Hanging device for unmanned aerial vehicle

Abstract

The utility model discloses a mounting device for an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicle mounting devices, the mounting device for the unmanned aerial vehicle comprises a vehicle body mechanism, and screw holes are formed in the four corners of the bottom end face of the vehicle body mechanism. And the sliding block assembly slides in the longitudinal groove, so that the insertion block mechanism can be quickly mounted and dismounted. Meanwhile, a guide assembly, a servo push rod, a clamping plate assembly, a convex block assembly and an anti-skid assembly at the bottom end of the insertion block mechanism work cooperatively, the hung objects can be accurately positioned and stably clamped, the problems that a hanging device is complex in connection and the objects are not stably lifted are effectively solved, the efficiency and safety of hanging and transporting the objects are improved, and the practicability is high. And through the four cover body assemblies on the outer side of the machine body mechanism, the inner assemblies of the machine body mechanism can be protected from being influenced by external collision, dust and other factors.

Description

Technical Field

[0001] This utility model relates to the technical field of drone mounting devices, specifically a mounting device for drones. Background Technology

[0002] Unmanned aerial vehicles (UAVs), or drones for short, are unmanned aircraft controlled by radio remote control equipment and onboard program control devices, or operated autonomously, either completely or intermittently, by an onboard computer. A current patent describes a drone mounting device (patent publication number CN222291992U), which includes a mounting device body mounted on the bottom of the drone body. The mounting device body includes a suspension release assembly, and a micro-motor on the suspension release assembly is powered by a power supply. The micro-motor is electrically connected to a control board, and both the control board and the power supply are installed inside the drone body. The bottom of the micro-motor is mounted on a fixed frame. When the drone reaches the desired delivery location, the micro-motor is activated via a remote control. The mounting rod is driven by the micro-motor, a turntable, and a transmission rod to move. The mounting rod has a horizontal, lateral movement structure, causing it to retract into a limiting hole, releasing the suspended item. The entire mounting device is compact, simple in structure, and lightweight, minimizing the load on the drone body and increasing its range.

[0003] Regarding the aforementioned technologies, the inventors believe that the following defects exist: When using existing drone mounting devices, the lack of an effective quick-disassembly structure makes the process of connecting the drone body and the mounting device relatively complicated, which can easily affect the lifting effect and stability of subsequent items. Therefore, we propose a drone mounting device to solve the above-mentioned problems. Utility Model Content

[0004] To address the shortcomings of existing technologies, this utility model provides a mounting device for drones, which solves the problem that existing drone mounting devices lack an effective quick-disassembly structure, making the connection process between the drone body and the mounting device complex and potentially affecting the lifting effect and stability of subsequent items.

[0005] To achieve the above objectives, this utility model is implemented through the following technical solution: a mounting device for a drone, comprising a body structure, wherein screw holes are provided at the four corners of the bottom end face of the body structure, and a mounting mechanism is installed at the bottom end of the body structure, wherein mounting holes are provided at the four corners of the interior of the mounting mechanism, and fixing bolts are installed inside the mounting holes and installed below the body structure through the fixing bolts;

[0006] A guide frame assembly is fixedly connected to the bottom surface of the mounting mechanism. The guide frame assembly has a longitudinal groove inside. There are two guide frame assemblies, arranged in a linear array and fixedly connected to the bottom surface of the mounting mechanism. An insert block mechanism is inserted into the longitudinal groove at the bottom of the guide frame assembly. The main body of the insert block mechanism is a rectangular block structure. Two opposing slider assemblies are fixedly connected to the outer side of each insert block mechanism. The insert block mechanism is inserted into the guide frame assembly through the slider assemblies fixedly connected to its outer side. A connecting rod is fixedly connected to the outer side of each insert block mechanism. The connecting rod is a lead screw structure, and a nut assembly for limiting the insert block mechanism is screwed onto the outer side of the connecting rod. Two guide assemblies are fixedly connected in a linear array on the bottom surface of each insert block mechanism. Two servo push rods are fixedly connected in opposing directions inside the guide assemblies. A clamping plate assembly is installed on the output end of the servo push rod. Two protrusion assemblies are fixedly connected in opposing directions to the outer side of the clamping plate assembly. Two anti-slip components are fixedly connected in a linear array to the inner side of the clamping plate assembly.

[0007] Preferably, a cover assembly is fixedly connected to the outside of the body mechanism, and the cover assembly has four locations.

[0008] Preferably, the four cover components are fixedly connected to the four corners of the outer side of the body structure.

