Manned hanging cabin for rescue based on unmanned aerial vehicle

Abstract

The invention discloses a manned hanging cabin for rescue based on an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicle manned hanging cabins, the manned hanging cabin comprises the unmanned aerial vehicle, the bottom of the unmanned aerial vehicle is provided with a hanging cabin mechanism for switching rescue modes, and the hanging cabin mechanism is internally provided with a rescue mounting mechanism for adjusting the swing amplitude of the wounded. A medical mechanism cabin used for rescuing and placing the wounded is arranged in the rescue mounting mechanism, and a mounting mechanism used for mounting the medical mechanism cabin and a support mechanism used for placing the wounded are arranged in the rescue mounting mechanism. When the unmanned aerial vehicle swings left and right in the air, the sliding groove plate pushes the limiting block to slide along the outer surface of the supporting arc rod through the first air cushion, the lateral movement of the unmanned aerial vehicle can be effectively converted into sliding instead of being directly transmitted to the medical shell, and therefore the influence of left-right swing on the wounded is remarkably reduced.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicle manned hanging cabins, and in particular to a manned hanging cabin based on unmanned aerial vehicle rescue. Background Art

[0002] The manned pod for drone rescue is a special device designed to rescue people in emergency situations using large drones.

[0003] For example, the patent document with publication number CN111776232A, the invention name is a mounting mechanism and a pod for detecting air pollution, the mounting mechanism includes a mounting plate, a groove plate and a limit block are arranged on the end face of the mounting plate close to the upper shell, and a slide groove is between the two groove plates; a snap-fit ​​protrusion is also arranged on the first clamping block, and a snap-fit ​​groove for snap-fitting with the snap-fit ​​protrusion is arranged on the upper shell. The present invention realizes flow monitoring by building a monitoring component into the pod and then mounting the pod by a drone, and the data obtained has a wide range and high reference value.

[0004] The above invention mainly detects the air by installing equipment in a pod, while the pod installed when using a drone for rescue requires strong stability to prevent personnel from suffering secondary injuries during the rescue process. In addition, when using a drone for rescue, the rescue method of the drone cannot be adjusted in time because the injuries of the rescue personnel are not clear. Therefore, the present application provides a manned pod based on drone rescue to meet the needs. Summary of the invention

[0005] The purpose of this application is to provide a manned hanging cabin based on drone rescue, which can effectively solve the problems raised in the above background technology.

[0006] To achieve the above-mentioned purpose, the present application provides the following technical solutions: a manned hanging cabin based on drone rescue, comprising a drone, a hanging cabin mechanism for switching rescue modes is arranged at the bottom of the drone, a rescue installation mechanism for adjusting the swing amplitude of the wounded is arranged inside the hanging cabin mechanism, a medical cabin for rescuing and placing the wounded is arranged inside the rescue installation mechanism, and a mounting mechanism for installing the medical cabin and a bracket mechanism for placing the wounded are arranged inside the rescue installation mechanism;

[0007] The cabin hanging mechanism comprises a cabin shell installed at the bottom of the UAV, the inner wall of the cabin shell is provided with a plurality of mounting racks, and the inner wall of the mounting rack is provided with a ring shaft;

[0008] The rescue installation mechanism comprises a half pipe, and both sides of the upper end of the installation frame are provided with sliding grooves for slidingly installing the mounting mechanism and the bracket mechanism.

[0009] Among them, support frames are symmetrically arranged on both sides of the bottom of the cabin shell, and two relatively moving leg frames are slidably installed in the middle of the lower end of the cabin shell;

[0010] Clamping rings for restricting the sliding of the hanging mechanism and the bracket mechanism are arranged on both sides of the cabin shell. Flat flow covers are rotatably installed at both ends of the cabin shell through hinges, and a connection device is arranged at the upper end of the cabin shell.

[0011] Among them, a half shell is jointly arranged in the middle of the upper ends of the two chutes. The half shell and the half tube are both fixedly installed inside the ring shaft. A plurality of support arc rods are arranged at equal intervals on the inner wall of the half tube. Limit blocks are slidably installed in the middle of the plurality of support arc rods, and springs sleeved on the outer surfaces of the support arc rods are arranged on both sides of the limit blocks.

[0012] Among them, the rescue installation mechanism further includes a chute plate. A plurality of first air cushions are arranged at equal intervals inside the chute plate. The first air cushions are used to restrict the up and down sliding of the limit blocks inside it. A first air cushion is arranged at the bottom of the chute plate, and an arc plate is arranged at the bottom of the outer surface of the first air cushion.

