Hanging mechanism and flying transporter

Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a mounting mechanism and a flight transporter. The hanging mechanism comprises a shell, a buckling arm and a hook, the shell is provided with a placement cavity, the buckling arm and the hook are both located in the placement cavity, the hook is rotationally connected with the shell, the buckling arm is rotationally or slidably connected with the shell, an avoiding groove communicated with the placement cavity is formed in the edge, facing the interior of the shell, of the shell, and the avoiding groove is located between the switching position of the buckling arm and the switching position of the hook; the hook is provided with a first rotating position and a second rotating position, and when the hook is located at the first rotating position, goods are hung on the hook or unloaded from the hook through the avoiding groove; and when the hook rotates to the second rotating position, the free end of the hook stretches across the avoiding groove and is buckled with the buckling arm. The rope of goods can be prevented from being separated from the hanging mechanism. The mounting mechanism provided by the embodiment is simple in structure, low in cost and high in reliability.

Description

Technical Field

[0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a mounting mechanism and a flying transporter. Background Art

[0002] UAV transportation of materials is an emerging logistics transportation method. It can use drones to quickly and efficiently deliver materials to the destination. It can deliver materials to the destination in a shorter time, avoid traffic congestion and terrain obstacles, shorten logistics distribution time, and improve transportation efficiency. With the continuous development and application of drone technology, drone transportation of materials will become an important logistics transportation method in the future.

[0003] The mounting or unloading of cargo to the drone is achieved through the mounting mechanism. The cargo can be mounted on the drone through the mounting mechanism, and after the drone flies to the destination, the mounting mechanism can unload the cargo so that the cargo can be thrown to the destination.

[0004] However, as the weight of UAV cargo continues to increase, the existing mounting mechanism has become more and more complex in order to adapt to the weight of the cargo, which not only has low reliability but also leads to excessively high costs of the mounting mechanism. Moreover, during the flight of the UAV, the vibration of the UAV may cause the mounting mechanism to fail, resulting in the cargo falling, and even causing serious falling accidents. Summary of the invention

[0005] The purpose of the embodiments of the present application is to provide a mounting mechanism, aiming to solve the problem of how to improve the reliability of the mounting mechanism and reduce the cost of the mounting mechanism.

[0006] To achieve the above purpose, the technical solution adopted in this application is:

[0007] In a first aspect, a mounting mechanism is provided for mounting cargo, the mounting mechanism comprising: a shell, a snap arm and a hook, the shell having a placement cavity, the snap arm and the hook both being located in the placement cavity, the hook being rotatably connected to the shell, the snap arm being rotatably or slidably connected to the shell, an edge of the shell being provided with an avoidance groove communicating with the placement cavity toward the inside of the shell, the avoidance groove being located between a transition point of the snap arm and a transition point of the hook; the hook having a first rotation position and a second rotation position, when the hook is in the first rotation position, the cargo is mounted on or unloaded from the hook through the avoidance groove; when the hook is rotated to the second rotation position, the free end of the hook spans the avoidance groove and snaps into the snap arm, and the position where the snap arm abuts against the hook moves a predetermined distance in a direction away from the hook, so that the hook switches to the first rotation position.

[0008] In some embodiments, the mounting mechanism also includes a reset member located in the mounting cavity and having an elastic restoring force, one end of the reset member is connected to the shell, and the other end of the reset member abuts against the snap arm, and when the hook switches from the first rotation position to the second rotation position, the hook drives the snap arm to compress the reset member, and when the hook is in the second rotation position, the reset member restricts the snap arm from detaching from the hook.

[0009] In some embodiments, the distance from the position where the hook abuts against the buckle arm to the rotation point of the hook is L1, the distance from the mounting point of the cargo to the rotation point of the hook is L2, and L1 is greater than L2.

[0010] In some embodiments, the snap arm is rotatably connected to the shell, and the mounting mechanism also includes a driver located in the placement cavity, and the driver is used to drive the snap arm to rotate in a direction away from the hook so that the hook switches to the first rotation position.

[0011] In some embodiments, the distance from the position where the driver drives the snap arm to the snap arm transition point is L3, the distance from the position where the snap arm abuts the hook to the snap arm transition point is L4, and L3 is greater than L4.