[0009] Preferably, a support plate is fixedly connected to the inner side of the cover assembly, and the support plate and the cover assembly together form a support structure for the servo motor.

[0010] Preferably, the servo motor is installed inside the support plate, and an output shaft is provided at the top of the servo motor.

[0011] Preferably, a fan blade unit is installed on the top output shaft of the servo motor.

[0012] Preferably, the servo motor and the fan blade unit together form a drive lifting structure for the machine body mechanism.

[0013] Beneficial effects

[0014] This invention provides a mounting device for unmanned aerial vehicles (UAVs). Compared with the prior art, it has the following advantages:

[0015] This mounting device for drones, through the cooperation of the insertion block mechanism and the guide frame assembly, utilizes the sliding of the slider assembly within the longitudinal groove to achieve rapid installation and disassembly of the insertion block mechanism. Simultaneously, the guide assembly, servo push rod, clamping plate assembly, protrusion assembly, and anti-slip assembly at the bottom of the insertion block mechanism work together to accurately position and stably clamp the mounted items, effectively solving the problems of complex connection of the mounting device and unstable lifting of items, thus improving the efficiency and safety of mounting and transporting items.

[0016] This mounting device for drones, through four protective enclosure components on the outside of the fuselage, not only protects the internal components from external impacts, dust, and other factors, extending the device's lifespan, but also optimizes the device's appearance and structure. The four enclosure components are fixed at the four corners of the fuselage, evenly distributing the protective force and enhancing the overall protection of the fuselage, thus improving the device's stability and reliability. This is an innovative design for the protective structure of traditional drone mounting devices. Attached Figure Description

[0017] Figure 1 This is a schematic diagram of the disassembled front side view of the mounting device of this utility model;

[0018] Figure 2 This is a side view of the mounting device of this utility model.

[0019] Figure 3 This is a schematic diagram of the mounting mechanism and mounting hole combination structure of the mounting device of this utility model;

[0020] Figure 4 This is a schematic diagram of the left side of the mounting device of this utility model;

[0021] Figure 5 This is a schematic diagram of the combined structure of the insertion block mechanism and the slider assembly of the mounting device of this utility model;

[0022] Figure 6 This is a front view structural diagram of the mounting device of this utility model.

[0023] In the diagram: 1. Body structure; 101. Cover assembly; 1011. Support plate; 1012. Servo motor; 1013. Fan blade unit; 2. Mounting mechanism; 201. Mounting hole; 2011. Fixing bolt; 2012. Guide frame assembly; 3. Insertion block mechanism; 301. Slider assembly; 3011. Connecting rod; 3012. Nut assembly; 3013. Guide assembly; 3014. Servo push rod; 3015. Clamping plate assembly; 3016. Protrusion assembly; 3017. Anti-slip assembly. Detailed Implementation

[0024] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0025] Please see Figure 1 - Figure 6This utility model provides a technical solution: a mounting device for a drone, including a body mechanism 1, with screw holes at the four corners of the bottom end face of the body mechanism 1, and a mounting mechanism 2 installed at the bottom end of the body mechanism 1. The mounting mechanism 2 has mounting holes 201 at the four corners of its interior, and fixing bolts 2011 are installed inside the mounting holes 201 and are installed below the body mechanism 1 through the fixing bolts 2011.

[0026] A guide frame assembly 2012 is fixedly connected to the bottom surface of the mounting mechanism 2. The guide frame assembly 2012 has a longitudinal groove inside. There are two guide frame assemblies 2012, which are fixedly connected to the bottom surface of the mounting mechanism 2 in a linear array. An insert block mechanism 3 is inserted into the longitudinal groove at the bottom of the guide frame assembly 2012. The main body of the insert block mechanism 3 is a rectangular block structure. Two opposing slider assemblies 301 are fixedly connected to the outer side of each insert block mechanism 3. The insert block mechanism 3 is inserted into the guide frame assembly 2012 through the slider assemblies 301 fixedly connected to its outer side. Each is fixedly connected with a connecting rod 3011, which is a lead screw structure. A nut assembly 3012 for limiting the insertion block mechanism 3 is screwed onto the outside of the connecting rod 3011. Two guide assemblies 3013 are fixedly connected in a linear array on the bottom end face of the two insertion block mechanisms 3. Two servo push rods 3014 are fixedly connected in opposite directions inside the guide assembly 3013. A clamping plate assembly 3015 is installed on the output end of the servo push rod 3014. Two protrusion assemblies 3016 are fixedly connected in opposite directions on the outside of the clamping plate assembly 3015. Two anti-slip components 3017 are fixedly connected in a linear array on the inside of the clamping plate assembly 3015.

