CN219799774U - Cabin formula is heat dissipation and protector for laser radar - Google Patents
Cabin formula is heat dissipation and protector for laser radar Download PDFInfo
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- CN219799774U CN219799774U CN202321261161.7U CN202321261161U CN219799774U CN 219799774 U CN219799774 U CN 219799774U CN 202321261161 U CN202321261161 U CN 202321261161U CN 219799774 U CN219799774 U CN 219799774U
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- laser radar
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- type laser
- fan
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/10—Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation
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Abstract
The utility model provides a heat dissipation and protection device for a cabin type laser radar, which belongs to the technical field of wind power and comprises the cabin type laser radar, wherein a cover plate is clamped at the upper end of the cabin type laser radar, a filtering frame is fixedly connected to the lower end of the cover plate, and a fan, a buffer assembly and a semiconductor refrigerating sheet are arranged at the left end of the cabin type laser radar. The utility model solves the problems that the existing cabin type laser radar cannot radiate heat to the cabin type laser radar, and when the cabin type laser radar works to generate higher heat, the cabin type laser radar cannot be cooled in time, so that each part in the cabin type laser radar is easily damaged due to high temperature, the service life of the part is reduced, the maintenance cost is increased, and the practicability is greatly reduced.
Description
Technical Field
The utility model belongs to the technical field of wind power, and particularly relates to a heat dissipation and protection device for a cabin type laser radar.
Background
Along with the continuous progress of technology, the intelligentization is an industrial wind vane, and the intelligentization development of wind generating sets is also a necessary trend. The wind is a key factor for restricting development of wind power projects, and is an energy source, the wind directly influences the design cost of the unit and threatens the operation safety of the unit, so that accurate wind measurement and error reduction are particularly important, the application of the laser radar in the wind power industry accelerates the intelligent development process, the cabin type laser radar provides more possibility for accurate wind measurement of the wind power unit, the next stage wind condition can be predicted in advance, a control target value can be revised in advance, a controller can globally optimize the longer time wind condition, the action frequency of the fan is reduced, the load is effectively reduced, the service life of the fan is longer, the heat dissipation performance of the cabin type laser radar body directly influences the working stability and reliability of the cabin type laser radar body, the cabin type laser radar body is of a closed structure, and the components such as a laser and a motor in the cabin type laser radar body can generate larger heat productivity in working, so that the internal elements of the cabin type laser radar are easily damaged.
The prior art CN211852053U discloses a cabin type laser radar mounting bracket of a large wind turbine generator, which comprises a lightning rod, a platform, a front supporting leg and a rear supporting leg; the lightning rod is arranged on a platform, the platform is supported by two front supporting legs and two rear supporting legs, and the front supporting legs and the rear supporting legs are arranged at the top of a cabin of the wind turbine generator set through bolts; the middle parts of the front support leg and the rear support leg all adopt square tubes, cables of the laser radar can be arranged inside the square tubes, cable holes are formed in the bottoms of the front support leg and the rear support leg, a hollow design is arranged in the middle of the bottom of the front support leg, rib plates are welded at the bottom of the front support leg, a flat plate is welded at the top of the front support leg, the top of the rear support leg is fixedly connected to the flat plate, and the bottom of the rear support leg is fixedly connected with the top of a cabin. The device can't dispel the heat to cabin formula lidar, and when cabin formula lidar work produced higher heat, can't in time cool down to cabin formula lidar, easily lead to each part in the cabin formula lidar to receive the damage because of the high temperature, reduced the life of part, increased maintenance cost, the practicality greatly reduced.
Disclosure of Invention
The utility model provides a heat dissipation and protection device for a cabin type laser radar, which aims to solve the problems that the existing cabin type laser radar cannot dissipate heat of the cabin type laser radar, and when the cabin type laser radar works to generate higher heat, the cabin type laser radar cannot be cooled in time, so that each part in the cabin type laser radar is easily damaged due to high temperature, the service life of the part is shortened, the maintenance cost is increased, and the practicability is greatly reduced.
The embodiment of the utility model provides a heat dissipation and protection device for a cabin type laser radar, which comprises the cabin type laser radar, wherein a cover plate is clamped at the upper end of the cabin type laser radar, a filtering frame is fixedly connected to the lower end of the cover plate, and a fan, a buffer assembly and a semiconductor refrigerating sheet are arranged at the left end of the cabin type laser radar.
Further, an air vent is reserved on the right end wall of the cabin type laser radar, a mounting groove, a through hole and a sliding groove are reserved on the left end wall of the cabin type laser radar, and the fan is located in the mounting groove.
By adopting the technical scheme, the installation of the buffer component is convenient.
Further, the outside of apron fixedly connected with sealing washer.
Through adopting above-mentioned technical scheme, be convenient for block or open the apron, and the lower extreme fixedly connected with filter frame of apron, when opening the apron, be convenient for take out filter frame from cabin formula laser radar in, the cleanness of the filter screen of being convenient for has improved the filter efficiency of filter screen to the interior dust of cabin formula laser radar, easy and simple to handle.
