Aircraft pod mounting structure

Abstract

The utility model provides an aircraft pod mounting structure which comprises an aircraft body, one side of the aircraft body is fixedly connected with a take-off and landing leg, the bottom of the aircraft body is fixedly connected with a sliding rail, a photoelectric pod is arranged below the aircraft body, the top of the photoelectric pod is fixedly connected with a T-shaped sliding block, and a limiting mechanism is arranged in the T-shaped sliding block. The limiting mechanism is used for fixing the photoelectric pod and comprises a positioning rod connected to the inner wall of the T-shaped sliding block in a sliding mode, and one end of the positioning rod is fixedly connected with a connecting block. The aircraft pod mounting structure provided by the utility model solves the problems that some existing aircraft pod mounting structures adopt screws to connect and fix a photoelectric pod and an aircraft, the screws are easy to rust in the later period, so that the stress of the screws is weakened, the strength is reduced, and the photoelectric pod cannot be disassembled every time when the photoelectric pod is assembled and disassembled. Tools are needed, and the effect of quick disassembly and assembly cannot be achieved.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft, in particular to an aircraft pod mounting structure. Background Art

[0002] Aircraft (UAV) are manufactured by humans, can fly off the ground and in space, and are controlled by humans. They are flying objects in the atmosphere. Through the use of aircraft, humans have enjoyed many conveniences. At present, aircraft usually have to carry various pods to meet mission requirements.

[0003] According to the utility model patent with authorization announcement number: CN204937521U, a photoelectric pod mounting structure used in power inspection is disclosed, which involves the field of helicopter / UAV power line inspection. Its beneficial effects are: to ensure the stability of the photoelectric pod mounting during flight, the connection method between the large photoelectric pod and the aircraft platform should include four mounting holes, and the mounting hole screw requirements are: M8 hexagon socket head screws, M8 self-locking nuts or M8I-type hexagon nuts, Φ8 flat washers and Φ8 spring washers.

[0004] The above technology connects and fixes the optoelectronic pod to the aircraft through multiple screws. However, the screws are prone to rust, which weakens the force and reduces the strength. Therefore, the connection ability will also deteriorate, and it is easy to loosen or break. At the same time, tools are required every time the optoelectronic pod is disassembled and assembled, so personnel need to carry tools with them, and the effect of quick disassembly and assembly cannot be achieved.

[0005] Therefore, it is necessary to provide a new aircraft pod mounting structure to solve the above technical problems. Utility Model Content

[0006] The purpose of the utility model is to provide an aircraft pod mounting structure to solve the problems raised in the above background technology.

[0007] The utility model provides an aircraft pod mounting structure, comprising a body, one side of the body is fixedly connected to a take-off and landing leg, the bottom of the body is fixedly connected to a slide rail, a photoelectric pod is arranged below the body, the top of the photoelectric pod is fixedly connected to a T-shaped slider, a limiting mechanism is arranged inside the T-shaped slider, and the limiting mechanism is used to fix the photoelectric pod.

[0008] In order to achieve the effect of fixing the optoelectronic pod to the fuselage, the utility model provides an aircraft pod mounting structure, preferably, the limiting mechanism includes a positioning rod slidably connected to the inner wall of the T-shaped slider, one end of the positioning rod is fixedly connected to a connecting block, one side of the connecting block is fixedly connected to a spring, the other side of the connecting block is fixedly connected to a paddle, and a positioning hole is opened on the inner wall of the slide rail.

[0009] In order to achieve the effect of stable movement of the connecting block, the utility model provides an aircraft pod mounting structure, preferably, the bottom of the connecting block is fixedly connected to a limiting block, the inner wall of the T-shaped slider is provided with a limiting groove, and the limiting block is slidably connected to the limiting groove.

[0010] In order to achieve a good fixing effect on the T-shaped slider and the slide rail, the utility model provides an aircraft pod mounting structure, preferably, the positioning rod is snap-fitted with the positioning hole, and one end of the positioning rod passes through the positioning hole.

