Space atmosphere lamp

Abstract

The utility model relates to the technical field of lamps, in particular to a space atmosphere lamp which comprises a polyhedron formed by splicing a plurality of polygonal semitransparent and semi-reflective lenses, a control assembly is arranged outside the polyhedron, lamp filaments are embedded between the spliced polygonal semitransparent and semi-reflective lenses respectively, and the lamp filaments are connected to the control assembly in a power-taking mode. The polygonal semitransparent and semi-reflective lenses are installed on the corresponding polygonal enclosure frame of the supporting framework, the lamp filaments are embedded in the splicing positions of the polygonal semitransparent and semi-reflective lenses, and the polygonal semitransparent and semi-reflective lenses are used for reflecting and projecting the lightened lamp filaments, so that a user can see the lamp filaments from any polygonal semitransparent and semi-reflective lens, and the user experience is improved. Therefore, the space atmosphere lamp is enabled to show strong sense of design and sense of space visually.

Description

Technical Field

[0001] The utility model relates to the technical field of lamps, in particular to a space atmosphere lamp. Background Art

[0002] In addition to providing lighting, general lamps can also be designed with a variety of aesthetic designs to provide lighting while also being beautiful.

[0003] For example, a lamp disclosed in the patent with publication number CN216844224U, although the lamp can be built by the user at home according to the user's own usage scenarios using the first light-emitting component and the second light-emitting component, and can be used in multiple scenarios. The user can prepare the first light-emitting component and the second light-emitting component according to their own needs to build a personalized lamp, avoiding the problem of wasting resources and occupying home space; however, the lamp composed of the first light-emitting component and the second light-emitting component lacks a sense of space when emitting light, resulting in poor aesthetics of the lamp, so it needs to be improved. Utility Model Content

[0004] The purpose of the utility model is to provide a space atmosphere lamp to solve the problems raised in the above background technology.

[0005] In order to achieve the above purpose, the utility model provides the following technical solutions:

[0006] A space atmosphere lamp comprises a control component and a polyhedron formed by splicing a plurality of polygonal semi-transparent and semi-reflective lenses. The control component is arranged outside the polyhedron. Filaments are respectively embedded between the spliced ​​polygonal semi-transparent and semi-reflective lenses. Each filament is electrically connected to the control component.

[0007] Furthermore, it also includes a supporting frame, which is formed with a plurality of polygonal frames, and the peripheral sides of each polygonal semi-transparent and semi-reflective lens are matched, snapped or glued to the corresponding polygonal frame; the filaments are respectively embedded in each polygonal frame.

[0008] Furthermore, a base is provided at the lower end of the polyhedron, and the control component is placed in the base.

[0009] Furthermore, a support portion that is lifted upward and connected to the lower end of the polyhedron is provided at the upper end of the base.

[0010] Furthermore, the control component includes a power driver, a power supply and a switch arranged in the base, and a circuit is formed between the power driver, the power supply, the switch and the filament; the power supply is a lithium battery built into the base or an external DC power supply; the switch is arranged on the base.

[0011] Furthermore, the filament is an LED ceramic filament or an LED flexible filament.

[0012] Furthermore, the filaments include a substrate, a plurality of light-emitting chips and a light-transmitting adhesive layer. The light-emitting chips are laid along the length direction of the front side of the substrate and the light-emitting chips are connected in series, in parallel or in series and parallel. The front and back sides of the substrate are covered with a light-transmitting adhesive layer, and the light-transmitting adhesive layer on the front side covers the light-emitting chips in a row.

[0013] Furthermore, a mounting cavity with an opening facing downward is provided in the base, a bottom cover is connected to the opening of the mounting cavity, and the control component is arranged in the mounting cavity and located on the upper side of the bottom cover.

[0014] Furthermore, a counterweight ring is fixedly connected in the installation cavity or on the bottom cover.

[0015] Furthermore, a lamp holder is provided at the lower end of the polyhedron, a control component is placed in the lamp holder, and the control component is a power driver, and the filaments are connected in series, in parallel, or in series and in parallel and then electrically connected to the lamp holder via the power driver.

