CN212361795U - Cooling mechanism of aviation obstruction light - Google Patents
Cooling mechanism of aviation obstruction light Download PDFInfo
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- CN212361795U CN212361795U CN202021447081.7U CN202021447081U CN212361795U CN 212361795 U CN212361795 U CN 212361795U CN 202021447081 U CN202021447081 U CN 202021447081U CN 212361795 U CN212361795 U CN 212361795U
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Abstract
The utility model provides a cooling mechanism of aviation obstruction beacon. Cooling mechanism of aviation obstruction lamp includes: a base frame; the lampshade is fixedly arranged at the top of the base frame; the first mounting frame is fixedly mounted on the outer wall of one side of the base frame; the second mounting frame is fixedly mounted on the outer wall of one side of the base frame; the filter element is arranged on the inner wall of the bottom of the second mounting frame; the connecting pipe, the connecting pipe fixed mounting be in the bottom of first installing frame, just the bottom of connecting pipe extends to in the second installing frame and with filter core fixed connection. The utility model provides a cooling mechanism of aviation obstruction beacon has convenient to use, increases the radiating effect, is convenient for change the advantage of suction fan.
Description
Technical Field
The utility model relates to a light equipment technical field that helps navigation especially relates to a cooling mechanism of 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.
Traditionally, aviation obstruction light is generally all to blow the air through the suction fan and dispel the heat to control system, and the suction fan generally all blows control system's top air, thereby drive the control system heat dissipation, thereby the less heat dissipation that can not be fine of the wind that some places of control system blow, and dispel the heat through the suction fan, can have the insufficient possibility of heat dissipation, and control system heat dissipation is insufficient, cause control system to damage easily, and the long service life of general aviation obstruction light is than the life of suction fan, so need maintain or change the suction fan in the use of aviation obstruction light, and general suction fan all is fixed mounting in aviation obstruction light, lead to changing or maintenance very inconvenient.
Therefore, it is necessary to provide a cooling mechanism for an aviation obstruction light to solve the above technical problems.
SUMMERY OF THE UTILITY MODEL
The utility model provides a technical problem provide a convenient to use, increase radiating effect, be convenient for change the cooling mechanism of aviation obstruction beacon of suction fan.
In order to solve the technical problem, the utility model provides a cooling mechanism of aviation obstruction beacon, include: a base frame; the lampshade is fixedly arranged at the top of the base frame; the first mounting frame is fixedly mounted on the outer wall of one side of the base frame; the second mounting frame is fixedly mounted on the outer wall of one side of the base frame; the filter element is arranged on the inner wall of the bottom of the second mounting frame; the connecting pipe is fixedly installed at the bottom of the first installation frame, the bottom end of the connecting pipe extends into the second installation frame and is fixedly connected with the filter element, and the top end of the connecting pipe extends into the first installation frame; the fixing plates are fixedly arranged on the inner walls of the two sides of the first mounting frame; the suction fan is arranged at the top of the fixed plate, and an air inlet of the suction fan is fixedly connected with the top end of the connecting pipe; the connecting plates are fixedly arranged on the inner walls of the two sides of the base frame, and one side of each connecting plate extends into the corresponding first mounting frame; the partition plate is fixedly arranged on the inner wall of the base frame; the third mounting frame is fixedly mounted on the outer wall of one side of the base frame; the baffles are fixedly arranged on the inner walls of the two sides of the third mounting frame; the filter screen is fixedly arranged on the top of the baffle, and the top of the filter screen is fixedly connected with the inner wall of the top of the third mounting frame; the small refrigerator is fixedly arranged on the inner wall of the bottom of the third mounting frame; the guide rod is arranged on the small refrigerator, and the other end of the guide rod extends into the base frame; a plurality of heat-conducting plates, it is a plurality of the equal fixed mounting of heat-conducting plate is in on the baffle, just the top of a plurality of heat-conducting plates all extends to the top of baffle, the bottom of heat-conducting plate all extends to the below of baffle.
