Unmanned aerial vehicle convenient to install rainfall catalysis bomb launcher

Abstract

The utility model provides an unmanned aerial vehicle convenient to install rainfall catalytic bomb launchers, which belongs to the technical field of launcher installation, and comprises an unmanned aerial vehicle, a pair of front wings and a pair of rear wings respectively arranged on the unmanned aerial vehicle, and catalytic bomb launchers arranged at the bottoms of the pair of front wings. A quick mounting assembly is arranged between the catalytic bomb launcher and the two wings of the unmanned aerial vehicle and comprises mounting shells arranged at the bottoms of the pair of front wings, guide grooves are formed in the bottoms of the mounting shells, U-shaped seats are arranged at one ends of the guide grooves, mounting frames are arranged in the mounting shells, and second U-shaped seats are rotationally arranged in the middles of the mounting frames. A push block is arranged on one side of the mounting frame, the cambered surface of the push block and the cambered surface of the second U-shaped seat are arranged in a sliding mode, and a limiting cylindrical block is arranged on the upper surface of the catalytic bomb launcher and located in the second U-shaped seat; according to the utility model, the use of bolts can be reduced, and meanwhile, the catalytic bomb launcher can be quickly mounted.

Description

Technical Field

[0001] The utility model relates to the technical field of launcher installation, in particular to an unmanned aerial vehicle (UAV) that is convenient for installing a rainfall catalytic missile launcher. Background Art

[0002] Artificial rainfall technology plays a crucial role in areas such as weather control, agricultural drought relief, and forest fire prevention. Unmanned aerial vehicles (UAVs), emerging meteorological platforms, are becoming a crucial tool in these operations due to their flexibility, wide coverage, and relatively low operating costs. Catalytic grenade launchers, key components of drone-based artificial rainfall operations, have a significant impact on rainfall effectiveness and efficiency, both in terms of performance and integration.

[0003] Traditional methods of installing catalytic grenade launchers often rely on bolting or welding. While these methods offer a certain degree of stability and reliability, they also present some challenges in actual use. For example, bolting requires a large number of bolts to secure the catalytic grenade launcher, consumes considerable time and manpower for installation and removal, and may not be able to respond quickly in emergency situations. Welding, on the other hand, has the drawback of being difficult to modify or upgrade once installed, and the welding process can generate stress concentration, compromising the strength and stability of the overall structure. Utility Model Content

[0004] In view of this, the present invention provides a UAV that is convenient for installing a rain catalytic grenade launcher. The present invention can reduce the use of bolts and can quickly install the catalytic grenade launcher.

[0005] In order to solve the above technical problems, the utility model provides a UAV which is convenient for installing a rain catalytic bomb launcher, including a UAV, a pair of front wings and a pair of rear wings are respectively provided on the UAV, the pair of front wings and the pair of rear wings are fixed on the UAV, the bottom of the pair of front wings are provided with catalytic bomb launchers, the catalytic bomb launchers are used to assemble the catalytic bombs, and also provide support for the catalytic bombs, a quick installation component is provided between the catalytic bomb launcher and the two wings of the UAV, the quick installation component includes a mounting shell provided at the bottom of the pair of front wings, the mounting shell is fixed to the bottom of the pair of front wings by welding or bolts, a guide groove is provided at the bottom of the mounting shell, a U-shaped seat is provided at one end of the guide groove, and a U-shaped seat is provided in the mounting shell. The invention relates to a mounting frame, wherein a U-shaped seat 2 is rotatably provided in the middle of the mounting frame, and a push block is provided on one side of the mounting frame. The arc surface of the push block is slidably provided with the arc surface of the U-shaped seat 2. A limiting cylindrical block is provided on the upper surface of the catalytic missile launcher, and the limiting cylindrical block is located inside the U-shaped seat 2; that is, the limiting cylindrical block on the upper surface of the catalytic missile launcher is aligned with the guide groove of the mounting shell. At this time, one end of the U-shaped seat 2 contacts the arc surface of the push block. As the limiting cylindrical block enters the U-shaped seat 2, the U-shaped seat 2 rotates 90 degrees clockwise in the mounting frame, so that the U-shaped seat 2 and the U-shaped seat 1 jam the limiting cylindrical block. Then, the horizontal surface of the push block touches the horizontal surface of the U-shaped seat 2, thereby preventing the U-shaped seat 2 from loosening, thereby allowing the catalytic missile launcher to be quickly installed.

[0006] The quick installation assembly also includes a pull-out rod that is arranged through the installation shell. The pull-out rod is located at one end of the installation frame. A connecting rod is rotatably arranged on one end of the upper surface of the pull-out rod. The connecting rod is located on the upper surface of the installation frame. When the pull-out rod slides, the connecting rod can be driven to slide on the installation frame; that is, the pull-out rod can drive the connecting rod to move.

