CN218153969U

CN218153969U - Solar aviation obstruction beacon

Info

Publication number: CN218153969U
Application number: CN202222496710.0U
Authority: CN
Inventors: 季立萍
Original assignee: Jiangsu Xingbo Navigation Aids Technology Co ltd
Current assignee: Jiangsu Xingbo Navigation Aids Technology Co ltd
Priority date: 2022-09-21
Filing date: 2022-09-21
Publication date: 2022-12-27
Anticipated expiration: 2032-09-21

Abstract

The utility model relates to an aviation obstruction beacon technical field, concretely relates to solar energy aviation obstruction beacon, its technical scheme is: including stand, obstacle lamp body and solar cell panel, still include switch, the control box subassembly of fixed mounting on the stand lower part, the protection machanism of fixed mounting on control box subassembly one side on the stand top of fixed mounting, protection machanism is including setting up the protection box subassembly and the receipts exhibition subassembly of fixed mounting in the protection box subassembly on control box subassembly one side, receipts exhibition subassembly top fixed mounting is on solar cell panel, the beneficial effects of the utility model are that: can realize when sleet hail weather, take in solar cell panel to the protection in the protective housing subassembly and protect, avoid solar cell panel to expose and receive the damage easily when externally to solar cell panel's life's phenomenon has been reduced.

Description

Solar aviation obstruction light

Technical Field

The utility model relates to an aviation obstruction beacon technical field, concretely relates to solar energy aviation obstruction beacon.

Background

The aviation obstruction light is a special lamp for marking an obstruction, is a special lamp for prompting an aircraft pilot, is usually installed on a high building, a high tower or other high buildings, can emit light at night to display the outline and the height of the building, and is convenient for the aircraft pilot to identify, so that the aircraft is prevented from colliding with the building.

Conventional solar energy aviation obstruction beacon adopts fixed external solar cell panel, collect the utilization through solar cell panel to light energy, but only can carry out effectual collection utilization to solar energy when weather is clear, when sleet hail weather, solar cell panel can't collect the utilization to solar energy, current solar energy aviation obstruction beacon can't be when meetting sleet hail weather, accomodate solar cell panel and protect, make solar cell panel expose and receive the damage easily when externally easily, thereby solar cell panel's life has been reduced.

Therefore, the solar aviation obstruction light is needed to be invented.

SUMMERY OF THE UTILITY MODEL

Therefore, the utility model provides a solar energy aviation obstruction light, through the switch, the control box subassembly, it can realize when sleet hail weather to receive solar cell panel to protect in the protection box subassembly to take in the subassembly to take in, avoided solar cell panel to expose and received the damage when externally easily, thereby solar cell panel's life's phenomenon has been reduced, with the solar cell panel of solving on the current solar energy aviation obstruction light can't take in the protection, when sleet hail weather, make solar cell panel expose and receive the damage when externally easily, thereby solar cell panel's life's problem has been reduced.

In order to achieve the above object, the present invention provides the following technical solutions: the solar aviation obstruction light comprises a stand column, an obstruction light body, a solar cell panel, a switch fixedly mounted on the lower portion of the stand column, a control box assembly fixedly mounted on the top end of the stand column, and a protection mechanism fixedly mounted on one side of the control box assembly;

protection mechanism is including setting up the protection box subassembly on control box subassembly one side and the receipts of fixed mounting in the protection box subassembly exhibition subassembly, receive and expand subassembly top fixed mounting on solar cell panel.

Preferably, the control box subassembly includes the box, box fixed mounting is on the top of stand, the top fixed mounting barrier lamp body of box, fixed mounting has battery, dc-to-ac converter, solar controller and controller in the box.

Preferably, one side fixed mounting protective box subassembly of box, the equal electric connection of controller and dc-to-ac converter, switch, obstruction light body and receipts exhibition subassembly, the equal electric connection of battery and dc-to-ac converter and solar controller, solar controller and solar cell panel electric connection.