[0013] Among them, a slot is opened on one side of the upper end of the chute plate, and a plug block is inserted into the slot. A wedge block is inserted into the plug block. Magnetic sheets for adsorbing the wedge block and preventing the wedge block from falling off during jitter are arranged on both sides of the plug block.

[0014] Among them, the medical institution cabin includes a medical shell. A T-rail is arranged at the bottom of the medical shell. An oxygen generator is arranged on one side of the medical shell. An oxygen pipe is arranged inside the oxygen generator, and one end of the oxygen pipe penetrates through the medical shell and extends into its interior and is fixedly installed with an oxygen mask. A second air cushion is arranged at the bottom of the oxygen mask. A plurality of elastic bands are arranged at equal intervals on the inner wall of the medical shell. The T-rail is slidably installed inside the chute plate.

[0015] Among them, the bracket mechanism includes a second half tube plate. Two second sliders are arranged at the upper end of the second half tube plate. A protective plate is arranged on one side of the second half tube plate. Rectangular groove blocks are symmetrically arranged on the inner wall of the second half tube plate. A plurality of straps are jointly arranged at the upper ends of the two rectangular groove blocks at equal intervals.

[0016] Among them, support rods are slidably installed inside the two rectangular groove blocks. A tension cloth is jointly arranged between the two support rods. A third air cushion is arranged at the bottom of the inner wall of the second half tube plate. The second slider is slidably installed inside the chute, and a second positioning ring block is arranged on the outer surface of one side of the second half tube plate. The second positioning ring block is slidably installed inside one of the clamping rings.

[0017] Among them, the mounting mechanism includes a first half tube plate. Two first sliders are arranged at the upper end of the first half tube plate, and both first sliders are slidably installed inside the chute. An installation groove track is arranged in the middle of the inner wall of the first half tube plate. A first positioning ring block is arranged on one side of the outer surface of the first half tube plate, and the first positioning ring block is slidably installed inside one of the snap rings.

[0018] In summary, the technical effects and advantages of the present invention are as follows:

[0019] 1. When the drone swings left and right in the air, the chute plate pushes the limiting block to slide along the outer surface of the support arc rod through the first air cushion, which can effectively convert the lateral movement of the drone into sliding instead of directly transmitting it to the medical shell, thus significantly reducing the impact of left and right swings on the wounded. After being squeezed, the spring can slow down the swinging amplitude of the medical shell, further absorb the vibration energy, and provide an additional buffering effect to ensure the stability of the wounded during transportation. When the drone encounters bumps during flight or landing, the first air cushion can contract or expand according to the change of external pressure. This self-adaptive characteristic enables it to maintain the best shock absorption effect under different conditions. As the first air cushion deforms, the chute plate can slide up and down inside it, which not only allows the medical shell to adjust its position accordingly, but also avoids directly transmitting the bumps to the wounded, thus protecting the wounded from secondary injuries. Moreover, the design of the hanging cabin mechanism is to keep the wounded in a relatively stable state throughout the flight. Even if the drone itself experiences irregular movements, this mechanism can offset these effects through the above shock absorption measures, providing a stable environment for the wounded. And the comprehensive shock absorption system composed of the first air cushion, spring, limiting block, and support arc rod can absorb vibrations and impacts from all directions in an all-round way, greatly improving the safety and comfort of the wounded.

[0020] 2. By pushing the half tube to drive the half shell and the ring shaft to rotate, the present invention can flexibly adjust the positions of the mounting mechanism and the bracket mechanism, and can quickly switch different rescue modes according to the actual situation. Whether using only the rescue installation mechanism or combining the mounting mechanism and the bracket mechanism, the configuration adjustment can be completed through simple mechanical actions to meet the rescue needs in different scenarios. When only using the rescue installation mechanism to rescue the wounded, the second half tube plate is located in the upper part, and the second positioning ring block enters the snap ring to prevent it from sliding. The leg frame at the bottom of the cabin shell is pulled out to support the second half tube plate, providing additional support for ground operation and making it safer and more convenient to carry the wounded on the stretched cloth. According to actual needs, choose to use only the rescue installation mechanism or combine the mounting mechanism and the bracket mechanism. It is suitable for rescuing one seriously wounded person and can also handle multiple slightly wounded people at the same time, improving the flexibility and efficiency of rescue, allowing for quick configuration adjustment to adapt to different rescue scenarios, and enhancing the ability to respond to emergencies. Especially in emergency situations, it can quickly respond and implement effective rescue operations. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] In order to more clearly illustrate the technical solutions in the embodiments of the present application or the prior art, the following will briefly introduce the drawings required for use in the description of the embodiments or the prior art. Obviously, the drawings in the following description are only some embodiments of the present application. For those skilled in the art, without creative efforts, other drawings can be obtained based on these drawings.

