CN215061539U

CN215061539U - High-reliability aviation obstruction beacon

Info

Publication number: CN215061539U
Application number: CN202121312667.7U
Authority: CN
Inventors: 甄勇; 万波
Original assignee: CHENGDU JINHUA UTILITY ELECTRICAL APPARATUS RESEARCH INSTITUTE CO LTD
Current assignee: CHENGDU JINHUA UTILITY ELECTRICAL APPARATUS RESEARCH INSTITUTE CO LTD
Priority date: 2021-06-12
Filing date: 2021-06-12
Publication date: 2021-12-07
Anticipated expiration: 2031-06-12

Abstract

The utility model provides a high-reliability aviation obstruction beacon, which comprises a main body and a lamp body arranged at the top of the main body; the below of the host computer body is equipped with the base, and the host computer is internal to be equipped with two vertical baffles and two vertical refrigeration boards. The two vertical partition plates and the two refrigerating plates are arranged in the main machine body, and the horizontal air guide partition plate is arranged between the refrigerating plates, so that an air channel in the main machine body is longer, and meanwhile, the exhaust guide pipe is communicated with the top of the main machine body, so that the hot air in the main machine body can be exhausted as soon as possible by utilizing the principle that thermal barrier cold-contraction hot air moves upwards, and a better cooling effect is achieved. Through setting up parts such as arc light-reflecting groove, bar blowing nozzle and with spiral elasticity air duct and the inside intercommunication of host computer body, the air can be followed bar blowing nozzle and spout when the fan is blown the cooling to host computer body inside like this, just so can blow away deposition or snow on the light-passing board and play the clean effect to the light-passing board, guarantees its light transmissivity.

Description

High-reliability aviation obstruction beacon

Technical Field

The utility model particularly relates to a high reliability aviation obstruction beacon.

Background

The aviation obstruction light is a special lamp for marking an obstruction, the aviation obstruction light is not normally on but flashes, the low-light-intensity aviation obstruction light is normally on, the medium-light-intensity aviation obstruction light and the high-light-intensity aviation obstruction light flash, the flashing frequency is not lower than twenty times per minute and not higher than sixty times per minute, and 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 play a role in warning.

Patent document with publication number CN212361795U discloses a technical scheme for cooling an aviation obstruction light, and this scheme utilizes the fan to realize the cooling of the aviation obstruction light, but the air duct in this structure is short and leads to the whole cooling effect unsatisfactory, and the lamp body surface of current aviation obstruction light often has deposition or snow simultaneously, leads to the illuminating effect to descend, therefore provides a high reliability aviation obstruction light on this basis in order to solve this problem.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to prior art not enough, provide a high reliability aviation obstruction beacon, this high reliability aviation obstruction beacon can solve above-mentioned problem well.

In order to meet the above requirements, the utility model adopts the following technical scheme: the high-reliability aviation obstruction light comprises a main machine body and a light body arranged at the top of the main machine body; a base is arranged below the main machine body, two vertical partition plates and two vertical refrigerating plates are arranged inside the main machine body, and at least five horizontal air guide partition plates are arranged between the two refrigerating plates in a staggered manner; the two refrigeration plates are arranged between the two vertical partition plates, the tops of the vertical partition plates are connected with the top of the end face of the inner side of the main machine body, and the bottoms of the refrigeration plates are connected with the bottom of the end face of the inner side of the main machine body; a lower ventilation groove is formed in the bottom of the base, a fan is arranged in the lower ventilation groove, an air outlet end of the top of the fan is communicated with the inside of the main body through a blowing pipe, and an opening in the top of the blowing pipe is located between the two refrigeration plates; the top of the left side of the main machine body is connected with an exhaust duct, and the bottom of the exhaust duct is communicated with the lower ventilation groove; the lamp body includes arc light-reflecting groove and sets up the light-passing board at arc light-reflecting groove top, arc light-reflecting groove bottom has connect the connecting plate, the connecting plate is through screwing up fixing bolt and semi-circular mounting panel swing joint, the bottom of semi-circular mounting panel with main engine body top is connected, main engine body right side end face top has connect spiral elasticity air duct, the one end of light-passing board is equipped with the bar blowing nozzle, the bar blowing nozzle with spiral elasticity air duct intercommunication.

