CN214840540U

CN214840540U - Bulb mounting base for low-light-intensity aviation obstruction light

Info

Publication number: CN214840540U
Application number: CN202121404473.XU
Authority: CN
Inventors: 秦楠; 汪钰翔
Original assignee: Jiangsu Pengxiang Aviation Technology Co ltd
Current assignee: Jiangsu Pengxiang Aviation Technology Co ltd
Priority date: 2021-06-23
Filing date: 2021-06-23
Publication date: 2021-11-23
Anticipated expiration: 2031-06-23

Abstract

The utility model discloses a bulb mount pad for low light intensity aviation obstruction beacon, including mount, bracket and mounting box, install first card frame in the mount, the fastening screw is run through helicitic texture to inside one side of mount, and the back mounted of first card frame has the bracket, installs the shell in the bracket, and the internally mounted of shell has servo motor, and the mounting box is installed through rotating the connection pad in the top of shell, and light induction assembly is installed to top one side of mounting box. The utility model discloses a run through threaded structure and install fastening screw in inside one side of mount, can make the quick card of mount solid at the mounted position through fastening screw, the device of being convenient for installs fast, has reduced staff high altitude installation device's the degree of difficulty, has improved staff's installation device's efficiency, has shortened the operating time of staff at the high altitude to the security of device when the high altitude installation has been improved.

Description

Bulb mounting base for low-light-intensity aviation obstruction light

Technical Field

The utility model relates to an aviation obstruction light technical field specifically is a bulb mount pad for low light intensity aviation obstruction light.

Background

The aviation obstruction light is not always on but flashes, the low-light-intensity aviation obstruction light is always on, the medium-light-intensity aviation obstruction light and the high-light-intensity aviation obstruction light flash, the flash frequency is not lower than 20 times per minute and is not higher than 60 times per minute, the aviation obstruction light has the function of displaying the outline of a structure, so that an aircraft operator can judge the height and the outline of the obstruction to play a role in warning.

The existing bulb mounting seat for the low-light-intensity aviation obstruction light has the defects that:

1. the existing bulb mounting base for the low-light-intensity aviation obstruction light is inconvenient to mount and fix quickly, and the low-light-intensity aviation obstruction light is generally mounted on a higher building, so that the difficulty of high-altitude mounting of workers is increased, the mounting speed of the device is reduced, the working time of the workers in high altitude is prolonged, and the danger of high-altitude operation of the workers is increased;

2. the current bulb mount pad that is used for low light intensity aviation obstruction beacon is mostly fixed, can't adjust it, leads to the unable furthest's of solar cell panel conversion sun, has reduced solar cell panel's conversion efficiency, influences the electric energy storage capacity, leads to low light intensity aviation obstruction beacon to lead to the unable warning of twinkling of strong aviation obstruction beacon because of the power supply problem, has aviation potential safety hazard problem.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a bulb mount pad for low light intensity aviation obstruction beacon to solve the problem that proposes among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a bulb mount pad for low light intensity aviation obstruction beacon, includes mount, bracket and mounting box, install first card frame in the mount, the fastening screw is installed through the helicitic texture in inside one side of mount, the fastening handle is installed to fastening screw's one end, the back mounted of first card frame has the bracket, install the shell in the bracket, the internally mounted of shell has servo motor, the mounting box is installed through rotatory connection pad in the top of shell, and the bottom of rotatory connection pad is connected with servo motor's output, the internally mounted of mounting box has the battery, the installation base is installed at the top of mounting box, the light induction subassembly is installed to top one side of mounting box.

Preferably, the front surface of the first clamping frame is provided with a second clamping frame through a shaft bolt, and one side of the inner part of the second clamping frame is provided with an adjusting groove.

Preferably, four groups of insulating rubber blocks are installed on one side of the shell, and one end of each insulating rubber block is connected with the back face of the first clamping frame.

Preferably, the mounting frame is installed on the outside of mounting box, and the top of mounting frame is installed solar cell panel through the shaft member.

Preferably, a support rod is installed in the light sensing assembly, and a light sensor is installed at the top of the support rod.

Preferably, the aviation warning light is installed at the top of installation base, and the lamp shade is installed at the top of aviation warning light.

Compared with the prior art, the beneficial effects of the utility model are that:

1. the utility model discloses a run through threaded structure and install fastening screw in inside one side of mount, can make the quick card of mount solid at the mounted position through fastening screw, the device of being convenient for installs fast, has reduced staff high altitude installation device's the degree of difficulty, has improved staff's installation device's efficiency, has shortened the operating time of staff at the high altitude to the security of device when the high altitude installation has been improved.

