Aviation lamp support

Abstract

The utility model provides an aviation lamp support, and belongs to the technical field of building construction. The aviation lamp support comprises a mounting base, a supporting rod piece and a connecting base. The connecting base is detachably mounted on the vertical keel, the supporting rod piece is detachably mounted on the connecting base, the mounting base is arranged at the top end of the supporting rod piece, and the aviation lamp is detachably arranged at the top end of the mounting base. The aviation lamp support is simple in structure, high in strength, attractive and light, and the aviation lamp is convenient to disassemble and assemble.

Description

Technical Field

[0001] This disclosure relates to the field of building construction technology, and in particular to an aviation light bracket. Background Technology

[0002] Existing aviation light brackets have large member dimensions, and most are installed by directly drilling holes in the main concrete structure. However, when the building facade is a full glass curtain wall, the vertical keel width of the glass curtain wall is small, making it difficult to drill holes for conventional brackets, resulting in inconvenient installation of aviation lights and poor aesthetics.

[0003] To solve the above problems, an aviation light bracket was designed. Utility Model Content

[0004] The purpose of this disclosure is to overcome the shortcomings of the prior art and provide an aviation light bracket that facilitates the installation and removal of aviation lights and improves the aesthetics of the aviation light bracket installation.

[0005] To achieve the aforementioned objectives of this utility model, the present disclosure adopts the following technical solution:

[0006] An aviation light bracket includes a mounting base, a support rod, and a connecting base;

[0007] The connecting base is detachably installed on the vertical keel, the support rod is detachably installed on the connecting base, the mounting base is located at the top of the support rod, and an aviation light is detachably installed at the top of the mounting base.

[0008] In one exemplary embodiment of this disclosure, the mounting base has at least one first bolt hole, and the mounting base is connected to the aviation light by bolts.

[0009] In one exemplary embodiment of this disclosure, the support rod includes a first support rod;

[0010] One end of the first support rod is detachably connected to the connecting base, and at least one second support rod is provided at the other end of the first support rod. The second support rod is perpendicular to the first support rod, and the mounting base is fixedly connected to the top of the second support rod.

[0011] In one exemplary embodiment of this disclosure, the connecting base includes a fixing part and a connecting part;

[0012] The fixing part is provided with at least one second bolt hole, and the fixing part is connected to the vertical keel by bolts;

[0013] The connecting part is disposed on the side wall of the fixing part away from the vertical keel, and the connecting part is detachably connected to the first support rod.

[0014] In one exemplary embodiment of this disclosure, the connecting portion is threadedly connected to the first support rod.

[0015] In one exemplary embodiment of this disclosure, a through hole is provided on the circumferential sidewall of the connecting part, and an anti-loosening nut is installed in the internal thread of the through hole.

[0016] In one exemplary embodiment of this disclosure, the width of the fixing part is less than or equal to the inner space of the cover of the vertical keel.

[0017] In one exemplary embodiment of this disclosure, the support rod is made of lightweight, high-strength metal.

[0018] The beneficial effects of this disclosure are:

[0019] This disclosure provides an aviation light bracket. The aviation light is bolted onto a mounting base, which is fixedly mounted onto a support rod. The support rod is threaded onto a connecting base and further secured with an anti-loosening nut. The connecting base is bolted onto the vertical keel of the glass curtain wall. The structure is simple, the bracket has high overall strength, is not easily deformed, and the aviation light is easy to install, disassemble, and maintain. The connecting base is located inside the cover of the vertical keel of the glass curtain wall, improving the overall aesthetics of the aviation light bracket. Attached Figure Description

[0020] The accompanying drawings, which are incorporated in and form part of this specification, illustrate embodiments consistent with this disclosure and, together with the description, serve to explain the principles of this disclosure. It is obvious that the drawings described below are merely some embodiments of this disclosure, and those skilled in the art can obtain other drawings based on these drawings without any inventive effort.

[0021] Figure 1 This is a schematic diagram of the installation of an aviation light bracket in one embodiment of the present disclosure;

[0022] Figure 2 This is a schematic diagram of the structure of an aviation light bracket in one embodiment of the present disclosure;

[0023] Figure 3 This is a schematic diagram of the structure of the mounting base in one embodiment of the present disclosure;

[0024] Figure 4 This is a schematic diagram of the structure of the support rod in one embodiment of the present disclosure;

[0025] Figure 5 This is a schematic diagram of the structure of the connecting base in one embodiment of the present disclosure. Figure 1 ;

[0026] Figure 6This is a schematic diagram of the structure of the connecting base in one embodiment of the present disclosure. Figure 2 .

