CN212160373U - Novel helicopter alarm clock structure - Google Patents
Novel helicopter alarm clock structure Download PDFInfo
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- CN212160373U CN212160373U CN202020544716.9U CN202020544716U CN212160373U CN 212160373 U CN212160373 U CN 212160373U CN 202020544716 U CN202020544716 U CN 202020544716U CN 212160373 U CN212160373 U CN 212160373U
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Abstract
本实用新型公开了一种新型直升机闹钟结构,包括设置有数字表盘的前壳体、设置有表针的机芯组件、卡扣组件、开设有第一空腔的后壳体、第一连接组件、第二连接组件、第一条形板和第二条形板,第一连接组件一端与前壳体底部连接,另一端与第一条形板连接,第二连接组件一端与前壳体底部连接,另一端与第二条形板连接,后壳体上设置有第一安装框体,机芯组件经第一安装框体放置于第一空腔中,卡扣组件可拆卸地与第一安装框体连接。本实用新型,占地面积小,对于摆放位置、摆放空间要求低,适用性高,机芯维护、更换方便。
The utility model discloses a novel helicopter alarm clock structure, which comprises a front casing provided with a digital dial, a movement component provided with a watch needle, a buckle component, a rear casing provided with a first cavity, a first connection component, The second connecting assembly, the first strip-shaped plate and the second strip-shaped plate, one end of the first connecting assembly is connected to the bottom of the front shell, the other end is connected to the first strip-shaped plate, and one end of the second connecting assembly is connected to the bottom of the front shell , the other end is connected with the second strip plate, the rear casing is provided with a first installation frame, the core assembly is placed in the first cavity through the first installation frame, and the buckle assembly is detachably installed with the first installation frame. Frame connection. The utility model has the advantages of small footprint, low requirements for the placement position and placement space, high applicability, and convenient maintenance and replacement of the movement.
Description
技术领域technical field
本实用新型属于闹钟结构技术领域,尤其涉及一种新型直升机闹钟结构。The utility model belongs to the technical field of alarm clock structures, in particular to a novel helicopter alarm clock structure.
背景技术Background technique
目前,现有闹钟结构大多为电子闹钟,比如申请号为CN200720118038,申请名称为电子闹钟,该专利公开的闹钟结构占地面积大,对摆放位置、摆放空间要求高,适用性低,利用LED显示屏作为时间显示的结构,如果LED显示屏损坏,因为飞机结构位于LED显示屏上方,维护起来较麻烦。At present, most of the existing alarm clock structures are electronic alarm clocks, for example, the application number is CN200720118038, and the application name is electronic alarm clock. The LED display screen is used as a time display structure. If the LED display screen is damaged, because the aircraft structure is located above the LED display screen, it is more troublesome to maintain.
因此,现有技术有待于改善。Therefore, the existing technology needs to be improved.
实用新型内容Utility model content
本实用新型的主要目的在于提出一种新型直升机闹钟结构,旨在解决背景技术中所提及的技术问题,占地面积小,对于摆放位置、摆放空间要求低,适用性高,机芯维护、更换方便。The main purpose of the present utility model is to propose a new type of helicopter alarm clock structure, which aims to solve the technical problems mentioned in the background art. Maintenance and replacement are convenient.
本实用新型的一种新型直升机闹钟结构,包括设置有数字表盘的前壳体、设置有表针的机芯组件、卡扣组件、开设有第一空腔的后壳体、第一连接组件、第二连接组件、第一条形板和第二条形板,第一连接组件一端与前壳体底部连接,另一端与第一条形板连接,第二连接组件一端与前壳体底部连接,另一端与第二条形板连接,后壳体上设置有第一安装框体,机芯组件经第一安装框体放置于第一空腔中,卡扣组件可拆卸地与第一安装框体连接。A novel helicopter alarm clock structure of the utility model comprises a front casing provided with a digital dial, a movement component provided with a watch needle, a buckle component, a rear casing provided with a first cavity, a first connection component, a second Two connecting assemblies, a first strip-shaped plate and a second strip-shaped plate, one end of the first connecting assembly is connected to the bottom of the front shell, the other end is connected to the first strip-shaped plate, and one end of the second connecting assembly is connected to the bottom of the front shell, The other end is connected to the second strip plate, the rear casing is provided with a first installation frame, the core assembly is placed in the first cavity through the first installation frame, and the buckle assembly is detachably connected to the first installation frame body connection.