Preferably, the suction fan is fixedly installed at the top of the fixing plate.
Preferably, a groove is formed in the outer wall of one side of the connecting plate, a plurality of first vent holes are formed in the bottom of the groove, a plurality of second vent holes are formed in the outer wall of one side of the second mounting frame, and a plurality of third vent holes are formed in the outer wall of one side of the third mounting frame.
Preferably, the top of the partition board is fixedly provided with a control system of the aviation obstruction light.
Preferably, two openings have been seted up on one side inner wall of base frame respectively, two openings all with the third installing frame is linked together, and two opening symmetries set up the both sides of baffle.
Preferably, fixed mounting has inlet tube and outlet pipe on one side outer wall of base frame, the inlet tube is located the below of outlet pipe, just the inlet tube with the outlet pipe all is located the below of baffle.
Preferably, the activity of suction fan sets up the top of fixed plate, the mounting groove has been seted up at the top of fixed plate, the bottom fixed mounting of suction fan has the mounting panel, the bottom of mounting panel extends to in the mounting groove and with mounting groove looks adaptation, the equal fixed mounting in top of fixed plate has two fixed blocks, the draw-in groove has all been seted up on the both sides outer wall of mounting panel, two in the fixed block all seted up the cavity, two all be provided with the fixture block in the cavity, one side that two fixture blocks are close to each other extends to respectively in two draw-in grooves, two one side that the fixture block was kept away from each other extends to outside two fixed blocks respectively.
Preferably, the inner walls of the two sides of the cavity are provided with sliding grooves, the outer walls of the two sides of the clamping block are fixedly provided with sliding blocks, the sliding blocks are connected with the sliding grooves in a sliding mode, the clamping block is sleeved with a spring, one end of the spring is fixedly connected with one outer wall of the sliding block, and the other end of the spring is fixedly connected with the inner wall of the cavity.
Preferably, an opening is formed in the outer wall of one side of the first mounting frame, a sealing door is arranged in the opening, and the sealing door is hinged to the first mounting frame.
Compared with the prior art, the utility model provides a cooling mechanism of aviation obstruction beacon has following beneficial effect:
the wind that blows out through the suction fan can blow the heat that control system distributed out outside the base frame, thereby dispel the heat to control system, and can be even dispel the heat to control system through a plurality of first air vents, can conduct the baffle below with the heat that control system distributed out through a plurality of heat-conducting plates, dispel the heat, the radiating efficiency is improved, and can let the temperature of clear water be less than the heat that control system distributed out always through small-size refrigerator and guide rod, let the heat-conducting plate can transmit the heat always, thereby control system's radiating effect has been increased.
Drawings
Fig. 1 is a schematic structural view of a first embodiment of a cooling mechanism of an aviation obstruction light provided by the present invention;
FIG. 2 is a side cross-sectional view of the base frame shown in FIG. 1;
FIG. 3 is a top cross-sectional view of the connection plate shown in FIG. 1;
fig. 4 is a schematic view of a second embodiment of the cooling mechanism of the aviation obstruction light provided by the present invention;
FIG. 5 is a side cross-sectional view of the first mounting frame shown in FIG. 4;
fig. 6 is an enlarged schematic view of a portion a shown in fig. 5.
Reference numbers in the figures: 1. a base frame; 2. a lamp shade; 3. a first mounting frame; 4. a second mounting frame; 5. a filter element; 6. a connecting pipe; 7. a fixing plate; 8. a suction fan; 9. a connecting plate; 10. a partition plate; 11. a third mounting frame; 12. a baffle plate; 13. a filter screen; 14. a small refrigerator; 15. a guide rod; 16. a heat conducting plate; 17. mounting grooves; 18. mounting a plate; 19. a fixed block; 20. a card slot; 21. a cavity; 22. a clamping block; 23. an opening; 24. and (4) sealing the door.
Detailed Description
The present invention will be further described with reference to the accompanying drawings and embodiments.
