Aircraft rescue recovery method and readable storage medium

Abstract

The invention discloses an aircraft rescue recovery method, and belongs to the field of aircraft rescue. The aircraft rescue recovery method comprises the steps that under the condition that an aircraft rushes out of a runway or the aircraft lands forcibly, the state of the aircraft is checked, the state of the aircraft comprises a non-damage state, a mild damage state and a severe damage state, and the damage degree of the aircraft in the mild damage state is smaller than that of the aircraft in the severe damage state; if the aircraft is in an undamaged state, stopping rescuing the aircraft, and moving the aircraft to the runway; if the aircraft is in the light damage state or the heavy damage state, the damage degree of the structure of the aircraft is detected, rescue recovery is conducted on the aircraft according to the damage degree of the structure of the aircraft, and the structure of the aircraft refers to a part on the aircraft.

Description

Technical Field

[0001] The invention belongs to the field of aircraft rescue, and in particular relates to an aircraft rescue recovery method and a readable storage medium. Background Art

[0002] With the development of science and technology, airplanes have become an important means of transportation. Aircraft can not only transport goods, but also passengers, and can also be used for combat during war. However, in the relevant technology, when an airplane runs off the runway or makes an emergency landing, making the airplane in need of rescue, there is no suitable rescue method to rescue the airplane. Summary of the invention

[0003] The purpose of the embodiments of the present application is to provide an aircraft rescue and recovery method, which at least solves the problem that when an aircraft runs off the runway or makes an emergency landing, causing the aircraft to need rescue, there is no suitable rescue method to rescue the aircraft.

[0004] In a first aspect, an embodiment of the present application provides an aircraft rescue and recovery method, the aircraft rescue and recovery method comprising:

[0005] In the case where an aircraft runs off the runway or makes an emergency landing, checking the state of the aircraft, the state of the aircraft including an undamaged state, a slightly damaged state, and a severely damaged state, the degree of damage of the aircraft in the slightly damaged state being less than the degree of damage of the aircraft in the severely damaged state;

[0006] If the aircraft is in an undamaged state, stopping the rescue of the aircraft and moving the aircraft to the runway;

[0007] If the aircraft is in a state of slight damage or a state of severe damage, the damage degree of the structure of the aircraft is detected, and the aircraft is rescued and restored according to the damage degree of the structure of the aircraft, wherein the structure of the aircraft refers to the components on the aircraft.

[0008] Optionally, checking the status of the aircraft includes:

[0009] Check the status of the outer surface of the aircraft and the status of the internal components of the aircraft, wherein the internal components of the aircraft include an oxygen system, a power system, and a control system.

[0010] Optionally, before rescuing the aircraft, the aircraft rescue and recovery method further includes:

[0011] If the internal components of the aircraft are slightly damaged or severely damaged, the battery inside the aircraft is disconnected and grounded, or the battery of the aircraft is removed from the aircraft.

[0012] Optionally, the aircraft includes landing gear;

[0013] Detecting the extent of damage to the structure of the aircraft, including:

[0014] Detecting the damage degree of the landing gear of the aircraft, wherein the damage degree of the landing gear includes the landing gear being undamaged and the landing gear being damaged;

[0015] Rescue and restore the aircraft according to the extent of structural damage to the aircraft, including:

[0016] When the landing gear is not damaged, jacking up the aircraft so that the aircraft is supported by the landing gear, and moving the aircraft to a repair position;

[0017] In the case that the landing gear is damaged, the aircraft is jacked up, and a reinforcement member is fixed on the landing gear to strengthen the landing gear, and the aircraft is towed to the maintenance position.

[0018] Optionally, before jacking up the aircraft, the aircraft rescue and recovery method further includes:

[0019] determining the degree of pressure of the ground at the location of the aircraft;

[0020] If the pressure level is greater than or equal to a preset pressure value, jacking up the aircraft by means of a jacking device;

[0021] If the pressure degree is less than the preset pressure value, filling material is laid on the ground where the aircraft is located until the pressure degree of the ground where the aircraft is located is greater than or equal to the preset pressure value.