[0027] The insertion block mechanism 3 slides within the longitudinal groove of the guide frame assembly 2012 via the slider assembly 301. It is limited by the connecting rod 3011 and the nut assembly 3012. The guide assembly 3013, servo push rod 3014, clamping plate assembly 3015, protrusion assembly 3016 and anti-slip assembly 3017 at the bottom of the insertion block mechanism 3 cooperate with each other to achieve rapid installation, disassembly and stable clamping of the mounted items. This solves the problem of complex connection process of the mounting device, which affects the lifting effect and stability of the items.

[0028] See Figure 1 , Figure 5 The outer side of the body mechanism 1 is fixedly connected to the cover assembly 101, which has four locations.

[0029] The four cover components 101 fixed to the outside of the body structure 1 can protect the body structure 1, reduce the impact of external factors on the internal components of the body structure 1, and also optimize the appearance structure of the device to a certain extent.

[0030] SeeFigure 3 , Figure 4 The four cover components 101 are respectively fixedly connected to the four corners of the outer side of the body mechanism 1;

[0031] By fixing the four cover components 101 to the four corners of the outer side of the body structure 1, this layout can distribute the protective force more evenly, enhance the overall protection of the body structure 1, and improve the stability and reliability of the device.

[0032] See Figure 2 , Figure 5 A support plate 1011 is fixedly connected to the inner side of the cover assembly 101. The support plate 1011 and the cover assembly 101 together form a support structure for the servo motor 1012.

[0033] The servo motor 1012 is supported by the support plate 1011 inside the cover assembly 101 together with the cover assembly 101, providing a stable mounting base for the servo motor 1012, ensuring that the servo motor 1012 remains stable during operation, thereby ensuring its driving effect and the normal operation of the device.

[0034] See Figure 1 , Figure 2 The servo motor 1012 is installed inside the support plate 1011, and the top of the servo motor 1012 is provided with an output shaft;

[0035] The servo motor 1012 is installed inside the support plate 1011, and its top output shaft provides a connection base for the subsequent installation of the fan blade unit 1013, ensuring the stability and accuracy of the power output of the servo motor 1012.

[0036] See Figure 3 , Figure 6 A fan blade unit 1013 is mounted on the top output shaft of the servo motor 1012;

[0037] The fan blade unit 1013, mounted on the top output shaft of the servo motor 1012, rotates under the drive of the servo motor 1012, generating upward lift. Together with the servo motor 1012, it forms a drive lifting structure to provide power support for the flight of the UAV.

[0038] See Figure 1 , Figure 2 The servo motor 1012 and the fan blade unit 1013 together form the driving lifting structure for the body mechanism 1.

[0039] The lifting structure, consisting of a servo motor 1012 and a fan blade unit 1013, generates lift through the rotation of the fan blade unit 1013, thereby enabling the lifting motion of the body mechanism 1 to meet the power requirements of the UAV flight and ensure that the UAV can fly stably.

[0040] During operation, the mounting mechanism 2 is first installed onto the body mechanism 1. The screw holes at the four corners of the bottom end face of the body mechanism 1 correspond to the mounting holes 201 at the four corners inside the mounting mechanism 2. The fixing bolt 2011 is passed through the mounting hole 201 and screwed into the screw hole of the body mechanism 1, thereby securely installing the mounting mechanism 2 under the body mechanism 1.

[0041] The guide frame assembly 2012, which is fixedly connected to the bottom surface of the mounting mechanism 2, has two longitudinal slots inside, arranged in a straight array. The main body of the insertion block mechanism 3 is a rectangular block structure. Two slider assemblies 301 are fixedly connected to the outside of each insertion block mechanism 3 and are inserted into the longitudinal slots at the bottom of the guide frame assembly 2012, so that the insertion block mechanism 3 can slide within the guide frame assembly 2012. The connecting rods 3011, which are fixedly connected to the outside of both insertion block mechanisms 3, are screw rod structures. After the insertion block mechanism 3 is adjusted to a suitable position, the nut assembly 3012 is screwed onto the outside of the connecting rod 3011 to limit the insertion block mechanism 3, prevent it from sliding randomly, and ensure the stability of the installation of the insertion block mechanism 3.