[0012] In some embodiments, the mounting mechanism also includes a limit column and a limit platform both located in the placement cavity, the limit column and the limit platform are both connected to the shell, the limit column is used to limit the rotation range of the hook from the first rotation position to the second rotation position, and the limit platform is used to limit the rotation range of the hook from the second rotation position to the first rotation position.

[0013] In some embodiments, the snap arm includes a first arm segment, a second arm segment and a third arm segment, the two ends of the second arm segment are respectively connected to the first arm segment and the third arm segment, the first arm segment is rotatably or slidably connected to the shell and is provided with a snap groove for snapping the hook.

[0014] In some embodiments, the hook has a hanging slot, and the hanging slot is used to hang the cargo.

[0015] In some embodiments, the mounting mechanism further includes a sensing switch located in the placement cavity, and the sensing switch is used to detect whether the hook is in the first rotation position or in the second rotation position.

[0016] In a second aspect, a flying transport vehicle is provided, which includes the mounting mechanism. The flying transport vehicle also includes a drone, and the mounting mechanism is connected to the drone.

[0017] The beneficial effects of the present application are as follows: the mounting mechanism includes a housing, a buckle arm and a hook, the buckle arm and the hook are respectively located on both sides of the avoidance groove, and when the hook is in the first rotation position, the cargo can be loaded onto the hook through the rope, or the hook releases the rope at the destination. When the hook is in the second rotation position, the rope of the cargo is limited to the area defined by the groove wall of the avoidance groove and the hook, preventing the rope of the cargo from detaching from the mounting mechanism. The mounting mechanism provided by this embodiment has a simple structure, low cost, and high reliability. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings required for use in the embodiments or exemplary technical descriptions will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0019] Figure 1 is a schematic diagram of the three-dimensional structure of the mounting mechanism provided in an embodiment of the present application;

[0020] Figure 2 yes Figure 1 A partial exploded schematic diagram of the hook being in a second rotation position;

[0021] Figure 3 yes Figure 2 A front view schematic diagram of a bottom shell;

[0022] Figure 4 yes Figure 1 A schematic structural diagram of a hook in a first rotation position;

[0023] Figure 5 yes Figure 2 Further explosion diagram of .

[0024] Among them, the reference numerals in the figure are:

[0025] 100, mounting mechanism; 101, housing; 102, hook; 103, buckle arm; 111, bottom shell; 112, top shell; 206, lever; 107, safety pin; 104, avoidance groove; 106, safety hole; 105, placement cavity; 201, reset member; 202, driver; 203, induction switch; 204, limit table; 205, limit column; 2061, operation hole; 1021, hanging slot; 1031, first arm section; 1032, second arm section; 1033, third arm section; DETAILED DESCRIPTION

[0026] In order to make the purpose, technical solution and advantages of the present application more clearly understood, the present application is further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention and are not used to limit the present application.

[0027] It should be noted that when a component is referred to as being "fixed on" or "disposed on" another component, it may be directly on the other component or indirectly on the other component. When a component is referred to as being "connected to" another component, it may be directly or indirectly connected to the other component. The orientation or positional relationship indicated by the terms "upper", "lower", "left", "right", etc. is based on the orientation or positional relationship shown in the accompanying drawings, and is only for the convenience of description, and does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present application. For ordinary technicians in this field, the specific meanings of the above terms can be understood according to the specific circumstances. The terms "first" and "second" are only used for the purpose of convenience of description, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of technical features. The meaning of "multiple" is two or more, unless otherwise clearly and specifically defined.

[0028] See also Figures 1 to 3 The embodiment of the present application provides a mounting mechanism 100 and a flying transporter having the same. The mounting mechanism 100 is used to mount cargo and unload the cargo at the destination after the flying transporter reaches the destination.

[0029] See also Figures 2 to 5 The mounting mechanism 100 includes: a shell 101, a buckle arm 103 and a hook 102. The shell 101 has a placement cavity 105. The buckle arm 103 and the hook 102 are both located in the placement cavity 105. The hook 102 is rotatably connected to the shell 101, and the buckle arm 103 is rotatably or slidably connected to the shell 101.

