Split type aviation plug sealing device

Abstract

The utility model discloses a split type aviation plug sealing device which comprises a sealing cover and an aviation socket, the sealing cover is connected to a mechanism plate, the sealing cover comprises an aviation plug cover, and the aviation socket is located on the aviation plug cover and fixedly connected with the mechanism plate. The aviation socket and the mechanism plate form a whole, and the aviation socket cover is a part of the sealing cover, so that the aviation socket and the aviation socket cover form a split structure and are independent from each other, the secondary line is independent, and the mechanism secondary line is not influenced when the external sealing cover is disassembled and assembled.

Description

Technical Field

[0001] The utility model belongs to the field of electrical technology and relates to a split-type aviation plug sealing device. Background Art

[0002] In the design of the sealing mechanism, the secondary wires inside the mechanism need to be led out, and the use and installation of the aviation socket need to be designed.

[0003] In the existing sealing mechanism, the aviation socket is generally fixed to the housing, which is inconvenient to disassemble and assemble, and usually requires a longer secondary line to be reserved inside.

[0004] Currently, aviation sockets do not have dust and water protection functions, which will affect the operation and use of the mechanism when the mechanism is in long-term operation. Summary of the invention

[0005] In order to overcome at least one deficiency of the prior art, the utility model provides a split aviation plug sealing device.

[0006] In order to achieve the above purpose, the utility model adopts the following technical scheme: a split aviation plug sealing device, including a sealing cover and an aviation socket, the sealing cover is connected to the mechanism plate, the sealing cover includes an aviation plug cover, the aviation socket is located in the aviation plug cover and is fixedly connected to the mechanism plate.

[0007] Furthermore, the aviation plug cover is a part of the sealing cover, and the aviation plug cover and the sealing cover are disassembled or installed synchronously.

[0008] Furthermore, a sealing component is provided between the aviation plug cover and the mechanism plate, and the aviation plug cover and the mechanism plate are sealed by the sealing component.

[0009] Furthermore, it also includes an aviation plug bracket, which is fixedly connected to the aviation socket and the mechanism plate respectively.

[0010] Furthermore, the aviation plug bracket and the aviation plug cover are detachably connected.

[0011] Furthermore, it also includes a sealing structure, which is arranged between the aviation plug bracket and the aviation plug cover and between the aviation plug bracket and the aviation socket.

[0012] Furthermore, the aviation plug cover includes a shell and a shell base, the shell and the shell base are fixedly connected, the shell base is fixedly connected to the mechanism plate, an installation cavity is provided in the shell, and the aviation socket is arranged in the installation cavity.

[0013] Furthermore, the housing is provided with a fixing plate, and the fixing plate is fixedly connected to the aviation socket via an aviation plug bracket.

[0014] Furthermore, the sealing assembly includes a first sealing gasket and a second sealing gasket, the first sealing gasket is arranged between the shell base and the mechanism plate, the mechanism plate is fixedly connected to the air box, and the second sealing gasket is arranged between the mechanism plate and the air box.

[0015] Furthermore, the sealing structure includes a third sealing gasket and a fourth sealing gasket, the third sealing gasket is arranged between the aviation plug bracket and the aviation plug cover, and the fourth sealing gasket is arranged between the aviation plug bracket and the aviation socket.

[0016] In summary, the utility model is beneficial in that:

[0017] 1) The utility model adds an aviation plug bracket to the mechanism plate, and installs the aviation socket on the aviation plug bracket, so that the aviation socket and the mechanism plate form a whole, and the aviation plug cover is a part of the sealing cover, so that the aviation socket and the aviation plug cover form a split structure, which are independent of each other, and the secondary line is independent. When the external sealing cover is disassembled, the secondary line of the mechanism is not affected.

[0018] 2) The utility model is provided with a sealing component and a sealing structure, which greatly improves the sealing, enables the mechanism to meet the requirements of the IP65 protection level, and avoids the influence of condensation and dust on the mechanism. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 It is a schematic diagram of the aviation plug sealing device of the utility model.