Preferably, the protective box subassembly includes first backup pad, first backup pad fixed mounting is on one side lower part of box, fixed mounting has the protection box in the first backup pad, one side top middle part fixed mounting that the protection box is close to the box has the installed part, the top of installed part is rotated through the pivot and is installed the rotation piece, the middle part of rotating the piece is provided with the coil spring, and the coil spring sliding sleeve establish in corresponding position pivot, the both ends of rotating the piece are fixed embedding respectively and are set up in the installed part and rotate the piece, it has the apron to rotate one side fixed mounting that is close to the protection box.

Preferably, the coil spring is in a compressed state, and the folding and unfolding component is fixedly installed in the protective box.

Preferably, the subassembly of taking up and exhibition includes the mounting panel, the mounting panel slides and sets up in the middle part of protection box, the even symmetry fixed mounting in bottom both ends of mounting panel has four electric telescopic handle of group, four groups electric telescopic handle's the equal fixed mounting in the bottom of protection box in bottom, be provided with adjusting part on the mounting panel, adjusting part's top fixed mounting is on solar cell panel's bottom.

Preferably, the mounting panel is close to the one end top fixed mounting of installed part has the ejector pin, four groups electric telescopic handle all with controller electric connection, the top of ejector pin and the bottom contact of apron.

Preferably, the adjusting part includes the second backup pad, the bottom fixed mounting of second backup pad is on the mounting panel keeps away from the one end top of box, the top of second backup pad is rotated through the pivot and is installed first notch plate, the rotation of the middle part of mounting panel installs the lead screw, the one end fixedly connected with motor of lead screw, the threaded connection that the lead screw surface set up has the slider, the bracing piece is installed through the pivot rotation in the top of slider, the second notch plate is installed through the pivot rotation in the top of bracing piece.

Preferably, the top ends of the first concave plate and the second concave plate are respectively and fixedly installed at two ends of the bottom of the solar cell panel, the shell of the motor is fixedly installed in the installation plate, the output shaft of the motor is fixedly connected with one end, close to the motor, of the screw rod, and the motor is electrically connected with the controller.

The utility model has the advantages that: can realize when sleet hail weather through switch, control box subassembly, exhibition subassembly and protective housing subassembly, accomodate solar cell panel to the protective housing subassembly in protect, avoided solar cell panel to expose and receive the damage easily when externally to reduced solar cell panel's life's phenomenon, the practicality is strong.

Drawings

Fig. 1 is a front view of a solar aviation obstruction light provided by the present invention;

FIG. 2 is a structural diagram of a control box assembly provided by the present invention;

FIG. 3 is a connection structure diagram of the protection direction component and the folding and unfolding component provided by the present invention;

fig. 4 is a perspective view of the cover plate and the rotating member provided by the present invention.

In the figure: 1-upright column, 2-box body, 3-barrier lamp body, 4-switch, 5-storage battery, 6-inverter, 7-solar controller, 8-controller, 9-first support plate, 10-protection box, 11-electric telescopic rod, 12-mounting plate, 13-screw rod, 14-slider, 15-motor, 16-second support plate, 17-first concave plate, 18-support rod, 19-solar panel, 20-second concave block, 21-ejector rod, 22-cover plate, 23-mounting piece, 24-coil spring and 25-rotating piece.

Detailed Description

The preferred embodiments of the present invention will be described hereinafter with reference to the accompanying drawings, and it should be understood that the preferred embodiments described herein are merely for purposes of illustration and explanation, and are not intended to limit the present invention.

Referring to the accompanying drawings 1-4, the utility model provides a solar energy aviation obstruction beacon, including stand 1, obstruction beacon body 3 and solar cell panel 19, still include switch 4 of fixed mounting on the stand lower part, fixed mounting control box subassembly on 1 top of stand, the protection machanism of fixed mounting on control box subassembly one side, protection machanism is including setting up the protection box subassembly and the fixed mounting of control box subassembly on one side of the control box subassembly and the subassembly of taking down and expand in the protection box subassembly, takes down and expands subassembly top fixed mounting on solar cell panel 19.