The high-reliability aviation obstruction light has the following advantages:

the two vertical partition plates and the two refrigerating plates are arranged in the main machine body, and the horizontal air guide partition plate is arranged between the refrigerating plates, so that an air channel in the main machine body is longer, and meanwhile, the exhaust guide pipe is communicated with the top of the main machine body, so that the hot air in the main machine body can be exhausted as soon as possible by utilizing the principle that thermal barrier cold-contraction hot air moves upwards, and a better cooling effect is achieved. Through setting up arc light-reflecting groove, bar blowing nozzle, spiral elasticity air duct, connecting plate, semi-circular mounting panel, screwing up fixing bolt and light-passing board and with spiral elasticity air duct and the inside intercommunication of host computer body, the air can be followed bar blowing nozzle and blowout when the fan is blown the cooling to host computer body inside like this, just so can blow away deposition or snow on the light-passing board and play the clean effect to the light-passing board, guarantees its light transmissivity.

Drawings

The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the application and together with the description serve to explain the application and not to limit the application. In the drawings:

fig. 1 schematically shows a structural view of a high-reliability aviation obstruction light according to an embodiment of the present application.

Fig. 2 schematically shows a structural diagram of a light-transmitting plate of a high-reliability aviation obstruction light according to an embodiment of the application.

Fig. 3 schematically shows a schematic structural view at a strip-shaped blowing nozzle of a high-reliability aviation obstruction light according to one embodiment of the application.

Wherein: 1. a lamp body; 2. a main body; 3. a base; 4. a vertical partition; 5. an exhaust conduit; 6. a control circuit component; 7. a power supply member; 8. a refrigeration plate; 9. a horizontal air guide clapboard; 10. a lower vent slot; 11. A blowpipe; 12. a fan; 13. a hollow wire cavity; 14. a gas filtering cover; 15. fixing the bolt; 16. an arc-shaped light reflecting groove; 17. a strip-shaped air blowing nozzle; 18. a helical elastic airway tube; 19. a connecting plate; 20. a semicircular mounting plate; 21. screwing down the fixing bolt; 22. a light-transmitting plate.

Detailed Description

In order to make the objects, technical solutions and advantages of the present application more apparent, the present application will be described in further detail with reference to the accompanying drawings and specific embodiments.

In the following description, references to "one embodiment," "an embodiment," "one example," "an example," etc., indicate that the embodiment or example so described may include a particular feature, structure, characteristic, property, element, or limitation, but every embodiment or example does not necessarily include the particular feature, structure, characteristic, property, element, or limitation. Moreover, repeated use of the phrase "in accordance with an embodiment of the present application" although it may possibly refer to the same embodiment, does not necessarily refer to the same embodiment.

Certain features that are well known to those skilled in the art have been omitted from the following description for the sake of simplicity.

According to an embodiment of the present application, there is provided a high-reliability aviation obstruction beacon, as shown in fig. 1, including a main body 2 and a lamp body 1 disposed on top of the main body 2; the below of the host computer body 2 is equipped with base 3, the inside two vertical baffles 4 and two vertical refrigeration boards 8 that are equipped with of the host computer body 2, the straggly is provided with five at least horizontally horizontal wind-guiding baffles 9 between two refrigeration boards 8.

According to an embodiment of the application, two of this high reliability aviation obstruction beacon refrigeration board 8 sets up two between the vertical baffle 4, the top of vertical baffle 4 with the medial surface top of the main engine body 2 is connected, refrigeration board 8's bottom with the medial surface bottom of the main engine body 2 is connected.