Further, a filter screen is fixedly connected to the filter frame, a rubber ring is fixedly connected to the lower end of the filter frame, and the lower end of the rubber ring is in contact with the bottom wall of the cabin type laser radar.
Through adopting above-mentioned technical scheme, arrange cabin formula lidar's operating unit in the filter screen inboard, when dispel the heat to cabin formula lidar, can accelerate the circulation of air in the cabin formula lidar, the setting of filter screen is favorable to fully filtering the dust in the entering cabin formula lidar, has avoided the adverse effect of dust to operating unit, has prolonged cabin formula lidar's life, has practiced thrift maintenance cost, and the practicality is strong.
Further, the buffer assembly comprises a connecting block fixed on the fan, the connecting block penetrates through the through hole, the other end of the connecting block is fixedly connected with a sliding block, the other end of the sliding block is fixedly connected with a spring, the other end of the spring is fixedly connected with the sliding groove, the sliding block is in sliding connection with the sliding groove, and the mounting groove is close to one end of the fan, which is fixedly connected with a rubber block.
Through adopting above-mentioned technical scheme, the setting of fan is convenient for accelerate the circulation of air in the cabin formula lidar, has realized the heat dissipation to cabin formula lidar, can produce the vibration at the fan during operation, and the connecting block drives the slider and removes in the spout this moment, utilizes the elasticity of spring and rubber piece, is convenient for cushion the vibration of fan, has reduced the adverse effect of fan vibration to cabin formula lidar, is favorable to the smooth operation of cabin formula lidar inside each part, has prolonged cabin formula lidar's life, is favorable to reducing cost of maintenance.
Further, the left end fixedly connected with mounting panel of semiconductor refrigeration piece, be reserved on the mounting panel and be had the ventilative mouth, the left end fixedly connected with electric fan of mounting panel.
Through adopting above-mentioned technical scheme, the setting of semiconductor refrigeration piece is convenient for cool down to the environment in the cabin formula lidar, has avoided the harm of high temperature to each part in the cabin formula lidar, sets up the electric fan at the heating face of semiconductor refrigeration piece, is convenient for dispel the heat to the semiconductor refrigeration piece of during operation, has improved the refrigeration efficiency of semiconductor refrigeration piece, cooperates the fan, and the fan accelerates the cold air flow in the cabin formula lidar, is favorable to carrying out quick cooling to the cabin formula lidar, and the practicality is strong.
The beneficial effects of the utility model are as follows:
1. according to the utility model, the running part of the cabin type laser radar is arranged at the inner side of the filter screen through the arrangement of the filter frame, when the cabin type laser radar is subjected to heat dissipation, the ventilation in the cabin type laser radar can be accelerated, the arrangement of the filter screen is beneficial to sufficiently filtering dust entering the cabin type laser radar, the adverse effect of the dust on the running part is avoided, the service life of the cabin type laser radar is prolonged, the maintenance cost is saved, and the practicability is strong.
2. According to the utility model, through the arrangement of the fan and the buffer assembly, the air circulation in the cabin type laser radar is conveniently accelerated, the heat dissipation of the cabin type laser radar is realized, the vibration is generated when the fan works, the connecting block drives the sliding block to move in the sliding groove, the vibration of the fan is conveniently buffered by utilizing the retractility of the spring and the rubber block, the adverse effect of the fan vibration on the cabin type laser radar is reduced, the smooth running of all parts in the cabin type laser radar is facilitated, the service life of the cabin type laser radar is prolonged, and the maintenance cost is reduced.
3. According to the utility model, through the arrangement of the semiconductor refrigerating sheets, the environment in the cabin type laser radar is conveniently cooled, the damage of the temperature to each part in the cabin type laser radar is avoided, the electric fan is arranged on the heating surface of the semiconductor refrigerating sheets, the semiconductor refrigerating sheets are conveniently cooled during working, the refrigerating efficiency of the semiconductor refrigerating sheets is improved, the fan is matched with the fan, the fan accelerates the flow of cold air in the cabin type laser radar, the cabin type laser radar is conveniently cooled rapidly, and the practicability is strong.
Additional features and advantages of the utility model will be set forth in the description which follows, and in part will be obvious from the description, or may be learned by practice of the utility model. The objectives and other advantages of the utility model may be realized and attained by the structure particularly pointed out in the written description and drawings.
Drawings
The accompanying drawings are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate the utility model and together with the embodiments of the utility model, serve to explain the utility model. In the drawings:
FIG. 1 is a schematic view of a front cross-sectional structure of an embodiment of the present utility model;
FIG. 2 is a schematic diagram of a front view structure of an embodiment of the present utility model;
FIG. 3 is a schematic bottom cross-sectional view of an embodiment of the present utility model;
FIG. 4 is an enlarged schematic view of the portion a of FIG. 1 according to an embodiment of the present utility model.