[0030] See also Figures 2 to 5 The edge of the shell 101 is provided with an escape groove 104 communicating with the placement cavity 105 toward the inside of the shell 101, and the escape groove 104 is located between the transition point of the buckle arm 103 and the transition point of the hook 102. During use, the shell 101 is arranged in the vertical direction, the escape groove 104 is opened at the lower end surface of the shell 101, and extends a certain distance toward the center position of the shell 101, and the escape groove 104 passes through the two opposite surfaces of the shell 101. The hook 102 rotates along the transition point between it and the shell 101, and can be partially exposed at the escape groove 104 to load or unload goods.

[0031] See also Figures 2 to 5The hook 102 has a first rotation position and a second rotation position. When the hook 102 is in the first rotation position, the goods are mounted on or unloaded from the hook 102 through the avoidance groove 104, thereby realizing the loading or delivery of the goods.

[0032] See also Figures 2 to 5 When the hook 102 rotates from the first rotation position to the second rotation position, the free end of the hook 102 crosses the avoidance groove 104 and is buckled with the buckle arm 103, and the buckle arm 103 can support the hook 102 and keep the hook 102 in the second rotation position. The free end of the hook 102 rotates to the other side of the avoidance groove 104 and is detachably connected to the buckle arm 103, so that the cargo can be stably mounted on the hook 102. It can be understood that the cargo can be mounted on the hook 102 by a rope, and the rope on the cargo is limited to the area defined by the groove wall of the avoidance groove 104 and the hook 102, so that the rope of the cargo can be prevented from being separated from the mounting mechanism 100 when the mounting mechanism 100 is vibrated, thereby improving the reliability of the mounting mechanism 100.

[0033] See also Figures 2 to 5 It is understood that the position where the snap arm 103 abuts against the hook 102 moves a predetermined distance in a direction away from the hook 102, so that the snap arm 103 is disengaged from the hook 102, and the hook 102 is switched to the first rotation position, so as to load or unload the goods. It is understood that the snap arm 103 can be rotated to connect the housing 101, so that the snap arm 103 is moved at the position where the snap arm abuts against the hook 102 through the rotation of the snap arm 103, so that the snap arm 103 is disengaged from the hook 102, and the angle value of the snap arm 103 rotation can be 5 degrees, 10 degrees or 30 degrees, which is not limited here and can be selected according to actual conditions.

[0034] See also Figures 2 to 5 It can also be understood that the snap arm 103 can be slidably connected to the shell 101, and the snap arm 103 can be moved in a straight line away from the hook 102 to achieve movement of the snap arm 103 to the position where it abuts the hook 102, thereby disengaging the snap arm 103 from the hook 102. The distance moved by the snap arm 103 can be 2 mm, 5 mm or 10 mm, which is not limited here and can be selected according to actual conditions.

[0035] See also Figures 2 to 5The mounting mechanism 100 provided in this embodiment includes a housing 101, a buckle arm 103 and a hook 102. The buckle arm 103 and the hook 102 are respectively located on both sides of the avoidance groove 104. When the hook 102 is in the first rotation position, the cargo can be loaded onto the hook 102 through the rope, or the hook 102 releases the rope at the destination. When the hook 102 is in the second rotation position, the rope of the cargo is limited to the area defined by the groove wall of the avoidance groove 104 and the hook 102, so as to prevent the rope of the cargo from escaping from the mounting mechanism 100. The mounting mechanism 100 provided in this embodiment has a simple structure, low cost and high reliability.

[0036] See also Figures 2 to 5 In some embodiments, the mounting mechanism 100 further includes a reset member 201 located in the placement cavity 105 and having elastic restoring force, and one end of the reset member 201 is connected to the shell 101 .

[0037] The other end of the reset member 201 abuts against the snap arm 103. When the hook 102 switches from the first rotation position to the second rotation position, the hook 102 drives the snap arm 103 to compress the reset member 201. When the hook 102 is in the second rotation position, the reset member 201 restricts the snap arm 103 from disengaging from the hook 102 and presses the snap arm 103 toward the hook 102, so that the snap arm 103 and the hook 102 remain tightly fastened, avoiding vibration of the mounting mechanism 100 and resulting in failure of cargo mounting.