According to an embodiment of the application, the bottom of the base 3 of the high-reliability aviation obstruction light is provided with a lower ventilation groove 10, a fan 12 is arranged inside the lower ventilation groove 10, the air outlet end at the top of the fan 12 is communicated with the inside of the main machine body 2 through a blowpipe 11, and the top opening of the blowpipe 11 is positioned between the two refrigeration plates 8.

According to an embodiment of the application, an exhaust duct is connected to the top of the left side of the main body of the high-reliability aviation obstruction light, and the bottom of the exhaust duct 5 is communicated with the lower ventilation groove 10.

According to an embodiment of this application, this high reliability aviation obstruction beacon's lamp body 1 includes arc reflection of light groove 16 and sets up the light-passing board 22 at arc reflection of light groove 16 top, arc reflection of light groove 16 bottom has connect connecting plate 19, connecting plate 19 is through screwing up fixing bolt 21 and semi-circular mounting panel 20 swing joint, semi-circular mounting panel 20 the bottom with main engine body 22 top is connected, 2 right side terminal surface tops of main engine body have connect spiral elasticity air duct 18, the one end of light-passing board 22 is equipped with bar blowing nozzle 17, bar blowing nozzle 17 with spiral elasticity air duct 18 intercommunication. Can unscrew as required during the use and screw up behind the fixing bolt 21 and rotate lamp body 1 and adjust to suitable angle and screw up fixing bolt 21 afterwards and screw up, arc reflection of light groove 16 inside is equipped with the lighting bulb, and arc reflection of light groove 16 is made for 1 arc reflecting material, and bar blowing nozzle 17's inner structure is shown in figure 3, and bar blowing nozzle 17 inside can set up two curved guide plates and be used for making the air that blows out more even.

According to one embodiment of the application, vertical fixing bolts 15 are inserted at the edge of the base 3 of the high-reliability aviation obstruction light.

According to one embodiment of the application, the main body 2 of the high-reliability aviation obstruction light is internally provided with a control circuit component 6 and a power supply component 7, wherein the control circuit component 6 and the power supply component 7 are respectively positioned between one vertical partition plate 4 and one refrigeration plate 8.

According to one embodiment of the application, the air inlet end of the fan 12 of the high-reliability aviation obstruction light extends out of the side end of the lower ventilating slot 10, and the air filter cover 14 is sleeved outside the air inlet end of the fan 12.

According to an embodiment of the application, a hollow conductor cavity 13 is arranged between the main body 2 and the base 3 of the high-reliability aviation obstruction light, the fan 12 is electrically connected with the control circuit part 6 and the power supply part 7 through a conductor penetrating through the hollow conductor cavity 13, and the control circuit part 6 is electrically connected with the power supply part through a conductor penetrating through the hollow conductor cavity 13.

According to one embodiment of the application, the front end and the rear end of the vertical partition plate 4, the refrigeration plate 8 and the horizontal air guide partition plate 9 of the high-reliability aviation obstruction light are respectively connected with the front end face and the rear end face inside the main machine body 2.

According to one embodiment of the application, the high-reliability aviation obstruction light can be fixed on the top of a building by using a fixing bolt 15, at the same time, the air is blown into the main body 2 by the fan 12, as shown in fig. 1, the blown air passes through the channel formed between the refrigerating plate 8 and the horizontal air guiding partition 9, and the cooled cold air enters the space between the vertical partition plate 4 and the refrigerating plate 8 to move downwards and cool the control circuit part 6 and the power supply part 7, then enters the area between the vertical partition plate 4 and the side wall of the main body 2, moves upwards, enters the exhaust duct 5 and then is discharged into the lower ventilation groove 10 from the bottom of the exhaust duct 5, the air is discharged from the lower ventilation groove 10, the air circulation speed of the lower ventilation groove 10 can be accelerated, and meanwhile, the air inlet end of the fan 12 can be isolated from the air outlet end of the exhaust duct 5.

