Floating aircraft with deformable airbag function

Abstract

The invention discloses a floating aircraft with a deformable airbag function, and relates to the technical field of floating aircrafts, the floating aircraft comprises an aerostat main body, a parking frame and a controller, the aerostat main body and the parking frame cooperate with each other, the aerostat main body comprises an airbag, a driving assembly, a steering assembly and an adjusting assembly, a passenger compartment and a cockpit are mounted at the bottom of the airbag, and the airbag is mounted in the passenger compartment. The driving cabin is matched with the air bag through the steering assembly, the clamping assembly is installed between the passenger compartment and the adjusting assembly, the driving assembly is connected with the air bag, the adjusting assembly is installed in the air bag, the adjusting assembly can adjust the shape of the air bag, and the clamping assembly can guarantee the safety of the passenger compartment and the driving cabin. The state of the air bag can be changed by utilizing the shape and components of the air bag, so that the air pressure in the air bag is adjusted, and the device can adapt to height change and has a floating or descending function.

Description

Technical Field

[0001] The present invention relates to the technical field of floating air vehicles, and in particular to a floating air vehicle with a deformable airbag function. Background Art

[0002] A floating air vehicle generally refers to an aircraft that is lighter than air and relies on atmospheric buoyancy to lift off. However, flying solely relying on buoyancy cannot achieve the best effect. At the same time, existing airships are easily affected by wind speed and weather and are not suitable in bad weather because the difficulty of operation for the pilot increases in bad weather, and safety cannot be ensured. Due to the poor maneuverability, airships do not have good practicality. Because existing airships are huge in size and relatively underpowered, and the ratio of wind resistance to power is too large, it is difficult to turn around like a large ship, resulting in poor maneuverability. Moreover, general airships use auxiliary airbags to change or adjust the pressure of the airbag in order to adapt to the change in the height of the airship and the needs of ascending and descending. However, the speed of inflating or deflating the auxiliary airbag is relatively slow, and thus the change in airbag pressure is also relatively slow. For this reason, the vertical takeoff and landing maneuverability of the airship is insufficient. In addition, the weight of the auxiliary airbag also reduces the effective load of the airship. Therefore, when facing the change in the height of the airship or ascending and descending, a simpler and more effective operation control scheme is needed to improve the maneuverability and economy of the aircraft. Summary of the Invention

[0003] The purpose of the present invention is to provide a floating air vehicle with a deformable airbag function to solve the problems raised in the prior art.

[0004] To achieve the above purpose, the present invention provides the following technical solution: A floating air vehicle with a deformable airbag function, comprising a floating air vehicle main body, a mooring rack, and a controller. The floating air vehicle main body cooperates with the mooring rack. The floating air vehicle main body includes an airbag, a driving assembly, a steering assembly, and an adjusting assembly. A passenger cabin and a cockpit are installed at the bottom of the airbag. The cockpit is cooperated with the airbag through the steering assembly. A clamping assembly is installed between the passenger cabin and the adjusting assembly. The driving assembly is connected to the airbag. The adjusting assembly is installed inside the airbag. The adjusting assembly can adjust the shape of the airbag, and the clamping assembly can ensure the safety of the passenger cabin and the cockpit.

[0005] Furthermore, the adjustment component can adjust the morphological changes of the airbag. By changing the total amount of gas in the airbag, the main body of the airship can be lifted or lowered. An installation ring and two sets of ring pipes are installed inside the airbag. The installation ring is horizontally installed in the middle of the airbag. The two sets of ring pipes are respectively installed at the top and bottom of the airbag. The two sets of ring pipes are parallel to the installation ring. A tension cable net is arranged between the airbag, the installation ring and the two sets of ring pipes. The adjustment component is installed between the installation ring and the two sets of ring pipes. The tension cable net cooperates with the adjustment component.

[0006] Furthermore, the adjustment component includes two sets of air flow channel pipe clamps, multiple sets of tension cables and multiple sets of telescopic sleeves. Multiple sets of telescopic sleeves are installed between the two sets of air flow channel pipe clamps. The other side of the air flow channel pipe clamp is matched with the inner surface of the airbag. One end of the tension cable is connected to the tension cable net. A winch gear and multiple sets of low-speed motors are installed at the bottom of the adjustment component. The low-speed motor cooperates with the winch gear. A limit block is installed above the winch gear. The limit block is connected to the tension cable.