[0038] See also Figures 2 to 5 It can be understood that when the position where the snap arm 103 abuts the hook 102 moves in a direction away from the hook 102, the snap arm 103 compresses the reset member 201. After the hook 102 switches from the second rotation position to the first rotation position, the snap arm 103 is disengaged from the hook 102, and the reset member 201 drives the snap arm 103 to reset.

[0039] See also Figures 2 to 5 Optionally, the reset member 201 is a torsion spring. When the snap arm 103 is rotated to connect to the shell 101, the main body of the torsion spring is arranged at the rotation point of the snap arm 103, and the two elastic arms of the torsion spring respectively abut against the shell 101 and the snap arm 103.

[0040] Optionally, the reset member 201 is a tube spring. When the snap arm 103 is slidably connected to the shell 101, the two ends of the tube spring are respectively connected to the shell 101 and the snap arm 103. When the snap arm 103 moves in a direction away from the hook 102, the tube spring is compressed and deformed.

[0041] See also Figures 2 to 5 In some embodiments, the distance from the position where the hook 102 abuts the buckle arm 103 to the rotation point of the hook 102 is L1, and the distance from the mounting point of the cargo to the rotation point of the hook 102 is L2, and L1 is greater than L2.

[0042] See also Figure 3 It can be understood that the support force of the buckle arm 103 on the hook 102 is F1, and the load pulling force of the cargo on the hook 102 is F2. According to the lever principle: F1*L1=F2*L2, under the premise of keeping F1 unchanged, by adjusting the lengths of L1 and L2, it is possible to adapt to the mounting of cargo of different weights, and the lever can be magnified by dozens of times. For example, the buckle arm 103 is moved a certain distance away from the hook 102 to increase L1, or the cargo mounting point is moved closer to the transfer point of the hook 102 to reduce L2.

[0043] See also Figures 2 to 5 In some embodiments, the snap arm 103 is rotatably connected to the shell 101, and the mounting mechanism 100 further includes a driver 202 located in the placement cavity 105, and the driver 202 is used to drive the snap arm 103 to rotate in a direction away from the hook 102 so that the hook 102 switches to the first rotation position.

[0044] See also Figures 2 to 5 Optionally, the driver 202 can be an electric push rod or an electromagnet. It can be understood that if the driver 202 is an electric push rod, the electric push rod and the hook 102 are located on the same side of the snap arm 103, and the output shaft of the electric push rod abuts against one end of the snap arm 103 and drives the snap arm 103 to rotate in a direction away from the hook 102 to disengage the snap arm 103 from the hook 102.

[0045] See also Figures 2 to 5 If the driver 202 is an electromagnet, the driver 202 and the hook 102 are respectively located on both sides of the buckle arm 103. The buckle arm 103 can be made of metal material, such as iron. Through the magnetic attraction of the electromagnet and the buckle arm 103, the buckle arm 103 is driven to rotate so that the buckle arm 103 and the hook 102 are disengaged.

[0046] See also Figure 3 In some embodiments, the distance from the position where the driver 202 drives the snap arm 103 to the transition point of the snap arm 103 is L3, and the distance from the position where the snap arm 103 abuts the hook 102 to the transition point of the snap arm 103 is L4, and L3 is greater than L4.

[0047] See also Figure 3 Optionally, the release force exerted by the driver 202 on the buckle arm 103 is F3, and the pressure exerted by the hook 102 on the buckle arm 103 is F4, wherein F1 and F4 are the action force and reaction force, which are equal in magnitude and opposite in direction. According to the lever principle, F3*L3=F4*L4, the release force required to release the goods can be calculated by this calculation formula, and a certain safety factor can be added when calculating the release force considering the actual load conditions.

[0048] See also Figure 3 According to F1*L1=F2*L2, F3*L3=F4*L4 and F1=F4, it can be concluded that F3=F2*(L2*L4) / (L1*L3). By adjusting the values ​​of L1, L2, L3, and L4, the magnification of the lever can reach dozens of times, so that it can adapt to different loads and release power sources. Please refer to the adjustment of L1 and L2 above, which will not be repeated here.

[0049] See also Figures 2 to 5 In some embodiments, the mounting mechanism 100 further includes a limit column 205 and a limit platform 204 both located in the placement cavity 105, the limit column 205 and the limit platform 204 are both connected to the shell 101, the limit column 205 is used to limit the rotation range of the hook 102 from the first rotation position to the second rotation position, and the limit platform 204 is used to limit the rotation range of the hook 102 from the second rotation position to the first rotation position.