[0016] Compared with the prior art, the beneficial effects of the utility model are:

[0017] 1. The utility model installs polygonal semi-transparent and semi-reflective lenses on corresponding polygonal frames of a supporting frame, embeds filaments at the joints of the polygonal semi-transparent and semi-reflective lenses, and uses the polygonal semi-transparent and semi-reflective lenses to reflect and project the lit filaments, so that users can see the reflections and double images of multiple lit filaments when looking through any polygonal semi-transparent and semi-reflective lenses, thereby making the space atmosphere lamp visually show a strong sense of design and space.

[0018] 2. The utility model, through the arrangement of the supporting part, can better realize the disassembly and assembly of the supporting frame on the base, so that the base can support the polyhedron.

[0019] 3. The utility model, through the provision of a counterweight ring, enables the counterweight ring to be installed on the installation cavity or the bottom cover, which can increase the counterweight of the base, thereby better enabling the base to stably support the polyhedron. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 The utility model is a structural schematic diagram of a space atmosphere lamp.

[0021] Figure 2 The utility model is a schematic diagram of a partial explosion structure of a space atmosphere lamp.

[0022] Figure 3 It is a structural schematic diagram of the support frame in the utility model.

[0023] Figure 4It is a schematic diagram of the explosion structure of the base in the utility model.

[0024] Figure 5 It is a schematic diagram of the composition of the filament in the utility model.

[0025] Figure 6 This is a schematic diagram of the structure of the lamp holder adopted in the utility model.

[0026] The meanings of the numbers in the figure are: 10, base; 11, support part; 20, polyhedron; 110, polygonal semi-transparent and semi-reflective lens; 120, filament; 130, bottom cover; 210, support frame; 311, polygonal frame; 312, connection part; 411, installation cavity; 412, ventilation groove; 421, recessed cavity; 01, substrate; 02, light-emitting chip; 03, light-transmitting adhesive layer; 04, pin; 100, lamp holder. DETAILED DESCRIPTION

[0027] In order to further understand the content of the utility model, the utility model is described in detail in conjunction with the accompanying drawings and embodiments. It should be understood that the embodiments are only used to explain the utility model but not to limit it.

[0028] The following is combined with Figure 1-Figure 6 This embodiment is described in further detail.

[0029] like Figure 1 As shown, a space atmosphere lamp in this embodiment includes a control component and a polyhedron 20 which is surrounded by a plurality of polygonal semi-transparent and semi-reflective lenses 110. The control component is arranged outside the polyhedron 20, and filaments 120 are respectively embedded between the polygonal semi-transparent and semi-reflective lenses 110. Each filament 120 is electrically connected to the control component.

[0030] In this embodiment, the control component is used to control the lighting of each filament 120. Since the filament 120 is embedded and installed on the edge of the polyhedron 20, when the filament 120 is lit, the polygonal semi-transparent and semi-reflective lens 110 reflects and projects the lit filament 120, so that when viewed from any polygonal semi-transparent and semi-reflective lens 110, the reflection and double images of multiple lit filaments 120 can be seen, that is, the spatial atmosphere lamp is reflected and projected by the polygonal semi-transparent and semi-reflective lens 110, so that the user can visually show a strong sense of design and space.

[0031] Combination Figure 2-3As shown, in this embodiment, a support frame 210 is further included. The support frame 210 is used to support the polyhedron 20. The support frame 210 is formed with a plurality of polygonal frames 311. The shape of the polygonal frames 311 is adapted to the polygonal semi-transparent and semi-reflective lenses 110, so that the circumference of each polygonal semi-transparent and semi-reflective lens 110 is respectively matched, snapped or bonded to the corresponding position of the polygonal frame 311; the filament 120 is respectively embedded in each polygonal frame 311, thereby better realizing the assembly of the polyhedron 20 on the support frame 210.

[0032] The support frame 210 may be opaque, but is preferably transparent or translucent, so that the perspective effect of the filament 120 is increased after being lit.