[0007] Furthermore, the drive component includes multiple sets of vector propellers. One set of vector propellers is respectively installed above the airbag, and the other set of vector propellers is installed between the passenger cabin and the cockpit. The steering component is installed between the vector propellers.

[0008] Furthermore, the steering component includes a power coupling shaft, a connecting shaft and a steering motor. The steering motor is installed at the upper end of the airbag. The output end of the steering motor is connected to the power coupling shaft. The power coupling shaft is connected to the limit block through a bearing. A connecting shaft is installed at the bottom of the power coupling shaft. The power coupling shaft is matched with the connecting shaft through an installation component. The other end of the connecting shaft is connected to the cockpit.

[0009] Furthermore, a falling induction component is arranged above the passenger cabin. The falling induction component includes a detection sleeve. A metal ball and two sets of pressure induction plates are arranged inside the detection sleeve. The pressure induction plates are respectively arranged on the inner top surface and the inner bottom surface of the detection sleeve. The metal ball cooperates with the pressure induction plates.

[0010] Furthermore, the clamping component includes a fixed motor and multiple sets of limit cylinders. The fixed motor and the limit cylinders are respectively installed inside the power coupling shaft. The output end of the fixed motor faces the passenger cabin. A fixed disk is installed at the output end of the fixed motor. The fixed disk is threadedly connected to the connecting shaft. The output end of the limit cylinder is installed with an L-shaped lever. The L-shaped lever cooperates with the connecting shaft.

[0011] Further, the parking rack includes a support ring, signal indicator lights, and multiple groups of support rods. One end of each support rod contacts the ground foundation. An elevating cylinder is installed above each group of support rods, and the other end of the elevating cylinder is connected to the support ring. The support ring cooperates with the installation ring. The signal indicator lights are installed on the ground foundation and are concentrically installed with the support ring.

[0012] Further, a controller is arranged inside the cockpit, and the controller is connected to the airship main body.

[0013] Compared with the prior art, the beneficial effects of the present invention are as follows: 1. When the device is in use, the operation is easier. Due to the shape of the airship main body, it can have great stability in case of bad weather. At the same time, it can automatically change the state of the airship main body according to the air flow speed to adapt to any weather, so that the driver can get great safety protection.

[0014] 2. When the adjusting component is in use, the air flow channel pipe clamp therein can prevent the airbag from blocking the vertical air flow channel due to expansion during inflation. Therefore, a lightweight air flow channel pipe clamp is set to maintain the smoothness of the air flow. When the shape of the airbag needs to be adjusted, the device can control multiple groups of telescopic sleeves at the same time, thereby raising or compressing the internal volume of the airbag. At the same time, through the cable gear, when the tension cable is tightened, the tension of the tension cable can be increased through the lever action, thereby improving the stability of the airbag. During specific use, since the tension cable is connected to the edge of the limit block, when the cable gear rotates, the limit block can be driven to rotate, so that the tension cable can be tightened to strengthen the tension of the tension cable on the tension cable network; 3. When a special situation occurs to the device, first, the fixing motor will reverse, so that the fixing disk installed at the output end of the fixing motor can be disengaged from the connecting shaft. After that, when the fixing disk is disengaged from the connecting shaft, the limit cylinder will tighten the L-shaped lever to disengage the L-shaped lever from the connecting shaft. Then, the upper airbag will be disengaged from the device. At the same time, the gas generator will generate a large amount of gas to push the buffer parachute to unfold, and then cooperate with the vector propeller at the bottom to slow down the descending speed and improve the safety of passengers and drivers. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 It is a schematic structural diagram of the combination of the airship main body and the parking rack of the present invention; Figure 2 It is an isometric structural diagram of the airship main body of the present invention; Figure 3 It is a schematic internal structure diagram of the airship main body of the present invention; Figure 4 It is a schematic structural diagram of the adjusting component of the present invention; Figure 5 Schematic connection structure diagram of the driving component, steering component and clamping component of the present invention; Figure 6 Schematic mating structure diagram of the clamping component of the present invention; Figure 7 Schematic cross-sectional structure diagram of the falling induction component of the present invention; Figure 8 Schematic structure diagram of the parking rack of the present invention.