[0022] Figure 1 First perspective three-dimensional structure schematic diagram of the manned suspension pod for drone rescue;

[0023] Figure 2 Second perspective three-dimensional structure schematic diagram of the manned suspension pod for drone rescue;

[0024] Figure 3 Third perspective three-dimensional structure schematic diagram of the manned suspension pod for drone rescue;

[0025] Figure 4 First form schematic diagram of the manned suspension pod for drone rescue;

[0026] Figure 5 Second form schematic diagram of the manned suspension pod for drone rescue;

[0027] Figure 6 Three-dimensional connection structure cross-sectional view of the manned suspension pod for drone rescue;

[0028] Figure 7 Second perspective three-dimensional connection structure schematic diagram of the manned suspension pod for drone rescue;

[0029] Figure 8 Partial three-dimensional connection structure schematic diagram of the manned suspension pod for drone rescue;

[0030] Figure 9 Three-dimensional connection structure schematic diagram of the mounting mechanism, medical institution cabin, rescue installation mechanism and rescue installation mechanism;

[0031] Figure 10 Expanded three-dimensional connection structure schematic diagram of the mounting mechanism, medical institution cabin, rescue installation mechanism and rescue installation mechanism;

[0032] Figure 11 First perspective three-dimensional connection structure schematic diagram of the rescue installation mechanism and the medical institution cabin;

[0033] Figure 12 Second perspective three-dimensional connection structure schematic diagram of the rescue installation mechanism and the medical institution cabin;

[0034] Figure 13Schematic diagram of the three-dimensional connection structure of the rescue installation mechanism;

[0035] Figure 14 Partial three-dimensional connection structure schematic diagram of the rescue installation mechanism;

[0036] Figure 15 Schematic diagram of the three-dimensional connection structure of the half pipe and the spring;

[0037] Figure 16 Schematic diagram of the three-dimensional connection structure of the first air cushion and the chute plate;

[0038] Figure 17 Cross-sectional view of the three-dimensional connection structure of the chute plate;

[0039] Figure 18 Exploded view of the three-dimensional connection structure of the rescue installation mechanism;

[0040] Figure 19 Schematic diagram of the three-dimensional connection structure of the medical institution cabin from the first perspective;

[0041] Figure 20 Schematic diagram of the three-dimensional connection structure of the medical institution cabin from the second perspective;

[0042] Figure 21 Schematic diagram of the three-dimensional connection structure of the support mechanism from the first perspective;

[0043] Figure 22 Schematic diagram of the three-dimensional connection structure of the support mechanism from the second perspective;

[0044] Figure 23 Schematic diagram of the three-dimensional connection structure of the tension cloth;

[0045] Figure 24 Schematic diagram of the three-dimensional connection structure of the mounting mechanism.

[0046] In the figure: 1. Hanging cabin mechanism; 11. Support frame; 13. Cabin shell; 14. Mounting frame; 15. Ring shaft; 16. Leg frame; 17. Snap ring; 2. UAV; 3. Mounting mechanism; 31. First half tube plate; 32. First slider; 33. Mounting groove rail; 34. First positioning ring block; 4. Rescue mounting mechanism; 41. Half shell; 42. Half tube; 43. Chute; 44. Chute plate; 45. Support arc rod; 46. Spring; 47. Limiting block; 48. First air cushion; 49. Arc piece; 411. Pin block; 412. Wedge block; 413. Slot; 414. Magnetic piece; 5. Medical institution cabin; 51. Medical shell; 52. Oxygen generator; 53. Elastic band; 54. Second air cushion; 55. Oxygen mask; 57. T-rail; 6. Bracket mechanism; 61. Second slider; 62. Protective plate; 63. Binding strap; 64. Third air cushion; 65. Tightening cloth; 66. Rectangular groove block; 67. Second half tube plate; 68. Second positioning ring block; 69. Support rod; 9. Advection cover; 10. Connection device. Specific implementation mode

[0047] 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.

