Escape system and method

By designing an escape system including a safety compartment backpack and drone components, the problem of escapees being unable to save themselves when mudslides occur is solved, and the escapees being able to rescue themselves and safely escape are achieved.

CN120135446APending Publication Date: 2025-06-13BEIJING XINSHUCHUANG ENVIRONMENTAL PROTECTION TECH CO LTD
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Patent Information

Application Number
CN202510550031.2
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-04-28
Publication Date
2025-06-13

AI Technical Summary

Technical Problem

In the prior art, escapees cannot save themselves when mudslides occur and need to rely on rescue personnel for rescue.

Method used

An escape system was designed, including a safety compartment backpack assembly and drone components. The body of the safety compartment backpack is used to fix the escape personnel. The balloon assembly lifts the public part of the intelligent connecting lock into the air through an inert gas balloon, and locks it with the female part of the intelligent connecting lock of the drone assembly. Finally, the drone carries the safety compartment backpack assembly and escape personnel to escape.

Benefits of technology

The escapees are realized when mudslides occur, and the escape personnel and escape systems are carried by the drone to ensure that the escape personnel can escape safely.

✦ Generated by Eureka AI based on patent content.

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Abstract

The invention provides an escape system and method, and relates to the technical field of urgent danger prevention. The system comprises a safety bin backpack assembly and an unmanned aerial vehicle assembly. Wherein the safety bin backpack assembly comprises a safety bin backpack body and a balloon assembly, and the unmanned aerial vehicle assembly comprises an unmanned aerial vehicle body and an intelligent connection lock nut part. The safety cabin backpack body is used for responding to an escape instruction and fixing an escape person; the inert gas balloon is used for lifting the intelligent connection lock male part into the air; the intelligent connection lock female part is used for being locked with the intelligent connection lock male part; and the unmanned aerial vehicle body is used for bearing the safety bin backpack assembly to escape from escape personnel after the intelligent connection lock female part and the intelligent connection lock male part are locked. In this way, when a debris flow disaster occurs, escape personnel are fixed to the safety bin backpack body firstly and then locked through the balloon assembly and the unmanned aerial vehicle assembly, so that the unmanned aerial vehicle can bear the safety bin backpack assembly to escape from the escape personnel, and self rescue of the escape personnel in the debris flow disaster is achieved.
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Description

Technical Field

[0001] This application relates to the technical field of emergency avoidance, and particularly to an escape system and method. Background Art

[0002] Debris flow is a highly destructive natural disaster that usually occurs in mountainous areas or valleys and is triggered by natural factors such as heavy rain, snowmelt, earthquakes, or human activities. Its essence is a special flood formed by a large amount of solid substances (such as sediment, stones, soil, etc.) mixed with water, with characteristics such as fast flow velocity, strong impact force, and wide destruction range. Debris flow is sudden and highly destructive. In the existing technology, generally, after a debris flow occurs, rescue personnel rescue the victims, and during the occurrence of the debris flow, the escaping people cannot carry out self-rescue.

[0003] In summary, how to enable the escaping people to carry out self-rescue during the occurrence of a debris flow is an urgent problem that needs to be solved by those skilled in the art. Summary of the Invention

[0004] In view of this, this application provides an escape system and method, aiming to enable the escaping people to carry out self-rescue during the occurrence of a debris flow.

[0005] In the first aspect, this application provides an escape system, including:

[0006] The safety cabin backpack assembly includes a safety cabin backpack body and a balloon assembly;

[0007] The safety cabin backpack body is used to fix the escaping people in response to an escape instruction;

[0008] The balloon assembly includes an inert gas balloon and a male part of an intelligent connection lock;

[0009] The inert gas balloon is used to lift the male part of the intelligent connection lock into the air;

[0010] The UAV assembly includes a UAV body and a female part of an intelligent connection lock;

[0011] The female part of the intelligent connection lock is used to lock with the male part of the intelligent connection lock;

[0012] The UAV body is used to carry the safety cabin backpack assembly and the escaping people to escape after the female part of the intelligent connection lock locks with the male part of the intelligent connection lock.