First embodiment
Referring to fig. 1-3, in a first embodiment of the present invention, a cooling mechanism for an aviation obstruction light includes: a base frame 1; the lampshade 2 is fixedly arranged on the top of the base frame 1; the first mounting frame 3 is fixedly mounted on the outer wall of one side of the base frame 1; the second mounting frame 4 is fixedly mounted on the outer wall of one side of the base frame 1; the filter element 5 is arranged on the inner wall of the bottom of the second mounting frame 4; the connecting pipe 6 is fixedly installed at the bottom of the first installation frame 3, the bottom end of the connecting pipe 6 extends into the second installation frame 4 and is fixedly connected with the filter element 5, and the top end of the connecting pipe 6 extends into the first installation frame 3; the fixing plates 7 are fixedly arranged on the inner walls of the two sides of the first mounting frame 3; the suction fan 8 is arranged at the top of the fixing plate 7, and an air inlet of the suction fan 8 is fixedly connected with the top end of the connecting pipe 6; the connecting plates 9 are fixedly arranged on the inner walls of the two sides of the base frame 1, and one side of each connecting plate 9 extends into the first mounting frame 3; the partition plate 10 is fixedly arranged on the inner wall of the base frame 1; the third mounting frame 11 is fixedly mounted on the outer wall of one side of the base frame 1; the baffle plates 12 are fixedly arranged on the inner walls of the two sides of the third mounting frame 11; the filter screen 13 is fixedly arranged on the top of the baffle plate 12, and the top of the filter screen 13 is fixedly connected with the inner wall of the top of the third mounting frame 11; the small refrigerator 14 is fixedly arranged on the inner wall of the bottom of the third mounting frame 11; the guide rod 15 is arranged on the small refrigerator 14, and the other end of the guide rod 15 extends into the base frame 1; a plurality of heat-conducting plates 16, it is a plurality of heat-conducting plates 16 all fixed mounting be in on the baffle 10, just the top of a plurality of heat-conducting plates 16 all extends to the top of baffle 10, the bottom of heat-conducting plate 16 all extends to the below of baffle 10.
The suction fan 8 is fixedly arranged at the top of the fixing plate 7.
The outer wall of one side of the connecting plate 9 is provided with a groove, the bottom of the groove is provided with a plurality of first vent holes, the outer wall of one side of the second mounting frame 4 is provided with a plurality of second vent holes, and the outer wall of one side of the third mounting frame 11 is provided with a plurality of third vent holes.
And the top of the partition board 10 is fixedly provided with a control system of the aviation obstruction light.
Two openings have been seted up on one side inner wall of base frame 1 respectively, two openings all with third installing frame 11 is linked together, and two opening symmetries set up the both sides of baffle 10.
Fixed mounting has inlet tube and outlet pipe on one side outer wall of base frame 1, the inlet tube is located the below of outlet pipe, just the inlet tube with the outlet pipe all is located the below of baffle 10.
In this embodiment:
when the water cooling device is used, the suction fan 8 is started, outside air is discharged into the first mounting frame 3 through the second vent holes and the filter element 5, then discharged into the base frame 1 through the grooves in the connecting plate 9 and the first vent holes, the control system on the top of the partition plate 10 is cooled, the control system can be uniformly cooled under the action of the first vent holes, then discharged out of the base frame 1 through the corresponding through holes, clean water is discharged into the space below the partition plate 10 through the water inlet pipe, the temperature of the water is lower than that of the control system due to the fact that the water is normal temperature, the heat dissipated by the control system is transferred to the position below the partition plate 10 through the heat conducting plates 16 under the heat transfer effect, the heat dissipation of the control system can be better assisted under the sitting of the heat conducting plates 16, and after the water temperature rises, the clean water is refrigerated through the small-sized refrigerator 14 and the guide rods 15, and the water temperature is lower than that of the control system is guaranteed, thus, heat can be conducted through the heat conducting plates 16 all the time, and the heat radiating efficiency of the control system is improved.