[0033] In this embodiment, a base 10 is provided at the lower end of the polyhedron 20 , and the base 10 is used to support the polyhedron 20 to form the space atmosphere lamp. The control component is placed in the base 10 to control the lighting of the filament 120 embedded on the edge of the polyhedron 20 .

[0034] In this embodiment, a support portion 11 which is lifted upward and connected to the lower end of the polyhedron 20 is disposed at the upper end of the base 10 .

[0035] In this embodiment, the support portion 11 is a threaded column arranged on the upper end surface of the base 10, and one of the multiple polygonal surrounding frames 311 is provided with a connecting portion 312 that is threadably matched with the threaded column, thereby preferably realizing a detachable connection of the support frame 210 on the base 10, and at the same time, being able to ensure the connection strength between the two, so that the base 10 supports the polyhedron 20;

[0036] Of course, any polygonal frame 311 in the support frame 210 is overlapped at the upper end of the support portion 11, and the support frame 210 can also be placed on the base 10 so that the base 10 supports the polyhedron 20;

[0037] It should be noted that when the support frame 210 is placed on the base 10 , the polygonal frame 311 that matches the base 10 may not be provided with the polygonal semi-transparent and semi-reflective lens 110 and the filament 120 , so as to facilitate the placement of the polyhedron 20 on the base 10 .

[0038] In this embodiment, the control component includes a power driver, a power supply and a switch arranged in the base 10, and a circuit is formed between the power driver, the power supply, the switch and the filament 120; the power supply is a lithium battery built into the base 10 or an external DC power supply; the switch is set on the base 10.

[0039] Through the above structure, this embodiment allows the user to turn the space atmosphere light on and off by simply using a switch, making it easy to use.

[0040] In actual use, if the present embodiment Figure 4 As shown, a mounting cavity 411 opening downward is provided in the base 10 , and the opening of the mounting cavity 411 is connected to the bottom cover 130 . The control component is disposed in the mounting cavity 411 and is located on the upper side of the bottom cover 130 .

[0041] In this embodiment, the bottom cover 130 is connected to the opening of the installation cavity 411 by threads, and is used to block the installation cavity 411, thereby preferably realizing the opening and closing of the installation cavity 411, and facilitating the inspection and maintenance of the control component;

[0042] In actual use, in order to dissipate the heat of the control components installed in the base 10, the outer wall of the base 10 is relatively provided with a ventilation groove 412 connected to the installation cavity 411. The ventilation groove 412 facilitates the air circulation between the installation cavity 411 and the outside, thereby dissipating the heat of the control components installed therein.

[0043] In actual use, in order to improve the stability of the placement of the space atmosphere lamp, a counterweight ring is fixedly connected in the installation cavity 411 or on the bottom cover 130, thereby increasing the counterweight of the base 10 and making it more stable to support the polyhedron 20;

[0044] The lower side of the bottom cover 130 is concave to form a recessed cavity 421, and the weight ring can be threadedly connected in the recessed cavity 421 to install the weight ring;

[0045] It should be pointed out that the counterweight ring can also be threadedly connected to the installation cavity 411 to achieve fixation of the counterweight ring in the installation cavity 411.

[0046] In this embodiment, the filament 120 is an LED ceramic filament or an LED flexible filament.

[0047] In this embodiment, refer to Figure 5 The filaments 120 include a substrate 01, a plurality of light-emitting chips 02 and a light-transmitting adhesive layer 03. Each light-emitting chip 02 is laid along the length direction of the front side of the substrate 01 and each light-emitting chip 02 is connected in series, in parallel or in series and in parallel through a guide wire or a printed circuit on the substrate 01. The front and back sides of the substrate 01 are covered with a light-transmitting adhesive layer 03, and the light-transmitting adhesive layer 03 on the front side covers each light-emitting chip 02 in a row. The two extreme ends of the light source module formed by connecting a plurality of light-emitting chips 02 in series, in parallel or in series and in parallel are electrically connected to pins 04, and the two pins 04 are connected to the two ends of the substrate 01. Each filament 120 is connected in series and in parallel through pins 04 and conductive cables.