[0013] Optionally, the male part of the intelligent connection lock includes a first lock head, a first UWB pulse signal transmitter, and a first magnetic attraction positioning device;

[0014] The female part of the intelligent connection lock includes a second lock head, a second UWB pulse signal transmitter, and a second magnetic attraction positioning device;

[0015] The male part and the female part of the intelligent connection lock are used for docking through the first UWB pulse signal transmitter, the second UWB pulse signal transmitter, the first magnetic attraction positioning device, and the second magnetic attraction positioning device;

[0016] The first lock head and the second lock head are used for locking when the male part and the female part of the intelligent connection lock are successfully docked.

[0017] Optionally, the safety cabin backpack body includes:

[0018] A safety belt assembly for fixing the escape personnel to the safety cabin backpack body in response to the escape instruction.

[0019] Optionally, the balloon assembly further includes:

[0020] A first compressed gas cylinder for inflating the inert gas balloon in response to the fixation of the escape personnel.

[0021] Optionally, the balloon assembly further includes:

[0022] A safety rope for connecting the inert gas balloon and the safety cabin backpack body.

[0023] Optionally, the safety cabin backpack assembly further includes:

[0024] An emergency rescue airbag cushion cabin including a plurality of buffer airbags;

[0025] When the escape personnel are in the air, the buffer airbags inflate automatically.

[0026] Optionally, the emergency rescue airbag cushion cabin further includes:

[0027] A second compressed gas cylinder for inflating the buffer airbags if the air pressure of the buffer airbags is less than a preset value after the buffer airbags have completed self-inflation.

[0028] Optionally, the system further includes:

[0029] The safety cabin backpack storage box includes a storage box body and a backup power supply;

[0030] The storage box body is used for storing the safety cabin backpack assembly;

[0031] The backup power supply is used for charging the safety cabin backpack assembly.

[0032] Optionally, the safety cabin backpack storage box further includes:

[0033] An alarm device for emitting an alarm when a disaster occurs.

[0034] In a second aspect, the present application provides an escape method, including:

[0035] In response to an escape instruction, using the safety compartment backpack body in the safety compartment backpack assembly to fix the escape personnel; the safety compartment backpack assembly includes the safety compartment backpack body and a balloon assembly; the balloon assembly includes an inert gas balloon and a male part of an intelligent connection lock;

[0036] Using the inert gas balloon to lift the male part of the intelligent connection lock into the air;

[0037] Locking the male part of the intelligent connection lock with the female part of the intelligent connection lock of the drone assembly; the drone assembly includes a drone body and the female part of the intelligent connection lock;

[0038] After the female part of the intelligent connection lock is locked with the male part of the intelligent connection lock, using the drone body to carry the safety compartment backpack assembly and the escape personnel to escape.

[0039] Optionally, the male part of the intelligent connection lock includes a first lock head, a first UWB pulse signal transmitter, and a first magnetic attraction positioning device; the female part of the intelligent connection lock includes a second lock head, a second UWB pulse signal transmitter, and a second magnetic attraction positioning device. The locking of the male part of the intelligent connection lock with the female part of the intelligent connection lock of the drone assembly includes:

[0040] Docking the male part of the intelligent connection lock and the female part of the intelligent connection lock through the first UWB pulse signal transmitter, the second UWB pulse signal transmitter, the first magnetic attraction positioning device, and the second magnetic attraction positioning device;

[0041] When the docking of the male part of the intelligent connection lock and the female part of the intelligent connection lock is completed, locking the first lock head and the second lock head.

[0042] Optionally, the safety compartment backpack body further includes a seat belt assembly. The using the safety compartment backpack body in the safety compartment backpack assembly to fix the escape personnel in response to an escape instruction includes:

[0043] In response to the escape instruction, using the seat belt assembly to fix the escape personnel to the safety compartment backpack body.

[0044] Optionally, the balloon assembly further includes a first compressed gas cylinder. Before using the inert gas balloon to lift the male part of the intelligent connection lock into the air, the method further includes:

[0045] In response to the escape personnel being fixed, using the first compressed gas cylinder to inflate the inert gas balloon.