[0007] The quick installation assembly also includes a push block arranged at one end of the connecting rod, and one end of the push block is fixed to one end of the connecting rod through a rotating column; that is, it can avoid the situation where the push block is stuck during the movement of the connecting rod.

[0008] The quick installation assembly also includes a limit block arranged in the installation shell. The limit block is a T-shaped structure and is fixed in the installation shell by welding. The limit block is located on one side of the push block; that is, the limit block provides a guide for the push block.

[0009] The quick installation assembly also includes spring 1 and spring 2 arranged in the installation shell. The two ends of spring 1 are respectively fixed to one end of the pull-out rod and the installation shell. Spring 2 is located in the installation frame. Spring 2 is fixed to the arc bottom of the U-shaped seat 2 and the installation shell; that is, spring 1 and spring 2 provide elastic support for the pull-out rod and the U-shaped seat 2.

[0010] A mounting frame is provided at the bottom of a pair of front wings, and the mounting frame is located on both sides of the mounting shell. A guide plate is provided at the bottom of the mounting frame, and a sliding plate is provided at the bottom of the catalytic missile launcher; that is, the guide plate facilitates supporting the bottom of the catalytic missile launcher.

[0011] Threaded holes are provided on both sides of the sliding plate, and fixing bolts are provided on both sides of the guide plate. The fixing bolts are located in the threaded holes; that is, the fixing bolts are inserted into the threaded holes, thereby further fixing the catalytic missile launcher.

[0012] In summary, compared with the prior art, this application has at least one of the following beneficial technical effects:

[0013] 1. The limiting cylindrical block on the upper surface of the catalytic missile launcher is aligned with the guide groove of the mounting shell. At this time, one end of the U-shaped seat 2 contacts the arc surface of the push block. As the limiting cylindrical block enters the U-shaped seat 2, the U-shaped seat 2 rotates 90 degrees clockwise in the mounting frame, so that the U-shaped seat 2 and the U-shaped seat 1 lock the limiting cylindrical block. Then the horizontal surface of the push block touches the horizontal surface of the U-shaped seat 2, which prevents the U-shaped seat 2 from loosening, so that the catalytic missile launcher can be quickly installed.

[0014] 2. Slide the sliding plate at the bottom of the catalytic missile launcher into the guide plate in the support frame, and then remove it into the sliding plate through the bolts on both sides of the guide plate, so that the catalytic missile launcher can be further fixed, while reducing the installation of bolts and the need for personnel to disassemble the bolts. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 This is a schematic structural diagram of a UAV that is convenient for installing a rain catalytic missile launcher according to the present invention;

[0016] Figure 2 This is a schematic structural diagram of the front wing of the present invention;

[0017] Figure 3 This is a schematic structural diagram of the catalytic bomb launcher of the utility model;

[0018] Figure 4 This is a schematic diagram of the structure of the installation shell of the utility model;

[0019] Figure 5 This is a structural diagram of the quick installation component of the utility model.

[0020] Description of reference numerals:

[0021] 100. UAV; 101. Rear wing; 102. Front wing; 103. Catalytic missile launcher; 104. Mounting frame; 105. Guide plate; 106. Fixing bolt; 107. Limiting cylindrical block; 108. Sliding plate;

[0022] 200, quick installation assembly; 201, guide groove; 202, U-shaped seat 1; 203, mounting shell; 204, pull rod; 205, mounting frame; 206, limit block; 207, connecting rod; 208, spring 1; 209, push block; 210, U-shaped seat 2; 211, spring 2; DETAILED DESCRIPTION

[0023] In order to make the purpose, technical solutions and advantages of the embodiment of the present invention clearer, the following will be combined with the appended drawings of the embodiment of the present invention. Figure 1-4 , clearly and completely describing the technical solutions of the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of them. Based on the described embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field fall within the scope of protection of the present invention.