[0048] Embodiment 1. Refer to Figures 1 to 24 A manned hanging cabin based on UAV rescue as shown, including a UAV 2. A hanging cabin mechanism 1 for converting the rescue mode is arranged at the bottom of the UAV 2. A rescue mounting mechanism 4 for adjusting the swinging amplitude of the wounded is arranged inside the hanging cabin mechanism 1. A medical institution cabin 5 for rescuing and placing the wounded is arranged inside the rescue mounting mechanism 4. A mounting mechanism 3 for mounting the medical institution cabin 5 and a bracket mechanism 6 for placing the wounded are arranged inside the rescue mounting mechanism 4;

[0049] It is worth noting that when using the UAV for rescue, first open the advection cover 9, and then rotate the positions of the rescue mounting mechanism 4, the mounting mechanism 3, and the bracket mechanism 6 according to the injuries or needs of the rescued personnel to adjust different rescue modes. When there is only one wounded person or the injuries of the wounded are serious and require emergency rescue, place the wounded inside the medical institution cabin 5, and then insert the medical institution cabin 5 into the rescue mounting mechanism 4 for fixation. At this time, the UAV can only rescue one wounded person, and the cooperation of the rescue mounting mechanism 4 and the medical institution cabin 5 can, to the greatest extent, avoid secondary injuries to the injuries of the rescued personnel due to the lifting and swinging during the UAV transportation. The advection cover 9 is made of light-transmitting explosion-proof glass material, which is convenient for lighting inside the cabin;

[0050] Among them, the wounded are placed in a specially designed medical institution cabin 5. The medical institution cabin 5 is used in conjunction with the rescue installation mechanism 4 to minimize the additional injuries caused to the injuries during transportation due to lifting and swinging, and is suitable for seriously injured patients who need to avoid moving as much as possible.

[0051] The medical institution cabin 5 is equipped with necessary medical facilities inside, such as vital sign monitoring and oxygen supply, which can maintain the stability of the vital signs of the wounded, provide a relatively enclosed and stable environment, and can provide preliminary treatment for the wounded in a limited space. And a communication device, a life detection and life support system are set in the medical institution cabin 5, such as real-time voice and video communication function, voice communication function in non-network areas (satellite communication), real-time transmission function of vital signs; video monitoring function, blood pressure, blood oxygen, respiration, pulse, heart rate detection and real-time transmission function; oxygen supply device, cold resistance and heat preservation and constant temperature function, high-pressure infusion function of non-ordinary infusion racks;

[0052] Moreover, the medical institution cabin 5 is mainly made of carbon fiber composite materials, and can be combined with other materials with high cost performance such as aluminum alloy. There are strengthening structures at the bottom and around.

[0053] Inserting the medical institution cabin 5 into the rescue installation mechanism 4 for fixation can help maintain the center of gravity balance of the drone, thereby improving the stability during flight.

[0054] When two or more people in need of assistance have minor injuries, the rescue installation mechanism 4 can be rotated to drive the hanging mechanism 3 and the support mechanism 6 to rotate synchronously. Then, the medical institution cabin 5 is inserted into the hanging mechanism 3. When people in need of assistance are required, the hanging mechanism 3 and the support mechanism 6 are pulled out from the inside of the rescue installation mechanism 4, and the people in need of assistance are placed in the medical institution cabin 5 and the support mechanism 6. Then, both the hanging mechanism 3 and the support mechanism 6 are slid into the inside of the rescue installation mechanism 4. Finally, the user can use pins or locks in the existing technology to fix the hanging mechanism 3 and the support mechanism 6 that have slid into the inside of the rescue installation mechanism 4, mainly to prevent the hanging mechanism 3 and the support mechanism 6 from sliding inside the rescue installation mechanism 4 during transportation.

[0055] Among them, by adjusting the hanging mechanism 3 and the support mechanism 6, multiple lightly injured patients can be rescued at the same time, increasing the number of rescued people per flight. Under limited time and resources, more people can be rescued, especially at the disaster site or in emergency situations. Moreover, it can be flexibly configured according to the actual situation. Whether it is to rescue one seriously injured patient or multiple lightly injured patients, it can be quickly adjusted to the most suitable rescue state.

