Anti-impact gyroscope external protection frame

Abstract

The utility model relates to the field of unmanned aerial vehicle protection, in particular to an anti-collision gyroscope external protection frame which comprises an unmanned aerial vehicle body, a gyroscope, a fixing block, a supporting rod, a protection assembly and the like. A cover plate is arranged on the unmanned aerial vehicle body; a gyroscope is mounted in the unmanned aerial vehicle body; a plurality of fixing blocks are mounted on the unmanned aerial vehicle body; a plurality of mounting frames are arranged on each fixing block; a protection assembly used for protecting the unmanned aerial vehicle body is installed on the unmanned aerial vehicle body. A plurality of unmanned aerial vehicles are stacked together and are uniformly placed in a special protective box body, so that a plurality of protective box bodies are not needed, the transportation and production cost is reduced, and meanwhile, the short rod end parts of the supporting rods protrude out of the side surface positions of the folded wings of the unmanned aerial vehicles, so that the unmanned aerial vehicles can be conveniently and quickly folded. Wing damage caused by scratching and collision between the wings and the inner wall of the protection box body is avoided, and therefore protection of the wings of the unmanned aerial vehicle is improved.

Description

Technical Field

[0001] This utility model relates to the field of drone protection, and in particular to an impact-resistant external protective frame for a gyroscope. Background Technology

[0002] As the tactile sensor of a drone's flight nervous system, the gyroscope has a decisive impact on the drone's flight safety and control experience. When a drone crashes unexpectedly, the violent impact may cause the precision components inside the gyroscope to shift or be damaged. To reduce the damage to the gyroscope, a protective frame is usually added to the drone's shell so that the protective frame impacts the ground before the drone's shell, thus protecting the drone. However, in large-scale drone shows, to ensure the safety of the drones, an independent transportation method of "one drone, one box" is usually adopted. Although independent packaging can effectively reduce the risk of equipment damage, large-scale shows usually require hundreds or even thousands of drones, each with its own box. The additional protective frame on the outside of the drone not only increases the overall size and weight of the box, but the time and manpower costs required for loading and unloading all the drones are also difficult to estimate.

[0003] In summary, this application proposes an impact-resistant external protective frame for a gyroscope, thereby addressing the aforementioned technical problems. Utility Model Content

[0004] To overcome the drawbacks of adding a protective frame to the outside of a drone, which not only increases the overall size and weight of the container but also makes the time and manpower costs required for all drone loading and unloading processes difficult to estimate, this utility model provides an impact-resistant external protective frame for a gyroscope.

[0005] The technical solution of this utility model is as follows: an impact-resistant gyroscope external protective frame, including an unmanned aerial vehicle (UAV) body and a gyroscope; the UAV body is provided with several wings for easy folding and storage, and the connection between each wing and the UAV body is a damped rotational connection, with the connection between the front wing and the UAV body being able to be pulled outwards; a cover plate is provided on the UAV body; a main control board is provided inside the UAV body, and an acceleration sensor is installed on the main control board; the gyroscope is installed inside the UAV body, and the gyroscope's wires are connected to the main control board; it also includes fixing blocks, support rods, and protective components; several fixing blocks are installed on the UAV body; several mounting frames are provided on each fixing block; each mounting frame is rotatably connected to a support rod for easy storage and stacking of the UAV body, the support rod consists of mutually perpendicular short rods and long rods, the short rods are rotatably connected to the mounting frames; each support rod's short rod is provided with a limit hole; a protective component for protecting the UAV body is installed on the UAV body.

[0006] As a preferred embodiment of this utility model, the external protective frame for the gyroscope includes a motor, a limiting block, and a protective cloth. A motor is fixedly connected to each mounting frame, and the short rod of each support rod is connected to the output end of the motor, driving adjacent support rods to rotate. A limiting block is connected to the end of the long rod of each support rod furthest from the motor, and a spring telescopic rod is fixedly connected between each limiting block and the long rod of the support rod. All support rods are connected together by a protective cloth for shielding from rain, and the protective cloth is made of an elastic deformable material. Several collars are provided on the protective cloth, and each collar is fitted onto the long rod of an adjacent support rod. A groove adapted to the limiting block is provided on the long rod of each support rod.