[0050] See also Figures 2 to 5 It can be understood that the limit platform 204 is set close to the first rotation position and is located at the bottom of the cavity 105, the limit column 205 is set close to the second rotation position and is located above the limit platform 204, the hook 102 is located between the limit platform 204 and the limit column 205, and the rotation range of the hook 102 is limited by the limit platform 204 and the limit column 205 to prevent the hook 102 from rotating excessively.

[0051] See also Figures 2 to 5 In some embodiments, the mounting mechanism 100 further includes a sensing switch 203 located in the placement cavity 105 , and the sensing switch 203 is used to detect whether the hook 102 is in the first rotation position or in the second rotation position.

[0052] See also Figures 2 to 5 It can be understood that when the hook 102 rotates from the first rotation position to the second rotation position, the hook 102 compresses the spring of the sensing switch 203, so that the sensing switch 203 detects that the hook 102 is in the second rotation position, and the sensing switch 203 feedbacks that the cargo mounting is completed, and the flying transporter can start flying.

[0053] See also Figures 2 to 5 When the hook 102 switches from the second rotation position to the first rotation position, the spring of the sensor switch 203 is released, and the sensor switch 203 detects that the hook 102 is in the first rotation position. The sensor switch 203 feedbacks that the cargo unloading and throwing are completed, and the flying transporter can carry out the next flying transportation.

[0054] See also Figures 2 to 5In some embodiments, the buckle arm 103 includes a first arm segment 1031, a second arm segment 1032 and a third arm segment 1033. The two ends of the second arm segment 1032 are respectively connected to the first arm segment 1031 and the third arm segment 1033. The first arm segment 1031 is rotatably or slidably connected to the housing 101 and is provided with a buckle slot for buckling the hook 102. The second arm segment 1032 is horizontally placed between the first arm segment 1031 and the third arm segment 1033, and the driver 202 acts on the third arm segment 1033.

[0055] See also Figures 2 to 5 It can be understood that when the cargo is mounted on the mounting mechanism 100 and the flying transport has not taken off, a safety pin 107 can be set on the shell 101, and the two side surfaces of the shell 101 that are opposite to each other are provided with safety holes 106 that are connected to the placement cavity 105. The two ends of the safety pin 107 are respectively located at the two safety holes 106, and the safety pin 107 is adjacent to the third arm segment 1033 to limit the movement of the buckle arm 103 in the direction away from the hook 102, so as to prevent the hook 102 from accidentally releasing the cargo, thereby improving safety, and when the flying transport takes off, the safety pin 107 is pulled out.

[0056] Optionally, an operating hole 2061 connected to the placement cavity 105 is also opened on the shell 101, and the mounting mechanism 100 also includes a lever 206, one end of the lever 206 passes through the operating hole 2061 and is connected to the third arm segment 1033. If the mounting mechanism 100 encounters a sudden failure and cannot be released automatically, the lever 206 is manually pulled outward to manually release the cargo after the flying transporter lands.

[0057] See also Figures 2 to 5 In some embodiments, the hook 102 has a hanging slot 1021, and the hanging slot 1021 is used to hang goods. It is understandable that the rope of the goods is inserted into the hanging slot 1021. When the hook 102 is in the first rotation position, the hanging slot 1021 is tilted downward, so that the rope of the goods can slide out of the hanging slot 1021 to achieve the throwing and release of the goods; similarly, it is also convenient to load the goods, so that the rope of the goods can be easily hung in the hanging slot 1021. When the hook 102 is in the second rotation position, the hanging slot 1021 rotates upward with the hook 102, and the hanging slot 1021 is tilted upward, and the rope of the goods is limited to the area defined by the slot wall of the hanging slot 1021 and the slot wall of the avoidance slot 104, so as to avoid the failure of the mounting when the mounting mechanism 100 is vibrated.

[0058] The present invention also proposes a flying transport vehicle, which includes a mounting mechanism 100. The specific structure of the mounting mechanism 100 refers to the above-mentioned embodiment. Since the flying transport vehicle adopts all the technical solutions of all the above-mentioned embodiments, it also has all the beneficial effects brought by the technical solutions of the above-mentioned embodiments, which will not be repeated here one by one.