2. The utility model discloses an internally mounted at the shell has servo motor, can drive the mounting box through servo motor and rotate to adjust solar cell panel's direction, make solar cell panel be in the sunny side always, make solar cell panel produce the electric energy sustainably, the conversion efficiency of solar energy of solar cell panel has been increased, the electric energy storage capacity has been increased, avoided not last because of the electric energy supply, and make the unable scintillation warning of low light intensity aviation obstruction light, the duration of the device has been increased.

Drawings

Fig. 1 is a schematic perspective view of the present invention;

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

fig. 3 is a schematic bottom view of the present invention;

fig. 4 is a schematic front structural view of the present invention;

fig. 5 is a schematic view of a sectional partial structure of the mounting box of the present invention.

In the figure: 1. a fixed mount; 101. a first clip frame; 102. a second clamping frame; 103. an adjustment groove; 2. a bracket; 201. a housing; 202. an insulating rubber block; 203. a servo motor; 3. a solar panel; 301. a mounting frame; 302. a shaft member; 4. mounting a box; 401. a storage battery; 402. installing a base; 403. rotating the connecting disc; 5. a light sensing assembly; 501. a support bar; 502. a light sensor; 6. an aviation warning light; 601. a lamp shade; 7. fastening a screw rod; 701. and (5) fastening the handle.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Referring to fig. 1-5, the present invention provides an embodiment: a bulb mounting seat for a low-light-intensity aviation obstruction light comprises a fixing frame 1, a bracket 2 and a mounting box 4, wherein a first clamping frame 101 is mounted in the fixing frame 1, the fixing frame 1 can provide a mounting position for a fastening screw 7 to facilitate mounting of the fastening screw 7, the first clamping frame 101 can provide a mounting position for the bracket 2 to facilitate mounting of the bracket 2, the fastening screw 7 is mounted on one side of the inside of the fixing frame 1 in a penetrating manner through a threaded structure, the fixing frame 1 can be rapidly clamped and fixed in the mounting position through the fastening screw 7 to facilitate rapid mounting of the device, the difficulty of the high-altitude mounting device of a worker is reduced, the efficiency of the mounting device of the worker is improved, the working time of the worker in high altitude is shortened, the safety of the device in high altitude mounting is improved, a fastening handle 701 is mounted at one end of the fastening screw 7, the fastening screw 7 can be driven to rotate by rotating the fastening handle 701, the rotary fastening screw 7 is matched with the internal thread of the first clamping frame 101 to enable the fastening screw 7 to rotate and move, so that the first clamping frame 101 and the second clamping frame 102 can be tightened, the installation work of the device is completed, workers can fasten the fixing frame 1 by the fastening screw 7 without an installation tool, the carrying burden of the workers is reduced, the condition that the installation tool drops in the high-altitude installation process of the workers is avoided, the safety in the installation of the device is improved, the bracket 2 is installed on the back surface of the first clamping frame 101, the bracket 2 can provide an installation position for the installation box 4, the installation box 4 is convenient to install, the shell 201 is installed in the bracket 2, the shell 201 can protect the servo motor 203, the servo motor 203 is prevented from water and short circuit damage, the servo motor 203 is installed in the shell 201, the installation box 4 can be driven to rotate by the servo motor 203, so as to adjust the direction of the solar panel 3, so that the solar panel 3 is always positioned on the sunny side, so that the solar panel 3 can continuously generate electric energy, the conversion efficiency of the solar energy of the solar panel 3 is increased, the electric energy storage capacity is increased, the problem that the low-light-intensity aviation obstruction light cannot flash for warning due to insufficient electric energy supply is avoided, the cruising ability of the device is increased, the mounting box 4 is mounted at the top of the shell 201 through the rotary connecting disc 403, the mounting box 4 can provide a mounting position for the storage battery 401, so that the storage battery 401 can be conveniently mounted, the bottom of the rotary connecting disc 403 is connected with the output end of the servo motor 203, the storage battery 401 is mounted inside the mounting box 4, the storage battery 401 can store the electric energy converted by the solar panel 3, so as to provide electric energy for the aviation warning light 6, the light sensing assembly 5 and the servo motor 203, installation base 402 is installed at the top of mounting box 4, and installation base 402 can provide the mounted position for aviation warning light 6, and the aviation warning light 6 of being convenient for installs, and light response subassembly 5 is installed to top one side of mounting box 4, and the response of light response subassembly 5 accessible to light to control aviation warning light 6 to open when light is darker and carry out the scintillation warning.

Further, the front of first card frame 101 is installed second card frame 102 through the pintle, but second card frame 102 and first card frame 101 cooperation centre gripping are installed in the outside of post dress object, and the inside one side of second card frame 102 is provided with adjustment tank 103, is convenient for fastening screw 7 through adjustment tank 103 and carries out the adjusting position, makes the mountable of mount 1 in the outside of the different column object of thickness, has increased the installation scope of device.