[0046] Optionally, the balloon assembly further includes a safety rope, and the method further includes:

[0047] Connecting the inert gas balloon and the safety cabin backpack body using the safety rope.

[0048] Optionally, the safety cabin backpack assembly further includes an emergency air cushion bin, and the emergency air cushion bin includes a plurality of buffer air bags. The method further includes:

[0049] When the escapee is in the air, the buffer air bags inflate automatically.

[0050] Optionally, the emergency air cushion bin further includes a second compressed gas cylinder. After the buffer air bags inflate automatically when the escapee is in the air, the method further includes:

[0051] After the buffer air bags complete self-inflation, if the air pressure of the buffer air bags is less than a preset value, use the second compressed gas cylinder to inflate the buffer air bags.

[0052] Optionally, the method further includes:

[0053] Using the storage box body of the safety cabin backpack storage box to store the safety cabin backpack assembly; the safety cabin backpack storage box includes the storage box body and a backup power supply;

[0054] Charging the safety cabin backpack assembly using the backup power supply.

[0055] Optionally, the safety cabin backpack storage box further includes an alarm device, and the method further includes:

[0056] When a disaster occurs, use the alarm device to issue an alarm.

[0057] The present application provides an escape system. The system includes: a safety cabin backpack assembly and a drone assembly; wherein, the safety cabin backpack assembly includes a safety cabin backpack body and a balloon assembly, and the drone assembly includes a drone body and an intelligent connection lock female part. The safety cabin backpack body is used to fix the escapee in response to an escape instruction; the inert gas balloon is used to lift the intelligent connection lock male part into the air; the intelligent connection lock female part is used to lock with the intelligent connection lock male part; the drone body is used to carry the safety cabin backpack assembly and the escapee to escape after the intelligent connection lock female part locks with the intelligent connection lock male part. In this way, when a debris flow disaster occurs, the escapee first fixes with the safety cabin backpack body, and then locks with the drone assembly through the balloon assembly, so that the drone can carry the safety cabin backpack assembly and the escapee to escape. In this way, self-rescue of the escapee when a debris flow occurs is realized. Description of the Drawings

[0058] To more clearly illustrate the technical solutions in this embodiment or the prior art, the following will briefly introduce the accompanying drawings required for the description of the embodiment or the prior art. Obviously, the accompanying drawings in the following description are only some embodiments of the present application. For those of ordinary skill in the art, without creative efforts, other accompanying drawings can also be obtained based on these drawings.

[0059] Figure 1 It is a schematic structural diagram of an escape system provided by an embodiment of the present application;

[0060] Figure 2 It is a schematic structural diagram of a safety cabin backpack assembly provided by an embodiment of the present application;

[0061] Figure 3 It is a schematic structural diagram of another safety cabin backpack assembly provided by an embodiment of the present application;

[0062] Figure 4 It is a schematic diagram of a drone body carrying an escapee to escape provided by an embodiment of the present application;

[0063] Figure 5 It is a schematic diagram of another drone body carrying an escapee to escape provided by an embodiment of the present application;

[0064] Figure 6 It is a flowchart of an escape method provided by an embodiment of the present application. Detailed implementation manners

[0065] The following will clearly and completely describe the technical solutions in the embodiments of the present application in conjunction with the accompanying drawings in the embodiments of the present application. An escape system and method provided by the present application are used in the technical field of emergency avoidance. The above is only an example and does not limit the application fields of the method and device names provided by the present application.

[0066] Debris flow is a highly destructive natural disaster that usually occurs in mountainous areas or valleys and is triggered by natural factors such as heavy rain, snowmelt, earthquakes, or human activities. Its essence is a special flood formed by a large amount of solid substances (such as sediment, stones, soil, etc.) mixed with water, and it has characteristics such as fast flow velocity, strong impact force, and wide damage range. Debris flow is sudden and highly destructive. In the prior art, generally, after a debris flow occurs, rescue personnel rescue the victims, and during the occurrence of a debris flow, the escapees cannot carry out self-rescue.