[0022] Optionally, determining the degree of pressure of the ground at the location of the aircraft includes:

[0023] determining a bearing factor, a soil bed slope angle of the ground at the location of the aircraft, a soil weight at the location of the aircraft, and a soil friction angle at the location of the aircraft;

[0024] determining an effective lateral pressure of the ground at the location of the aircraft and a base area of ​​the ground at the location of the aircraft;

[0025] The compression degree of the ground at the location where the aircraft is located is determined based on the bearing factor, the soil bed slope angle, the soil density, the soil friction angle, the effective lateral pressure, and the foundation area.

[0026] Optionally, before jacking up the aircraft, the aircraft rescue and recovery method further includes:

[0027] Reducing the weight of said aircraft.

[0028] Optionally, the aircraft has a fuel tank, and before jacking up the aircraft, the aircraft rescue and recovery method further includes:

[0029] Check whether the fuel tank has fuel;

[0030] If there is fuel in the fuel tank, the fuel in the fuel tank is drained until there is no fuel in the fuel tank.

[0031] Optionally, before checking the status of the aircraft, the aircraft rescue and recovery method further includes:

[0032] Check whether the pilots in said aircraft are wearing oxygen masks;

[0033] If the driver is wearing an oxygen mask, removing the oxygen mask and rescuing the driver;

[0034] If the driver is not wearing an oxygen mask, directly rescuing the driver;

[0035] In a second aspect, an embodiment of the present application provides a storage medium, on which a program or instruction is stored, and when the program or instruction is executed by a processor, the steps of the aircraft rescue and recovery method described in the first aspect above are implemented.

[0036] In a third aspect, an embodiment of the present application provides a chip, comprising a processor and a communication interface, wherein the communication interface is coupled to the processor, and the processor is used to run a program or instruction to implement the method described in the first aspect.

[0037] In a fourth aspect, an embodiment of the present application provides a computer program product, which is stored in a storage medium and is executed by at least one processor to implement the method described in the first aspect.

[0038] In an embodiment of the present application, when the aircraft runs off the runway or makes an emergency landing, the aircraft status is checked, and the aircraft status includes an undamaged state, a slightly damaged state, and a severely damaged state. The degree of damage when the aircraft is in a slightly damaged state is less than the degree of damage when the aircraft is in a severely damaged state; if the aircraft is in an undamaged state, the rescue of the aircraft is terminated and the aircraft is moved to the runway; if the aircraft is in a slightly damaged state or a severely damaged state, the degree of damage to the aircraft structure is detected, and the aircraft is rescued and recovered according to the degree of damage to the aircraft structure. That is, in this embodiment, when the aircraft runs off the runway or makes an emergency landing, the aircraft can be effectively rescued and recovered, and it is ensured that the aircraft is rescued and recovered in time. BRIEF DESCRIPTION OF THE DRAWINGS

[0039] Figure 1 A flowchart showing an aircraft rescue and recovery method provided by an embodiment of the present application;

[0040] Figure 2 A schematic diagram showing different degrees of ground pressure provided in an embodiment of the present application. DETAILED DESCRIPTION

[0041] The following will be combined with the drawings in the embodiments of the present application to clearly describe the technical solutions in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, rather than all the embodiments. All other embodiments obtained by ordinary technicians in this field based on the embodiments in the present application belong to the scope of protection of this application.

[0042] Reference Figure 1 , showing a flow chart of an aircraft rescue and recovery method provided in an embodiment of the present application.

[0043] like Figure 1 As shown, the aircraft rescue and recovery method includes:

[0044] Step 101: In the case where the aircraft runs off the runway or makes an emergency landing, check the status of the aircraft, which includes an undamaged state, a slightly damaged state, and a severely damaged state. The degree of damage when the aircraft is in the slightly damaged state is less than the degree of damage when the aircraft is in the severely damaged state.

