CN218762838U

CN218762838U - Combined LED aviation obstruction beacon

Info

Publication number: CN218762838U
Application number: CN202222615417.1U
Authority: CN
Inventors: 孔一腾
Original assignee: Suzhou Pastoral Robot Co ltd
Current assignee: Chengdu Hanghuan Technology Co ltd
Priority date: 2022-10-02
Filing date: 2022-10-02
Publication date: 2023-03-28
Anticipated expiration: 2032-10-02

Abstract

The utility model relates to an aviation obstruction beacon technical field, concretely designs a modular LED aviation obstruction beacon, its technical scheme is: including lamp shade and mount pad, install quick installation dismounting device at the inner wall of lamp shade and the top of mount pad, the beneficial effects of the utility model are that: through installing the mount pad, the fixed column, a spacing groove, the hypotenuse piece, no. two spacing grooves, the dead lever, the button, the function of quick installation dismantlement has been realized to the stopper, press the button, make the bottom of button push the hypotenuse piece into a spacing inslot, the hypotenuse piece is shifted out from the recess of lamp shade, the lamp shade can be taken out, when the installation, the fixed column gets into in the lamp shade, the hypotenuse piece gets into a spacing inslot with the inner wall contact of the spout of lamp shade in the hypotenuse piece, when reacing the bottom recess, the hypotenuse piece breaks away from the contact with the inner wall of spout, a spring reset extension drives the hypotenuse piece and removes in getting into the recess, thereby the function of quick installation dismantlement has been realized.

Description

Combined LED aviation obstruction beacon

Technical Field

The utility model relates to an aviation obstruction beacon technical field, concretely relates to modular LED aviation obstruction beacon.

Background

The aviation obstruction light is a special lamp for marking obstacles, belongs to the industry of the aviation obstruction light, and is a range of lamp types under the seat of the aviation obstruction light. In order to distinguish from the illuminating lamp for general use, the aviation obstruction light is not normally on but is flashing, the low-light-intensity aviation obstruction light is normally on, and the medium-light-intensity aviation obstruction light and the high-light-intensity aviation obstruction light are flashing. The aviation obstruction light is used for displaying the outline of a structure, so that an aircraft operator can judge the height and the outline of the obstruction, and the warning effect is achieved. With the development of the LED technology, the LED lamp is gradually applied to the LED aviation obstruction light as a light source.

The prior art has the following defects: the main body part of the existing LED aviation obstruction light is generally installed on an I-shaped installation seat through screws, the installation seat is fixed at the top end of a building through bolts, and the main body part of the LED aviation obstruction light is installed on the installation seat through the screws and installed at the top end of the building, so that the LED aviation obstruction light is troublesome to assemble and disassemble, and when the LED aviation obstruction light is replaced, the bolts are easily lost, and the replacement efficiency of the LED aviation obstruction light is influenced.

Therefore, the invention is necessary to invent a combined LED aviation obstruction light.

SUMMERY OF THE UTILITY MODEL

Therefore, the utility model provides a modular LED aviation obstruction beacon, through pressing the button, the stopper of button area both sides removes along the dead lever No. two spacing inslots, and No. two spring atress shrink for the bottom of button pushes the hypotenuse piece No. one spacing inslot, and a spring atress shrink makes the hypotenuse piece shifted out from the recess of lamp shade, and the lamp shade can be taken out, with the problem of solving inconvenient dismantlement.

In order to achieve the above object, the present invention provides the following technical solutions: the utility model provides a modular LED aviation obstruction beacon, includes lamp shade and mount pad, the inner wall fixed mounting of lamp shade has the fixed plate, LED banks spare is installed at the top of fixed plate, quick installation dismounting device is installed at the inner wall of lamp shade and the top of mount pad.

Preferably, quick installation dismounting device includes the fixed column, the fixed column is installed to the top symmetry of mount pad, a spacing groove has been seted up to the inner wall of fixed column, a spring is installed to the inner wall of a spacing groove, the hypotenuse piece is installed to the one end of a spring, and hypotenuse piece and fixed column sliding connection.

Preferably, install dismounting device fast includes No. two spacing grooves, no. two spacing grooves are installed to the inner wall symmetry of lamp shade, the inner wall fixed mounting of No. two spacing grooves has the dead lever, no. two springs are installed to the outer wall of dead lever.

Preferably, the button is installed to the outer wall of lamp shade, the stopper is installed to the outer wall symmetry of button.

Preferably, T type piece is installed to the inner wall symmetry of lamp shade, and T type piece has four, T type groove has been seted up to the outer wall symmetry of mount pad, T type groove has four, and the position corresponds with T type piece.

Preferably, the fan is installed to the inner wall of mount pad, the filter screen is installed at the top of mount pad, the air-out pipeline has been seted up to the inner wall of mount pad, and the dust screen is installed to the one end of air-out pipeline.

Preferably, the bottom fixed mounting of mount pad has the connecting plate, the screwed pipe has been seted up to the inner wall symmetry of connecting plate, the nut is installed to the inner wall of screwed pipe, and nut and screwed pipe meshing.