[0007] As a preferred technical solution of this utility model, the protective components of the above-mentioned gyroscope external protective frame further include folded plates, elastic elements, and protective blocks; several folded plates are slidably connected to the cover plate of the drone body; several connecting parts are provided on the gyroscope, and the lower side of each folded plate contacts the adjacent connecting part; several elastic elements are fixedly connected inside the drone body; several mounting seats are provided on the main control board for placing the gyroscope; each elastic element passes through the adjacent mounting seat and is connected to the connecting part; a protective block for protecting the gyroscope is provided on the cover plate of the drone body, and the inner side of the protective block is made of elastic and soft material.

[0008] As a preferred technical solution of this utility model, in the above-mentioned external protective frame for the gyroscope, the short end of the support rod protrudes from the side of the UAV wing after it is folded.

[0009] As a preferred technical solution of this utility model, in the above-mentioned external protective frame for the gyroscope, each support rod is provided with a spiral protrusion on its long rod to restrict the movement of the collar, and the spiral protrusion is made of rubber.

[0010] As a preferred technical solution of this utility model, in the above-mentioned external protective frame for the gyroscope, each folded plate is provided with a limiting part, and each limiting part is made of rubber.

[0011] As a preferred technical solution of this utility model, in the above-mentioned external protective frame of the gyroscope, all the collars are distributed at the four corners of the protective cloth.

[0012] As a preferred embodiment of this utility model, the external protective frame of the gyroscope also includes a mounting plate; the mounting plate is rotatably connected to the cover plate of the unmanned aerial vehicle body, and the protective block is located on the mounting plate.

[0013] As a preferred technical solution of this utility model, the protective cloth in the above-mentioned gyroscope external protective frame is made of waterproof material.

[0014] The usage of impact-resistant gyroscope external protective frames includes the following:

[0015] S1: Adjust the frame status and control the motor to drive the support rods to rotate, so that the four support rods are in a vertical position, which makes it easier to stack multiple drones;

[0016] S2: Emergency protection. In the event of an accidental drone crash, the control motor drives the support rod to rotate, which works in conjunction with the protective cloth to act as a parachute, slowing down the drone's descent speed due to wind resistance.

[0017] S3: Gyroscope protection. The motor drives the support rod to rotate and separate from the folding plate, thus separating the gyroscope from the main control board. This prevents damage to the gyroscope caused by the rigid connection and improves the protection effect of the gyroscope.

[0018] Beneficial effects: This utility model enables multiple drones to be stacked together and placed into a single protective box, eliminating the need for multiple protective boxes, reducing transportation and production costs. At the same time, by having the short end of the support rod protrude from the side of the drone's folded wings, it avoids scratching and collisions between the wings and the inner wall of the protective box, thus preventing wing damage and improving the protection of the drone's wings.

[0019] By guiding and limiting the loops on the protective cloth with support rods, the protective cloth will be stretched upward by the wind to form a parachute, thereby slowing down the fall speed of the drone and avoiding a strong impact with the ground, thus improving the protection of the internal parts of the drone.

[0020] The spiral protrusions of the support rod are tightly attached to the cover plate, blocking and limiting the collars of the adjacent protective cloth. This prevents the collars from sliding past the spiral protrusions, thus preventing the protective cloth from sliding on the long rod of the support rod due to wind force after the drone takes off, folding and piling up to one side, and reducing the protective cloth's shielding effect on the upper side of the drone.

[0021] By rotating the support rods, the state of the four support rods is changed, forming the external frame of the drone when it is not in use. This facilitates the stacking of multiple drones, reducing transportation and production costs. When the drone is in flight, it works with the protective cloth to reduce the fall speed of a drone that accidentally falls. At the same time, it works with the folding plate to separate the gyroscope from the main control board, preventing damage to the gyroscope caused by rigid connections and improving the protection of the gyroscope. Attached Figure Description

[0022] Figure 1 This is a three-dimensional structural diagram of the impact-resistant external protective frame for the gyroscope of this utility model.

[0023] Figure 2This is a three-dimensional structural diagram of the fixing block, support rod, and protective components of this utility model;

[0024] Figure 3 This is a three-dimensional structural diagram of the fixing block and support rod of this utility model;

[0025] Figure 4 This is a three-dimensional structural diagram of the motor and limiting block of this utility model;

[0026] Figure 5 This is a schematic diagram of the motor mounting position according to this utility model;

[0027] Figure 6 This is a three-dimensional structural diagram of the folded plate, elastic element, and protective block of this utility model;

[0028] Figure 7 This is a cross-sectional view of the protective block of this utility model;

[0029] Figure 8 This is a three-dimensional structural diagram of the gyroscope of this utility model.

