CN218846018U

CN218846018U - Socket type aviation obstruction light installation device

Info

Publication number: CN218846018U
Application number: CN202320168529.9U
Authority: CN
Inventors: 万修强; 王小龙; 孙勇; 徐丹阳; 吴迪; 史永明; 陈金华
Original assignee: China Construction Eighth Engineering Division Decoration Engineering Co Ltd
Current assignee: China Construction Eighth Engineering Division Decoration Engineering Co Ltd
Priority date: 2023-02-09
Filing date: 2023-02-09
Publication date: 2023-04-11
Anticipated expiration: 2033-02-09

Abstract

The utility model relates to the technical field of aviation obstruction light installation, in particular to a socket type aviation obstruction light installation device, which comprises a base end and a bolt end, wherein the base end and the bolt end are both in tubular structures and also comprises; the locking device comprises a base end, a plurality of locking components and a plurality of locking components, wherein the locking components are arranged between the inner wall of the base end and a bolt end, the locking components are distributed at equal intervals in the vertical direction, each locking component comprises an annular sinking groove and two installation cavities, the annular sinking groove is formed in the circumferential inner wall of the base end, the installation cavities are formed in the circumferential outer wall of the bolt end, the two adjacent installation cavities are symmetrically distributed around the bolt end, and one side inner wall of each installation cavity is fixedly connected with a tensioning spring; the utility model discloses a set up the hasp subassembly into a plurality ofly, can adjust the grafting length that bolt end and base held to conveniently adjust follow-up mounting platform's vertical height, and be favorable to improving the installation and the change efficiency of aviation obstruction light.

Description

Socket type aviation obstruction light installation device

Technical Field

The utility model relates to an aviation obstruction light installation technical field specifically is a socket joint formula aviation obstruction light installation device.

Background

The aviation obstruction light is a special lamp for marking an obstruction and belongs to the industry of the aviation obstruction light, and the aviation obstruction light is a light range under the seat of the aviation obstruction light.

In the prior art, the following problems exist:

traditional aviation obstruction beacon base mounting means adopts the mode of welding or bolt, wholly exposes outside parapet or other structure positions, and installation procedure is loaded down with trivial details, changes the difficulty, and the impression effect is relatively poor.

For strengthening the whole impression effect of the exterior finish, improve aviation obstruction light installation and change efficiency, a socket type aviation obstruction light installation device is specially developed, and the problem existing in the traditional installation mode is avoided.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a socket joint formula aviation obstruction beacon installation device to solve the problem that proposes in the above-mentioned background art.

The technical scheme of the utility model is that: a socket type aviation obstruction light installation device comprises a base end and a bolt end, wherein the base end and the bolt end are both in tubular structures;

the locking assembly is arranged between the inner wall of the base end and the bolt end, the locking assemblies are distributed equidistantly in the vertical direction, each locking assembly comprises an annular sinking groove and two installation cavities, the annular sinking groove is formed in the inner wall of the circumference of the base end, the installation cavities are formed in the outer wall of the circumference of the bolt end, the two adjacent installation cavities are symmetrically distributed about the bolt end, each installation cavity is fixedly connected with a tensioning spring on the inner wall of one side of the installation cavity, and the end part of the tensioning spring is fixedly connected with a hemispherical convex block.

Preferably, the outer diameter of the pin end and the inner diameter of the base end are matched with each other.

Preferably, a mounting platform is fixed to the top of the bolt end.

Preferably, the base end is fixedly connected with a base plate at the bottom end.

Preferably, a plurality of reinforcing rib pieces are fixedly connected between the mounting platform and the bolt end and between the base plate and the base end.

Preferably, the reinforcing rib pieces are in a triangular structure.

The utility model discloses an improve and provide a socket joint formula aviation obstruction beacon installation device here, compare with prior art, have following improvement and advantage:

one is as follows: the utility model can adjust the inserting length of the bolt end and the base end by arranging a plurality of lock catch components, thereby adjusting the vertical height of the subsequent mounting platform and being beneficial to improving the mounting and replacing efficiency of the aviation obstruction light;

and the second step is as follows: the utility model discloses can avoid wholly exposing at outdoor face, be favorable to strengthening the holistic impression effect of exterior finish.

Drawings

The invention is further explained below with reference to the drawings and examples:

FIG. 1 is a schematic sectional view of the whole structure of the present invention;

fig. 2 is a schematic perspective view of the latch end and the base end of the present invention;

fig. 3 is a schematic cross-sectional view of the latch assembly of the present invention.

Description of the reference numerals:

1. a plug end; 11. mounting a platform; 2. a latch assembly; 21. a hemispherical convex block; 22. an annular sinking groove; 23. a mounting cavity; 24. tensioning the spring; 3. a base end; 31. a base plate; 4. reinforcing rib pieces.

Detailed Description

The present invention will be described in detail below, and it is apparent that the technical solutions in the embodiments of the present invention are described clearly and completely. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts all belong to the protection scope of the present invention.