优选地,卡扣组件包括第一板材,第一板材顶部设置有第一凸柱和第二凸柱,第一板材底部设置有卡入部,第一安装框体顶部开设有第一通孔和第二通孔,第一安装框体底部开设有第一卡槽。Preferably, the buckle assembly includes a first plate, the top of the first plate is provided with a first convex column and a second convex column, the bottom of the first plate is provided with a snap-in portion, and the top of the first installation frame is provided with a first through hole and a second convex column. There are two through holes, and the bottom of the first installation frame is provided with a first card slot.
优选地,还包括螺钉,前壳体上设置有螺丝柱,后壳体上开设有螺钉孔,螺钉穿过螺钉孔与螺丝孔连接。Preferably, it also includes screws, the front casing is provided with screw posts, the rear casing is provided with screw holes, and the screws pass through the screw holes and are connected with the screw holes.
优选地,前壳体包括前板材部分、中板材部分和后板材部分,中板材部分顶部设置有主桨叶结构,后板材部分设置有尾桨结构,数字表盘设置于中板材部分上,前板材部分和后板材部分通过中板材部分连接。Preferably, the front casing includes a front plate part, a middle plate part and a rear plate part, the top of the middle plate part is provided with a main paddle structure, the rear plate part is provided with a tail rotor structure, the digital dial is arranged on the middle plate part, the front plate The part and the rear panel part are connected by the middle panel part.
本实用新型的新型直升机闹钟结构,利用第一条形板和第二条形板作为底座,占地面积小,对于摆放位置、摆放空间要求低,适用性高;且第一安装框体和卡扣组件之间的拆卸式连接方式,使得机芯便于维护。The novel helicopter alarm clock structure of the utility model utilizes the first strip-shaped plate and the second strip-shaped plate as the base, occupies a small area, has low requirements for the placement position and placement space, and has high applicability; and the first installation frame body The detachable connection method between the clip and the buckle assembly makes the movement easy to maintain.
附图说明Description of drawings
图1为本实用新型新型直升机闹钟结构的三维示意图;Fig. 1 is the three-dimensional schematic diagram of the structure of the utility model helicopter alarm clock;
图2为本实用新型新型直升机闹钟结构的结构拆分图;Fig. 2 is the structure disassembly diagram of the utility model helicopter alarm clock structure;
图3为本实用新型新型直升机闹钟结构的爆炸图。FIG. 3 is an exploded view of the structure of the helicopter alarm clock of the utility model.
本实用新型目的的实现、功能特点及优点将结合实施例,参照附图做进一步说明。The realization, functional characteristics and advantages of the purpose of the present utility model will be further described with reference to the accompanying drawings in conjunction with the embodiments.
具体实施方式Detailed ways
应当理解,此处所描述的具体实施例仅仅用以解释本实用新型,并不用于限定本实用新型。需要注意的是,相关术语如“第一”、“第二”等可以用于描述各种组件,但是这些术语并不限制该组件。这些术语仅用于区分一个组件和另一组件。例如,不脱离本实用新型的范围,第一组件可以被称为第二组件,并且第二组件类似地也可以被称为第一组件。术语“和/或”是指相关项和描述项的任何一个或多个的组合。It should be understood that the specific embodiments described herein are only used to explain the present invention, and are not intended to limit the present invention. It should be noted that related terms such as "first", "second", etc. may be used to describe various components, but these terms do not limit the component. These terms are only used to distinguish one component from another. For example, without departing from the scope of the present invention, a first component could be termed a second component, and a second component could similarly be termed a first component. The term "and/or" refers to a combination of any one or more of the associated and described items.