[0030] Wherein: 1-Unmanned aircraft body, 1001-Cover plate, 1002-Main control board, 1003-Mounting base, 2-Fixing block, 2001-Mounting frame, 3-Support rod, 3001-Limiting hole, 3002-Spiral convex strip, 4-Gyroscope, 4001-Connecting part, 101-Motor, 102-Limiting block, 103-Protective cloth, 10301-Collar, 201-Folded plate, 20101-Limiting part, 202-Elastic element, 203-Protective block, 301-Mounting plate, 30101-Clocking block. Detailed Implementation

[0031] The present invention will be described in detail below with reference to the accompanying drawings and specific embodiments, but this is not intended to limit the present invention.

[0032] Example 1

[0033] Impact-resistant gyroscope external protective frame, such as Figures 1-8 As shown, the device includes a drone body 1 and a gyroscope 4. The drone body 1 is equipped with four wings for easy folding and storage, and the connection between each wing and the drone body 1 is a damped rotational connection. The connection between the two front wings and the drone body 1 can be pulled outward. The drone body 1 is equipped with a cover plate 1001. The drone body 1 is equipped with a main control board 1002, and an acceleration sensor is installed on the main control board 1002. The drone body 1 is equipped with a gyroscope 4, and the wires of the gyroscope 4 are connected to the main control board 1002.

[0034] It also includes a fixing block 2, a support rod 3, and a protective component; two front-to-back symmetrical fixing blocks 2 are installed on the unmanned aerial vehicle body 1; each fixing block 2 is provided with two left-to-right symmetrical mounting frames 2001; each mounting frame 2001 is rotatably connected to a support rod 3, the support rod 3 is composed of mutually perpendicular short rods and long rods, the short rods are rotatably connected to the mounting frames 2001; each support rod 3 has a limit hole 3001 on its short rod; the unmanned aerial vehicle body 1 is equipped with a protective component.

[0035] The protective assembly includes a motor 101, a limiting block 102, and a protective cloth 103. A motor 101 is fixedly connected to each mounting frame 2001, and the short rod of each support rod 3 is connected to the output end of the motor 101, driving the adjacent support rod 3 to rotate. A limiting block 102 is connected to the end of the long rod of each support rod 3 away from the motor 101, and a spring telescopic rod is fixedly connected between each limiting block 102 and the long rod of the support rod 3. All support rods 3 are connected together by a protective cloth 103, which is made of an elastic material. Four collars 10301 are provided on the protective cloth 103, and each collar 10301 is fitted onto the long rod of the adjacent support rod 3. A groove adapted to the limiting block 102 is provided on the long rod of each support rod 3.

[0036] The protective components also include a folded plate 201, an elastic element 202, and a protective block 203; two symmetrical folded plates 201 are slidably connected to the cover plate 1001 of the unmanned aircraft body 1; two symmetrical connecting parts 4001 are provided on the gyroscope 4, and the lower side of each folded plate 201 contacts the adjacent connecting part 4001; four elastic elements 202 are fixedly connected inside the unmanned aircraft body 1, and the elastic elements 202 are elastic telescopic rods; two symmetrical mounting seats 1003 are provided on the main control board 1002; each elastic element 202 passes through the adjacent mounting seat 1003 and is connected to the connecting part 4001; a protective block 203 is provided on the cover plate 1001 of the unmanned aircraft body 1, and the inner side of the protective block 203 is made of elastic and soft material.

[0037] The short end of support rod 3 protrudes from the side of the drone's folded wing.

[0038] Each support rod 3 has a spiral protrusion 3002 on its long rod, and the spiral protrusion 3002 is made of rubber.

[0039] Each folded plate 201 is provided with a limiting part 20101, and each limiting part 20101 is made of rubber material to increase the friction between the long rod of the support rod 3 and the folded plate 201, thereby enhancing the limiting effect of the support rod 3 on the folded plate 201.

[0040] All the loops 10301 are distributed at the four corners of the protective cloth 103.

[0041] The method for using an impact-resistant gyroscope external protective frame includes the following steps:

[0042] S1: Adjust the frame state and control the motor 101 to drive the support rod 3 to rotate, so that the four support rods 3 are in a vertical state, which makes it easier to stack multiple drones.