The beneficial effects of the utility model are that:

1. the utility model discloses an install the mount pad, the fixed column, a spacing groove, the sloping piece, no. two spacing grooves, the dead lever, a button, the stopper has realized quick installation dismantlement function, when needs are dismantled, press the button, the stopper of button area both sides moves along the dead lever in No. two spacing grooves, no. two spring atress shrink, make the bottom of button push the sloping piece into No. one spacing groove, no. one spring atress shrink, make the sloping piece shift out from the recess of lamp shade, the lamp shade can be taken out, thereby can maintain and change the aviation obstruction light, when the installation, insert T type piece in T type groove, move down along T type groove, the fixed column gets into the lamp shade, the sloping of sloping piece and the inner wall contact of the spout of lamp shade make the sloping piece enter into No. one spacing groove, no. one spring atress shrink, when arriving bottom recess, the sloping piece breaks away from the contact with the inner wall of spout, a spring reset extension drives the sloping piece and moves into the recess, thereby make the lamp shade and mount pad be connected fixedly, thereby the function of quick installation dismantlement has been realized;

2. the utility model discloses an install fan, filter screen, air-out pipeline, dust screen and realized having started the radiating function of aviation obstruction light, the fan blows off inside heat through the air-out pipeline, and dust screen and filter screen can prevent that internals from receiving the damage of dust to the radiating function of aviation obstruction light has been realized.

Drawings

Fig. 1 is a schematic front structural view provided by the present invention;

fig. 2 is a schematic top view of the present invention;

fig. 3 is a schematic diagram of an enlarged partial structure at a in fig. 1 according to the present invention;

fig. 4 is a schematic diagram of an enlarged partial structure at B of fig. 1 according to the present invention;

fig. 5 is a schematic diagram of an enlarged partial structure at C of fig. 1 according to the present invention.

In the figure: 1. a lamp shade; 101. a fixing plate; 102. an LED lamp assembly; 2. a mounting seat; 201. fixing a column; 202. a first limit groove; 203. a first spring; 204. a bevel edge block; 3. a second limiting groove; 301. fixing the rod; 302. a second spring; 4. a button; 401. a limiting block; 5. a T-shaped block; 501. a T-shaped groove; 6. a fan; 601. filtering with a screen; 602. an air outlet pipeline; 603. a dust screen; 7. a connecting plate; 701. a threaded pipe; 702. And a nut.

Detailed Description

The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are presented herein only to illustrate and explain the present invention, and not to limit the present invention.

Referring to the attached drawings 1-5, the utility model provides a combined LED aviation obstruction beacon, including a lampshade 1 and a mounting seat 2, a fixed plate 101 is fixedly installed on the inner wall of the lampshade 1, an LED lamp assembly 102 is installed on the top of the fixed plate 101, a fixed column 201 is symmetrically installed on the top of the mounting seat 2, a first limit groove 202 is opened on the inner wall of the fixed column 201, a first spring 203 is installed on the inner wall of the first limit groove 202, an inclined edge block 204 is installed on one end of the first spring 203, the inclined edge block 204 is slidably connected with the fixed column 201, a second limit groove 3 is symmetrically installed on the inner wall of the lampshade 1, a fixed rod 301 is fixedly installed on the inner wall of the second limit groove 3, a second spring 302 is installed on the outer wall of the fixed rod 301, a button 4 is installed on the outer wall of the lampshade 1, a limit block 401 is symmetrically installed on the outer wall of the button 4, T-shaped blocks 5 are symmetrically installed on the inner wall of the lampshade 1, and there are four T-shaped blocks 5, T-shaped grooves 501 are symmetrically formed in the outer wall of the mounting seat 2, four T-shaped grooves 501 are formed in the outer wall of the mounting seat 2, the positions of the T-shaped grooves 501 correspond to those of T-shaped blocks 5, specifically, the T-shaped blocks 5 are connected with the T-shaped grooves 501 to enable the lampshade 1 to be connected with the mounting seat 2 more stably, the fixing rod 301 penetrates through the limiting blocks 401 to be connected with the limiting blocks 401 in a sliding mode, the second spring 302 is in contact with the limiting blocks 401 to enable the button 4 to be connected with the lampshade 1 in a sliding mode, when the disassembling is needed, the button 4 is pressed down, the limiting blocks 401 on the two sides of the button 4 are moved in the second limiting groove 3 along the fixing rod 301, the second spring 302 is contracted under stress, the bottom end of the button 4 enables the inclined edge block 204 to be pushed into the first limiting groove 202, the first spring 203 is contracted under stress, the inclined edge block 204 is moved out of the groove of the lampshade 1, the lampshade 1 can be drawn out, the aircraft obstruction light can be maintained and replaced, and when the aircraft obstruction light is installed, insert T type piece 5 in T type groove 501, move down along T type groove 501, fixed column 201 gets into in the lamp shade 1, the hypotenuse of hypotenuse piece 204 makes the hypotenuse piece 204 get into a spacing groove 202 with the inner wall contact of the spout of lamp shade 1, spring 203 atress shrink, when reacing the bottom recess, hypotenuse piece 204 breaks away from the contact with the inner wall of spout, spring 203 resets to extend and drives the hypotenuse piece 204 and move and get into in the recess, thereby make lamp shade 1 be connected fixedly with mount pad 2, thereby realized the function of quick installation dismantlement.