[0016] In the figure: 1, aerostat main body; 2, parking rack; 21, support ring; 22, signal indicator light; 23, support rod; 24, lifting cylinder; 3, airbag; 31, mounting ring; 32, ring pipe; 33, tension cable net; 4, driving component; 41, vector propeller; 5, steering component; 51, power coupling shaft; 52, connecting shaft; 53, steering motor; 6, adjusting component; 61, air flow channel pipe clamp; 62, pull cable; 63, telescopic sleeve; 64, cable gear; 65, low-speed motor; 66, limit block; 7, clamping component; 71, fixed motor; 72, limit cylinder; 73, L-shaped lever; 8, falling induction component; 81, detection sleeve; 82, metal ball; 83, pressure induction plate; 9, controller. Detailed implementation manners

[0017] Next, the technical solutions in the embodiments of the present invention will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0018] Embodiment: As Figures 1 - 8 shown, the present invention provides a technical solution for an aerostatic flying vehicle with a deformable airbag function, including an aerostat main body 1, a parking rack 2 and a controller 9. The aerostat main body 1 cooperates with the parking rack 2. The aerostat main body 1 includes an airbag 3, a driving component 4, a steering component 5 and an adjusting component 6. A passenger cabin and a cockpit are installed at the bottom of the airbag 3. The cockpit cooperates with the airbag 3 through the steering component 5. A clamping component 7 is installed between the passenger cabin and the adjusting component 6. The driving component 4 is connected to the airbag 3. The adjusting component 6 is installed inside the airbag 3. The adjusting component 6 can adjust the shape of the airbag 3, and the clamping component 7 can ensure the safety of the passenger cabin and the cockpit; When the floating aircraft is not in use, it is usually docked on a dedicated docking rack 2. At this time, passengers and pilots can enter the passenger cabin and cockpit respectively through escalators. After that, the staff can inject gas into the airbag 3 to expand the airbag 3 to generate buoyancy. At the same time, the driving component 4 will also generate thrust, so that the device can gradually rise into the sky and float in the sky. When the device is flying, the cockpit can be driven to turn through the steering component 5 without affecting the passenger cabin and the airbag 3. When the airbag 3 is floating, due to the instability of the external airflow, when the external airflow is large, the adjustment component 6 will adjust the current state and shape of the airbag 3. The adjustment component 6 can also play a role when the device is rising or falling, because the internal air pressure of the airbag 3 needs to be adjusted when the device is rising or falling, and the adjustment component 6 can adjust the current capacity of the airbag 3 to better match the current state.

[0019] like Figures 1 - 3 As shown, in this embodiment, specifically, the adjustment component 6 can adjust the shape change of the airbag 3, and the airship body 1 can be raised or lowered by changing the total amount of gas in the airbag 3. A mounting ring 31 and two groups of ring tubes 32 are installed inside the airbag 3. The mounting ring 31 is horizontally installed in the middle of the airbag 3, and the two groups of ring tubes 32 are respectively installed at the top and bottom of the airbag 3. The two groups of ring tubes 32 are parallel to the mounting ring 31. A tension cable net 33 is arranged between the airbag 3, the mounting ring 31 and the two groups of ring tubes 32. The adjustment component 6 is installed between the mounting ring 31 and the two groups of ring tubes 32, and the tension cable net 33 cooperates with the adjustment component 6; The airbag 3 of the device is in the shape of an oblate sharp-edged shape, so when airflow hits the airbag 3, the airflow can be dissipated along with the shape of the airbag 3, thereby reducing the direct resistance of the airflow to the airbag 3, and the mounting ring 31 in the airbag 3 mainly limits the diameter and size of the airbag 3, wherein the adjustment component 6 can limit the height of the airbag 3, and the two groups of ring tubes 32 can limit the shape and position of the upper and lower ends of the airbag 3, and then cooperate with the tension rope net 33 to define a complete airbag 3. When adjusting the height of the airbag 3, the adjustment component 6 mainly pulls the tension rope net 33, thereby changing the state of the airbag 3 so that it can better match the external environment.