[0067] The inventor proposed the technical solution of this application through research. The escape system includes: a safety cabin backpack assembly and a drone component; among them, the safety cabin backpack assembly includes a safety cabin backpack body and a balloon component, and the drone component includes a drone body and an intelligent connection lock female part. The safety cabin backpack body is used to fix the escape personnel in response to an escape instruction; the inert gas balloon is used to lift the intelligent connection lock male part into the air; the intelligent connection lock female part is used to lock with the intelligent connection lock male part; the drone body is used to carry the safety cabin backpack assembly and the escape personnel to escape after the intelligent connection lock female part and the intelligent connection lock male part are locked. In this way, when a debris flow disaster occurs, the escape personnel first fix themselves to the safety cabin backpack body, and then lock with the drone component through the balloon component, so that the drone can carry the safety cabin backpack assembly and the escape personnel to escape. In this way, the self-rescue of the escape personnel during the debris flow is realized.

[0068] In order to enable the personnel in the technical field to better understand the solution of this application, the following further detailed description of this application will be given in conjunction with the drawings and specific implementation manners. Obviously, the described embodiments are only a part of the embodiments of this application, rather than all the embodiments. Based on the embodiments in this application, all other embodiments obtained by those of ordinary skill in the art without making creative efforts shall fall within the protection scope of this application. It should be noted that, for the sake of convenience of description, only the parts related to the invention are shown in the drawings. Without conflict, the embodiments in this application and the features in the embodiments can be combined with each other.

[0069] See Figure 1 , Figure 1 is a schematic structural diagram of an escape system provided by an embodiment of this application, including:

[0070] A safety cabin backpack assembly 110 and a drone component 120; among them, the safety cabin backpack assembly 110 includes a safety cabin backpack body and a balloon component, and the drone component includes a drone body and an intelligent connection lock female part.

[0071] The safety cabin backpack body is used to fix the escape personnel in response to an escape instruction. Among them, the escape instruction can be issued by the escape personnel through a remote control. Specifically, the safety cabin backpack assembly 110 further includes: a seat belt component, which fixes the escape personnel to the safety cabin backpack body in response to the escape instruction. Figure 2 As described above, Figure 2 is a schematic structural diagram of a safety cabin backpack assembly provided by an embodiment of this application, including: a safety cabin backpack body 01 and a seat belt component 02. In actual application, the escape personnel can carry the safety cabin backpack body 01 on their backs, and then fix themselves to the safety cabin backpack body 01 through the seat belt component 02.

[0072] As Figure 3 described above, Figure 2It is a schematic structural diagram of another safety compartment backpack assembly provided by an embodiment of the present application. The safety compartment backpack assembly 110 further includes a safety rope 05. The balloon assembly includes an inert gas balloon 03 and a male part of an intelligent connection lock 04. After the safety compartment backpack body 01 of the escape personnel is fixed, the inert gas balloon 03 is inflated by a first compressed gas cylinder, so that the inert gas balloon 03 raises the male part of the intelligent connection lock 04 into the air, and the safety rope 03 is used to connect the inert gas balloon 03 and the safety compartment backpack body 01. After the male part of the intelligent connection lock 04 rises into the air, the female part of the intelligent connection lock is used to lock with the male part of the intelligent connection lock. Specifically, the male part of the intelligent connection lock 04 includes a first lock head, a first UWB pulse signal transmitter, and a first magnetic attraction positioning device, while the female part of the intelligent connection lock of the UAV assembly includes a second lock head, a second UWB pulse signal transmitter, and a second magnetic attraction positioning device. The male part and the female part of the intelligent connection lock are docked through the first UWB pulse signal transmitter, the second UWB pulse signal transmitter, the first magnetic attraction positioning device, and the second magnetic attraction positioning device. Specifically, the male part and the female part of the intelligent connection lock are docked through the interaction of the first UWB pulse signal transmitter and the second UWB pulse signal transmitter, and the first magnetic attraction positioning device and the second magnetic attraction positioning device are docked to make the first lock head and the second lock head in the correct docking state. Finally, the first lock head and the second lock head are locked when the male part and the female part of the intelligent connection lock are successfully docked. Then, as Figure 4 shown, Figure 4 It is a schematic diagram of a UAV body carrying an escape personnel to escape provided by an embodiment of the present application. After the first lock head and the second lock head are locked, the UAV body 06 carries the escape personnel to escape.