[0043] S2: Emergency protection. In the event of an accidental fall of the drone, the control motor 101 drives the support rod 3 to rotate, and works in conjunction with the protective cloth 103 to act as a parachute, slowing down the fall speed of the drone under the action of wind resistance.

[0044] S3: Protects the gyroscope. The motor 101 drives the support rod 3 to rotate and separate from the folding plate 201, so that the gyroscope 4 is separated from the main control board 1002, preventing the rigid connection from damaging the gyroscope 4 and improving the protection effect of the gyroscope 4.

[0045] The working process of this embodiment is as follows:

[0046] In large-scale drone shows, to ensure the safety of drones, an independent transportation method of "one drone per box" is usually adopted. Although independent packaging can effectively reduce the risk of equipment damage, large-scale shows usually require hundreds or even thousands of drones, and each drone has an independent box. Not only is the volume and weight of transportation very large, but the time and manpower costs required for loading and unloading are also difficult to estimate.

[0047] To solve the above problems, when the drone needs to be stored in the housing, the two rear wings of the drone body 1 are first folded towards the left and right sides of the drone body 1, respectively, so that the wings are in contact with the adjacent side walls of the drone body 1. Then, the two front wings are pulled outward and folded towards the side walls of the drone body 1, so that the two front wings are in contact with the two rear wings. Initially, all four support rods 3 are in a horizontal position. On this basis, the support rods 3 are manually rotated so that the limiting holes 3001 of each support rod 3 are facing upward. At this time, the ends of the long rods of each support rod 3 are lower than the lower side of the folded wings. Figure 3As shown, repeat the above steps to store the second drone. After completing the above operations, insert the lower ends of the four support rods 3 of the second drone into the four limiting holes 3001 on the support rod 3 of the first drone, so that the two drones are stacked. Then repeat the above steps to stack multiple drones together. The specific number depends on the size of the protective box. Finally, put the stacked drones into the protective box. In this way, multiple drones are loaded, thereby reducing transportation and production costs. At the same time, since the short rod ends of the support rods 3 protrude from the side of the drone wings after folding, manual storage will effectively avoid scratches and collisions between the wings and the inner wall of the protective box, which could damage the wings and improve the protection of the drone wings.

[0048] Considering that if the drone crashes during flight, it will damage the gyroscope 4 inside the drone body 1. To reduce the extent of damage during a crash, before takeoff, all motors 101 are controlled to rotate adjacent support rods 3, making all support rods 3 parallel to the cover plate 1001 of the drone body 1. Then, the limiting blocks 102 on the support rods 3 are pressed down, so that the limiting blocks 102 fit into the grooves of the long rods of the support rods 3. Then, the collars 10301 of the protective cloth 103 are passed through the limiting blocks 102 and fitted onto the long rods of the support rods 3. Then, the limiting blocks 102 are released, and the spring telescopic rods on the support rods 3 drive the limiting blocks 102 to reset. The above operation steps are repeated until all four collars 10301 of the protective cloth 103 are fitted onto the adjacent support rods 3. Then, the protective cloth 103 is laid flat on top of the cover plate 1001 of the drone body 1. Figure 1 As shown, the drone is then started. At the same time, the spiral protrusion 3002 of the support rod 3 is tightly attached to the cover plate 1001, blocking and limiting the collar 10301 of the adjacent protective cloth 103, preventing the collar 10301 from sliding over the spiral protrusion 3002. This prevents the protective cloth 103 from sliding on the long rod of the support rod 3 due to wind force after the drone takes off, causing it to fold and pile up to one side, reducing the shielding effect of the protective cloth 103 on the upper side of the drone. It should be noted that in the above process, the motor 101 is used to rotate the support rod 3 instead of manually for storage.

[0049] When the drone crashes unexpectedly, the accelerometer on the main control board 1002 will be triggered. Based on the signal from the accelerometer, the control module controls the motor 101 to rapidly rotate the adjacent support rods 3 until the long rods of the front and rear support rods 3 form an inverted V-shape. Simultaneously, as the support rods 3 rotate, the spiral protrusions 3002 of the support rods 3 separate from the cover plate 1001, no longer blocking the loops 10301 of the protective cloth 103. The four loops 10301 will slide along the long rods of the adjacent support rods 3 towards the limiting block 102 until they are blocked by the limiting block 102. The protective cloth 103 will then be stretched upwards by the wind, forming an arch shape, acting as a parachute to reduce wind resistance. This design slows down the descent speed of the drone, preventing a strong impact with the ground and thus improving the protection of the drone's internal components. Simultaneously, the long rod of the support rod 3 guides and limits the sliding of the loops 10301 on the protective cloth 103. Compared to the prior art of directly installing a parachute on the drone, this invention effectively avoids the parachute lines becoming tangled and unable to open smoothly during deployment. Furthermore, since the four loops 10301 are distributed at the four corners of the protective cloth 103, the protective cloth 103 will form a larger effective wind-blocking area when it expands outwards, increasing resistance. The corner layout also helps the protective cloth 103 remain flat under airflow, reducing wrinkles and improving the drone's descent slowing effect.