[0020] like Figures 3 - 4 As shown, in this embodiment, specifically, the adjustment component 6 includes two groups of airflow channel hoops 61, multiple groups of tension cables 62 and multiple groups of telescopic sleeves 63, multiple groups of telescopic sleeves 63 are between the two groups of airflow channel hoops 61, the other side of the airflow channel hoops 61 cooperates with the inner surface of the airbag 3, one end of the tension cable 62 is connected to the tension cable net 33, and a cable gear 64 and multiple groups of low-speed motors 65 are installed at the bottom of the adjustment component 6, the low-speed motor 65 cooperates with the cable gear 64, and a limit block 66 is installed above the cable gear 64, and the limit block 66 is connected to the tension cable 62; When the adjustment component 6 of the device is in use, the air flow channel clamp 61 therein can prevent the air bag 3 from blocking the vertical air flow channel due to expansion during inflation. Therefore, a lightweight air flow channel clamp 61 is provided to maintain the smoothness of the air flow. When it is necessary to adjust the shape of the air bag 3, the device can simultaneously control multiple sets of telescopic sleeves 63, thereby increasing or compressing the internal volume of the air bag 3. At the same time, through the cable winch gear 64, when the cable 62 is tightened, the tension of the cable 62 can be increased through the lever action, thereby improving the stability of the air bag 3. Specifically, during use, since the cable 62 is connected to the edge of the limit block 66, when the cable winch gear 64 rotates, it can drive the limit block 66 to rotate, so that the cable 62 can be tightened, strengthening the tension of the cable 62 on the tension cable net 33. Then, through the air flow channel clamp 61, the cable 62 and the telescopic sleeve 63, the shape of the air bag 3 can be changed. When the air flow channel clamp 61 contracts through the tension cable net 33, the air pressure inside the air bag 3 can be changed, thereby realizing the adjustment function of the device.

[0021] As Figures 1 - 3 and Figure 5 shown, in this embodiment, specifically, the drive component 4 includes multiple sets of vector propellers 41. One set of vector propellers 41 is respectively installed above the air bag 3, and the other set of vector propellers 41 is installed between the passenger cabin and the cockpit. A steering component 5 is installed between the vector propellers 41; When the drive component 4 of the device is in use, it can generate sufficient thrust to push the device to fly upward. Specifically, during use, the vector propellers 41 can rotate, thereby generating thrust to push the device to fly upward. Since the air bag 3 can generate buoyancy, it can cooperate with the vector propellers 41 to make the device float in the air more easily. By changing the current direction, the vector propellers 41 can move in different directions. The steering component 5 installed at the bottom of the vector propellers 41 will not be affected by the drive component 4 during use and can directly drive the cockpit to turn.

[0022] As Figures 1 - 3 shown, in this embodiment, specifically, the steering component 5 includes a power coupling shaft 51, a connecting shaft 52 and a steering motor 53. The steering motor 53 is installed at the upper end of the air bag 3. The output end of the steering motor 53 is connected to the power coupling shaft 51. The power coupling shaft 51 is connected to the limit block 66 through a bearing. A connecting shaft 52 is installed at the bottom of the power coupling shaft 51. The power coupling shaft 51 is matched with the connecting shaft 52 through a mounting component. The other end of the connecting shaft 52 is connected to the cockpit; When the steering component 5 of the device is in use, it can drive the cockpit to steer. When steering, it will not affect the airbag 3 and the passenger cabin. Specifically in use, the steering motor 53 can drive the power coupling shaft 51 to steer. Since the bottom of the power coupling shaft 51 is connected to the connecting shaft 52 through the clamping component 7, it can drive the connecting shaft 52 to rotate together. The other end of the connecting shaft 52 is connected to the cockpit. Therefore, when steering is required, the steering motor 53 can drive the cockpit to steer so that the driver in the cockpit can better control the flight direction and ensure flight safety.

[0023] As Figure 7 shown, in this embodiment, specifically, a falling induction component 8 is provided above the passenger cabin. The falling induction component 8 includes a detection sleeve 81. Inside the detection sleeve 81, there are a metal ball 82 and two groups of pressure induction plates 83. The pressure induction plates 83 are respectively arranged on the inner top surface and the inner bottom surface of the detection sleeve 81, and the metal ball 82 cooperates with the pressure induction plates 83; The falling induction component 8 of the device can sense the current falling speed to ensure that the device falls smoothly when descending, preventing a large downward force. Since the device rises and descends vertically, a large pressure and downward force cannot be generated at one time during ascent or descent, so as not to have an adverse impact on the passengers in the passenger cabin. Specifically in use, when the device rises, the pressure generated during ascent can cause the metal ball 82 to squeeze the pressure induction plate 83 at the bottom, so that the driver can know the pressure received by the current passenger cabin and slow down the ascent speed. When descending, the metal ball 82 will contact the pressure induction plate 83 at the top under the influence of the downward force. When the value of the upper pressure induction plate 83 exceeds the threshold, it indicates that the current downward force is likely to make the passengers feel uncomfortable. Then the driver can relieve the current descending speed to give the passengers a better riding experience.