[0045] Among them, when the plane runs off the runway or makes an emergency landing, the plane may have a malfunction. Therefore, it is necessary to check the status of the plane, that is, to check whether the plane is damaged, and then determine the specific rescue method for the plane.

[0046] In addition, in some practical ways, the practical way to check the status of the aircraft may be: checking the status of the outer surface of the aircraft and the status of the internal components of the aircraft, the internal components of the aircraft including the oxygen system, the power system, and the control system.

[0047] The outer surface of the aircraft usually has a skin, etc., and below the skin are the aircraft's structural parts. Therefore, it is necessary to check the state of the aircraft's outer surface, that is, to check the state of the aircraft's skin. If the outer surface of the aircraft is damaged, the structural parts below the skin may be damaged, so it is necessary to further check the state of the structural parts around the damaged part of the outer surface of the aircraft. In addition, the interior of the aircraft is equipped with internal devices, which may also be damaged when the aircraft runs off the runway or makes an emergency landing. Therefore, it is necessary to check the state of the aircraft's internal devices.

[0048] It should be noted that the internal devices of the aircraft may also include other components. For example, the internal devices of the aircraft may include a navigation system, an air conditioning system, a lighting system, and the like.

[0049] In addition, in some implementations, before rescuing the aircraft, the aircraft rescue and recovery method may also include: if the internal components of the aircraft are slightly damaged or severely damaged, disconnecting the battery inside the aircraft and grounding the battery, or removing the battery of the aircraft from the aircraft.

[0050] Among them, the internal devices of the aircraft are usually connected to the battery inside the aircraft, and the battery is used to power the internal system of the aircraft so that the internal components of the aircraft can operate. Once the internal components of the aircraft are damaged, in order to ensure safety, it is necessary to disconnect the battery inside the aircraft and ground the battery, that is, disconnect the connection between the battery inside the aircraft and the internal components of the aircraft to ensure that the battery no longer powers the internal components of the aircraft, so that when the aircraft is subsequently rescued, the internal components of the aircraft will not have safety problems caused by short circuits or leakage. Of course, the battery can also be directly removed from the aircraft to avoid short circuits or leakage in the internal components of the aircraft, which can also improve the safety of aircraft rescue.

[0051] In addition, in some real-life scenarios, before checking the status of the aircraft, the aircraft rescue and recovery method may also include: checking whether the pilot in the aircraft is wearing an oxygen mask; if the pilot is wearing an oxygen mask, removing the oxygen mask and rescuing the pilot; if the pilot is not wearing an oxygen mask, directly rescuing the pilot.

[0052] Among them, the aircraft is usually driven by the pilot. When the aircraft runs off the runway or makes an emergency landing, the pilot may feel unwell. Therefore, before checking the status of the aircraft, the pilot can be rescued first to ensure the safety of the pilot. If the aircraft performs a combat mission, that is, the aircraft is a combat aircraft, the pilot usually wears an oxygen mask; if the aircraft is a civil aircraft or a transport aircraft, the pilot does not wear an oxygen mask, so different rescues can be performed on the pilot according to different aircraft types.

[0053] If the pilot is wearing an oxygen mask, in order to prevent the oxygen mask from causing damage to the pilot during rescue, the oxygen mask needs to be removed to rescue the pilot. Specifically, the buckle on the driver's seat can be removed, or the seat belt and other parts can be cut off to ensure that the driver can leave the driver's seat in time for rescue. In addition, when removing the oxygen mask, the oxygen mask can be disconnected from the oxygen system in the aircraft.

[0054] If the driver is not wearing an oxygen mask, rescue can be carried out directly on the driver. For example, the seat belts and buckles can be removed to ensure that the driver can leave the driver's seat in time.

[0055] Step 102: If the aircraft is in an undamaged state, the rescue of the aircraft is terminated and the aircraft is moved to the runway.

[0056] Among them, if the aircraft is in an undamaged state, the rescue of the aircraft will be terminated, and the aircraft only needs to be moved to the runway so that the aircraft can continue to perform the corresponding mission relying on its own power.