[0050] Furthermore, considering that the gyroscope 4, as the tactile sensor of the drone's flight nervous system, has a decisive impact on the drone's flight safety and control experience, the gyroscope 4 inside the drone is usually connected to the main control board 1002 by bolts. When the drone crashes and collides with the ground, this rigid connection will cause severe damage to the gyroscope 4 on the main control board 1002. Existing technology only increases cushioning by wrapping the gyroscope 4 with a soft material to reduce the damage caused by the collision. However, the gyroscope 4 generates heat after long-term operation, and the soft material wrapped around it will significantly hinder the absorption of heat. Heat dissipation caused the gyroscope 4 to overheat and be damaged. To solve this problem, initially, each support rod 3 is parallel to the cover plate 1001 of the unmanned aerial vehicle body 1, and each folded plate 201 is squeezed by the adjacent support rod 3. Correspondingly, the two connecting parts 4001 of the gyroscope 4 are squeezed by the adjacent folded plates 201, and the telescopic end of the elastic element 202 is squeezed by the connecting parts 4001, which is in a compressed state. When the motor 101 drives the adjacent support rod 3 to rotate rapidly, the support rod 3 will separate from the folded plate 201, the downward pressure on the folded plate 201 will disappear, and the folded plate 201 will be squeezed by the elastic element 2001. The gyroscope 4 moves upward due to the rebound and reset action of the elastic element 202. Simultaneously, the telescopic end of the elastic element 202 presses against the connecting part 4001 of the gyroscope 4, causing the connecting part 4001 of the gyroscope 4 to detach from the mounting base 1003. Pushed by the elastic element 202, the gyroscope 4 enters the protective block 203, fitting against the inner side of the protective block 203. The soft material inside the protective block 203 then wraps and protects the gyroscope 4. Therefore, during normal flight of the drone, the design of the protective block 203 does not affect the normal heat dissipation of the gyroscope 4. Furthermore, in the event of a drone crash, the gyroscope 4 is protected by connecting it to the main control board 1002. Separation is achieved to prevent damage to the gyroscope 4 caused by the rigid connection, thus improving the protection of the gyroscope 4. By rotating the support rod 3, the state of the four support rods 3 is changed. When the drone is not in use, it forms the external frame of the drone, which facilitates the stacking of multiple drones and reduces transportation and production costs. When the drone is in flight, it works with the protective cloth 103 to reduce the fall speed of the drone in case of an accidental fall. At the same time, it works with the folding plate 201 to separate the gyroscope 4 from the main control board 1002, preventing damage to the gyroscope 4 caused by the rigid connection and improving the protection of the gyroscope 4.

[0051] Example 2

[0052] Based on Example 1, such as Figure 1 , Figure 2 , Figure 6 and Figure 7 As shown, it also includes a mounting plate 301; the mounting plate 301 is rotatably connected to the cover plate 1001 of the unmanned body 1, and the protective block 203 is located on the mounting plate 301.

[0053] Protective fabric 103 is made of waterproof material.

[0054] The working steps of this embodiment are as follows:

[0055] To facilitate manual inspection and maintenance of the gyroscope 4, the operator only needs to pull the locking block 30101 upwards, causing the mounting plate 301 to rotate the protective block 203 upwards, thus removing the protective block 203 from obstructing the gyroscope 4. This allows the operator to directly observe whether the gyroscope 4 inside the drone has shifted, eliminating the need to disassemble the entire drone and improving the ease of use of the device. At the same time, since the protective cloth 103 is made of waterproof material, it protects the upper side of the drone during flight, preventing rainwater from dripping onto the mounting plate 301 and the cover plate 1001, thereby improving the drone's waterproof performance.

