image of the B-mode ultrasound mode, it has the function of detecting blood flow. It can not only provide intuitive circulating blood flow images, but also display the time and space information of blood flow in the heart and blood vessels. It is widely used in auxiliary examinations of cardiovascular diseases. The M-mode ultrasound mode applies the display principle of echocardiography and uses a single sound beam to scan the heart. It is often used to display the movement of heart and blood vessels to diagnose heart diseases, understand myocardial activity, and determine the type of arrhythmia. The image is processed locally by the host to give diagnostic opinions on typical critical and severe injuries such as rupture of solid organs in the chest and abdominal cavity, craniocerebral injury, massive hemorrhage, and spinal and limb fractures. The image and diagnosis are displayed together at the specified position on the display screen.

[0052] The stethoscope consists of a double-sided adhesive ring, a stethoscope head, an ESP32 chip, a connecting part, a lithium battery power supply, and a display screen. The double-sided adhesive ring surface at the stethoscope head is extremely narrow and thin, with good airtightness and can prevent movement. The physical noise reduction effect is significantly better than that of shockproof rubber rings or rubber tubes, which are easy to deform or move and can generate certain noise. On the basis of the physical noise reduction of the double-sided adhesive ring, triple noise reduction is achieved through MEMS digital microphones and software codes. The sound is transmitted to the smart glasses and the host via Bluetooth, and the classification and diagnosis of the stethoscope sound are given after local processing by the host, and displayed together with the visual waveform on the smart glasses and monitoring screen.

[0053] Embodiment 3: According to Figure 1 and Figure 2 As shown, the first aid equipment includes a defibrillator, a suction device, a ventilator, an oxygen concentrator, a video laryngoscope, and cardiopulmonary resuscitation equipment. The rescue function also includes first aid medicines and consumables built into the rescue cabin.

[0054] In this embodiment, the defibrillator uses AED technology and is easy to operate;

[0055] The cardiopulmonary resuscitation equipment performs chest compressions at a preset frequency and depth, allowing at least one medical staff member to perform other rescue operations and avoiding fatigue and irregularities that may occur during manual compressions;

[0056] The respirator is a pneumatic and electrically controlled emergency transport breathing device with four ventilation modes: control / assist (A / C), synchronized intermittent command (SIMV), spontaneous breathing (SPONT) and manual control (Manual). It is compact and has a total mass of about 1kg.

[0057] The oxygen concentrator is a molecular sieve adsorption type oxygen concentrator with an oxygen production capacity of 8L / min, an oxygen purity of 96±3%, and a maximum alveolar oxygen concentration of 54%, which can meet the oxygen demand under various pathological and physiological conditions in pre-hospital and transport emergency treatment;

[0058] The suction device has two modes: suction and aspiration, which can remove foreign matter or secretions from the respiratory tract, and blood and fluid accumulation in the serous cavity of the surgical field;

[0059] Video laryngoscope and endotracheal intubation related equipment, which facilitate endotracheal intubation and effective airway management when necessary;

[0060] In addition, the rescue cabin is equipped with some emergency medicines and consumables, most of which are infusion and blood transfusion medicines. The infusion uses an electric non-gravity infusion device, including an infusion pump, a portable field intelligent infusion device, a CNC pressure infusion machine, an electric pressurized infusion device, etc. It has anti-backflow and bubble monitoring functions, and can accurately control the infusion speed and dosage in harsh environments and limited transportation conditions. The blood transfusion device can store and manage a certain amount of blood and blood components for a short period of time (5-7 days), has blood filtration and pressurization functions, and is safe and efficient.

[0061] To ensure that rescue work can be carried out in harsh environments and emergency situations, all equipment must undergo quality inspection and reliability testing under the same working conditions, be maintained and calibrated monthly, and medical staff must master and practice the use of these first aid devices to keep people and machines in the best condition and be ready to deal with various emergencies of astronauts during the return of manned spaceflight.