[0024] As Figures 5 - 6 shown, in this embodiment, specifically, the clamping component 7 includes a fixed motor 71 and multiple groups of limit cylinders 72. The fixed motor 71 and the limit cylinders 72 are respectively installed inside the power coupling shaft 51. The output end of the fixed motor 71 faces the passenger cabin. A fixed disk is installed at the output end of the fixed motor 71, and the fixed disk is threadedly connected to the connecting shaft 52. The output end of the limit cylinder 72 is installed with an L-shaped lever 73, and the L-shaped lever 73 cooperates with the connecting shaft 52; When the clamping assembly 7 of the device is in use, it mainly connects the power coupling shaft 51 and the connecting shaft 52 through the fixed motor 71 and multiple groups of limit cylinders 72, so that the cockpit can turn normally during the operation of the device. Specifically, during use, the fixed motor 71 can be threadedly connected to the connecting shaft 52 through the output shaft, thereby achieving primary fixation. When the limit cylinder 72 is in use, it can push the L-shaped lever 73, so that the L-shaped lever 73 can cooperate with the connecting shaft 52, thereby achieving secondary fixation, enabling the steering assembly 5 to turn smoothly when steering the cockpit, and during subsequent maintenance, the airbag 3 can be quickly separated from the passenger compartment, thereby facilitating the maintenance of the device.

[0025] As Figure 8 shown, in this embodiment, specifically, the docking rack 2 includes a support ring 21, a signal indicator light 22, and multiple groups of support rods 23. One end of the support rod 23 contacts the ground foundation, and a lifting cylinder 24 is installed above each group of support rods 23. The other end of the lifting cylinder 24 is connected to the support ring 21. The support ring 21 cooperates with the mounting ring 31, and the signal indicator light 22 is installed on the ground foundation and is concentrically installed with the support ring 21; When the docking rack 2 of the device is in use, it is only suitable for matching the airship main body 1. The support ring 21 on the docking rack 2 can match the mounting ring 31, thereby being able to support the entire airship main body 1. The light emitted by the signal indicator light 22 enables the driver to observe the landing point on the ground at high altitude, thereby facilitating the driver to drive the device to descend.

[0026] As Figures 1 - 3 shown, in this embodiment, specifically, a controller 9 is provided inside the cockpit, and the controller 9 is connected to the airship main body 1; The driver can control the device through the controller 9 inside the cockpit, so that the driver can control the airship main body 1 to operate safely.

[0027] Working principle: When the floating aircraft is not in use, it is usually docked on the dedicated docking rack 2. At this time, passengers and the driver can enter the passenger cabin and the cockpit respectively through the escalator. Then, the staff can inject gas into the airbag 3 to make the airbag 3 expand and generate buoyancy. At the same time, the driving component 4 will also generate thrust, enabling the device to gradually rise into the sky and float in the air. When the device is flying, the steering component 5 can drive the cockpit to turn without affecting the passenger cabin and the airbag 3. When the airbag 3 is floating in the air, due to the instability of the external air flow, when the external air flow is large, the adjustment component 6 will adjust the current state and shape of the airbag 3. The adjustment component 6 can also play a role when the device is ascending or descending. Because when the device is ascending or descending, it is necessary to adjust the internal air pressure of the airbag 3, and the adjustment component 6 can adjust the current capacity of the airbag 3 to better match the current state.

[0028] For those skilled in the art, it is obvious that the present invention is not limited to the details of the above exemplary embodiments, and the present invention can be implemented in other specific forms without departing from the spirit or basic characteristics of the present invention. Therefore, in any regard, the embodiments should be regarded as exemplary and non-restrictive. The scope of the present invention is defined by the appended claims rather than the above description. Therefore, all changes falling within the meaning and scope of the equivalent elements of the claims are intended to be included in the present invention. Any reference signs in the claims should not be regarded as limiting the claimed invention.

Claims

1. A floating air vehicle with a deformable airbag function, comprising a floating body (1), a mooring rack (2) and a controller (9), characterized in that: The airship main body (1) cooperates with the mooring rack (2). The airship main body (1) includes a gasbag (3), a driving assembly (4), a steering assembly (5) and an adjusting assembly (6). A passenger cabin and a cockpit are installed at the bottom of the gasbag (3). The cockpit is cooperated with the gasbag (3) through the steering assembly (5). A clamping assembly (7) is installed between the passenger cabin and the adjusting assembly (6). The driving assembly (4) is connected to the gasbag (3). The adjusting assembly (6) is installed inside the gasbag (3). The adjusting assembly (6) can adjust the shape of the gasbag (3), and the clamping assembly (7) can ensure the safety of the passenger cabin and the cockpit.