Compared with the prior art, the utility model provides a cooling mechanism of aviation obstruction beacon has following beneficial effect:
the wind that blows out through suction fan 8 can blow the heat that control system distributed out outside base frame 1, thereby dispel the heat to control system, and can be even dispel the heat to control system through a plurality of first air vents, can conduct the heat that control system distributed out to baffle 10 below through a plurality of heat-conducting plates 16, dispel the heat, the heat dissipation efficiency is improved, and can let the temperature of fresh water be less than the heat that control system distributed out always through small-size refrigerator 14 and guide rod 15, let heat-conducting plate 16 can transmit the heat always, thereby the radiating effect of control system has been increased.
Second embodiment:
based on the cooling mechanism of the aviation obstruction light provided by the first embodiment of the application, the second embodiment of the application provides another cooling mechanism of the aviation obstruction light. The second embodiment is merely a preferred way of the first embodiment, and the implementation of the second embodiment does not affect the implementation of the first embodiment alone.
The second embodiment of the present invention will be further explained with reference to the drawings and the embodiments.
Referring to fig. 4-6 in combination, in a second embodiment of the cooling mechanism for the aviation obstruction light, the suction fan 8 is movably disposed above the fixing plate 7, the top of the fixing plate 7 is provided with a mounting groove 17, the bottom of the suction fan 8 is fixedly provided with a mounting plate 18, the bottom of the mounting plate 18 extends into the mounting groove 17 and is matched with the mounting groove 17, the top of the fixing plate 7 is fixedly provided with two fixing blocks 19, the outer walls of the two sides of the mounting plate 18 are provided with clamping grooves 20, the two fixing blocks 19 are provided with cavities 21, the two cavities 21 are provided with clamping blocks 22, one side of each of the two clamping blocks close to each other extends into the two clamping grooves 20, and one side of each of the two clamping blocks 22 away from each other extends out of the two fixing blocks 19.
The improved structure of the spring comprises a cavity 21, and is characterized in that sliding grooves are formed in the inner walls of the two sides of the cavity 21, sliding blocks are fixedly mounted on the outer walls of the two sides of a clamping block 22, the sliding blocks are connected with the sliding grooves in a sliding mode, springs are sleeved on the clamping block 22, one ends of the springs are fixedly connected with the outer wall of one side of the sliding block, and the other ends of the springs are fixedly connected with the inner wall of one side of the cavity 21.
An opening 23 is formed in the outer wall of one side of the first mounting frame 3, a sealing door 24 is arranged in the opening 23, and the sealing door 24 is hinged to the first mounting frame 3.
In this embodiment:
pulling sealing door 24, then two fixture blocks 22 of pulling respectively again make two blocks 22 break away from two draw-in grooves 20 respectively, at this moment alright with take out first installing frame 3 with the suction fan 8 and maintain and with trading, easy operation, it is quick convenient.
The above only is the embodiment of the present invention, not limiting the scope of the present invention, all the equivalent structures or equivalent processes of the present invention are used in the specification and the attached drawings, or directly or indirectly applied to other related technical fields, and the same principle is included in the protection scope of the present invention.
Claims (9)
1. The utility model provides a cooling mechanism of aviation obstruction beacon which characterized in that includes:
a base frame;
the lampshade is fixedly arranged at the top of the base frame;
the first mounting frame is fixedly mounted on the outer wall of one side of the base frame;
the second mounting frame is fixedly mounted on the outer wall of one side of the base frame;
the filter element is arranged on the inner wall of the bottom of the second mounting frame;
the connecting pipe is fixedly installed at the bottom of the first installation frame, the bottom end of the connecting pipe extends into the second installation frame and is fixedly connected with the filter element, and the top end of the connecting pipe extends into the first installation frame;
the fixing plates are fixedly arranged on the inner walls of the two sides of the first mounting frame;
the suction fan is arranged at the top of the fixed plate, and an air inlet of the suction fan is fixedly connected with the top end of the connecting pipe;
the connecting plates are fixedly arranged on the inner walls of the two sides of the base frame, and one side of each connecting plate extends into the corresponding first mounting frame;
the partition plate is fixedly arranged on the inner wall of the base frame;
the third mounting frame is fixedly mounted on the outer wall of one side of the base frame;
the baffles are fixedly arranged on the inner walls of the two sides of the third mounting frame;
the filter screen is fixedly arranged on the top of the baffle, and the top of the filter screen is fixedly connected with the inner wall of the top of the third mounting frame;
the small refrigerator is fixedly arranged on the inner wall of the bottom of the third mounting frame;
the guide rod is arranged on the small refrigerator, and the other end of the guide rod extends into the base frame;
a plurality of heat-conducting plates, it is a plurality of the equal fixed mounting of heat-conducting plate is in on the baffle, just the top of a plurality of heat-conducting plates all extends to the top of baffle, the bottom of heat-conducting plate all extends to the below of baffle.