Furthermore, four groups of insulating rubber blocks 202 are installed on one side of the shell 201, one end of each insulating rubber block 202 is connected with the back face of the first clamping frame 101, the shell 201 and the first clamping frame 101 can be insulated and isolated through the insulating rubber blocks 202, and damage to the device caused by lightning stroke can be prevented.

Further, mounting bracket 301 is installed in the outside of mounting box 4, and mounting bracket 301 can provide the mounted position for solar cell panel 3, and the solar cell panel 3 of being convenient for is installed, and the top of mounting bracket 301 installs solar cell panel 3 through axle piece 302, and solar cell panel 3 can turn into the electric energy to the light energy to provide the electric energy for the electrical apparatus in the device.

Further, install bracing piece 501 in the light response subassembly 5, bracing piece 501 can provide mounted position for light sensor 502, the light sensor 502 of being convenient for installs, and light sensor 502 is installed at the top of bracing piece 501, light sensor 502 can respond to the intensity of light, thereby detect the luminance of current environment, be convenient for according to the current ambient brightness that light sensor 502 detected, control aviation warning light 6 is opened and is carried out the scintillation warning.

Further, aviation warning light 6 is installed at the top of installation base 402, and aviation warning light 6 can twinkle to the height and the profile of suggestion high altitude building, and lamp shade 601 is installed at the top of aviation warning light 6, and lamp shade 601 can protect the inside bulb of aviation warning light 6, prevents that rainwater from causing the bulb short circuit to damage, has prolonged the life of bulb.

The working principle is as follows: can drive fastening screw 7 through rotatory fastening handle 701 and rotate, utilize rotatory fastening screw 7 and the inside screw-thread fit of first card frame 101 to make fastening screw 7 rotatory removal, thereby can tighten up first card frame 101 and second card frame 102, the installation of completion device, rethread light response subassembly 5 can be to the response of light, thereby control aviation warning light 6 and open and carry out the scintillation warning when light is darker, solar cell panel 3 can turn into the electric energy to the light, and carry the electric energy to battery 401 through the wire, can drive mounting box 4 through servo motor 203 and rotate, so that adjust solar cell panel 3's direction, make solar cell panel 3 be in sunny side always.

The details of the present invention are well known to those skilled in the art.

Finally, it is to be noted that: the above embodiments are only used for illustrating the technical solutions of the present invention and not for limiting, and although the present invention has been described in detail with reference to the examples, it should be understood by those skilled in the art that the technical solutions of the present invention can be modified and replaced with equivalents without departing from the spirit and scope of the technical solutions of the present invention, which should be covered by the scope of the claims of the present invention.

Claims

1. The utility model provides a bulb mount pad for low light intensity aviation obstruction beacon, includes mount (1), bracket (2) and mounting box (4), its characterized in that: a first clamping frame (101) is arranged in the fixed frame (1), a fastening screw rod (7) is arranged on one side of the inner part of the fixed frame (1) in a penetrating way through a thread structure, a fastening handle (701) is arranged at one end of the fastening screw rod (7), a bracket (2) is arranged on the back surface of the first clamping frame (101), a shell (201) is arranged in the bracket (2), a servo motor (203) is arranged in the shell (201), the top of the shell (201) is provided with a mounting box (4) through a rotary connecting disc (403), and the bottom of the rotary connecting disc (403) is connected with the output end of the servo motor (203), a storage battery (401) is arranged in the mounting box (4), a mounting base (402) is arranged at the top of the mounting box (4), and a light sensing component (5) is installed on one side of the top of the installation box (4).

2. A light bulb mounting socket for a low light intensity aviation obstruction light as recited in claim 1, wherein: the front surface of the first clamping frame (101) is provided with a second clamping frame (102) through a shaft bolt, and one side of the inside of the second clamping frame (102) is provided with an adjusting groove (103).

3. A light bulb mounting socket for a low light intensity aviation obstruction light as recited in claim 1, wherein: four groups of insulating rubber blocks (202) are installed on one side of the shell (201), and one end of each insulating rubber block (202) is connected with the back of the first clamping frame (101).

4. A light bulb mounting socket for a low light intensity aviation obstruction light as recited in claim 1, wherein: mounting bracket (301) is installed in the outside of mounting box (4), and solar cell panel (3) are installed through axle piece (302) in the top of mounting bracket (301).

5. A light bulb mounting socket for a low light intensity aviation obstruction light as recited in claim 1, wherein: a supporting rod (501) is installed in the light sensing assembly (5), and a light sensor (502) is installed at the top of the supporting rod (501).

6. A light bulb mounting socket for a low light intensity aviation obstruction light as recited in claim 1, wherein: aviation warning light (6) are installed at the top of installation base (402), and lamp shade (601) are installed at the top of aviation warning light (6).