[0011] In order to achieve the effect of enabling the T-shaped slider to be installed in the slide rail, the utility model provides an aircraft pod mounting structure, preferably, the inner wall of the slide rail is provided with a T-shaped slide groove used in conjunction with the T-shaped slider.

[0012] Compared with the prior art, the beneficial effects of the utility model are:

[0013] The aircraft pod mounting structure installs a T-shaped slider into a T-shaped slide groove, and fixes the optoelectronic pod to the aircraft body under the action of a limiting mechanism, which is convenient and quick to disassemble later, replacing the screw fixing method, and no tools are required during the disassembly and assembly process. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 A structural schematic diagram of a preferred embodiment of an aircraft pod mounting structure provided by the utility model;

[0015] Figure 2 This is a schematic diagram of the structure of the slide rail and the T-block in the utility model;

[0016] Figure 3 for Figure 2 A schematic diagram of the enlarged structure at point A in the middle.

[0017] Numbers in the figure: 1, fuselage; 2, take-off and landing legs; 3, slide rail; 4, optoelectronic pod; 5, T-shaped slider; 6, limit mechanism; 61, positioning rod; 62, connecting block; 63, spring; 64, paddle; 65, positioning hole; 7, limit block; 8, limit groove. DETAILED DESCRIPTION

[0018] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments of the utility model, all other embodiments obtained by ordinary technicians in this field without making creative work belong to the protection scope of the utility model. It is understandable that the drawings are only provided for reference and illustration, and are not used to limit the utility model. The connection relationship shown in the drawings is only for the convenience of clear description and does not limit the connection method.

[0019] Please refer to Figure 1 , Figure 2 and Figure 3 ,in, Figure 1 A structural schematic diagram of a preferred embodiment of an aircraft pod mounting structure provided by the utility model; Figure 2 This is a schematic diagram of the structure of the slide rail and the T-block in the utility model; Figure 3 for Figure 2 A schematic diagram of the structure at A in the middle is an enlarged view. An aircraft pod mounting structure includes a body 1, a take-off and landing leg 2 is fixedly connected to one side of the body 1, a slide rail 3 is fixedly connected to the bottom of the body 1, an optoelectronic pod 4 is arranged below the body 1, a T-shaped slider 5 is fixedly connected to the top of the optoelectronic pod 4, and a limiting mechanism 6 is arranged inside the T-shaped slider 5, and the limiting mechanism 6 is used to fix the optoelectronic pod 4.

[0020] It should be noted that: when installing the photoelectric pod 4, the photoelectric pod 4 is moved to install the T-shaped slider 5 into the slide rail 3. The T-shaped slider 5 and the slide rail 3 are used to facilitate the installation of the photoelectric pod 4. Then, the T-shaped slider 5 can be fixed in the slide rail 3 through the limiting mechanism 6, thereby fixing the photoelectric pod 4 to the body 1. The disassembly and assembly is quick and convenient, replacing the screw fixing method, and no tools are required during the disassembly and assembly process.

[0021] In the specific implementation process, Figure 1 , Figure 2 and Figure 3 As shown, the limiting mechanism 6 includes a positioning rod 61 slidably connected to the inner wall of the T-shaped slider 5, one end of the positioning rod 61 is fixedly connected to a connecting block 62, one side of the connecting block 62 is fixedly connected to a spring 63, the other side of the connecting block 62 is fixedly connected to a paddle 64, and a positioning hole 65 is opened on the inner wall of the slide rail 3.

[0022] refer to Figure 1 , Figure 2 and Figure 3 As shown, the bottom of the connecting block 62 is fixedly connected with a limiting block 7, the inner wall of the T-shaped sliding block 5 is provided with a limiting groove 8, the limiting block 7 is slidably connected with the limiting groove 8, and the number of the limiting blocks 7 is two.

[0023] refer to Figure 1 , Figure 2 and Figure 3 As shown, the positioning rod 61 is engaged with the positioning hole 65 , and one end of the positioning rod 61 passes through the positioning hole 65 .

[0024] refer to Figure 1 , Figure 2 and Figure 3 The inner wall of the slide rail 3 is provided with a T-shaped slide groove for use with the T-shaped slide block 5.