[0027] Explanation of reference numerals in the attached figures:

[0028] 1. Mounting base; 2. Support rod; 3. Connecting base; 4. Vertical keel; 5. First bolt hole; 6. First support rod; 7. Second support rod; 8. Fixing part; 9. Connecting part; 10. Second bolt hole; 11. Anti-loosening nut. Detailed Implementation

[0029] Exemplary embodiments will now be described more fully with reference to the accompanying drawings. However, these exemplary embodiments can be implemented in many forms and should not be construed as limited to the embodiments set forth herein; rather, they are provided so that this disclosure will be thorough and complete, and will fully convey the concept of the exemplary embodiments to those skilled in the art. The same reference numerals in the drawings denote the same or similar structures, and therefore detailed descriptions of them will be omitted. Furthermore, the drawings are merely illustrative of this disclosure and are not necessarily drawn to scale.

[0030] Although relative terms such as "up" and "down" are used in this specification to describe the relative relationship of one component of an icon to another, these terms are used only for convenience, such as according to the orientation of the examples shown in the accompanying drawings. It is understood that if the device of the icon is flipped upside down, the component described as "up" will become the component described as "down." When a structure is "up" of another structure, it may mean that the structure is integrally formed on the other structure, or that the structure is "directly" mounted on the other structure, or that the structure is "indirectly" mounted on the other structure through another structure.

[0031] The terms “a,” “one,” “the,” “the,” and “at least one” are used to indicate the presence of one or more elements / components / etc.; the terms “including” and “having” are used to indicate an open-ended inclusion and to mean that there may be other elements / components / etc. in addition to the listed elements / components / etc.; the terms “first,” “second,” and “third,” etc., are used only as markers and are not a limitation on the number of objects.

[0032] This disclosure provides an aviation light bracket, see [link / reference] Figure 1 and Figure 2 It includes a mounting base 1, a support rod 2, and a connecting base 3; the connecting base 3 is detachably mounted on the vertical keel 4, the support rod 2 is detachably mounted on the connecting base 3, the mounting base 1 is located at the top of the support rod 2, and an aviation light is detachably mounted at the top of the mounting base 1.

[0033] In this embodiment, the aviation light bracket consists of a mounting base 1, a support rod 2, and a connecting base 3. The connecting base 3 is detachably mounted on the vertical keel 4 of the glass curtain wall, the support rod 2 is detachably mounted on the connecting base 3, the mounting base 1 is fixedly mounted on the support rod 2, and the aviation light is detachably mounted on the top of the mounting base 1.

[0034] Compared to the existing method of installing by drilling holes in the main concrete structure, this aviation light bracket has a simple structure, high overall strength, is not easily deformed, and is convenient for the installation, disassembly and maintenance of aviation lights, thus improving the overall aesthetics of the aviation light bracket.

[0035] In one embodiment of this disclosure, see [link to relevant documentation]. Figures 1 to 3 The mounting base 1 has at least one first bolt hole 5, and the mounting base 1 is connected to the aviation light by bolts. This allows for quick installation and removal of the aviation light, improving the efficiency of its installation and replacement.

[0036] Optionally, the first bolt hole 5 is circular in shape.

[0037] In one example, there are four first bolt holes 5, which are located on the diagonal lines of the four corners of the mounting base 1.

[0038] In one embodiment of this disclosure, see [link to relevant documentation]. Figure 1 , Figure 2 and Figure 4 The support rod 2 includes a first support rod 6; one end of the first support rod 6 is detachably connected to the connecting base 3, and the other end of the first support rod 6 is provided with at least one second support rod 7, which is perpendicular to the first support rod 6. The mounting base 1 is fixedly connected to the top of the second support rod 7. In this way, the strength of the support rod 2 can be improved, making it easier to install the aviation light on the mounting base 1 and preventing deformation after the aviation light is installed.

[0039] Optionally, the mounting base 1 is welded to the second support rod 7.

[0040] In one example, there are two second support rods 7, which are spaced apart on the first support rod 6, and the mounting base 1 is welded to the top of the two second support rods 7.

[0041] In one embodiment of this disclosure, see [link to relevant documentation]. Figure 1 , Figure 5 and Figure 6The connecting base 3 includes a fixing part 8 and a connecting part 9. The fixing part 8 has at least one second bolt hole 10, and is connected to the vertical keel 4 by bolts. The connecting part 9 is located on the side wall of the fixing part 8 away from the vertical keel 4, and is detachably connected to the first support rod 6. This allows for quick assembly and disassembly of the connecting base 3 and the vertical keel 4, thereby improving the installation efficiency of the aviation light.

[0042] Optionally, the connecting part 9 is threadedly connected to the first support rod 6. This allows for quick assembly and disassembly of the mounting base 1 and the support rod 2, facilitating subsequent maintenance and disassembly of the entire bracket.

[0043] Optionally, the second bolt hole 10 is circular in shape, and the connecting part 9 is cylindrical in shape.