The control box assembly comprises a box body 2, the box body 2 is fixedly installed on the top end of a stand column 1, a barrier lamp body 3 is fixedly installed on the top end of the box body 2, a storage battery 5, an inverter 6, a solar controller 7 and a controller 8 are fixedly installed in the box body 2, a protection box assembly is fixedly installed on one side of the box body 2, the controller 8 is electrically connected with the inverter 6, a switch 4, the barrier lamp body 3 and a folding and unfolding assembly, the storage battery 5 is electrically connected with the inverter 6 and the solar controller 7, the solar controller 7 is electrically connected with a solar panel 19, solar energy is converted into electric energy through the solar panel 19, the solar panel 19 converts the solar energy into the electric energy which is stored in the storage battery 5 through the solar controller 7, direct current electric energy in the storage battery 5 is converted into alternating current electric energy through the inverter 6 and is conveyed into the controller 8, the barrier lamp body 3, the switch 4, a motor 15 and four groups of electric telescopic rods 11 are powered through the controller 8, when the barrier lamp body 3 needs to be turned on, a worker can generate a signal to the controller 8, and turn on the barrier lamp body 3.

The protection box assembly comprises a first support plate 9, the first support plate 9 is fixedly installed on the lower portion of one side of the box body 2, a protection box 10 is fixedly installed on the first support plate 9, the protection box 10 is used for protecting the solar cell panel 19 when the solar cell panel 19 is stored in the protection box 10, an installation part 23 is fixedly installed in the middle of the top end of one side, close to the box body 2, of the protection box 10, a rotating part 25 is installed at the top end of the installation part 23 in a rotating mode through a rotating shaft, a coil spring 24 is arranged in the middle of the rotating part 25, the coil spring 24 is slidably sleeved on the rotating shaft at the corresponding position, the arranged coil spring 24 is used for driving the rotating part 25 and a cover plate 22 to rotate reversely and automatically reset to cover the top of the protection box 10, therefore the fact that the solar cell panel 19 is located in a closed environment is achieved, the phenomenon that the solar cell panel 19 is exposed to be damaged outside is avoided, the two ends of the rotating part 25 are fixedly embedded into the installation part 23 and the rotating part 25 respectively, a cover plate 22 is fixedly installed on one side, the rotating part 25, the side, the rotating part 25 is fixedly installed with the cover plate 22, the rotating part 25, the cover plate 22 is close to be close to the side of the rotating part 25, the rotating part 25 is in a compression state 24 is in a compression state, the cover plate 22 can enable the cover plate 22 to be covered on the protection box 10, the cover plate 22, and can enable the cover assembly, and the coil spring 24 is fixedly installed in the protection box 10.

The folding and unfolding component comprises a mounting plate 12, the mounting plate 12 is arranged in the middle of the protection box 10 in a sliding manner, four groups of electric telescopic rods 11 are uniformly and symmetrically fixedly arranged at two ends of the bottom of the mounting plate 12, the bottom ends of the four groups of electric telescopic rods 11 are fixedly arranged in the bottom end of the protection box 10, the four groups of electric telescopic rods 12 are used for driving the mounting plate 12 and the solar cell panel 19 to move in the vertical direction, so that the solar cell panel 19 comes out of the protection box 10 or the solar cell panel 19 enters the protection box 10, an adjusting component is arranged on the mounting plate 12, the top end of the adjusting component is fixedly arranged on the bottom end of the solar cell panel 19, a top rod 21 is fixedly arranged at the top of one end of the mounting plate 12 close to the mounting part 23, the top rod 21 is used for pushing the cover plate 22 to rotate when the solar cell panel 19 moves upwards, so that the top end of the protection box 10 is opened by the cover plate 22, the four groups of electric telescopic rods 11 are electrically connected with the controller 8, the controller 8 controls the opening and closing of the four groups of electric telescopic rods 11 and the expansion and contraction of the output ends of the four groups of electric telescopic rods 11, the top end of the ejector rod 21 is contacted with the bottom of the cover plate 22, the adjusting component comprises a second support plate 16, the bottom end of the second support plate 16 is fixedly installed on the top of one end of the mounting plate 12 far away from the box body 2, the top end of the second support plate 16 is rotatably provided with a first concave plate 17 through a rotating shaft, the solar cell panel 19 can rotate around the top end of the second support plate 16, the middle part of the mounting plate 12 is rotatably provided with a lead screw 13, one end of the lead screw 13 is fixedly connected with a motor 15, the lead screw 13 is driven to rotate through the motor 15, the thread arranged on the surface of the lead screw 13 is connected with a sliding block 14, the sliding block 14 can move in the horizontal direction through the rotation of the lead screw 13 and the sliding block 14 is rotatably provided with a support rod 18 through the rotating shaft, can realize that slider 14 moves the bottom that drives bracing piece 18 on the horizontal direction and moves on the horizontal direction, the top of bracing piece 18 is rotated through the pivot and is installed second notch plate 20, the top of first notch plate 17 and second notch plate 20 is fixed mounting respectively on the both ends of solar cell panel 19 bottom, the bottom that can realize bracing piece 18 moves the top that drives solar cell panel 19 around second backup pad 16 on the horizontal direction and rotates, motor 15's casing fixed mounting is in mounting panel 12, motor 15's output shaft and lead screw 13 are close to the one end fixed connection of motor 15,