[0057] In addition, when the aircraft runs off the runway, once the aircraft is stuck in the area outside the runway, it is difficult for the aircraft to escape from the area outside the runway on its own, and the aircraft is not damaged. At this time, it only needs to be towed to the runway by a tractor, that is, the aircraft is moved to the runway so that the aircraft can continue to move along the runway.

[0058] Step 103: If the aircraft is slightly damaged or severely damaged, the damage degree of the aircraft structure is detected, and the aircraft is rescued and restored according to the damage degree of the aircraft structure, wherein the aircraft structure refers to the components on the aircraft.

[0059] When detecting the damage degree of the aircraft structure, the rescuers can visually detect the damage degree of the aircraft structure. Of course, the rescuers can also detect the damage degree of the aircraft structure through detection equipment. Specifically, the rescuers can place the detection equipment at the location of the damage of the aircraft, and then determine the damage degree of the aircraft through the value displayed by the detection equipment.

[0060] When the damage to the aircraft is minor, that is, the aircraft is in a state of light damage, the rescuers can directly rescue the aircraft on site, that is, repair the slightly damaged structure of the aircraft, for example, if the skin is damaged, the skin can be repaired directly at the rescue site. When the damage to the aircraft is serious, that is, the aircraft is in a state of severe damage, the rescuers need to move the aircraft to a repair shop for rescue.

[0061] In addition, the aircraft includes a landing gear. In some implementations, the implementation method of detecting the degree of damage to the aircraft structure may be: detecting damage to the aircraft landing gear, wherein the degree of damage to the landing gear includes the landing gear being undamaged and the landing gear being damaged. According to the degree of damage to the aircraft structure, the implementation method of rescuing and recovering the aircraft may be: when the landing gear is undamaged, jacking up the aircraft so that the aircraft is supported by the landing gear and moving the aircraft to a repair position; when the landing gear is damaged, jacking up the aircraft and fixing a reinforcement member on the landing gear to reinforce the landing gear, and towing the aircraft to a repair position.

[0062] Among them, once the landing gear of the aircraft is not damaged, that is, when the aircraft lands, the landing gear is in the upper lock state, the wings and fuselage of the aircraft touch the ground, and the landing gear is not damaged, the aircraft can be lifted up, and after the aircraft is lifted up, the landing gear is lowered and placed in the lower lock state, so that the landing gear can support the aircraft, so that the aircraft can be towed and moved, and thus the aircraft can be moved to the repair position; and when the landing gear is damaged, after the aircraft is lifted up, it is necessary to fix a reinforcement piece on the landing gear to strengthen the landing gear, so that the landing gear is in the lower lock state after the aircraft is lifted up, and then the aircraft can be towed to move the aircraft to the repair position.

[0063] It should be noted that the reinforcement member may be a fixed column, and in this case, the fixed column may be used to temporarily reinforce the landing gear, that is, the fixed column may be welded to the landing gear to temporarily reinforce the landing gear.

[0064] In addition, in some implementations, before lifting the aircraft, the aircraft rescue and recovery method may further include: determining the degree of pressure on the ground where the aircraft is located; if the degree of pressure is greater than or equal to a preset pressure value, lifting the aircraft by a lifting device; if the degree of pressure is less than the preset pressure value, laying filler on the ground where the aircraft is located until the degree of pressure on the ground where the aircraft is located is greater than or equal to the preset pressure value.

[0065] Before lifting the aircraft, it is necessary to detect the degree of pressure on the ground where the aircraft is located, so as to ensure that the ground where the aircraft is located can provide sufficient support when lifting the aircraft. If the degree of pressure is greater than or equal to the preset pressure value, it means that the ground where the aircraft is located can bear the weight of the aircraft, and the aircraft can be lifted by the lifting device, and then the aircraft can be towed to the repair location; if the degree of pressure is less than the preset pressure value, it means that the ground where the aircraft is located cannot bear the weight of the aircraft.