[0073] As Figure 5 shown, Figure 5 It is a schematic diagram of another UAV body carrying an escape personnel to escape provided by an embodiment of the present application. The safety compartment backpack assembly 110 further includes: an emergency air cushion compartment 07. The emergency air cushion compartment 07 includes a plurality of buffer air bags 08. When the escape personnel are in the air, the buffer air bags 08 are self-inflated. The self-inflation of the buffer air bags 08 adopts the principle and technical solution of a vehicle-mounted airbag, that is, a large amount of nitrogen is generated after sodium azide is heated. The advantage is that the triggering time is short, only 30 milliseconds, but this substance is highly toxic, so mature solutions such as potassium nitrate and silicon dioxide are used. In addition, it should be specifically noted that only the inflation method of the buffer air bag and the landing bracket air bag is exemplarily described in this embodiment, and the specific inflation method is not limited. In addition, the emergency air cushion compartment 07 further includes a second compressed gas cylinder. After the buffer air bags 08 are self-inflated, if the air pressure of the buffer air bags 08 is less than the preset value, the buffer air bags 08 are inflated.

[0074] In addition, the escape system further includes a safety capsule backpack storage box, which includes a storage box body, a backup power supply, and an alarm device. The storage box body is used to store the safety capsule backpack assembly 110, and the backup power supply is used to charge the safety capsule backpack assembly 110. When a disaster occurs, the alarm device can issue an alarm.

[0075] In the embodiment of the present application, the escape system includes: a safety capsule backpack assembly and a drone component; wherein, the safety capsule backpack assembly includes a safety capsule backpack body and a balloon component, and the drone component includes a drone body and an intelligent connection lock female part. The safety capsule backpack body is used to fix the escape personnel in response to an escape instruction; the inert gas balloon is used to lift the intelligent connection lock male part into the air; the intelligent connection lock female part is used to lock with the intelligent connection lock male part; the drone body is used to carry the safety capsule backpack assembly and the escape personnel to escape after the intelligent connection lock female part and the intelligent connection lock male part are locked. In this way, when a debris flow disaster occurs, the escape personnel first fix themselves to the safety capsule backpack body, and then lock with the drone component through the balloon component, so that the drone can carry the safety capsule backpack assembly and the escape personnel to escape. In this way, the self-rescue of the escape personnel when the debris flow occurs is realized.

[0076] The above is an escape system provided by the embodiment of the present application. Based on this, the present application also provides a corresponding method, as Figure 6 shown Figure 6 is a flowchart of an escape method provided by the embodiment of the present application, including:

[0077] S601: In response to an escape instruction, use the safety capsule backpack body in the safety capsule backpack assembly to fix the escape personnel.

[0078] The safety capsule backpack assembly includes a safety capsule backpack body and a seat belt component. In response to an escape instruction, use the safety capsule backpack body in the safety capsule backpack assembly to fix the escape personnel, wherein the escape instruction can be issued by the escape personnel through a remote control. Specifically, in response to the escape instruction, the seat belt component fixes the escape personnel to the safety capsule backpack body.

[0079] S602: Use the inert gas balloon to lift the intelligent connection lock male part into the air.

[0080] The safety capsule backpack assembly further includes a first compressed gas cylinder, a balloon component, and a safety rope. The balloon component includes an inert gas balloon and an intelligent connection lock male part. After the escape personnel are fixed to the safety capsule backpack body, the inert gas balloon is inflated through the first compressed gas cylinder, so that the inert gas balloon lifts the intelligent connection lock male part into the air, and the safety rope is used to connect the inert gas balloon and the safety capsule backpack body.

[0081] S603: Lock the intelligent connection lock male part with the intelligent connection lock female part of the drone component.