[0059] In some embodiments, the flying transporter also includes a drone, and the mounting mechanism 100 is connected to the drone.

[0060] See also Figures 2 to 5 Optionally, the housing 101 includes a bottom shell 111 and a top shell 112, the bottom shell 111 and the top shell 112 together form a placement cavity 105, and the buckle arm 103 and the hook 102 are both connected to the bottom shell 111. The two ends of the avoidance groove 104 pass through the bottom shell 111 and the top shell 112 respectively, and the two safety holes 106 are respectively located in the bottom shell 111 and the top shell 112.

[0061] The above are only optional embodiments of the present application and are not intended to limit the present application. For those skilled in the art, the present application may have various changes and variations. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application should be included in the scope of the claims of the present application.

Claims

1. A mounting mechanism for mounting cargo, characterized in that: The mounting mechanism includes: a shell, a snap arm and a hook, the shell having a placement cavity, the snap arm and the hook are both located in the placement cavity, the hook is rotatably connected to the shell, the snap arm is rotatably or slidably connected to the shell, the edge of the shell is provided with an avoidance groove connected to the placement cavity toward the shell, the avoidance groove is located between the transition point of the snap arm and the transition point of the hook; the hook has a first rotation position and a second rotation position, when the hook is in the first rotation position, the cargo is mounted on the hook or unloaded from the hook through the avoidance groove; when the hook is rotated to the second rotation position, the free end of the hook spans the avoidance groove and is buckled with the snap arm, and the position where the snap arm abuts against the hook moves a predetermined distance in a direction away from the hook, so that the hook switches to the first rotation position.

2. The mounting mechanism according to claim 1, characterized in that: The mounting mechanism also includes a reset member located in the placement cavity and having an elastic restoring force, one end of the reset member is connected to the shell, and the other end of the reset member abuts against the snap arm. When the hook switches from the first rotation position to the second rotation position, the hook drives the snap arm to compress the reset member, and when the hook is in the second rotation position, the reset member restricts the snap arm from disengaging from the hook.

3. The mounting mechanism according to claim 1, characterized in that: The distance from the position where the hook abuts against the buckle arm to the hook rotation point is L1, and the distance from the cargo mounting point to the hook rotation point is L2, and L1 is greater than L2.

4. The mounting mechanism according to any one of claims 1 to 3, characterized in that: The buckle arm is rotatably connected to the shell, and the mounting mechanism also includes a driver located in the placement cavity, and the driver is used to drive the buckle arm to rotate in a direction away from the hook so that the hook switches to the first rotation position.

5. The mounting mechanism according to claim 4, characterized in that: The distance from the position where the driver drives the buckle arm to the buckle arm transition point is L3, and the distance from the position where the buckle arm abuts the hook to the buckle arm transition point is L4, and L3 is greater than L4.

6. The mounting mechanism according to any one of claims 1 to 3, characterized in that: The mounting mechanism also includes a limit column and a limit platform both located in the placement cavity, the limit column and the limit platform are both connected to the shell, the limit column is used to limit the rotation range of the hook from the first rotation position to the second rotation position, and the limit platform is used to limit the rotation range of the hook from the second rotation position to the first rotation position.

7. The mounting mechanism according to any one of claims 1 to 3, characterized in that: The buckle arm includes a first arm segment, a second arm segment and a third arm segment. The two ends of the second arm segment are respectively connected to the first arm segment and the third arm segment. The first arm segment is rotatably or slidably connected to the shell and is provided with a buckle groove for buckling the hook.

8. The mounting mechanism according to any one of claims 1 to 3, characterized in that: The hook has a hanging slot, and the hanging slot is used for hanging the goods.

9. The mounting mechanism according to any one of claims 1 to 3, characterized in that: The mounting mechanism further includes an induction switch located in the placement cavity, and the induction switch is used to detect whether the hook is in the first rotation position or in the second rotation position.

10. A flying transport, characterized in that: It includes the mounting mechanism as described in any one of claims 1-9, the flying transporter also includes a drone, and the mounting mechanism is connected to the drone.

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