According to an embodiment of the application, this high reliability aviation obstruction light is through setting up two vertical baffles 4 and two refrigeration boards 8 and setting up horizontal wind-guiding baffle between the refrigeration board inside the main engine body 2, can make the inside wind channel of main engine body 2 longer like this, and the principle that switches on exhaust pipe 5 can utilize the upward motion of thermal barrier shrinkage hot-air at main engine body 2 top simultaneously can utilize the inside hot-air outgoing of main engine body 2 to realize better cooling effect as early as possible. By arranging the arc-shaped light reflecting groove 16, the strip-shaped air blowing nozzle 17, the spiral elastic air guide pipe 18, the connecting plate 19, the semicircular mounting plate 20, screwing the fixing bolt 21 and the light-transmitting plate 22 and communicating the spiral elastic air guide pipe 18 with the inside of the main machine body 2, air can be sprayed out from the strip-shaped air blowing nozzle 17 when the fan 12 blows air to cool the inside of the main machine body 2, so that accumulated dust or accumulated snow on the light-transmitting plate 22 can be blown off to clean the light-transmitting plate 22, and the light transmittance of the light-transmitting plate is ensured.

The above-described embodiments are merely illustrative of several embodiments of the present invention, which are described in detail and detail, but should not be construed as limiting the scope of the present invention. It should be noted that, for those skilled in the art, without departing from the spirit of the present invention, several variations and modifications can be made, which are within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the claims.

Claims

1. A high reliability aviation obstruction beacon which characterized in that: comprises a main machine body and a lamp body arranged at the top of the main machine body;

a base is arranged below the main machine body, two vertical partition plates and two vertical refrigerating plates are arranged inside the main machine body, and at least five horizontal air guide partition plates are arranged between the two refrigerating plates in a staggered manner;

the two refrigeration plates are arranged between the two vertical partition plates, the tops of the vertical partition plates are connected with the top of the end face of the inner side of the main machine body, and the bottoms of the refrigeration plates are connected with the bottom of the end face of the inner side of the main machine body;

a lower ventilation groove is formed in the bottom of the base, a fan is arranged in the lower ventilation groove, an air outlet end of the top of the fan is communicated with the inside of the main body through a blowing pipe, and an opening in the top of the blowing pipe is located between the two refrigeration plates;

the top of the left side of the main machine body is connected with an exhaust duct, and the bottom of the exhaust duct is communicated with the lower ventilation groove;

the lamp body includes arc light-reflecting groove and sets up the light-passing board at arc light-reflecting groove top, arc light-reflecting groove bottom has connect the connecting plate, the connecting plate is through screwing up fixing bolt and semi-circular mounting panel swing joint, the bottom of semi-circular mounting panel with main engine body top is connected, main engine body right side end face top has connect spiral elasticity air duct, the one end of light-passing board is equipped with the bar blowing nozzle, the bar blowing nozzle with spiral elasticity air duct intercommunication.

2. The high reliability aviation obstruction light of claim 1, wherein: vertical fixing bolts are inserted into the edge of the base.

3. The high reliability aviation obstruction light of claim 1, wherein: the main machine body is internally provided with a control circuit component and a power supply component, and the power supply component of the control circuit component is respectively positioned between a vertical clapboard and a refrigerating plate.

4. The high reliability aviation obstruction light of claim 1, wherein: the air inlet end of the fan is extended out of the side end of the lower ventilating groove, and an air filtering cover is sleeved outside the air inlet end of the fan.

5. The high reliability aviation obstruction light of claim 1, wherein: the main engine body with be equipped with the cavity wire cavity between the base, the fan is through passing the wire of cavity wire cavity is connected with control circuit part and power supply part electricity, the control circuit part is through passing the wire of cavity wire cavity is connected with power supply part electricity.

6. The high reliability aviation obstruction light of claim 1, wherein: the front end and the rear end of the vertical partition plate and the front end and the rear end of the refrigeration plate are respectively connected with the front end face and the rear end face inside the main machine body.