[0066] Then fillers are laid on the ground where the aircraft is located to increase the pressure on the ground, and the pressure on the ground is tested again after laying the fillers until the pressure on the ground where the aircraft is located is greater than or equal to the preset pressure value, and then the laying of fillers is stopped, and the aircraft is lifted up by the lifting device. The fillers may be stone slabs, gravel, etc.

[0067] In addition, in determining the degree of ground pressure at the location of the aircraft, if Figure 2 As shown, it can be determined based on the ground bearing capacity diagram, which shows different load-bearing degrees, that is, the degree of compression of different ground surfaces.

[0068] It should be noted that the preset pressure value may be related to the weight of the aircraft, the preset pressure value may be equal to the weight of the aircraft, or the preset pressure value may be greater than the weight of the aircraft. In this regard, the embodiment of the present application is no longer limited here. In addition, in the embodiment of the present application, the jacking device may be a jack. The jack may be a hydraulic jack.

[0069] In addition, in some practical methods, the practical method of determining the degree of compression of the ground where the aircraft is located can also be: determining the bearing coefficient, the slope angle of the soil bed where the aircraft is located, the soil density at the location of the aircraft, and the soil friction angle at the location of the aircraft; determining the effective lateral pressure of the ground where the aircraft is located and the base area of ​​the ground where the aircraft is located; determining the degree of compression of the ground where the aircraft is located based on the bearing coefficient, the slope angle of the soil bed, the soil density, the soil friction angle, the effective lateral pressure and the base area.

[0070] The electric heating method for determining the pressure degree of the ground where the aircraft is located based on the bearing coefficient, the slope angle of the soil bed, the soil weight, the soil friction angle, the effective lateral pressure and the foundation area can be:

[0071] Q=N*(α-δ)*A+γ*D*A

[0072] In the above formula, Q represents the degree of ground compression at the location of the aircraft, N represents the bearing coefficient, α represents the slope angle of the soil bed, δ represents the effective lateral pressure, A represents the base area, γ represents the soil density, and D represents the soil friction angle.

[0073] In addition, the load factor can be predetermined based on experience, or the load factor can be searched from a preset table, which is a table with multiple load factors, and each load factor corresponds to a different ground type, so that the load factor corresponding to the ground type that is the same as the ground type of the current aircraft can be searched in the preset table according to the ground type of the ground where the aircraft is located. Among them, for each ground type, the corresponding load factor can be predetermined and formed into a table.

[0074] Additionally, in some implementations, before jacking up the aircraft, the aircraft rescue and recovery method may further include: reducing the weight of the aircraft.

[0075] Among them, before lifting the aircraft, in order to ensure the convenience of lifting the aircraft, the weight of the aircraft can also be reduced to ensure that the aircraft is easy to be lifted, thereby facilitating the subsequent rescue of the aircraft.

[0076] In addition, in some implementations, the weight of the aircraft can be reduced by disassembling aircraft components or taking out luggage from a luggage compartment on the aircraft. When disassembling aircraft components, components not related to the flight of the aircraft can be temporarily removed to reduce the weight of the aircraft.

[0077] In addition, in some implementations, the aircraft has a fuel tank. Before jacking up the aircraft, the aircraft rescue and recovery method may also include: detecting whether the fuel tank has fuel; if the fuel tank has fuel, draining the fuel in the fuel tank until there is no fuel in the fuel tank.

[0078] Among them, the aircraft is provided with a fuel tank. Before jacking up the aircraft, in order to ensure safety and to reduce the weight of the aircraft, it is possible to detect whether there is fuel in the fuel tank. If there is fuel in the fuel tank, safety problems may arise when jacking up the aircraft, and the weight of the aircraft will be large, making it inconvenient to jack up. Therefore, the fuel in the fuel tank can be drained until there is no fuel in the fuel tank, and then the aircraft can be jacked up, thereby effectively improving safety during the process of jacking up the aircraft.

[0079] For example, an airplane has fuel in its fuel tank, and when the airplane is lifted up, the fuel may be shaken, causing the fuel to explode.