[0056] The medical institution cabin 5 includes a medical shell 51. A T-rail 57 is provided at the bottom of the medical shell 51. An oxygen generator 52 is provided on one side of the medical shell 51. An oxygen pipe is arranged inside the oxygen generator 52, and one end of the oxygen pipe penetrates through the medical shell 51 and extends into its interior and is fixedly installed with an oxygen mask 55. A second air cushion 54 is provided at the bottom of the oxygen mask 55. A plurality of elastic bands 53 are arranged on the inner wall of the medical shell 51 at equal intervals. The T-rail 57 is slidably installed inside the chute plate 44.

[0057] It should be noted that the wounded are placed on the second air cushion 54, and then the elastic bands 53 are used to fix the wounded. Then the oxygen mask 55 is worn on the face of the wounded, and the oxygen generator 52 provides oxygen for the oxygen mask 55. The second air cushion 54 can prevent the wounded from jolting during transportation and increasing the pain of the wounded.

[0058] The rescue installation mechanism 4 includes a semi-tube 42. Chutes 43 for slidably installing the hanging mechanism 3 and the bracket mechanism 6 are provided on both sides of the upper end of the mounting frame 14.

[0059] A slot 413 is opened on one side of the upper end of the chute plate 44. A pin block 411 is inserted into the slot 413 of the cut. A wedge block 412 is inserted into the pin block 411. Magnetic sheets 414 for adsorbing the wedge block 412 and preventing the wedge block 412 from falling off during jitter are provided on both sides of the pin block 411.

[0060] Among them, after the wounded are placed inside the medical shell 51, the user lifts the medical shell 51 through the handles on both sides of the medical shell 51, inserts the T-rail 57 into the chute plate 44, then inserts the pin block 411 into the slot 413, and finally inserts the wedge block 412 into the pin block 411. The provided magnetic sheets 414 can fix the position of the wedge block 412 to prevent subsequent detachment. The pin block 411 can limit the position of the medical shell 51 and prevent the medical shell 51 from sliding out of the chute plate 44 during the process of the drone transporting the wounded.

[0061] Among them, the second air cushion 54 made of an inflatable or elastic material can effectively buffer the bumps during transportation and reduce the additional pain caused to the wounded. This is particularly important for the wounded because even a slight vibration may exacerbate their discomfort.

[0062] By using the elastic bands 53 to fix the wounded, it not only ensures safety but also does not cause over-tight compression, which helps to maintain the stable position of the wounded during transportation and prevent unnecessary movement.

[0063] In the middle of the upper ends of the two sliding grooves 43, a half shell 41 is jointly arranged. Both the half shell 41 and the half pipe 42 are fixedly installed inside the ring shaft 15. A plurality of support arc rods 45 are arranged on the inner wall of the half pipe 42 at equal intervals. A limiting block 47 is slidably installed in the middle of each of the plurality of support arc rods 45, and springs 46 sleeved on the outer surface of the support arc rods 45 are arranged on both sides of the limiting block 47.

[0064] It should be noted that during the transportation of the wounded, when the drone swings left and right in the air, the chute plate 44 will also push the limiting block 47 to slide on the outer surface of the support arc rod 45 through the first air cushion 48, and the spring 46 will slow down the swinging amplitude of the medical shell 51 after being compressed, and through the cooperation of the hanging cabin mechanism 1, the wounded can always be in a stable state.

[0065] The rescue installation mechanism 4 further includes a chute plate 44. A plurality of first air cushions 48 are arranged in the chute plate 44 at equal intervals. The first air cushions 48 are used to limit the up and down sliding of the limiting block 47 inside it. A first air cushion 48 is arranged at the bottom of the chute plate 44, and an arc piece 49 is arranged at the bottom of the outer surface of the first air cushion 48.

[0066] Among them, when the drone is jolted during flight or landing, the first air cushion 48 is compressed and contracted at this time, and the chute plate 44 swings up and down with the deformation of the first air cushion 48 at this time, and the first air cushion 48 can allow the limiting block 47 to slide up and down inside the first air cushion 48, so that the installed medical shell 51 will not be jolted by external factors, thus ensuring that the wounded will not be secondarily injured.

[0067] Among them, when the drone swings left and right in the air, the chute plate 44 pushes the limiting block 47 to slide along the outer surface of the support arc rod 45 through the first air cushion 48, which can effectively convert the lateral movement of the drone into sliding instead of directly transmitting it to the medical shell 51, thereby significantly reducing the impact of left and right swinging on the wounded.