[0044] Optionally, the vertical keel 4 is provided with a through hole or through groove corresponding to the second bolt hole 10.

[0045] Optionally, the vertical keel 4 is provided with bolts corresponding to the second bolt holes 10.

[0046] In one example, the connecting part 9 is located in the middle of the fixing part 8, and there are four second bolt holes 10, which are symmetrically distributed on both sides of the connecting part 9.

[0047] In one embodiment of this disclosure, see [link to relevant documentation]. Figure 1 , Figure 5 and Figure 6 The connecting part 9 has a through hole on its circumferential side wall, and an anti-loosening nut 11 is installed in the threaded part of the through hole. In this way, the first support rod 6 can be fixed, improving the firmness of the connection between the connecting part 9 and the first support rod 6, preventing the support rod 2 from deflecting, and thus preventing the position of the aviation light from changing.

[0048] In one embodiment of this disclosure, see [link to relevant documentation]. Figure 1 The width of the fixing part 8 is less than or equal to the inner space of the cover of the vertical keel 4. In this way, the fixing part 8 can be installed inside the cover of the vertical keel 4 of the glass curtain wall, improving the aesthetics of the aviation light bracket and the glass curtain wall.

[0049] In one embodiment of this disclosure, see [link to relevant documentation]. Figure 1 The support rod 2 is made of lightweight, high-strength metal. This improves both the strength and lightness of the support rod 2, facilitating the installation of the aviation light bracket.

[0050] In one example, the support rod 2 is made of aluminum alloy.

[0051] In one embodiment of this disclosure, see [link to relevant documentation]. Figures 1 to 6The fixing part 8 is parallel to the vertical keel 4. The fixing part 8 is vertically installed on the vertical keel 4 by bolts. The connecting part 9 is horizontally connected to the middle of the fixing part 8. The first support rod 6 is coaxially threaded to the connecting part 9. Two second support rods 7 are spaced apart at the top of the first support rod 6. The second support rods 7 are perpendicular to the first support rod 6. The mounting base 1 is horizontally welded to the top of the two second support rods 7.

[0052] In one embodiment of this disclosure, see Figures 1 to 6 The working process of this aviation light bracket is briefly described as follows:

[0053] In use, the fixing part 8 is first installed on the inside of the cover of the vertical keel 4 with bolts. Then, the mounting base 1 is welded to the top of the second support rod 7. The first support rod 6 is threaded onto the connecting part 9 so that the second support rod 7 is in a vertical state. The anti-loosening nut 11 is screwed onto the connecting part 9 to fix the first support rod 6 and ensure that the second support rod 7 is in a vertical state. Finally, the aviation light is installed on the top of the mounting base 1 with bolts.

[0054] Other embodiments of this disclosure will readily occur to those skilled in the art upon consideration of the specification and practice of the utility models disclosed herein. This application is intended to cover any variations, uses, or adaptations of this disclosure that follow the general principles of this disclosure and include common knowledge or customary techniques in the art not disclosed herein. The specification and examples are to be considered exemplary only, and the true scope and spirit of this disclosure are indicated by the appended claims.

Claims

1. An aviation light bracket, characterized in that, It includes a mounting base (1), a support rod (2), and a connecting base (3); The connecting base (3) is detachably installed on the vertical keel (4). The supporting rod (2) includes a first support rod (6). One end of the first support rod (6) is detachably connected to the connecting base (3). At least one second support rod (7) is provided at the other end of the first support rod (6). The second support rod (7) is perpendicular to the first support rod (6). The mounting base (1) is located at the top of the second support rod (7). An aviation light is detachably provided at the top of the mounting base (1).

2. The aviation light bracket according to claim 1, characterized in that, The mounting base (1) has at least one first bolt hole (5), and the mounting base (1) is connected to the aviation light by bolts.

3. The aviation light bracket according to claim 1, characterized in that, The connecting base (3) includes a fixing part (8) and a connecting part (9); The fixing part (8) is provided with at least one second bolt hole (10), and the fixing part (8) is connected to the vertical keel (4) by bolts; The connecting part (9) is disposed on the side wall of the fixing part (8) away from the vertical keel (4), and the connecting part (9) is detachably connected to the first support rod (6).

4. The aviation light bracket according to claim 3, characterized in that, The connecting part (9) is threadedly connected to the first support rod (6).

5. The aviation light bracket according to claim 3, characterized in that, The connecting part (9) has a through hole on its circumferential side wall, and an anti-loosening nut (11) is installed in the through hole by an internal thread.

6. The aviation light bracket according to claim 3, characterized in that, The width of the fixing part (8) is less than or equal to the inner space of the cover of the vertical keel (4).

7. The aviation light bracket according to claim 1, characterized in that, The support rod (2) is made of aluminum alloy.

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