2. The cooling mechanism for aviation obstruction lights according to claim 1, wherein the suction fan is fixedly mounted on the top of the fixing plate.
3. The cooling mechanism for the aviation obstruction light as claimed in claim 1, wherein a groove is formed in an outer wall of one side of the connecting plate, a plurality of first vent holes are formed in the bottom of the groove, a plurality of second vent holes are formed in an outer wall of one side of the second mounting frame, and a plurality of third vent holes are formed in an outer wall of one side of the third mounting frame.
4. The cooling mechanism for aviation obstruction lights according to claim 1, wherein a control system of the aviation obstruction light is fixedly installed at the top of the partition board.
5. The cooling mechanism for aviation obstruction lights according to claim 1, wherein two through holes are respectively formed on an inner wall of one side of the base frame, both of the through holes are communicated with the third mounting frame, and the two through holes are symmetrically arranged on two sides of the partition plate.
6. The cooling mechanism of aviation obstruction light of claim 1, wherein a water inlet pipe and a water outlet pipe are fixedly mounted on the outer wall of one side of the base frame, the water inlet pipe is located below the water outlet pipe, and the water inlet pipe and the water outlet pipe are both located below the partition plate.
7. The cooling mechanism for aviation obstruction lights according to claim 1, wherein the suction fan is movably disposed above the fixing plate, a mounting groove is formed in the top of the fixing plate, a mounting plate is fixedly mounted at the bottom of the suction fan, the bottom of the mounting plate extends into the mounting groove and is matched with the mounting groove, two fixing blocks are fixedly mounted at the top of the fixing plate, clamping grooves are formed in outer walls of two sides of the mounting plate, cavities are formed in the two fixing blocks, clamping blocks are disposed in the two cavities, one side, close to each other, of each clamping block extends into the two clamping grooves, and one side, far away from each other, of each clamping block extends out of the two fixing blocks.
8. The cooling mechanism for the aviation obstruction light as claimed in claim 7, wherein sliding grooves are formed in the inner walls of the two sides of the cavity, sliding blocks are fixedly mounted on the outer walls of the two sides of the clamping block, the sliding blocks are slidably connected with the sliding grooves, a spring is sleeved on the clamping block, one end of the spring is fixedly connected with one outer wall of any one of the sliding blocks, and the other end of the spring is fixedly connected with one inner wall of the cavity.
9. The cooling mechanism for the aviation obstruction light of claim 7, wherein an opening is formed in an outer wall of one side of the first mounting frame, a sealing door is arranged in the opening, and the sealing door is hinged to the first mounting frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021447081.7U CN212361795U (en) | 2020-07-21 | 2020-07-21 | Cooling mechanism of aviation obstruction light |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021447081.7U CN212361795U (en) | 2020-07-21 | 2020-07-21 | Cooling mechanism of aviation obstruction light |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212361795U true CN212361795U (en) | 2021-01-15 |
Family
ID=74131267
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021447081.7U Active CN212361795U (en) | 2020-07-21 | 2020-07-21 | Cooling mechanism of aviation obstruction light |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212361795U (en) |
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2020
- 2020-07-21 CN CN202021447081.7U patent/CN212361795U/en active Active
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