CN211048563U

CN211048563U - Intelligent bracelet shell convenient to dismantle

Info

Publication number: CN211048563U
Application number: CN201921142426.5U
Authority: CN
Inventors: 钟华平
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-07-19
Filing date: 2019-07-19
Publication date: 2020-07-21
Anticipated expiration: 2029-07-19

Abstract

The utility model discloses an intelligence bracelet shell convenient to dismantle, including installing the host computer in the fuselage, have an installation cavity that holds the host computer in the fuselage, the both sides of installation cavity are provided with the elasticity buckle structure respectively, and host computer top-down packs into in the fuselage and pins the host computer both ends through the elasticity buckle structure. The utility model discloses can realize the convenient dismantlement of host computer, not hinder the fuselage during dismouting, assemble seamless, more firm behind the installation.

Description

Intelligent bracelet shell convenient to dismantle

Technical Field

The utility model relates to an intelligence bracelet shell convenient to dismantle.

Background

The assembly mode between intelligence bracelet and the host computer has a lot of, and these dismouting structures at present are mostly complicated in structure, very inconvenience when the dismouting, damage the host computer easily moreover, and the assembly back fastness is poor, and easy pine takes off, and the aesthetic property is poor, produces more not enough.

Disclosure of Invention

The utility model aims to solve the technical problem that an intelligence bracelet shell convenient to dismantle adopts an elasticity buckle structure, can realize convenient dismouting, and the assembly is firm, and the appearance is pleasing to the eye, can effectively solve not enough among the prior art.

The utility model discloses a realize through following technical scheme: the utility model provides an intelligence bracelet shell convenient to dismantle, is including installing the host computer in the fuselage, has an installation cavity that holds the host computer in the fuselage and use, and the both sides of installation cavity are provided with the elasticity buckle structure respectively, and host computer top-down is packed into in the fuselage and pins the host computer both ends through the elasticity buckle structure.

According to a preferable technical scheme, each elastic buckle structure comprises a buckle, a lug generating needle and a spring, a through hole is transversely formed in the middle of each buckle, the lug generating needle penetrates through the through hole of the whole buckle and extends out of the buckle, and the buckle is rotatably installed on the machine body through the lug generating needle;

one end of the spring is fixedly sleeved on the main body and pushes out the movable end of the buckle, and the main body is arranged between the two buckles and locked.

As the preferred technical scheme, the machine body is a zinc alloy machine body, and the buckle is made of plastic or silica gel materials.

The utility model has the advantages that: the utility model discloses can realize the convenient dismantlement of host computer, not hinder the fuselage during dismouting, assemble seamless, more firm behind the installation.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.

Fig. 1 is a schematic diagram of the explosion structure of the present invention.

Detailed Description

All of the features disclosed in this specification, or all of the steps in any method or process so disclosed, may be combined in any combination, except combinations of features and/or steps that are mutually exclusive.

Any feature disclosed in this specification (including any accompanying claims, abstract and drawings), may be replaced by alternative features serving equivalent or similar purposes, unless expressly stated otherwise. That is, unless expressly stated otherwise, each feature is only an example of a generic series of equivalent or similar features.

In the description of the present invention, it is to be understood that the terms "one end", "the other end", "the outside", "upper", "inside", "horizontal", "coaxial", "central", "end", "length", "outer end", etc. indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

Furthermore, in the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless specifically limited otherwise.

The use of terms herein such as "upper," "above," "lower," "below," and the like in describing relative spatial positions is for the purpose of facilitating description to describe one element or feature's relationship to another element or feature as illustrated in the figures. The spatially relative positional terms may be intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as "below" or "beneath" other elements or features would then be oriented "above" the other elements or features. Thus, the exemplary term "below" can encompass both an orientation of above and below. The device may be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.

In the present invention, unless otherwise explicitly specified or limited, the terms "set", "coupled", "connected", "penetrating", "plugging", and the like are to be understood in a broad sense, and may be, for example, fixedly connected, detachably connected, or integrated; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

As shown in figure 1, an intelligence bracelet shell convenient to dismantle, including installing host computer 1 in fuselage 6, have a installation cavity 5 that holds the host computer in fuselage 6, the both sides of installation cavity 5 are provided with the elasticity buckle structure respectively, and host computer 1 top-down is packed into in fuselage 6 and pins host computer 1 both ends through the elasticity buckle structure.

The elastic buckle structures comprise a buckle 3, a lug generating needle 7 and a spring 2, a through hole 4 is transversely formed in the middle of the buckle 3, the lug generating needle 7 penetrates through the through hole 4 of the whole buckle 3 and extends out of the buckle 3, and the buckle 3 is rotatably arranged on the machine body 6 through the lug generating needle 7;

one end of the spring 2 is fixedly sleeved on the machine body 6 and pushes out the movable end of the buckle 3 outwards, and the main machine 1 is arranged between the two buckles 3 and locked. When the host is installed, the buckle can be locked by being installed in the machine body from top to bottom, and when the host is disassembled, the buckle is stirred by hands, so that the host can be loosened, the disassembly is completed, and the convenience is very high.

In this embodiment, the body 6 is a zinc alloy body, and the buckle 3 is made of plastic or silica gel material. Because the buckle is plastic or silica gel, consequently protection host computer that can be fine prevents to scrape the flower, and the texture is soft.

The above description is only for the specific embodiments of the present invention, but the scope of the present invention is not limited thereto, and any changes or substitutions that are not thought of through the creative work should be covered within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the protection scope defined by the claims.

Claims

1. The utility model provides an intelligence bracelet shell convenient to dismantle, its characterized in that: including installing host computer (1) in fuselage (6), have one in fuselage (6) and hold installation cavity (5) that the host computer was used, the both sides of installation cavity (5) are provided with the elasticity buckle structure respectively, and host computer (1) top-down is packed into in fuselage (6) and pins host computer (1) both ends through the elasticity buckle structure.

2. The intelligent bracelet shell convenient to detach of claim 1, wherein: the elastic buckle structures comprise buckles (3), ear generating needles (7) and springs (2), a through hole (4) is transversely formed in the middle of each buckle (3), each ear generating needle (7) penetrates through the through hole (4) of the whole buckle (3) and extends out of the buckle, and the buckles (3) are rotatably mounted on the machine body (6) through the ear generating needles (7);

one end of the spring (2) is fixedly sleeved on the machine body (6) and pushes out the movable end of the buckle (3) outwards, and the host (1) is installed between the two buckles (3) and locked.

3. The intelligent bracelet shell convenient to detach of claim 1, wherein: the fuselage (6) are aluminum alloy fuselages, buckle (3) are made for plastic or silica gel material.