[0080] In addition, in this embodiment, when discharging the fuel in the fuel tank, the fuel in the fuel tank can be sucked out through the fuel drain valve, or the fuel in the fuel tank can be pressurized by the fuel emergency electric pump to discharge the fuel from the fuel tank.

[0081] In this embodiment, when the aircraft runs off the runway or makes an emergency landing, the aircraft status is checked, and the aircraft status includes an undamaged state, a slightly damaged state, and a severely damaged state. The damage degree of the aircraft in the slightly damaged state is less than the damage degree of the aircraft in the severely damaged state. If the aircraft is in an undamaged state, the rescue of the aircraft is stopped and the aircraft is moved to the runway. If the aircraft is in a slightly damaged state or a severely damaged state, the damage degree of the aircraft structure is detected, and the aircraft is rescued and recovered according to the damage degree of the aircraft structure. That is, in the embodiment of the present application, when the aircraft runs off the runway or makes an emergency landing, the aircraft can be effectively rescued and recovered, and it is ensured that the aircraft is rescued and recovered in time.

[0082] An embodiment of the present application also provides a readable storage medium, on which a program or instruction is stored. When the program or instruction is executed by a processor, each process of the above-mentioned aircraft rescue and recovery method embodiment is implemented, and the same technical effect can be achieved. To avoid repetition, it will not be repeated here.

[0083] The processor is the processor in the electronic device described in the above embodiment. The readable storage medium includes a computer readable storage medium, such as a computer read-only memory ROM, a random access memory RAM, a magnetic disk or an optical disk.

[0084] An embodiment of the present application further provides a chip, which includes a processor and a communication interface, wherein the communication interface is coupled to the processor, and the processor is used to run programs or instructions to implement the various processes of the above-mentioned aircraft rescue and recovery method embodiment, and can achieve the same technical effect. To avoid repetition, it will not be repeated here.

[0085] It should be understood that the chip mentioned in the embodiments of the present application can also be called a system-level chip, a system chip, a chip system or a system-on-chip chip, etc.

[0086] An embodiment of the present application provides a computer program product, which is stored in a storage medium. The program product is executed by at least one processor to implement the various processes of the above-mentioned aircraft rescue and recovery method embodiment, and can achieve the same technical effect. To avoid repetition, it will not be repeated here.

[0087] It should be noted that, in this article, the terms "comprise", "include" or any other variant thereof are intended to cover non-exclusive inclusion, so that the process, method, article or device including a series of elements includes not only those elements, but also includes other elements not explicitly listed, or also includes elements inherent to such process, method, article or device. In the absence of further restrictions, the elements defined by the sentence "comprise one..." do not exclude the presence of other identical elements in the process, method, article or device including the element. In addition, it should be pointed out that the scope of the methods and devices in the embodiments of the present application is not limited to performing functions in the order shown or discussed, and may also include performing functions in a substantially simultaneous manner or in reverse order according to the functions involved, for example, the described method may be performed in an order different from that described, and various steps may also be added, omitted, or combined. In addition, the features described with reference to certain examples may be combined in other examples.

[0088] Through the description of the above implementation methods, those skilled in the art can clearly understand that the above-mentioned embodiment methods can be implemented by means of software plus a necessary general hardware platform, and of course by hardware, but in many cases the former is a better implementation method. Based on such an understanding, the technical solution of the present application, or the part that contributes to the prior art, can be embodied in the form of a computer software product, which is stored in a storage medium (such as ROM / RAM, a disk, or an optical disk), and includes a number of instructions for a terminal (which can be a mobile phone, a computer, a server, or a network device, etc.) to execute the methods described in each embodiment of the present application.

[0089] The embodiments of the present application are described above in conjunction with the accompanying drawings, but the present application is not limited to the above-mentioned specific implementation methods. The above-mentioned specific implementation methods are merely illustrative and not restrictive. Under the guidance of the present application, ordinary technicians in this field can also make many forms without departing from the purpose of the present application and the scope of protection of the claims, all of which are within the protection of the present application.

