An easily assembled assembly, assembly body and tower fan

Abstract

This application relates to an easily assembled assembly component, assembly body, and tower fan. The assembly component includes a fuselage unit and a chassis unit. The chassis unit has a split structure, including a first chassis portion and a second chassis portion. The first chassis portion and the second chassis portion are assembled to each other via mating parts. The mating parts include mounting members and mounting portions respectively disposed on the first chassis portion and the second chassis portion. The mounting portions are fitted over the mounting members, so that the first chassis portion and the second chassis portion are assembled into a whole. This application has the technical advantages of small packaging size, very convenient installation and disassembly, and reliable assembly.

Description

Technical Field

[0001] This application relates to an easily assembled assembly component, assembly body, and tower fan. Background Technology

[0002] In existing column-type electrical appliances, especially those with similarly sized chassis and columns, such as tower fans and air purifiers, there are typically two assembly methods for the chassis assembly. The first method integrates the chassis assembly and the main unit as a single unit, resulting in larger packaging and inconvenient transportation. The second method packages the chassis assembly and the main unit separately, requiring user assembly. This usually involves fasteners such as screws or nuts at the assembly points, making disassembly of the chassis assembly and the main unit cumbersome and inconvenient to use.

[0003] Therefore, there is a need in the prior art for a tower fan that is small in size, easy to install and disassemble, and has a secure assembly. Utility Model Content

[0004] The purpose of this application is to provide an easy-to-assemble assembly component, assembly body, and tower fan, wherein the chassis is divided into left and right parts, the body is inserted into the chassis for positioning, and the body is locked in the chassis by rotation, so that the chassis and body can be assembled and disassembled without the aid of tools during use, and the product packaging size can also be reduced.

[0005] This application relates to an easily assembled assembly component, including a fuselage unit and a chassis unit. The chassis unit is a split structure, including a first chassis portion and a second chassis portion. The first chassis portion and the second chassis portion are assembled to each other by mating parts. The mating parts include mounting parts and mounting portions respectively disposed on the first chassis portion and the second chassis portion. The mounting portions are sleeved on the outside of the mounting parts, so that the first chassis portion and the second chassis portion are assembled into a whole.

[0006] The first chassis portion and the second chassis portion may be respectively provided with mutually cooperating elastic fasteners and fastening parts. During assembly, the elastic fasteners are fastened to the fastening parts. The body unit and the chassis unit may be respectively provided with locking parts and locking holes for accommodating the locking parts. The locking parts are fitted into the locking holes.

[0007] The locking component can be fitted into the locking hole via an elastic locking part; the elastic locking part can be a separate component or integrally formed with the chassis unit; an opening can be provided on the side of the locking hole, and the elastic locking part can be disposed between the locking hole and the opening; the body unit and the chassis unit can be respectively provided with mutually cooperating positioning components and positioning holes, and the positioning components are accommodated in the positioning holes; the body unit and the chassis unit can be respectively provided with mutually cooperating plug-in parts and plug-in interfaces.

[0008] This application also relates to an assembly comprising the assembly components described above. The assembly may be a tower fan, an air purifier, or the like.

[0009] According to the present application, an easily assembled assembly component, assembly body, and tower fan have the following technical advantages:

[0010] (1) This application divides the chassis unit into a first chassis part and a second chassis part, on which mounting parts and mounting sections that can be assembled are respectively provided. The mounting section can be directly put on the outside of the mounting part by hand, making assembly and disassembly very convenient, and the assembly is reliable.

[0011] (2) By providing elastic fasteners and fastening parts on the first chassis part and the second chassis part respectively, this application makes the assembly of the first chassis part and the second chassis part more secure and convenient to disassemble and assemble.

[0012] (3) This application provides a locking hole on the chassis unit for accommodating the locking member of the fuselage unit. The locking member can be locked in the locking hole, so that the fuselage unit can be securely locked and installed with the chassis unit. It is easy to operate and easy to install without the need for additional fasteners.

[0013] (4) The elastic snap-fit ​​part is formed by setting an opening on the side of the snap-fit ​​hole, so that the elastic snap-fit ​​part can be integrally formed with the chassis, which is very convenient to manufacture and use, and there is no need to set a separate elastic snap-fit ​​part. Attached Figure Description

[0014] Figure 1 This is a schematic diagram of the disassembled chassis unit of this application.

[0015] Figure 2 This is a schematic diagram of the assembly state of the chassis unit of this application.

[0016] Figure 3 This is a schematic diagram showing the disassembled state of the fuselage unit and chassis unit of this application.

[0017] Figure 4 This is a schematic diagram of the chassis unit of this application.

[0018] Figure 5 This is a schematic diagram of the assembly state of the fuselage unit and chassis unit of this application. Detailed Implementation

[0019] To make the objectives, technical solutions, and advantages of this application clearer, the technical solutions of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this application, not all embodiments. Based on the embodiments of this application, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this application.