[0068] After being compressed, the spring 46 can slow down the swinging amplitude of the medical shell 51, further absorb the vibration energy, provide an additional buffering effect, and ensure the stability of the wounded during transportation. When the drone encounters bumps during flight or landing, the first air cushion 48 can contract or expand according to the change of external pressure, and this adaptive characteristic enables it to maintain the best shock absorption effect under different conditions.

[0069] As the first air cushion 48 deforms, the chute plate 44 can slide up and down inside it, which not only allows the medical shell 51 to adjust its position accordingly, but also avoids directly transmitting bumps to the wounded, thereby protecting the wounded from secondary injuries. Moreover, the design of the hanging cabin mechanism 1 is to keep the wounded in a relatively stable state throughout the flight. Even if the UAV itself experiences irregular movements, this mechanism can offset these effects through the above shock absorption measures, providing a stable environment for the wounded.

[0070] And the comprehensive shock absorption system composed of the first air cushion 48, the spring 46, the limiting block 47, and the supporting arc rod 45 can absorb vibrations and impacts from all directions in an all-round way, greatly improving the safety and comfort of the wounded.

[0071] Embodiment 2. Based on the hanging cabin mechanism 1 and the bracket mechanism 6 proposed in Embodiment 1, this embodiment provides further technical solutions for the hanging cabin mechanism 1 and the bracket mechanism 6.

[0072] The hanging cabin mechanism 1 includes a cabin shell 13 installed at the bottom of the UAV 2. The inner wall of the cabin shell 13 is provided with a plurality of mounting frames 14, and the inner wall of the mounting frame 14 is provided with a ring shaft 15. And the cabin shell 13 has a total of 3 layers of structures. The outermost layer is made of carbon fiber composite material with a thickness of about 2.5 mm. The middle layer is an environmentally friendly, fireproof, and heat-insulating material with a thickness of about 5 mm to ensure that the temperature inside the cabin is not easily lost. The inner layer is made of carbon fiber composite material with a thickness of about 2.5 mm, so that the provided cabin shell 13 has a heat-insulating effect.

[0073] On both sides of the bottom of the cabin shell 13, support frames 11 are symmetrically arranged. In the middle of the lower end of the cabin shell 13, two relatively moving leg frames 16 are slidably installed. At both ends of the cabin shell 13, a flat-flow cover 9 is rotatably installed through a hinge, and a connection device 10 is arranged at the upper end of the cabin shell 13.

[0074] Among them, the provided flat-flow cover 9 can reduce wind resistance, and the connection device 10 can be connected to different types of UAVs, so that the entire manned hanging cabin can be adapted to a variety of UAVs.

[0075] On both sides of the cabin shell 13, snap rings 17 are provided for restricting the sliding of the hanging mechanism 3 and the bracket mechanism 6.

[0076] It should be noted that when it is necessary to adjust the rescue state, pushing the half-tube 42 drives the half-shell 41 to rotate, and both the half-tube 42 and the half-shell 41 drive the ring shaft 15 to rotate, and the positions of the hanging mechanism 3 and the bracket mechanism 6 are adjusted by the rotation of the half-tube 42.

[0077] The support mechanism 6 includes a second half tube plate 67. Two second sliders 61 are arranged at the upper end of the second half tube plate 67. A protective plate 62 is arranged on one side of the second half tube plate 67. Rectangular groove blocks 66 are symmetrically arranged on the inner wall of the second half tube plate 67. A plurality of straps 63 arranged at equal intervals are jointly arranged at the upper ends of the two rectangular groove blocks 66.

[0078] Among them, when there are multiple persons in need of rescue, the rescued persons are placed on the tensioned cloth 65, and then the rescued persons are fixed by the straps 63. The provided third air cushion 64 can prevent the rescued persons from being bumped and bruised, and the provided protective plate 62 can play a protective role.

[0079] Support rods 69 are slidably installed inside both of the two rectangular groove blocks 66. A tensioned cloth 65 is jointly arranged between the two support rods 69. A third air cushion 64 is arranged at the bottom of the inner wall of the second half tube plate 67. The second slider 61 is slidably installed inside the chute 43, and a second positioning ring block 68 is arranged on one side of the outer surface of the second half tube plate 67. The second positioning ring block 68 is slidably installed inside one of the snap rings 17.