motor

15 and 8 electric connection of controller, the opening and closing of motor 15 and the direction of rotation of motor 15 output shaft are controlled through 8 controllers.

The utility model discloses a use as follows: when the weather is good, a worker can generate a signal to the controller 8 through the switch 4 to start the four groups of electric telescopic rods 11, the four groups of electric telescopic rods 11 can push the mounting plate 12, the ejector rods 21 and the solar cell panel 19 to move upwards, so that the ejector rods 21 jack the cover plate 22, the cover plate 22 rotates anticlockwise to further compress the coil springs 24, the solar cell panel 19 can slide out of the protection box 10, then the signal is generated to the controller 8 through the switch 4, the motor 15 is started through the controller 8, the motor 15 can drive the lead screw 13 to rotate, the lead screw 13 rotates to be matched with the slider 14, the slider 14 can move to one side close to the box body 2, the slider 14 moves to drive the bottom end of the supporting rod 18 to move to one side close to the box body 2, and the solar cell panel 19 rotates around the top end of the second supporting plate 16, therefore, the solar cell panel 19 is in an inclined state, namely, the solar energy is converted into electric energy by the solar cell panel 19, the solar energy is converted into the electric energy by the solar cell panel 19, the electric energy is stored in the storage battery 5 through the solar controller 7, the direct current electric energy in the storage battery 5 is converted into the alternating current electric energy through the inverter 6 and is transmitted into the controller 8, the barrier lamp body 3, the switch 4, the motor 15 and the four groups of electric telescopic rods 11 are supplied with power through the controller 8, when the barrier lamp body 3 needs to be turned on, a worker can generate a signal to the controller 8 through the switch 4, the controller 8 turns on the barrier lamp body 3, when the weather is rainy and snowy, the worker can firstly turn on the motor 15 through the switch 4 and the controller 8 and enable the output shaft of the motor 15 to rotate reversely, so that the sliding block 14 moves to one side far away from the box body 2, thereby make solar cell panel 19 rotate to horizontal position, then start four electric telescopic handle 11 of group and make four electric telescopic handle 11's of group output shrink through switch 4 and controller 8, even make mounting panel 12 and solar cell panel 19 remove downwards, thereby make ejector pin 21 remove downwards, the effort of wind spring 24 drives apron 22 antiport and resets simultaneously, thereby make solar cell panel 19 accomodate to protection box 10 in, apron 22 plugs up the top of protection box 10, thereby avoided when sleet weather, solar cell panel 19 exposes and leads to sleet to cause the phenomenon that the damage leads to solar cell panel 19's life to shorten to solar cell panel 19 externally, thereby realize protecting solar cell panel 19.

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 protection claimed by the present invention as far as possible.