[0024] like Figure 1-4 As shown: This embodiment provides a drone that is easy to install a rain catalytic bomb launcher, including a drone 100. The drone 100 and the drone 100 are respectively provided with a pair of front wings 102 and a pair of rear wings 101 for providing flight stability and maneuverability. Catalytic bomb launchers 103 are provided at the bottom of the pair of front wings 102. At the same time, the catalytic bomb launchers 103 are used to launch rain catalytic bombs to promote rainfall. A quick installation component 200 is provided between the catalytic bomb launchers 103 and the two wings of the drone 100. The quick installation component 200 includes a mounting shell 203 provided at the bottom of the pair of front wings 102. The mounting shell 203 is provided at the bottom of the front wings 102 to provide a mounting base for the catalytic bomb launcher 103. A guide groove 201 is provided on the mounting shell 203. A U-shaped seat 202 is provided at one end of the guide groove 201 for guiding the installation of the catalytic bomb launcher 103. A mounting frame 200 is provided in the mounting shell 203. 5. The mounting frame 205 is fixed in the mounting shell 203 by welding. A second U-shaped seat 210 is rotatably provided in the middle of the mounting frame 205. The second U-shaped seat 210 is rotatably provided in the middle of the mounting frame 205 and is used to cooperate with the limiting cylindrical block 107 on the catalytic missile launcher 103 to achieve a stable connection. A push block 209 is provided on one side of the mounting frame 205. The arc surface of the push block 209 slides with the arc surface of the second U-shaped seat 210. By pushing the push block 209, the push block 209 is pushed. The horizontal surface of the 9 contacts the horizontal surface of the second U-shaped seat 210, thereby locking or releasing the catalytic missile launcher 103. A limiting cylindrical block 107 is provided on the upper surface of the catalytic missile launcher 103. The limiting cylindrical block 107 is fixed to the catalytic missile launcher 103 by welding. The limiting cylindrical block 107 is located inside the second U-shaped seat 210. The limiting cylindrical block 107 cooperates with the second U-shaped seat 210 to ensure the stability and safety of the catalytic missile launcher 103 after installation.

[0025] Align the catalytic missile launcher 103 with the guide groove 201 and slide it along the guide groove 201. At this time, one end of the U-shaped seat 210 contacts the arc surface of the push block 209 until the limiting cylindrical block 107 enters the range of the U-shaped seat 210. Then, as the limiting cylindrical block 107 moves forward, the U-shaped seat 210 rotates 90 degrees. At this time, the U-shaped seat 210 and the U-shaped seat 1 202 are staggered and tightly hold the limiting cylindrical block 107, so that the horizontal surface of the push block 209 contacts the horizontal surface of the U-shaped seat 210, thereby achieving a stable connection between the catalytic missile launcher 103 and the drone 100, so that the catalytic missile launcher 103 can be quickly installed.

[0026] During disassembly, the push block 209 is moved away from the U-shaped seat 210, so that the U-shaped seat 210 begins to rotate and the U-shaped seat 210 is in a vertical state, thereby facilitating the removal of the catalytic missile launcher 103, and then the arc surface of the push block 209 is brought into contact with the U-shaped seat 210.

[0027] Quick installation assembly 200 Figure 5 As shown,

[0028] The quick installation assembly 200 further includes a pull rod 204 extending through the installation housing 203. The pull rod 204 is located at one end of the installation frame 205. A connecting rod 207 is rotatably provided on one end of the upper surface of the pull rod 204. The connecting rod 207 is located on the upper surface of the installation frame 205. The pull rod 204 facilitates a person to pull the pull rod 204, thereby driving the connecting rod 207 to rotate.

[0029] The quick installation assembly 200 further includes a push block 209 provided at one end of the connecting rod 207. One end of the push block 209 is fixed to one end of the connecting rod 207 via a rotating column. The push block 209 is installed on the connecting rod 207, so that the connecting rod 207 can drive the push block to move, thereby driving the push block 209.

[0030] The quick installation assembly 200 further includes a limit block 206 disposed within the installation housing 203. The limit block 206 is fixed within the installation housing 203 by welding, thereby guiding the push block 209. The limit block 206 is located on one side of the push block 209.

[0031] The quick installation assembly 200 also includes a first spring 208 and a second spring 211 disposed within the mounting housing 203. The two ends of the first spring 208 are respectively fixed to one end of the pull rod 204 and the mounting housing 203, thereby providing elasticity for the pull rod 204. The second spring 211 is located within the mounting frame 205. The second spring 211 is fixed to the curved bottom of the second U-shaped seat 210 and the mounting housing 203, thereby fixing one end of the second spring 211 to the bottom of the rotation point of the second U-shaped seat 210. Therefore, when there is no limit of the push block 209, the second U-shaped seat 210 rotates as the spring contracts.

[0032] The pull rod 204 can be pulled in the installation frame 205, so that the pull rod 204 can stretch the spring, and the connecting rod 207 will rotate accordingly. The connecting rod 207 is located on the upper surface of the installation frame 205. Through its rotation, it can indirectly drive the push block 209 to move, and indirectly release the limit on the U-shaped seat 210.