[0025] It should be noted that: the T-shaped slider 5 is installed into the T-shaped slot in the slide rail 3, and then the photoelectric pod 4 is moved to make the T-shaped slider 5 move along the T-shaped slot. When one end of the T-shaped slider 5 is about to completely enter the T-shaped slot, it stops moving, and the paddle 64 is moved to make the two connecting blocks 62 approach each other and drive the positioning rod 61 and the limit block 7 to move, and the positioning rod 61 is retracted into the T-shaped slider 5. At this time, the spring 63 is in a compressed state, and when the limit block 7 moves through the limit groove 8, the stability of the connecting block 62 during movement can be improved. Then the T-shaped slider 5 is completely moved into the T-shaped slot. At this time, the positioning rod 61 is level with the positioning hole 65, and then the paddle 64 is released. The resilience of the spring 63 can make the connecting block 62 drive the positioning rod 61 to automatically reset, and the positioning rod 61 is inserted into and passes through the positioning hole 65, thereby completing the connection and fixation of the photoelectric pod 4 and the body 1. The photoelectric pod 4 can be disassembled from the body 1 by reverse operation. The operation is convenient and no tools are required during the entire disassembly and assembly process.

[0026] The working principle of an aircraft pod mounting structure provided by the utility model is as follows:

[0027] When in use, the photoelectric pod 4 is moved to install the T-shaped slider 5 into the slide rail 3, so that the T-shaped slider 5 is connected to the T-shaped slide groove, and then the T-shaped slider 5 is fixed in the slide rail 3 through the limiting mechanism 6, so that the photoelectric pod 4 and the body 1 are fixed, and the photoelectric pod 4 and the body 1 can be disassembled and assembled by reverse operation, thereby achieving the purpose of quick disassembly and assembly, replacing the screw fixing method, and the disassembly and assembly process is convenient and does not require the use of any tools.

[0028] In the above detailed description, reference is made to the accompanying drawings, which form a part of this document. In the accompanying drawings, similar symbols typically identify similar components unless the context indicates otherwise. The illustrated embodiments described in the detailed description, drawings, and claims are not meant to be limiting. Other embodiments may be used, and other changes may be made, without departing from the spirit or scope of the subject matter presented herein.

[0029] The above description is only the preferred embodiment of the utility model, and is not intended to limit the utility model. For those skilled in the art, the utility model can have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the utility model shall be included in the protection scope of the utility model.

Claims

1. An aircraft pod mounting structure, characterized in that: The invention comprises a machine body (1), one side of the machine body (1) is fixedly connected to a take-off and landing leg (2), the bottom of the machine body (1) is fixedly connected to a slide rail (3), a photoelectric pod (4) is arranged below the machine body (1), the top of the photoelectric pod (4) is fixedly connected to a T-shaped slider (5), a limiting mechanism (6) is arranged inside the T-shaped slider (5), and the limiting mechanism (6) is used to fix the photoelectric pod (4).

2. The aircraft pod mounting structure according to claim 1, characterized in that: The limiting mechanism (6) comprises a positioning rod (61) slidably connected to the inner wall of the T-shaped sliding block (5); one end of the positioning rod (61) is fixedly connected to a connecting block (62); one side of the connecting block (62) is fixedly connected to a spring (63); the other side of the connecting block (62) is fixedly connected to a paddle (64); and a positioning hole (65) is provided on the inner wall of the slide rail (3).

3. The aircraft pod mounting structure according to claim 2, characterized in that: The bottom of the connecting block (62) is fixedly connected to a limiting block (7), the inner wall of the T-shaped sliding block (5) is provided with a limiting groove (8), and the limiting block (7) is slidably connected to the limiting groove (8).

4. The aircraft pod mounting structure according to claim 2, characterized in that: The positioning rod (61) is snap-connected with the positioning hole (65), and one end of the positioning rod (61) passes through the positioning hole (65).

5. The aircraft pod mounting structure according to claim 1, characterized in that: The inner wall of the slide rail (3) is provided with a T-shaped slide groove for use with the T-shaped slide block (5).

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