Fan 6 is installed to the inner wall of mount pad 2, filter screen 601 is installed at the top of mount pad 2, air-out pipeline 602 has been seted up to the inner wall of mount pad 2, and the dust screen 603 is installed to the one end of air-out pipeline 602, the bottom fixed mounting of mount pad 2 has connecting plate 7, screwed pipe 701 has been seted up to the inner wall symmetry of connecting plate 7, nut 702 is installed to the inner wall of screwed pipe 701, and nut 702 and screwed pipe 701 mesh, concretely, the aviation obstruction lamp passes through nut 702 on the connecting plate 7 and fixes the aviation obstruction lamp at high building top, fan 6 starts, blow out inside heat through air-out pipeline 602, dust screen 603 and filter screen 601 can prevent that internals from receiving the damage of dust, thereby realized the radiating function of aviation obstruction lamp.

The utility model discloses a use as follows: the technical personnel in the field press button 4, button 4 takes stopper 401 of both sides to remove along dead lever 301 in No. two spacing grooves 3, no. two spring 302 atress shrink, make button 4's bottom push away the sloping piece 204 in No. one spacing groove 202, no. one spring 203 atress shrink, make the sloping piece 204 shifted out from the recess of lamp shade 1, lamp shade 1 can be taken out, thereby can maintain the change to the aviation obstruction light, when the installation, insert T type piece 5 in T type groove 501, move down along T type groove 501, fixed column 201 gets into in lamp shade 1, the sloping of sloping piece 204 makes the sloping piece 204 enter No. one spacing groove 202 with the inner wall contact of the spout of lamp shade 1, no. one spring 203 atress shrink, when reacing the bottom recess, the inner wall that a spring 204 and spout break away from the contact, a spring 203 reset the extension drives the sloping piece 204 to move and gets into in the recess, thereby make lamp shade 1 and mount pad 2 connect fixedly, thereby realized the function of quick installation dismantlement, fan 6 starts, blow off the heat of inside through the hypotenuse 602, the dust screen 601 can be prevented from damaging with the aviation obstruction light, thereby the heat dissipation function of dust screen 601 has been realized.

The above description is only a preferred embodiment of the present invention, and any person skilled in the art may modify the present invention or modify it into an equivalent technical solution by using the technical solutions described above. Therefore, any simple modifications or equivalent replacements made according to the technical solution of the present invention belong to the scope of the claimed invention as far as possible.

Claims

1. The utility model provides a modular LED aviation obstruction beacon, includes lamp shade (1) and mount pad (2), its characterized in that: the LED lamp is characterized in that a fixing plate (101) is fixedly mounted on the inner wall of the lampshade (1), an LED lamp assembly (102) is mounted at the top of the fixing plate (101), and a quick mounting and dismounting device is mounted on the inner wall of the lampshade (1) and the top of the mounting seat (2).

2. The combined LED aviation obstruction light of claim 1, wherein: install dismounting device fast includes fixed column (201), fixed column (201) are installed to the top symmetry of mount pad (2), spacing groove (202) have been seted up No. one to the inner wall of fixed column (201), spring (203) are installed to the inner wall of spacing groove (202), hypotenuse piece (204) is installed to the one end of spring (203), and hypotenuse piece (204) and fixed column (201) sliding connection.

3. The combined LED aviation obstruction light of claim 2, wherein: install dismounting device fast includes No. two spacing grooves (3), no. two spacing grooves (3) are installed to the inner wall symmetry of lamp shade (1), the inner wall fixed mounting of No. two spacing grooves (3) has dead lever (301), no. two spring (302) are installed to the outer wall of dead lever (301).

4. The combined LED aviation obstruction light of claim 3, wherein: button (4) are installed to the outer wall of lamp shade (1), stopper (401) are installed to the outer wall symmetry of button (4).

5. The combined LED aviation obstruction light of claim 4, wherein: t type piece (5) are installed to the inner wall symmetry of lamp shade (1), and T type piece (5) have four, T type groove (501) have been seted up to the outer wall symmetry of mount pad (2), T type groove (501) have four, and the position corresponds with T type piece (5).

6. The combined LED aviation obstruction light of claim 1, wherein: fan (6) are installed to the inner wall of mount pad (2), filter screen (601) are installed at the top of mount pad (2), air-out pipeline (602) have been seted up to the inner wall of mount pad (2), and install dust screen (603) to the one end of air-out pipeline (602).

7. The combined LED aviation obstruction light of claim 1, wherein: the bottom fixed mounting of mount pad (2) has connecting plate (7), screwed pipe (701) have been seted up to the inner wall symmetry of connecting plate (7), nut (702) is installed to the inner wall of screwed pipe (701), and nut (702) and screwed pipe (701) meshing.