[0062] Embodiment 4: According to Figure 1 , Figure 4 , Figure 5 and Figure 6 As shown in the figure, the autonomous flight function is achieved by equipping eight sets of arms outside the rescue cabin, each set of arms is equipped with a set of coaxial twin propellers. The helicopter deployment function is achieved by designing the arms to be foldable so that the arms can be folded and retracted during deployment and withdrawal. The cabin body of the rescue cabin adopts a streamlined design. The propeller blades of the coaxial twin propellers are made of carbon fiber T1100, and the brushless DC motor driven by the sensorless FOC driver controls the rotation of the coaxial twin propellers.

[0063] The fuselage of the treatment cabin is made of carbon fiber reinforced plastic and aluminum alloy materials, using a manufacturing process that combines CNC machining and 3D printing. The surface of the fuselage is covered with polyvinylidene fluoride fluorocarbon coating. The power redundancy system uses 12 sets of condensed aviation batteries installed at the bottom of the treatment cabin to monitor the battery voltage, current, temperature and other status in real time.

[0064] In this embodiment, the materials and design of the coaxial twin propellers greatly save the space and parts required for the installation of propellers and motors; the blades are made of carbon fiber T1100, which is high in strength and light in weight, and use an independent Kirin 9000s CPU inference engine for sensor reception and flight control calculations, which can accurately control the flight attitude and trajectory.

[0065] Since the weight of batteries accounts for about 1 / 3 of the empty cabin weight of the rescue cabin, battery weight reduction will greatly increase the flight range. Therefore, the battery uses 12 sets of condensed aviation batteries. Unlike lithium-ion batteries with liquid electrolytes and all-solid-state electrolyte batteries, it uses high-power bionic condensed electrolytes, high-nickel ternary positive electrodes, graphite or silicon-based negative electrodes and adaptive mesh diaphragms, with an energy density of 500Wh / kg. It has the characteristics of smaller size, higher safety and long cycle life. The 12-set battery system provides a large amount of power redundancy backup. Even if one or several sets of batteries fail, the power system can still work normally. The fuselage structure uses carbon fiber reinforced plastics and aluminum alloys to optimize strength and rigidity, maximize the strength-to-weight ratio, and have both lightweight and rigidity; the surface is covered with fluorocarbon coatings of polyvinylidene fluoride (PVDF), which are resistant to weather, heat, low temperature and corrosion, and can resist erosion and damage in extreme environments. Together with the strong fuselage, it forms a solid structural foundation for the rescue cabin.

[0066] For components with complex structures, such as cabin frames and key connectors, CNC is used to achieve precise processing; 3D printing is used to manufacture components with special shapes that are difficult to process using traditional processes, such as medical equipment structures and housings. It can achieve rapid prototyping and mass production, greatly shortening the R&D cycle.

[0067] The method of use and working principle of this device: When astronauts suffer physical injuries or sudden illnesses after landing, the integrated life-saving cabin can quickly arrive at the scene. It is beneficial for the navigation system to quickly and accurately locate the astronauts. After entering the rescue cabin, medical personnel can use the advanced medical equipment equipped in the cabin to immediately conduct a comprehensive physical examination and diagnosis for the astronauts. From vital sign monitoring to wound treatment, from infusion and blood transfusion to emergency surgery, the rescue cabin can provide corresponding conditions and support. At the same time, through efficient transportation methods, such as rapid docking with helicopters or autonomous flight, astronauts can be safely and quickly transferred to temporary bases or medical institutions. During the transportation process, medical personnel can continue to monitor and treat the astronauts to ensure that their condition is stable.