[0056] Although this disclosure has been described with respect to only a limited number of embodiments, those skilled in the art who benefit from this disclosure will understand that various other embodiments can be devised without departing from the scope of this invention. Therefore, the scope of this invention should be limited only by the appended claims.

Claims

1. Anti-collision gyroscope external protection frame, including unmanned aerial vehicle body (1) and gyroscope (4); A plurality of folding storage wings are arranged on the unmanned aerial vehicle body (1), and the connecting parts of each wing and the unmanned aerial vehicle body (1) are arranged as damping rotary connections; The connecting part of the wing located in front and the unmanned aerial vehicle body (1) can be pulled outwards; The unmanned aerial vehicle body (1) is provided with a cover plate (1001); The unmanned aerial vehicle body (1) is provided with a main control board (1002), and an acceleration sensor is installed on the main control board (1002); The unmanned aerial vehicle body (1) is provided with a gyroscope (4), and the wire of the gyroscope (4) is connected with the main control board (1002); The characteristic is, It also includes a fixing block (2), a support rod (3) and a protective component; several fixing blocks (2) are installed on the unmanned aircraft body (1); several mounting frames (2001) are provided on each fixing block (2); a support rod (3) is rotatably connected to each mounting frame (2001) to facilitate the storage and stacking of the unmanned aircraft body (1), the support rod (3) is composed of short rods and long rods that are perpendicular to each other, and the short rods are rotatably connected to the mounting frames (2001); a limit hole (3001) is provided on the short rod of each support rod (3); a protective component for protecting the unmanned aircraft body (1) is installed on the unmanned aircraft body (1).

2. The crashworthy gyroscopic outer containment frame of claim 1, wherein, The protective assembly includes a motor (101), a limiting block (102), and a protective cloth (103); a motor (101) is fixedly connected in each mounting frame (2001), and the short rod of each support rod (3) is connected to the output end of the motor (101), so that the adjacent support rod (3) can be rotated by the motor (101); the long rod of each support rod (3) is connected to the limiting block (102) at the end away from the motor (101), and each limiting block (102) Spring telescopic rods are fixedly connected to the long rods of the support rods (3); a protective cloth (103) for shielding rainwater is connected to all the support rods (3), and the protective cloth (103) is made of elastic deformation material; a number of collars (10301) are provided on the protective cloth (103), and each collar (10301) is sleeved on the long rod of the adjacent support rod (3); a groove adapted to the limiting block (102) is opened on the long rod of each support rod (3).

3. The anti-impact, gyroscopic outer protective frame according to claim 2, characterized in that, The protective components also include a folded plate (201), an elastic element (202), and a protective block (203); several folded plates (201) are slidably connected to the cover plate (1001) of the unmanned aircraft body (1); several connecting parts (4001) are provided on the gyroscope (4), and the lower side of each folded plate (201) is in contact with the adjacent connecting part (4001); several elastic elements (202) are fixedly connected inside the unmanned aircraft body (1); several mounting seats (1003) are provided on the main control board (1002) for placing the gyroscope (4); each elastic element (202) passes through the adjacent mounting seat (1003) and is connected to the connecting part (4001); a protective block (203) for protecting the gyroscope (4) is provided on the cover plate (1001) of the unmanned aircraft body (1), and the inner side of the protective block (203) is made of elastic and soft material.

4. The crashworthy gyroscopic outer containment frame of claim 1, wherein, The short end of the support rod (3) protrudes from the side of the UAV wing after it is folded.

5. The crashworthy gyroscopic outer containment frame of claim 2, wherein, Each support rod (3) has a spiral protrusion (3002) on its long rod to restrict the movement of the collar (10301), and the spiral protrusion (3002) is made of rubber.

6. The impact-resistant gyroscope external protective frame according to claim 3, characterized in that, Each folded plate (201) is provided with a limiting part (20101), and each limiting part (20101) is made of rubber.

7. The impact-resistant gyroscope external protective frame according to claim 2, characterized in that, All the loops (10301) are distributed at the four corners of the protective cloth (103).

8. The impact-resistant gyroscope external protective frame according to claim 3, characterized in that, It also includes a mounting plate (301); the mounting plate (301) is rotatably connected to the cover plate (1001) of the unmanned body (1), and the protective block (203) is located on the mounting plate (301).

9. The impact-resistant gyroscope external protective frame according to claim 2, characterized in that, The protective fabric (103) is made of waterproof material.

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