[0042] When an item needs to be hung, the guide assembly 3013, which is fixedly connected in a linear array on the bottom end face of the two insertion block mechanisms 3, comes into play. The two servo push rods 3014, which are fixedly connected in opposite directions inside the guide assembly 3013, are activated, pushing the clamping plate assembly 3015 installed at its output end to move. The protrusion assembly 3016 on the outer side of the clamping plate assembly 3015 facilitates cooperation with the specific structure of the item to be hung, so as to achieve precise positioning. The two anti-slip components 3017, which are fixedly connected in a linear array inside the clamping plate assembly 3015, increase the friction between the clamping plate assembly 3015 and the item to be hung, preventing the item from slipping. By controlling the extension and retraction of the servo push rods 3014, the clamping plate assembly 3015 is driven to clamp or release the item to complete the hanging or unloading operation.

[0043] The cover assembly 101 is fixedly connected to the four corners of the outer side of the body mechanism 1. The support plate 1011 fixedly connected to the inner side of the cover assembly 101 together supports the servo motor 1012. The servo motor 1012 is installed inside the support plate 1011. The fan blade unit 1013 is installed on the top output shaft of the servo motor 1012. When the servo motor 1012 is started, it drives the fan blade unit 1013 to rotate. The rotation of the fan blade unit 1013 generates upward lift, which together with the servo motor 1012 forms a driving lifting structure to provide the body mechanism 1 with the power to rise or fall, so as to realize the flight movement of the UAV.

[0044] In summary, the device can protect the fan blade unit 1013 by providing the cover assembly 101.

[0045] Furthermore, any content not described in detail in this specification is existing technology known to those skilled in the art.

Claims

1. A mounting device for an unmanned aerial vehicle (UAV), comprising a body structure (1), characterized in that: The bottom end face of the body mechanism (1) is provided with screw holes at the four corners. The bottom end of the body mechanism (1) is provided with an installation mechanism (2). The four corners of the installation mechanism (2) are provided with installation holes (201). Fixing bolts (2011) are installed inside the installation holes (201) and installed below the body mechanism (1) through fixing bolts (2011). A guide frame assembly (2012) is fixedly connected to the bottom end face of the mounting mechanism (2). The guide frame assembly (2012) has a longitudinal groove inside. There are two guide frame assemblies (2012). The two guide frame assemblies (2012) are fixedly connected to the bottom end face of the mounting mechanism (2) in a linear array. An insert block mechanism (3) is inserted into the longitudinal groove at the bottom end of the guide frame assembly (2012). The main body of the insert block mechanism (3) is a rectangular block structure. Two slider assemblies (301) with protruding structures are fixedly connected to the outside of each insert block mechanism (3) in opposite directions. The insert block mechanism (3) is inserted into the guide frame assembly (2012) through the slider assemblies (301) fixedly connected to its outside. The two insert block mechanisms (3) are fixedly connected to the bottom end face of the guide frame assembly (2012) in a linear array. A connecting rod (3011) is fixedly connected to each side. The connecting rod (3011) is a screw rod structure. A nut assembly (3012) for limiting the insertion block mechanism (3) is screwed onto the outside of the connecting rod (3011). Two guide assemblies (3013) are fixedly connected in a linear array on the bottom surface of the two insertion block mechanisms (3). Two servo push rods (3014) are fixedly connected in opposite directions inside the guide assembly (3013). A clamping plate assembly (3015) is installed on the output end of the servo push rod (3014). Two protrusion assemblies (3016) are fixedly connected in opposite directions on the outside of the clamping plate assembly (3015). Two anti-slip assemblies (3017) are fixedly connected in a linear array on the inside of the clamping plate assembly (3015).

2. The mounting device for a drone according to claim 1, characterized in that: The outer side of the body mechanism (1) is fixedly connected to a cover assembly (101), and the cover assembly (101) has four locations.

3. A mounting device for a drone according to claim 2, characterized in that: The four cover components (101) are respectively fixedly connected to the four corners of the outer side of the body mechanism (1).

4. A mounting device for an unmanned aerial vehicle according to claim 3, characterized in that: A support plate (1011) is fixedly connected to the inner side of the cover assembly (101). The support plate (1011) and the cover assembly (101) together form a support structure for the servo motor (1012).

5. A mounting device for an unmanned aerial vehicle according to claim 4, characterized in that: The servo motor (1012) is installed inside the support plate (1011), and an output shaft is provided at the top of the servo motor (1012).

6. A mounting device for an unmanned aerial vehicle according to claim 5, characterized in that: A fan blade unit (1013) is mounted on the top output shaft of the servo motor (1012).

7. A mounting device for an unmanned aerial vehicle according to claim 6, characterized in that: The servo motor (1012) and the fan blade unit (1013) together form the driving and lifting structure for the body mechanism (1).

Images