[0068] Although the present invention has been described in detail with reference to the aforementioned embodiments, it is still possible for those skilled in the art to modify the technical solutions described in the aforementioned embodiments, or to make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. Desert space rescue integrated life-saving cabin, characterized by: It includes five functional modules: The medical rescue function module is mainly divided into two parts: monitoring function and treatment function. Among them, the monitoring function is realized by equipping the treatment cabin with monitoring equipment, which is used to grasp the physical condition and rescue information of the injured; among them, the treatment function is realized by the built-in first aid device in the treatment cabin, which is used to carry out treatment work in harsh environments and emergency situations; The auxiliary function module is mainly divided into three parts: AI diagnosis function, temperature control function and sealing and ventilation function. Among them, the AI ​​diagnosis function transmits and processes monitoring information through Bluetooth 5.4, and the monitoring information is generated by the inference engine in the main body, and finally the inference engine analyzes and obtains AI diagnosis. Among them, the automatic air-conditioning system uses the compressor for heating and cooling to realize the temperature control function. Among them, the treatment cabin adopts a sealed design, and the fan assists the automatic air-conditioning system to adjust the ventilation volume to realize the sealing and ventilation functions. The flight function module mainly includes the helicopter deployment function and the autonomous flight function. The helicopter deployment function is realized by cooperating with the hook on the top of the rescue cabin and the helicopter hook delivery system to quickly deploy and withdraw the rescue cabin. The autonomous flight function includes the power redundancy system, unmanned operating system, control redundancy system, background planning system, intelligent obstacle avoidance function, and intelligent self-checking function. The communication function module is mainly divided into communication ad hoc network, satellite communication, cellular network communication, and internal communication; the communication ad hoc network is used for the IoT signal connection of the rescue cabin; satellite communication is used to maintain a stable signal connection between the rescue cabin and the outside world; cellular network communication is used to establish a signal connection with a remote hospital; and internal communication is used for near-field anti-interference signal connection; As well as the background planning function module, the control center is responsible for receiving, processing and analyzing data through the control console, the tablet device is responsible for personnel monitoring and management of the command post members, and the server software is responsible for the integration of data displayed in different modes.

2. The desert space rescue integrated life-saving cabin according to claim 1 is characterized by: Monitoring equipment includes ECG monitor, blood pressure cuff monitor, blood oxygen saturation monitor, ear thermometer, respiratory monitor, handheld ultrasound and stethoscope.

3. The desert space rescue integrated life-saving cabin according to claim 1 is characterized by: The first aid equipment includes a defibrillator, a suction device, a ventilator, an oxygen concentrator, a video laryngoscope, and cardiopulmonary resuscitation equipment. The rescue function also includes first aid medicines and consumables built into the treatment cabin.

4. The desert space rescue integrated life-saving cabin according to claim 2 is characterized by: The handheld ultrasound has two built-in voltage sensors. The scanning method of the voltage sensor is at least one of using a high-frequency linear sensor for superficial scanning and using a curved sensor for deep scanning. The handheld ultrasound switches between three modes: B-type, M-type, and D-type ultrasound. The ultrasound image is formed after chip processing and transmitted to the inference engine via Bluetooth 5.

4. The inference engine analyzes and obtains AI diagnosis, and the image and AI diagnosis results are displayed together.

5. The desert space rescue integrated life-saving cabin according to claim 2 is characterized by: The diagnostic sound of the stethoscope is transmitted to the inference engine via Bluetooth 5.4, which processes the sound locally to give a classification and diagnosis of the auscultation sound and displays it together with the visualized waveform.

6. The desert space rescue integrated life-saving cabin according to claim 1 is characterized by: The autonomous flight function is achieved by equipping eight sets of arms outside the treatment cabin, each set of arms is equipped with a set of coaxial double propellers.

7. The desert space rescue integrated life-saving cabin according to claim 6 is characterized by: The helicopter deployment function is achieved by designing the arms to be foldable so that they can be folded and stowed during deployment and withdrawal. The cabin of the rescue cabin adopts a streamlined design.

8. The desert space rescue integrated life-saving cabin according to claim 6 is characterized by: The propeller blades of the coaxial twin propellers are made of carbon fiber T1100, and the coaxial twin propellers are driven to rotate by a brushless DC motor controlled by a sensorless FOC driver.

9. The desert space rescue integrated life-saving cabin according to claim 1 is characterized by: The power redundancy system uses 12 sets of condensed matter aviation batteries, which are installed at the bottom of the treatment cabin to monitor the battery voltage, current, and temperature status in real time.

10. The desert space rescue integrated life-saving cabin according to claim 1 is characterized by: The fuselage of the treatment cabin is made of carbon fiber reinforced plastic and aluminum alloy materials, using a manufacturing process that combines CNC machining and 3D printing. The surface of the fuselage is covered with polyvinylidene fluoride fluorocarbon coating.

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