2. The floating air vehicle with a deformable airbag function according to claim 1, wherein: The adjusting assembly (6) can adjust the morphological change of the gasbag (3). By changing the shape of the gasbag (3) and the total amount of gas, the airship main body (1) can rise or fall. An installation ring (31) and two groups of ring pipes (32) are installed inside the gasbag (3). The installation ring (31) is horizontally installed in the middle of the gasbag (3). The two groups of ring pipes (32) are respectively installed at the top and bottom of the gasbag (3). The two groups of ring pipes (32) are parallel to the installation ring (31). A tension cable net (33) is arranged between the gasbag (3), the installation ring (31) and the two groups of ring pipes (32). The adjusting assembly (6) is installed between the installation ring (31) and the two groups of ring pipes (32). The tension cable net (33) is cooperated with the adjusting assembly (6).

3. The levitating aircraft with a deformable airbag function according to claim 2, characterized in that: The adjusting assembly (6) includes two groups of air flow channel pipe clamps (61), multiple groups of tension cables (62) and multiple groups of telescopic sleeves (63). Multiple groups of telescopic sleeves (63) are installed between the two groups of air flow channel pipe clamps (61). The other side of the air flow channel pipe clamp (61) is matched with the inner surface of the gasbag (3). One end of the tension cable (62) is connected to the tension cable net (33). A winch gear (64) and multiple groups of low-speed motors (65) are installed at the bottom of the adjusting assembly (6). The low-speed motor (65) is cooperated with the winch gear (64). A limit block (66) is installed above the winch gear (64). The limit block (66) is connected to the tension cable (62).

4. The levitating aircraft with a deformable airbag function according to claim 3, wherein: The driving assembly (4) includes multiple groups of vector propellers (41). One group of vector propellers (41) is respectively installed above the gasbag (3), and the other group of vector propellers (41) is installed between the passenger cabin and the cockpit. The steering assembly (5) is installed between the vector propellers (41).

5. A floating aircraft with a deformable airbag function according to claim 4, characterized in that: The steering assembly (5) includes a power coupling shaft (51), a connecting shaft (52) and a steering motor (53). The steering motor (53) is installed at the upper end of the gasbag (3). The output end of the steering motor (53) is connected to the power coupling shaft (51). The power coupling shaft (51) is connected to the limit block (66) through a bearing. A connecting shaft (52) is installed at the bottom of the power coupling shaft (51). The power coupling shaft (51) is cooperated with the connecting shaft (52) through an installation component. The other end of the connecting shaft (52) is connected to the cockpit.

6. The floating air vehicle with a deformable airbag function according to claim 5, characterized in that: Above the passenger cabin, a falling induction component (8) is provided. The falling induction component (8) includes a detection sleeve (81). Inside the detection sleeve (81), there are a metal ball (82) and two groups of pressure induction plates (83). The pressure induction plates (83) are respectively arranged on the inner top surface and the inner bottom surface of the detection sleeve (81). The metal ball (82) is matched with the pressure induction plates (83).

7. The floating air vehicle with a deformable airbag function according to claim 6, characterized in that: The clamping component (7) includes a fixed motor (71) and multiple groups of limit cylinders (72). The fixed motor (71) and the limit cylinders (72) are respectively installed inside the power coupling shaft (51). The output end of the fixed motor (71) faces the passenger cabin. A fixed disk is installed at the output end of the fixed motor (71). The fixed disk is threadedly connected to the connecting shaft (52). The output end of the limit cylinder (72) is installed with an L-shaped lever (73). The L-shaped lever (73) is matched with the connecting shaft (52).

8. The levitating aircraft with a deformable airbag function according to claim 7, wherein: The docking rack (2) includes a support ring (21), a signal indicator light (22) and multiple groups of support rods (23). One end of each support rod (23) contacts the ground foundation. Above each group of support rods (23), a lifting cylinder (24) is respectively installed. The other end of the lifting cylinder (24) is connected to the support ring (21). The support ring (21) is matched with the installation ring (31). The signal indicator light (22) is installed on the ground foundation. The signal indicator light (22) is concentrically installed with the support ring (21).

9. The floating air vehicle with a deformable airbag function according to claim 8, characterized in that: Inside the cockpit, the controller (9) is provided. The controller (9) is connected to the airship main body (1).

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