Claims

1. Solar energy aviation obstruction beacon, including stand (1), obstruction beacon body (3) and solar cell panel (19), its characterized in that: the device also comprises a switch (4) fixedly arranged on the lower part of the upright post, a control box component fixedly arranged on the top end of the upright post (1), and a protection mechanism fixedly arranged on one side of the control box component;

the protection mechanism comprises a protection box component arranged on one side of the control box component and a folding and unfolding component fixedly installed in the protection box component, and the top end of the folding and unfolding component is fixedly installed on the solar cell panel (19).

2. The solar aviation obstruction light of claim 1, wherein: the control box subassembly includes box (2), box (2) fixed mounting is on the top of stand (1), the top fixed mounting barrier lamp body (3) of box (2), fixed mounting has battery (5), dc-to-ac converter (6), solar control ware (7) and controller (8) in box (2).

3. The solar aviation obstruction light of claim 2, wherein: one side fixed mounting protective box subassembly of box (2), controller (8) and dc-to-ac converter (6), switch (4), obstacle lamp body (3) and the equal electric connection of exhibition subassembly of taking up, battery (5) and dc-to-ac converter (6) and the equal electric connection of solar control ware (7), solar control ware (7) and solar cell panel (19) electric connection.

4. The solar aviation obstruction light of claim 3, wherein: the protective box subassembly includes first backup pad (9), first backup pad (9) fixed mounting is on one side lower part of box (2), fixed mounting has protection box (10) on first backup pad (9), one side top middle part fixed mounting that protection box (10) are close to box (2) has installed part (23), the top of installed part (23) is rotated through the pivot and is installed rotation piece (25), the middle part that rotates piece (25) is provided with wind spring (24), and wind spring (24) slip cap is established in corresponding position pivot, the both ends of rotating piece (25) are fixed the embedding respectively and are set up in installed part (23) and rotation piece (25), it has apron (22) to rotate one side fixed mounting that piece (25) are close to protection box (10).

5. The solar aviation obstruction light of claim 4, wherein: the coil spring (24) is in a compressed state, and the folding and unfolding component is fixedly installed in the protection box (10).

6. The solar aviation obstruction light of claim 4, wherein: the folding and unfolding assembly comprises a mounting plate (12), the mounting plate (12) is arranged in the middle of the protection box (10) in a sliding manner, four groups of electric telescopic rods (11) and four groups of electric telescopic rods are fixedly arranged at two ends of the bottom of the mounting plate (12) in the bottom end of the protection box (10) in an even symmetrical manner, an adjusting assembly is arranged on the mounting plate (12), and the top end of the adjusting assembly is fixedly arranged at the bottom end of the solar cell panel (19).

7. The solar aviation obstruction light of claim 6, wherein: one end top fixed mounting that mounting panel (12) are close to installed part (23) has ejector pin (21), four groups electric telescopic handle (11) all with controller (8) electric connection, the top of ejector pin (21) and the bottom contact of apron (22).

8. The solar aviation obstruction light of claim 7, wherein: the adjusting part comprises a second supporting plate (16), the bottom end of the second supporting plate (16) is fixedly installed on the top of one end of the mounting plate (12) far away from the box body (2), a first concave plate (17) is installed on the top of the second supporting plate (16) through rotation of a rotating shaft, a lead screw (13) is installed in the middle of the mounting plate (12) in a rotating mode, a motor (15) is fixedly connected with one end of the lead screw (13), a sliding block (14) is connected to the surface of the lead screw (13) through threads, a supporting rod (18) is installed on the top of the sliding block (14) through rotation of the rotating shaft, and a second concave plate (20) is installed on the top of the supporting rod (18) through rotation of the rotating shaft.

9. The solar aviation obstruction light of claim 8, wherein: the top of first notch plate (17) and second notch plate (20) is fixed mounting respectively on the both ends of solar cell panel (19) bottom, the casing fixed mounting of motor (15) is in mounting panel (12), the output shaft of motor (15) and lead screw (13) are close to the one end fixed connection of motor (15), motor (15) and controller (8) electric connection.