如图1、图2、图3所示,图1为本实用新型新型直升机闹钟结构的三维示意图;图2为本实用新型新型直升机闹钟结构的结构拆分图;图3为本实用新型新型直升机闹钟结构的爆炸图。本实用新型的一种新型直升机闹钟结构,包括设置有数字表盘11的前壳体10、设置有表针51的机芯组件50、卡扣组件200、开设有第一空腔84的后壳体80、第一连接组件23、第二连接组件24、第一条形板21和第二条形板22,第一连接组件23一端与前壳体10底部连接,另一端与第一条形板连接,第二连接组件24一端与前壳体10底部连接,另一端与第二条形板连接,后壳体80上设置有第一安装框体800,机芯组件50经第一安装框体800放置于第一空腔84中,卡扣组件200可拆卸地与第一安装框体800连接。本实用新型的新型直升机闹钟结构,利用第一条形板和第二条形板作为底座,占地面积小,对于摆放位置、摆放空间要求低,适用性高;且第一安装框体和卡扣组件之间的拆卸式连接方式,使得机芯便于维护。且本实用新型结构新颖,整体呈直升飞机状。As shown in Figure 1, Figure 2, Figure 3, Figure 1 is a three-dimensional schematic diagram of the structure of the utility model helicopter alarm clock; Figure 2 is a structural disassembly diagram of the structure of the utility model helicopter alarm clock; Figure 3 is the utility model helicopter alarm clock structure Exploded diagram of the structure of the alarm clock. A novel helicopter alarm clock structure of the present invention includes a
如图2、图3所示,优选地,卡扣组件200包括第一板材71,第一板材71顶部设置有第一凸柱73和第二凸柱74,第一板材底部设置有卡入部72,第一安装框体800顶部开设有第一通孔82和第二通孔81,第一安装框体底部开设有第一卡槽85;本优选实施例对于卡扣组件、第一安装框体进行具体结构限定,在安装时,将机芯组件50经第一安装框体放置于第一空腔84后,将第一板材71上的第一凸柱73和第二凸柱74分别嵌入第一安装框体上的第一通孔82和第二通孔81内,利用第一板材底部的卡入部72卡入第一安装框体底部的第一卡槽85内,实现卡扣式连接。对于拆卸,同样地,首先将卡入部72从第一卡槽85内脱离,再将第一凸柱73和第二凸柱74分别脱离第一安装框体上的第一通孔82和第二通孔81,实现拆卸,以方便更换机芯组件50。As shown in FIGS. 2 and 3 , preferably, the
其中,对于将机芯组件50经第一安装框体放置于第一空腔84中;具体指,从第一安装框体外侧将机芯组件50放置于位于第一安装框体内侧的第一空腔84内。机芯组件50是一种现有的应用于闹钟的驱动机构,主要用于带动表针51转动。前壳体包括ABS塑料壳体;对于后壳体,同样地,后壳体包括ABS塑料壳体;使得整体结构轻便、耐用。Wherein, for placing the
如图2所示,优选地,还包括螺钉(图中未示),前壳体上设置有螺丝柱103,后壳体上开设有螺钉孔83,螺钉穿过螺钉孔与螺丝孔连接;本优选实施例对于前壳体、后壳体的具体结构进行限定,以实现,前壳体设置于后壳体上,且从图2可以看出,前壳体的形状和后壳体的形状整体相似,两者适配。As shown in FIG. 2, preferably, it also includes screws (not shown in the figure), the front housing is provided with
如图2所示,优选地,前壳体包括前板材部分102、中板材部分101和后板材部分100,中板材部分顶部设置有主桨叶结构26,后板材部分设置有尾桨结构25,数字表盘设置于中板材部分上,前板材部分和后板材部分通过中板材部分连接。本优选实施例对于前壳体进行具体限定,使得本实用新型结构新颖,整体呈直升飞机状。As shown in FIG. 2 , preferably, the front casing includes a front plate part 102 , a middle plate part 101 and a
以上仅为本实用新型的优选实施例,并非因此限制本实用新型的专利范围,凡是利用本实用新型说明书及附图内容所作的等效结构或等效流程变换,或直接或间接运用在其他相关的技术领域,均同理包括在本实用新型的专利保护范围内。The above are only the preferred embodiments of the present utility model, and are not intended to limit the scope of the present utility model patent. Any equivalent structure or equivalent process transformation made by using the contents of the present utility model description and accompanying drawings, or directly or indirectly applied to other related The technical fields of the present invention are similarly included in the scope of patent protection of the present invention.
Claims (4)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020544716.9U CN212160373U (en) | 2020-04-14 | 2020-04-14 | Novel helicopter alarm clock structure |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202020544716.9U CN212160373U (en) | 2020-04-14 | 2020-04-14 | Novel helicopter alarm clock structure |
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| CN212160373U true CN212160373U (en) | 2020-12-15 |
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| CN202020544716.9U Expired - Fee Related CN212160373U (en) | 2020-04-14 | 2020-04-14 | Novel helicopter alarm clock structure |
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