[0082] The UAV component includes an intelligent connecting and locking female part and a UAV body. When the intelligent connecting and locking male part rises into the air, the intelligent connecting and locking female part is used to lock with the intelligent connecting and locking male part. Specifically, the intelligent connecting and locking male part includes a first lock head, a first UWB pulse signal transmitter, and a first magnetic attraction positioning device, while the intelligent connecting and locking female part of the UAV component includes a second lock head, a second UWB pulse signal transmitter, and a second magnetic attraction positioning device. The intelligent connecting and locking male part and the intelligent connecting and locking female part are docked through the first UWB pulse signal transmitter, the second UWB pulse signal transmitter, the first magnetic attraction positioning device, and the second magnetic attraction positioning device. Specifically, the intelligent connecting and locking male part and the intelligent connecting and locking female part are docked through the interaction of the first UWB pulse signal transmitter and the second UWB pulse signal transmitter, and the first magnetic attraction positioning device and the second magnetic attraction positioning device are docked to make the first lock head and the second lock head in the correct docking state. Finally, the first lock head and the second lock head are locked when the intelligent connecting and locking male part and the intelligent connecting and locking female part complete the docking.

[0083] S604: After the intelligent connecting and locking female part locks with the intelligent connecting and locking male part, use the UAV body to carry the safety cabin backpack assembly and the escape personnel to escape.

[0084] On this basis, the safety cabin backpack assembly further includes an emergency rescue airbag cushion compartment, and the emergency rescue airbag cushion compartment includes a plurality of buffer airbags. When the escape personnel are in the air, the buffer airbags are self-inflated. The self-inflation of the buffer airbags adopts the principle and technical solution of vehicle-mounted airbags, heating sodium azide to generate a large amount of nitrogen. The advantage is that the triggering time is short, only 30 milliseconds, but this substance is highly toxic, so mature solutions such as potassium nitrate and silicon dioxide are used. In addition, it should be specifically noted that this embodiment only exemplarily illustrates the inflation method of the buffer airbags and the landing support airbags, and does not limit its specific inflation method. In addition, the emergency rescue airbag cushion compartment further includes a second compressed gas cylinder. After the buffer airbags complete self-inflation, if the air pressure of the buffer airbags is less than the preset value, the buffer airbags are inflated.

[0085] In addition, the escape system further includes a safety cabin backpack storage box, which includes a storage box body, a backup power supply, and an alarm device. The storage box body is used to store the safety cabin backpack assembly, the backup power supply is used to charge the safety cabin backpack assembly, and when a disaster occurs, the alarm device is used to send an alarm.

[0086] The embodiment of the present application also provides a corresponding device and a computer storage medium for implementing the solution provided by the embodiment of the present application.

[0087] Among them, the device includes a memory and a processor. The memory is used to store instructions or codes, and the processor is used to execute the instructions or codes so that the device executes the method described in any embodiment of the present application.

[0088] The computer storage medium stores code, and when the code is run, the device running the code implements the method described in any embodiment of the present application.

[0089] From the description of the above embodiments, those skilled in the art can clearly understand that all or part of the steps in the above method embodiments can be implemented by means of software plus a general hardware platform. Based on this understanding, the technical solution of the present application can be embodied in the form of a software product, which can be stored in a storage medium, such as a read-only memory (ROM) / RAM, magnetic disk, optical disk, etc., and includes several instructions for causing a computer device (which may be a personal computer, a server, or a network communication device such as a router) to execute the methods described in various embodiments or some parts of the embodiments of the present application.

[0090] It should be noted that in this document, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the term "comprising", "including" or any other variation thereof is intended to cover a non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements but also other elements not expressly listed, or also includes elements inherent to such process, method, article or device. Without further limitation, an element defined by the phrase "comprising a..." does not exclude the presence of additional identical elements in the process, method, article or device including the element.