[0033] Front wing 102 Figure 2 As shown,

[0034] A mounting frame 104 is provided at the bottom of the pair of front wings 102. The mounting frame 104 is located on both sides of the mounting shell 203 and is fixed to the front wings 102 by bolts. A guide plate 105 is provided at the bottom of the mounting frame 104. A sliding plate 108 is provided at the bottom of the catalytic missile launcher 103. The guide plate 105 is fixed to the mounting frame 104 by welding, so that the sliding plate 108 at the bottom of the catalytic missile launcher 103 can be easily inserted into the guide plate 105, so that the sliding plate 108 supports the catalytic missile launcher 103.

[0035] Sliding plate 108 Figure 2 As shown,

[0036] Threaded holes are provided on both sides of the sliding plate 108, and fixing bolts 106 are provided on both sides of the guide plate 105. The fixing bolts 106 are located in the threaded holes, so that the fixing bolts 106 are inserted into the sliding plate 108, thereby further fixing the guide plate 105;

[0037] Furthermore, it should be noted that, in the description of this utility model, unless otherwise expressly specified or limited, the terms "installed," "connected," and "connected" should be understood in a broad sense. For example, they can refer to fixed connections, detachable connections, or integral connections; mechanical connections, electrical connections; direct connections, indirect connections through an intermediate medium, and internal connections between two components. Those skilled in the art will understand the specific meanings of the above terms in this utility model based on specific circumstances.

[0038] The above is a preferred embodiment of the present invention. It should be pointed out that for ordinary technicians in this technical field, several improvements and modifications can be made without departing from the principles described in the present invention. These improvements and modifications should also be regarded as the scope of protection of the present invention.

Claims

1. A UAV that is convenient for installing a rain catalytic missile launcher, characterized by: The invention comprises an unmanned aerial vehicle (100), wherein the unmanned aerial vehicle (100) and the unmanned aerial vehicle (100) are respectively provided with a pair of front wings (102) and a pair of rear wings (101), the bottom of each of the pair of front wings (102) is provided with a catalytic missile launcher (103), a quick installation component (200) is provided between the catalytic missile launcher (103) and the two wings of the unmanned aerial vehicle (100), the quick installation component (200) comprises a mounting shell (203) provided at the bottom of the pair of front wings (102), a guide is provided at the bottom of the mounting shell (203), and a guide is provided at the bottom of the mounting shell (203). A guide groove (201) is provided at one end of the guide groove (201) with a U-shaped seat 1 (202), a mounting frame (205) is provided in the mounting shell (203), a U-shaped seat 2 (210) is rotatably provided in the middle of the mounting frame (205), a push block (209) is provided on one side of the mounting frame (205), the arc surface of the push block (209) is slidably provided with the arc surface of the U-shaped seat 2 (210), a limiting cylindrical block (107) is provided on the upper surface of the catalytic missile launcher (103), and the limiting cylindrical block (107) is located inside the U-shaped seat 2 (210).

2. The UAV that is convenient for installing a rain catalytic missile launcher according to claim 1, characterized in that: The quick installation assembly (200) further includes a pull-out rod (204) disposed in the installation shell (203), the pull-out rod (204) being located at one end of the installation frame (205), and a connecting rod (207) being rotatably disposed on one end of the upper surface of the pull-out rod (204), the connecting rod (207) being located on the upper surface of the installation frame (205).

3. The UAV that is convenient for installing a rain catalytic missile launcher according to claim 2, characterized in that: The quick installation assembly (200) further comprises a push block (209) which is provided through one end of the connecting rod (207), and one end of the push block (209) is fixed to one end of the connecting rod (207) via a rotating column.

4. The UAV that is convenient for installing a rain catalytic missile launcher according to claim 3, characterized in that: The quick installation assembly (200) further comprises a limit block (206) arranged in the installation shell (203), and the limit block (206) is located on one side of the push block (209).

5. The UAV that is convenient for installing a rain catalytic missile launcher according to claim 4, characterized in that: The quick installation assembly (200) also includes a spring 1 (208) and a spring 2 (211) arranged in the installation shell (203), the two ends of the spring 1 (208) are respectively fixed to one end of the pull rod (204) and the installation shell (203), the spring 2 (211) is located in the installation frame (205), and the spring 2 (211) is fixed to the arc bottom of the U-shaped seat 2 (210) and the installation shell (203).

6. The UAV that is convenient for installing a rain catalytic missile launcher according to claim 1, characterized in that: A mounting frame (104) is provided at the bottom of a pair of front wings (102), and the mounting frame (104) is located on both sides of the mounting shell (203). A guide plate (105) is provided at the bottom of the mounting frame (104), and a sliding plate (108) is provided at the bottom of the catalytic missile launcher (103).

7. The UAV that is convenient for installing a rain catalytic missile launcher according to claim 6, characterized in that: Threaded holes are provided on both sides of the sliding plate (108), and fixing bolts (106) are provided on both sides of the guide plate (105), and the fixing bolts (106) are located in the threaded holes.

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