[0080] Among them, when only the rescue installation mechanism 4 is used to rescue the wounded, at this time the second half tube plate 67 is located in the upper part and the second positioning ring block 68 will also choose to enter into the snap ring 17. The snap ring 17 can prevent the second half tube plate 67 from sliding inside the chute 43 through the second slider 61. When placing or carrying the wounded on the tensioned cloth 65, the second half tube plate 67 is pushed to drive the second slider 61 to slide inside the chute 43, and then the leg frame 16 at the bottom of the cabin shell 13 is pulled out. The leg frame 16 is used to support the second half tube plate 67, so as to facilitate the carrying of the wounded on the tensioned cloth 65.

[0081] The hanging mechanism 3 includes a first half tube plate 31. Two first sliders 32 are arranged at the upper end of the first half tube plate 31, and both of the two first sliders 32 are slidably installed inside the chute 43. An installation groove track 33 is arranged in the middle of the inner wall of the first half tube plate 31. A first positioning ring block 34 is arranged on one side of the outer surface of the first half tube plate 31, and the first positioning ring block 34 is slidably installed inside one of the snap rings 17.

[0082] It should be noted that when the second half tube plate 67 is used, the first half tube plate 31 can be pulled out. The first half tube plate 31 drives the first slider 32 to slide inside the chute 43. Then align the T-rail 57 with the installation groove rail 33, and then push the medical shell 51 into the inside of the first half tube plate 31, and place the wounded in the medical shell 51. After the wounded is placed, push the first half tube plate 31 into the inside of the half shell 41, and also push the second half tube plate 67 into the inside of the half shell 41. Then the user fixes the second slider 61 and the first slider 32 inside the chute 43 by means of a lock or a bolt.

[0083] And when the wounded is placed through the rescue installation mechanism 4 or the mounting mechanism 3 and the support mechanism 6, due to the gravity of the wounded, it can be ensured that the mechanism for placing the wounded is located below, and it is ensured that only the rescue installation mechanism 4 can be used alone or the mounting mechanism 3 and the support mechanism 6 can be used through the adjustment of the hanging cabin mechanism 1.

[0084] Among them, by pushing the half tube 42 to drive the half shell 41 and the ring shaft 15 to rotate, the positions of the mounting mechanism 3 and the support mechanism 6 can be flexibly adjusted, and different rescue modes can be quickly switched according to the actual situation. Whether using the rescue installation mechanism 4 alone or combining the mounting mechanism 3 and the support mechanism 6, the configuration adjustment can be completed through simple mechanical actions to meet the rescue needs in different scenarios.

[0085] When only the rescue installation mechanism 4 is used to rescue the wounded, the second half tube plate 67 is located at the upper part, and the second positioning ring block 68 enters the clamping ring 17 to prevent it from sliding. The leg frame 16 at the bottom of the cabin shell 13 is pulled out to support the second half tube plate 67, providing additional support for ground operation and making it safer and more convenient to carry the wounded on the tension cloth 65.

[0086] Select to use the rescue installation mechanism 4 alone or combine the mounting mechanism 3 and the support mechanism 6 according to actual needs. It is suitable for rescuing one seriously wounded person and can also handle multiple slightly wounded people at the same time, improving the flexibility and efficiency of rescue, allowing for quick configuration adjustment to adapt to different rescue scenarios, enhancing the ability to respond to emergencies, especially in emergency situations, being able to quickly respond and implement effective rescue operations.

[0087] Finally, it should be noted that the above are only the preferred embodiments of the present invention and are not used to limit the present invention. Although the present invention has been described in detail with reference to the foregoing embodiments, for those skilled in the art, they can still modify the technical solutions recorded in the foregoing embodiments, or perform equivalent replacements for some of the technical features. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention shall be included within the protection scope of the present invention.

Claims

1. A manned suspension pod for drone rescue, comprising a drone (2), characterized in that: A hanging cabin mechanism (1) for switching the rescue mode is provided at the bottom of the drone (2). A rescue installation mechanism (4) for adjusting the swinging amplitude of the wounded is provided inside the hanging cabin mechanism (1). A medical institution cabin (5) for rescuing and placing the wounded is provided inside the rescue installation mechanism (4). A mounting mechanism (3) for mounting the medical institution cabin (5) and a support mechanism (6) for placing the wounded are provided inside the rescue installation mechanism (4). The hanging cabin mechanism (1) includes a cabin shell (13) mounted at the bottom of the drone (2). A plurality of mounting frames (14) are provided on the inner wall of the cabin shell (13), and a ring shaft (15) is provided on the inner wall of the mounting frame (14). The rescue installation mechanism (4) includes a half pipe (42). Slide grooves (43) for slidably mounting the mounting mechanism (3) and the support mechanism (6) are provided on both sides of the upper end of the mounting frame (14).