The utility model discloses an improve and provide a socket joint formula aviation obstruction beacon installation device here, the technical scheme of the utility model is:

as shown in fig. 1-3, a socket type aviation obstruction light mounting device comprises a base end 3 and a plug end 1, wherein both the base end 3 and the plug end 1 are tubular structures, and the socket type aviation obstruction light mounting device also comprises;

a plurality of hasp subassemblies 2, a plurality of hasp subassemblies 2 set up between 3 inner walls of base end and bolt end 1, and a plurality of hasp subassemblies 2 are the equidistance and distribute in vertical direction, every hasp subassembly 2 all includes an annular heavy groove 22 and two

installation cavities

23, 3 circumference inner walls of base end are seted up to annular heavy groove 22, the circumference outer wall of bolt end 1 is seted up to installation cavity 23, and two adjacent installation cavities 23 are about bolt end 1 symmetric distribution, the equal fixedly connected with tensioning spring 24 of one side inner wall of every installation cavity 23, and the equal fixedly connected with hemisphere face lug 21 of tip of tensioning spring 24.

Through the structure, the plurality of locking components 2 are used for locking the bolt end 1 and the base end 3 mutually, and the specific operation steps are that the bolt end 1 is inserted into the base end 3, firstly, the hemispherical convex block 21 is drawn back into the installation cavity 23 under the extrusion force, and when the installation cavity 23 is aligned with the annular sunken groove 22, the hemispherical convex block 21 can be popped out under the action of the tensioning spring 24, so that the hemispherical convex block 21 and the annular sunken groove 22 are clamped mutually, and the bolt end 1 is fixed; through setting up hasp subassembly 2 into a plurality ofly, can adjust the grafting length of bolt end 1 and base end 3 to adjust follow-up mounting platform 11's vertical height, and be favorable to improving aviation obstruction beacon's installation and change efficiency.

As a further proposal of the utility model, the outer diameter of the bolt end 1 is matched with the inner diameter of the base end 3; through the above arrangement, the stable insertion of the plug pin end 1 into the base end 3 can be ensured.

Further, a mounting platform 11 is fixed at the top of the bolt end 1; the mounting platform 11 is used for mounting the barrier lamp.

Further, the bottom end of the base end 3 is fixedly connected with a base plate 31; the base plate 31 is used for fixing with the ground.

As a further scheme of the utility model, equal a plurality of strengthening rib pieces of fixedly connected with 4 between mounting platform 11 and the bolt end 1 and between bed plate 31 and the base end 3.

Furthermore, the reinforcing rib pieces 4 are in a triangular structure; through the strengthening rib piece 4 that sets up, can effectively improve mounting platform 11 and bed plate 31 fixed connection's stability.

The specific working method comprises the following steps:

s1, determining an installation position: the selection of the position of the aviation obstruction light must be capable of marking the overall outline of the obstruction, and no obstruction is required to cause invisible obstruction to the lamp at the installation place;

s2, arranging a line pipe: arranging a line pipe not less than phi 25 according to the number of required wires;

s3, threading a lead: the wiring of the conducting wires is required to arrange barrier lamp cables according to a circuit diagram;

s4, fixing the base end 3: the bottom of the base plate 31 below the base end 3 is fixed by screws, and an annular sinking groove 22 needs to be reserved in the base end 3 during processing;

s5, installing a bolt end 1; the specific operation steps are that the bolt end 1 is inserted into the base end 3, at first, the hemispherical convex block 21 is retracted into the installation cavity 23 under the extrusion force, when the installation cavity 23 is aligned with the annular sunken groove 22, the hemispherical convex block 21 can be popped out under the action of the tension spring 24, so that the hemispherical convex block 21 and the annular sunken groove 22 are mutually clamped;

s6, lamp installation and debugging: and after the power is switched on, testing whether the function of the barrier lamp is effective and reliable.

Claims

1. The utility model provides a socket joint formula aviation obstruction beacon installation device, includes base end (3) and bolt end (1), base end (3) and bolt end (1) all are tubular structure, its characterized in that: also includes;

a plurality of hasp subassemblies (2), it is a plurality of hasp subassemblies (2) set up between base end (3) inner wall and bolt end (1), and a plurality of hasp subassemblies (2) are equidistance distribution in vertical direction, every hasp subassembly (2) all include that an annular sinks groove (22) and two installation cavity (23), and the annular sinks groove (22) and sets up in base end (3) circumference inner wall, the circumference outer wall of bolt end (1) is seted up in installation cavity (23), and two adjacent installation cavity (23) about bolt end (1) symmetric distribution, every the equal fixedly connected with tensioning spring (24) of one side inner wall of installation cavity (23), and the equal fixedly connected with hemisphere face lug (21) of tip of tensioning spring (24).

2. A socket type aviation obstruction light mounting device according to claim 1, wherein: the outer diameter of the bolt end (1) is matched with the inner diameter of the base end (3).

3. A socket type aviation obstruction light mounting device according to claim 1, wherein: and a mounting platform (11) is fixed at the top of the bolt end (1).

4. A socket type aviation obstruction light mounting device according to claim 3, wherein: the bottom end of the base end (3) is fixedly connected with a base plate (31).

5. The socket type aviation obstruction light mounting device of claim 4, wherein: a plurality of strengthening rib pieces (4) are fixedly connected between the installation platform (11) and the bolt end (1) and between the base plate (31) and the base end (3).

6. A socket type aviation obstruction light mounting device according to claim 5, wherein: the reinforcing rib pieces (4) are of triangular structures.