[0048] The space atmosphere lamp in this embodiment is achieved by installing a polygonal translucent and semi-reflective lens 110 on a corresponding polygonal frame 311 of a supporting frame 210, and embedding a filament 120 at the joint of the polygonal translucent and semi-reflective lens 110. The polygonal translucent and semi-reflective lens 110 is used to reflect and project the lit filament 120, so that a user can see the reflection and double images of multiple lit filaments 120 when looking through any polygonal translucent and semi-reflective lens 110. As a result, the space atmosphere lamp visually presents a stronger sense of design and space.

[0049] Another embodiment, referring to Figure 6 A lamp holder 100 is provided at the lower end of the polyhedron 20, and a control component is placed in the lamp holder 100, and the control component is a power driver. The filaments 120 are connected in series, parallel, or series-parallel and then connected to the lamp holder 100 through the power driver, so that the lamp can be directly screwed into the screw lamp holder through the lamp holder 100, and the filaments 120 on the lamp can be lit by supplying power to the screw lamp holder.

Claims

1. A space atmosphere lamp, characterized in that: It comprises a control component and a polyhedron (20) formed by splicing a plurality of polygonal semi-transparent and semi-reflective lenses (110), the control component being arranged outside the polyhedron (20), filaments (120) being respectively embedded between the spliced ​​polygonal semi-transparent and semi-reflective lenses (110), and each filament (120) being electrically connected to the control component.

2. A space atmosphere lamp according to claim 1, characterized in that: It also includes a support frame (210), the support frame (210) is formed with a plurality of polygonal surrounding frames (311), the peripheral sides of each polygonal semi-transparent and semi-reflective lens (110) are matched, snap-fitted or bonded in a corresponding position of the polygonal surrounding frame (311); the filament (120) is respectively embedded in each polygonal surrounding frame (311).

3. The space atmosphere lamp according to claim 1, characterized in that: A base (10) is provided at the lower end of the polyhedron (20), and the control component is placed in the base (10).

4. A space atmosphere lamp according to claim 3, characterized in that: The upper end of the base (10) is provided with a support portion (11) which is lifted upward and connected to the lower end of the polyhedron (20).

5. The space atmosphere lamp according to claim 3, characterized in that: The control component comprises a power driver, a power source and a switch arranged in the base (10), wherein a circuit is formed between the power driver, the power source, the switch and the filament (120); the power source is a lithium battery built into the base (10) or an external direct current power source; and the switch is arranged on the base (10).

6. The space atmosphere lamp according to claim 1, characterized in that: The filament (120) is an LED ceramic filament or an LED flexible filament.

7. A space atmosphere lamp according to claim 1 or 6, characterized in that: The filament (120) comprises a substrate (01), a plurality of light-emitting chips (02) and a light-transmitting adhesive layer (03); the light-emitting chips (02) are laid along the length direction of the front surface of the substrate (01), and the light-emitting chips (02) are connected in series, in parallel or in series and in parallel; the front and back surfaces of the substrate (01) are covered with a light-transmitting adhesive layer (03), and the light-transmitting adhesive layer (03) on the front surface covers the light-emitting chips (02) in a row.

8. The space atmosphere lamp according to claim 3, characterized in that: A mounting cavity (411) opening downward is provided in the base (10); the opening of the mounting cavity (411) is connected to a bottom cover (130); and the control component is arranged in the mounting cavity (411) and is located on the upper side of the bottom cover (130).

9. The space atmosphere lamp according to claim 8, characterized in that: A counterweight ring is fixedly connected in the installation cavity (411) or on the bottom cover (130).

10. The space atmosphere lamp according to claim 1, characterized in that: A lamp holder (100) is provided at the lower end of the polyhedron (20), a control component is disposed in the lamp holder (100), and the control component is a power driver. The filaments (120) are connected in series, in parallel, or in series and in parallel and then electrically connected to the lamp holder (100) via the power driver.

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