[0020] Figure 2 It is a schematic diagram of the exploded view of the aviation plug sealing device of the utility model.

[0021] Figure 3 It is a schematic diagram of the aerial plug bracket of the utility model.

[0022] Figure 4 It is a schematic diagram of the aerial plug bracket of the utility model.

[0023] Figure 5 It is a half-section schematic diagram of the aviation plug sealing device of the utility model.

[0024] Markings in the figure: sealing cover 1, aviation socket 2, mechanism plate 4, aviation plug bracket 5, aviation plug cover 10, positioning plate 21, first sealing gasket 31, second sealing gasket 32, first plate 51, second plate 52, third plate 53, third sealing gasket 61, fourth sealing gasket 62, outer shell 101, outer shell base 102, installation cavity 103, and fixing plate 104. DETAILED DESCRIPTION

[0025] The following describes the implementation of the present invention through specific examples, and those skilled in the art can easily understand other advantages and effects of the present invention from the contents disclosed in this specification. The present invention can also be implemented or applied through other different specific implementations, and the details in this specification can also be modified or changed in various ways based on different viewpoints and applications without departing from the spirit of the present invention. It should be noted that the following embodiments and features in the embodiments can be combined with each other without conflict.

[0026] It should be noted that the illustrations provided in the following embodiments are only schematic illustrations of the basic concept of the present invention, and thus the drawings only show components related to the present invention rather than being drawn according to the number, shape and size of components in actual implementation. In actual implementation, the type, quantity and proportion of each component may be changed at will, and the component layout may also be more complicated.

[0027] All directional indications in the embodiments of the present invention (such as up, down, left, right, front, back, horizontal, vertical...) are only used to explain the relative position relationship, movement status, etc. between the components in a certain specific posture. If the specific posture changes, the directional indication will also change accordingly.

[0028] Due to installation errors and other reasons, the parallel relationship referred to in the embodiments of the present invention may actually be an approximately parallel relationship, and the vertical relationship may actually be an approximately vertical relationship.

[0029] Embodiment 1:

[0030] like Figure 1-Figure 5 As shown, a split aviation plug sealing device includes a sealing cover 1 and an aviation socket 2. The sealing cover 1 is connected to the mechanism plate 4. The sealing cover 1 includes an aviation plug cover 10. The aviation socket 2 is located in the aviation plug cover 10 and is fixedly connected to the mechanism plate 4.

[0031] The sealing cover 1 is configured as a closed cover welded entirely of metal, and a cavity is also provided inside the sealing cover 1, in which a mechanism is installed.

[0032] The aviation plug cover 10 is a part of the sealing cover 1 , and the aviation plug cover 10 and the sealing cover 1 are disassembled or installed synchronously.

[0033] The aviation socket cover 10 includes a shell 101 and a shell base 102 . The shell 101 and the shell base 102 are fixedly connected. The shell base 102 is fixedly connected to the mechanism plate 4 . An installation cavity 103 is provided in the shell 101 . The aviation socket 2 is arranged in the installation cavity 103 .

[0034] A fixing plate 104 is provided on the end surface of the housing 101 . The fixing plate 104 is connected to the aviation socket 2 . The fixing plate 104 is fixed on the end surface of the housing 101 for easy disassembly.

[0035] A sealing component is provided between the aviation plug cover 10 and the mechanism plate 4 , and the aviation plug cover 10 and the mechanism plate 4 are sealed by the sealing component.

[0036] The sealing assembly includes a first sealing gasket 31 and a second sealing gasket 32. The first sealing gasket 31 is arranged between the shell base 102 and the mechanism plate 4, and the second sealing gasket 32 ​​is fixedly arranged on the outside of the mechanism plate 4. The mechanism plate 4 is fixedly connected to the air box (not shown in the figure), and the second sealing gasket 32 ​​is arranged between the mechanism plate 4 and the air box.

[0037] The aviation socket 2 is provided with a positioning plate 21 , and the positioning plate 21 is fixedly connected to the aviation socket bracket 5 .