Claims

1. An aircraft rescue and recovery method, characterized in that: The aircraft rescue and recovery method comprises: In the event of an aircraft running off the runway or making an emergency landing, check the aircraft's status, which includes an undamaged state, a slightly damaged state, and a severely damaged state. The degree of damage when the aircraft is in a slightly damaged state is less than that when the aircraft is in a severely damaged state; If the aircraft is in an undamaged state, stop rescuing the aircraft and move it to the runway; If the aircraft is in a state of slight damage or severe damage, the damage degree of the aircraft structure is detected, and the aircraft is rescued and restored according to the damage degree of the aircraft structure, wherein the aircraft structure refers to the components on the aircraft.

2. The aircraft rescue and recovery method according to claim 1, characterized in that: The checking the status of the aircraft comprises: Check the state of the outer surface of the aircraft and the state of the internal components of the aircraft, wherein the internal components of the aircraft include an oxygen system, a power system, and a control system.

3. The aircraft rescue and recovery method according to claim 2 comprises: Before rescuing the aircraft, the aircraft rescue and recovery method further includes: If the internal components of the aircraft are slightly damaged or severely damaged, the battery inside the aircraft is disconnected and grounded, or the battery of the aircraft is removed from the aircraft.

4. The aircraft rescue and recovery method according to claim 1, characterized in that: The aircraft includes landing gear; Detecting the extent of damage to the structure of the aircraft, including: Detecting the damage degree of the landing gear of the aircraft, wherein the damage degree of the landing gear includes the landing gear being undamaged and the landing gear being damaged; Rescue and restore the aircraft according to the extent of structural damage to the aircraft, including: When the landing gear is not damaged, jacking up the aircraft so that the aircraft is supported by the landing gear, and moving the aircraft to a repair position; In the case that the landing gear is damaged, the aircraft is jacked up, and a reinforcement member is fixed on the landing gear to strengthen the landing gear, and the aircraft is towed to the maintenance position.

5. The rescue and recovery method according to claim 4, characterized in that: Before jacking up the aircraft, the aircraft rescue and recovery method further includes: determining the degree of pressure of the ground at the location of the aircraft; If the pressure level is greater than or equal to a preset pressure value, jacking up the aircraft by means of a jacking device; If the pressure degree is less than the preset pressure value, filling material is laid on the ground where the aircraft is located until the pressure degree of the ground where the aircraft is located is greater than or equal to the preset pressure value.

6. The aircraft rescue and recovery method according to claim 5, characterized in that: Determining the degree of pressure on the ground at the location of the aircraft includes: determining a bearing factor, a soil bed slope angle of the ground at the location of the aircraft, a soil weight at the location of the aircraft, and a soil friction angle at the location of the aircraft; determining the effective lateral pressure of the ground at the location of the aircraft and the base area of ​​the ground at the location of the aircraft; The compression degree of the ground at the location where the aircraft is located is determined based on the bearing factor, the soil bed slope angle, the soil density, the soil friction angle, the effective lateral pressure, and the foundation area.

7. The aircraft rescue and recovery method according to claim 4, characterized in that: Before jacking up the aircraft, the aircraft rescue and recovery method further includes: Reducing the weight of said aircraft.

8. The aircraft rescue and recovery method according to claim 4, characterized in that: The aircraft has a fuel tank. Before jacking up the aircraft, the aircraft rescue and recovery method further includes: detecting whether the fuel tank has fuel; If the fuel tank contains fuel, the fuel in the fuel tank is drained until the fuel tank contains no fuel.

9. The aircraft rescue and recovery method according to claim 1, characterized in that: Before checking the status of the aircraft, the aircraft rescue and recovery method further includes: Check whether the pilots in said aircraft are wearing oxygen masks; If the driver is wearing an oxygen mask, removing the oxygen mask and rescuing the driver; If the driver is not wearing an oxygen mask, rescue the driver directly.

10. A storage medium, characterized in that: The storage medium stores a program or instruction, and when the program or instruction is executed by the processor, the steps of the aircraft rescue and recovery method as described in any one of claims 1 to 9 are implemented.

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