2. The manned suspension pod based on drone rescue according to claim 1, wherein: Support frames (11) are symmetrically provided on both sides of the bottom of the cabin shell (13). Two relatively moving leg frames (16) are slidably mounted in the middle of the lower end of the cabin shell (13). Snap rings (17) for restricting the sliding of the mounting mechanism (3) and the support mechanism (6) are provided on both sides of the cabin shell (13). Advection covers (9) are rotatably mounted at both ends of the cabin shell (13) through hinges. A connection device (10) is provided at the upper end of the cabin shell (13).

3. The manned suspension pod for drone-based rescue according to claim 1, wherein: A half shell (41) is commonly provided in the middle of the upper ends of the two slide grooves (43). The half shell (41) and the half pipe (42) are both fixedly mounted inside the ring shaft (15). A plurality of support arc rods (45) are provided on the inner wall of the half pipe (42) at equal intervals. A limiting block (47) is slidably mounted in the middle of each of the plurality of support arc rods (45). Springs (46) sleeved on the outer surface of the support arc rods (45) are provided on both sides of the limiting block (47).

4. The manned suspension pod based on drone rescue according to claim 3, wherein: The rescue installation mechanism (4) further includes a slide groove plate (44). A plurality of first air cushions (48) are provided in the slide groove plate (44) at equal intervals. The first air cushions (48) are used to restrict the up and down sliding of the limiting block (47) inside it. A first air cushion (48) is provided at the bottom of the slide groove plate (44). An arc piece (49) is provided at the bottom of the outer surface of the first air cushion (48).

5. The manned suspension pod based on drone rescue according to claim 4, characterized in that: A slot (413) is opened on one side of the upper end of the slide groove plate (44). A plug block (411) is inserted into the slot (413). A wedge block (412) is inserted into the plug block (411). Magnetic sheets (414) for adsorbing the wedge block (412) and preventing the wedge block (412) from falling off during jitter are provided on both sides of the plug block (411).

6. The manned suspension pod based on drone rescue according to claim 1, wherein: The medical institution cabin (5) includes a medical shell (51). A T-rail (57) is provided at the bottom of the medical shell (51). An oxygen generator (52) is provided on one side of the medical shell (51). An oxygen pipe is provided inside the oxygen generator (52), and one end of the oxygen pipe penetrates through the medical shell (51) and extends into its interior and is fixedly installed with an oxygen mask (55). A second air cushion (54) is provided at the bottom of the oxygen mask (55). A plurality of elastic bands (53) are provided on the inner wall of the medical shell (51) at equal intervals. The T-rail (57) is slidably installed inside the chute plate (44).

7. The manned suspension pod based on drone rescue according to claim 1, wherein: The bracket mechanism (6) includes a second half pipe plate (67). Two second sliders (61) are provided at the upper end of the second half pipe plate (67). A protective plate (62) is provided on one side of the second half pipe plate (67). Rectangular groove blocks (66) are symmetrically provided on the inner wall of the second half pipe plate (67). A plurality of straps (63) are provided at equal intervals on the upper ends of the two rectangular groove blocks (66) together.

8. The manned suspension pod based on drone rescue according to claim 7, wherein: Support rods (69) are slidably installed inside the two rectangular groove blocks (66) respectively. A tension cloth (65) is provided between the two support rods (69). A third air cushion (64) is provided at the bottom of the inner wall of the second half pipe plate (67). The second slider (61) is slidably installed inside the chute (43), and a second positioning ring block (68) is provided on the outer surface of one side of the second half pipe plate (67). The second positioning ring block (68) is slidably installed inside one of the snap rings (17).

9. The manned suspension pod for drone-based rescue according to claim 1, wherein: The mounting mechanism (3) includes a first half pipe plate (31). Two first sliders (32) are provided at the upper end of the first half pipe plate (31), and both of the two first sliders (32) are slidably installed inside the chute (43). An installation groove rail (33) is provided in the middle of the inner wall of the first half pipe plate (31). A first positioning ring block (34) is provided on the outer surface of one side of the first half pipe plate (31), and the first positioning ring block (34) is slidably installed inside one of the snap rings (17).

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