[0038] An aviation plug bracket 5 is provided between the aviation socket 2 and the mechanism plate 4 . One end of the aviation plug bracket 5 is connected to the aviation socket 2 , and the other end is connected to the aviation socket 2 and the housing 101 of the aviation plug cover 10 .

[0039] The aviation socket bracket 5 includes a first plate 51 , a second plate 52 and a third plate 53 . The second plate 52 is vertically connected to the first plate 51 and the third plate 53 respectively to form a Z-shaped structure. The first plate 51 is connected to the mechanism plate 4 , and the second plate 52 is connected to the aviation socket 2 .

[0040] The aviation plug sealing device further comprises a sealing structure, which is arranged between the aviation plug bracket 5 and the aviation plug cover 10 and between the aviation plug bracket 5 and the aviation socket 2 .

[0041] The sealing structure includes a third sealing gasket 61 and a fourth sealing gasket 62 . The third sealing gasket 61 is disposed between the second plate 52 and the fixing plate 104 , and the fourth sealing gasket 62 is disposed between the second plate 52 and the positioning plate 21 .

[0042] In this embodiment, the fixed connection between the housing 101 and the housing base 102 can be achieved by welding, gluing or other sealing connection methods.

[0043] In this embodiment, the aviation plug sealing device can be used alone in existing equipment, and the structure not described in the mechanism adopts existing components, which will not be described in detail here.

[0044] Obviously, the described embodiments are only some embodiments of the utility model, not all embodiments. Based on the embodiments of the utility model, all other embodiments obtained by ordinary technicians in this field without creative work should fall within the scope of protection of the utility model.

Claims

1. A split-type aviation plug sealing device, characterized in that: It includes a sealing cover and an aviation socket. The sealing cover is connected to the mechanism plate. The sealing cover includes an aviation plug cover. The aviation socket is located in the aviation plug cover and is fixedly connected to the mechanism plate.

2. A split-type aviation plug sealing device according to claim 1, characterized in that: The aviation plug cover is a part of the sealing cover, and the aviation plug cover and the sealing cover are disassembled or installed synchronously.

3. A split-type aviation plug sealing device according to claim 1, characterized in that: A sealing component is provided between the aviation plug cover and the mechanism plate, and the aviation plug cover and the mechanism plate are sealed by the sealing component.

4. A split-type aviation plug sealing device according to claim 1, characterized in that: It also includes an aviation plug bracket, which is fixedly connected to the aviation socket and the mechanism plate respectively.

5. A split-type aviation plug sealing device according to claim 4, characterized in that: The aviation plug bracket is detachably connected to the aviation plug cover.

6. A split-type aviation plug sealing device according to claim 5, characterized in that: It also includes a sealing structure, which is arranged between the aviation plug bracket and the aviation plug cover and between the aviation plug bracket and the aviation socket.

7. A split-type aviation plug sealing device according to claim 3, characterized in that: The aviation plug cover comprises a shell and a shell base, the shell and the shell base are fixedly connected, the shell base is fixedly connected to the mechanism plate, an installation cavity is arranged in the shell, and the aviation socket is arranged in the installation cavity.

8. A split-type aviation plug sealing device according to claim 7, characterized in that: The housing is provided with a fixing plate, and the fixing plate is fixedly connected to the aviation socket through an aviation plug bracket.

9. A split-type aviation plug sealing device according to claim 7, characterized in that: The sealing assembly comprises a first sealing gasket and a second sealing gasket, wherein the first sealing gasket is arranged between the housing base and the mechanism plate, the mechanism plate is fixedly connected to the air box, and the second sealing gasket is arranged between the mechanism plate and the air box.

10. A split-type aviation plug sealing device according to claim 6, characterized in that: The sealing structure comprises a third sealing pad and a fourth sealing pad. The third sealing pad is arranged between the aviation plug bracket and the aviation plug cover, and the fourth sealing pad is arranged between the aviation plug bracket and the aviation socket.

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