[0091] It should also be noted that the various embodiments in this specification are described in a progressive manner, and the same or similar parts between the various embodiments can be referred to each other. Each embodiment focuses on the differences from other embodiments. In particular, for the device and apparatus embodiments, since they are basically similar to the method embodiments, the description is relatively simple, and the relevant parts can be referred to the description of the method embodiments. The device embodiments described above are only illustrative. The units described as separate components may or may not be physically separated, and the components described as units may or may not be physical units, that is, they may be located in one place, or may be distributed to multiple network units. Some or all of the modules can be selected according to actual needs to achieve the purpose of the solution of this embodiment. Those of ordinary skill in the art can understand and implement it without creative efforts.

[0092] As described above, it is only a specific implementation manner of the present application, but the protection scope of the present application is not limited thereto. Any changes or substitutions that can be easily thought of by those skilled in the art within the technical scope disclosed in the present application should be covered within the protection scope of the present application. Therefore, the protection scope of the present application should be subject to the protection scope of the claims.

Claims

1. An escape system, characterized in that: include: The safety compartment backpack assembly includes a safety compartment backpack body and a balloon assembly; The safety compartment backpack body is used to respond to the escape command and fix the escapee; The balloon assembly includes an inert gas balloon and an intelligent docking lock male part; The inert gas balloon is used to lift the male part of the smart docking lock into the air; The drone assembly includes the drone body and the intelligent docking lock mother part; The female part of the smart docking lock is used to lock with the male part of the smart docking lock; The drone body is used to carry the safety compartment backpack assembly and the escapee to escape after the female part of the smart docking lock and the male part of the smart docking lock are locked.

2. The system according to claim 1, characterized in that The male part of the intelligent docking lock includes a first lock, a first uwb pulse signal transmitter, and a first magnetic positioning device; The intelligent docking lock mother part includes a second lock head, a second UWB pulse signal transmitter, and a second magnetic positioning device; The male part of the smart docking lock and the female part of the smart docking lock are used to dock through the first uwb pulse signal transmitter, the second uwb pulse signal transmitter, the first magnetic attraction positioning device and the second magnetic attraction positioning device; The first lock head and the second lock head are used to lock when the male part of the smart docking lock is docked with the female part of the smart docking lock.

3. The system according to claim 1, characterized in that The safety compartment backpack body comprises: A safety belt assembly is used to fix the escapee to the safety compartment backpack body in response to the escape instruction.

4. The system according to claim 1, characterized in that The balloon assembly further comprises: The first compressed gas cylinder is used for inflating the inert gas balloon in response to the escapee being secured.

5. The system according to claim 1, characterized in that The balloon assembly further comprises: A safety rope is used to connect the inert gas balloon and the safety compartment backpack body.

6. The system according to claim 1, characterized in that The safety compartment backpack assembly further includes: An emergency life-saving airbag cushion chamber, wherein the emergency life-saving airbag cushion chamber comprises a plurality of cushioning airbags; When the escapee is in the air, the cushioning airbag inflates itself.

7. The system according to claim 6, characterized in that The emergency airbag cushion chamber also includes: The second compressed gas cylinder is used to inflate the buffer airbag after the buffer airbag completes self-inflation if the air pressure of the buffer airbag is less than a preset value.

8. The system according to claim 1, characterized in that The system further comprises: The safety compartment backpack storage box includes a storage box body and a backup power supply; The storage box body is used to store the safety compartment backpack assembly; The backup power supply is used to charge the safety compartment backpack assembly.

9. The system according to claim 8, characterized in that The safety compartment backpack storage box also includes: The alarm device is used to sound an alarm when a disaster occurs.

10. An escape method, characterized in that: include: In response to an escape command, the escapee is fixed by using the safety compartment backpack body in the safety compartment backpack assembly; The safety bin backpack assembly includes the safety bin backpack body and a balloon assembly; the balloon assembly includes an inert gas balloon and a smart docking lock male part; Using the inert gas balloon to lift the male part of the smart docking lock into the air; The male part of the smart docking lock is locked with the female part of the smart docking lock of the drone assembly; the drone assembly includes a drone body and the female part of the smart docking lock; After the female part of the smart docking lock is locked with the male part of the smart docking lock, the drone body is used to carry the safety cabin backpack assembly and the escapee to escape.