[0020] like Figure 1-5 As shown, this application proposes an easily assembled assembly component, which includes a fuselage unit 20 and a chassis unit 10. The chassis unit 10 is a split structure, including a first chassis portion 11 and a second chassis portion 12. The first chassis portion 11 and the second chassis portion 12 are assembled to each other via mating parts. Specifically, the mating parts may include a mounting member 14 and a mounting part 13 respectively disposed on the first chassis portion 11 and the second chassis portion 12. The mounting part 13 can be sleeved on the outside of the mounting member 14 to achieve the combined assembly of the first chassis portion 11 and the second chassis portion 12. The mounting member 14 and the mounting part 13 may respectively take the form of a mounting post and a mounting sleeve. Figure 1 In the illustrated embodiment, four sets of mating parts are provided between the first chassis portion 11 and the second chassis portion 12. During installation, the mounting part 13 can be directly fitted onto the outside of the mounting part 14 to achieve mutual fixation between the two. Preferably, to further ensure a secure installation between the first chassis portion and the second chassis portion, mutually cooperating elastic fasteners 15 and fastening parts 31 can be provided on the first chassis portion 11 and the second chassis portion 12, respectively. When the mating parts between the first chassis portion 11 and the second chassis portion 12 are assembled, the elastic fastener 15 can also be simultaneously fastened onto the fastening part 31, thereby making the assembly of the chassis unit more secure and stable. Figure 2 The diagram shows the assembled assembly components, in which the mounting part 13 and the mounting component 14 are installed together, and the elastic fastener 15 and the fastener part 31 are fastened together.

[0021] like Figure 3-5The diagram shows a fuselage unit 20 and a chassis unit 10 assembled together. The fuselage unit 20 has a positioning element 22 and a locking element 21 at its bottom end, and a insertion portion 23 at the center of its bottom. The chassis unit 10 has positioning holes 16 for accommodating the positioning element 22, and a insertion interface 32 at its center for accommodating the insertion portion 23. As shown, there are three positioning elements 22 and three positioning holes 16. Those skilled in the art will understand that the number can be set according to actual needs, and their positions can also be reversed as needed.

[0022] The chassis unit 10 is also provided with a locking hole 17 for accommodating the locking member 21, which can be locked into the locking hole 17. More specifically, such as Figure 4 As shown, the locking member 21 can be locked into the locking hole 17 via the elastic locking part 19. The elastic locking part 19 can be a separate component or a combination thereof. Figure 4 It is formed in the form shown. For example... Figure 4 As shown, the elastic locking portion 19 is strip-shaped and has protrusions for engaging the locking member 21. The elastic locking portion 19 can be provided independently or in the form of an opening 18 on the side of the locking hole 17. In this case, since the locking hole 17 and the opening 18 are on both sides of the elastic locking portion 19, the elastic locking portion 19 can not only be integrally formed with the chassis, but also deform through the openings on both sides, thereby meeting the needs of engaging and disengaging the locking member 21.

[0023] like Figure 3-5 As shown, when assembling the fuselage unit 20 and the chassis unit 10, the positioning member 22 and the locking member 21 on the fuselage unit 20 are inserted into the positioning hole 16 and the locking hole 17 respectively. Then, the fuselage unit 20 or the chassis unit 10 is rotated so that the locking member 21 is firmly locked into the locking hole 17. Conversely, when it is necessary to disassemble the fuselage unit 20 and the chassis unit 10, simply rotate the fuselage unit 20 or the chassis unit 10 in the opposite direction so that the locking member 21 is released from the elastic locking part 19.

[0024] This application also relates to an assembly comprising a fuselage unit and a chassis unit, wherein the fuselage unit and the chassis unit are assembled together by the assembly components described above. The assembly of this application may be a fan or an air purifier, and the fan may be a tower fan.

[0025] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of this application, and are not intended to limit them. Although this application has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some of the technical features. Such modifications or substitutions do not cause the essence of the corresponding technical solutions to deviate from the spirit and scope of the technical solutions of the embodiments of this application.

Claims

1. An easily assembled assembly comprising a fuselage unit and a chassis unit, characterized in that, The chassis unit is a split structure, including a first chassis part and a second chassis part, which are assembled together by mating parts; The mating components include mounting members and mounting parts respectively disposed on the first chassis portion and the second chassis portion. The mounting parts are sleeved on the outside of the mounting members, so that the first chassis portion and the second chassis portion are assembled into a whole.

2. The assembly of claim 1, wherein, The first chassis portion and the second chassis portion are respectively provided with mutually cooperating elastic fasteners and fastening parts. During assembly, the elastic fasteners are fastened to the fastening parts.

3. The assembly of claim 1 or 2, wherein, The fuselage unit and the chassis unit are respectively provided with a locking component and a locking hole for accommodating the locking component, and the locking component is fitted into the locking hole.

4. The assembly of claim 3, wherein, The locking component is fitted into the locking hole via an elastic locking part.

5. The assembly of claim 4, wherein, The elastic snap-fit ​​part is a separate component or is integrally formed with the chassis unit.

6. The assembly of claim 4, wherein, An opening is provided on the side of the locking hole, and the elastic locking part is disposed between the locking hole and the opening.

7. The assembly of any of claims 1-2, 4-6, wherein, The fuselage unit and the chassis unit are respectively provided with mutually cooperating positioning components and positioning holes, and the positioning components are accommodated in the positioning holes.

8. The assembly of any of claims 1-2, 4-6, wherein, The fuselage unit and the chassis unit are respectively provided with mutually cooperating plug-in parts and plug-in interfaces.

9. An assembly comprising an assembly component, characterized by The assembly component is the assembly component according to any one of claims 1-8.

10. A tower fan comprising an assembly of components, characterised in that, The assembly component is the assembly component according to any one of claims 1-8.

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