Reference numerals: 1. cabin type laser radar; 11. a vent; 12. a mounting groove; 13. a through hole; 14. a chute; 2. a cover plate; 21. a seal ring; 3. a filter frame; 31. a filter screen; 32. a rubber ring; 4. a blower; 5. a buffer assembly; 51. a connecting block; 52. a slide block; 53. a spring; 54. a rubber block; 6. a semiconductor refrigeration sheet; 61. a mounting plate; 62. a ventilation port; 63. an electric fan.
Detailed Description
In order to make the objects, technical solutions and advantages of the technical solutions of the present utility model more clear, the technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings of specific embodiments of the present utility model. Like reference numerals in the drawings denote like parts. It should be noted that the described embodiments are some, but not all embodiments of the present utility model. All other embodiments, which can be made by a person skilled in the art without creative efforts, based on the described embodiments of the present utility model fall within the protection scope of the present utility model.
Referring to fig. 1-4, an embodiment of the utility model provides a heat dissipation and protection device for a cabin type laser radar, which comprises a cabin type laser radar 1, wherein a vent 11 is reserved on the right end wall of the cabin type laser radar 1, a mounting groove 12, a through hole 13 and a sliding groove 14 are reserved on the left end wall of the cabin type laser radar 1, and a fan 4 is positioned in the mounting groove 12, so that the installation of a buffer assembly 5 is facilitated.
Referring to fig. 1, the upper end block of cabin formula lidar 1 has apron 2, and the outside fixedly connected with sealing washer 21 of apron 2 is convenient for block or open apron 2, and the lower extreme fixedly connected with of apron 2 filters frame 3, when opening apron 2, is convenient for take out filter frame 3 from cabin formula lidar 1 in, and the cleanness of filter screen 31 of being convenient for has improved the filtering efficiency of filter screen 31 to the interior dust of cabin formula lidar 1, easy and simple to handle.
Referring to fig. 1 and 3, the lower extreme fixedly connected with filter frame 3 of apron 2, fixedly connected with filter screen 31 on the filter frame 3, the lower extreme fixedly connected with rubber circle 32 of filter frame 3, the lower extreme of rubber circle 32 contacts with the diapire of cabin formula lidar 1, the operating unit of cabin formula lidar 1 is arranged to the inboard at filter screen 31, when dispel the heat to cabin formula lidar 1, can accelerate the circulation of air in the cabin formula lidar 1, filter screen 31's setting is favorable to fully filtering the dust that gets into in the cabin formula lidar 1, avoided the adverse effect of dust to operating unit, the life of cabin formula lidar 1 has been prolonged, maintenance cost has been practiced thrift, and the practicality is strong.
Referring to fig. 1-4, the left end of cabin formula lidar 1 is provided with fan 4 and buffer assembly 5, buffer assembly 5 includes the connecting block 51 of fixing on fan 4, connecting block 51 passes through hole 13, the other end fixedly connected with slider 52 of connecting block 51, the other end fixedly connected with spring 53 of slider 52, the other end and spout 14 fixed connection of spring 53, slider 52 and spout 14 sliding connection, the one end fixedly connected with rubber piece 54 of mounting groove 12 being close to fan 4, fan 4's setting, be convenient for accelerate the circulation of air in the cabin formula lidar 1, the heat dissipation to cabin formula lidar 1 has been realized, can produce the vibration at fan 4 during operation, at this moment, connecting block 51 drives slider 52 and removes in spout 14, utilize the elasticity of spring 53 and rubber piece 54, be convenient for cushion the vibration to fan 4, the adverse effect of fan 4 vibration to cabin formula lidar 1 has been reduced, be favorable to the smooth operation of cabin formula lidar 1 inside each part, the life of cabin formula lidar 1 has been prolonged, be favorable to reducing cost of maintenance.
Referring to fig. 1, a semiconductor cooling plate 6 is arranged at the left end of a cabin type laser radar 1, a mounting plate 61 is fixedly connected to the left end of the semiconductor cooling plate 6, a ventilation port 62 is reserved on the mounting plate 61, an electric fan 63 is fixedly connected to the left end of the mounting plate 61, the semiconductor cooling plate 6 is arranged to cool the environment in the cabin type laser radar 1 conveniently, damage to various components in the cabin type laser radar 1 due to overhigh temperature is avoided, the electric fan 63 is arranged on the heating surface of the semiconductor cooling plate 6 to facilitate heat dissipation of the semiconductor cooling plate 6 during operation, the cooling efficiency of the semiconductor cooling plate 6 is improved, the fan 4 is matched, the fan 4 accelerates cold air flow in the cabin type laser radar 1, rapid cooling is facilitated for the cabin type laser radar 1, and the practicability is strong.
The implementation mode specifically comprises the following steps: during the use, block apron 2, apron 2 lower extreme fixed connection's filter frame 3 enters into cabin formula laser radar 1 in, when cabin formula laser radar 1 generates heat, open fan 4, accelerate the air flow in the cabin formula laser radar 1, when the heat is too high around, open semiconductor refrigeration piece 6 and electric fan 63, electric fan 63 dispels the heat to the semiconductor refrigeration piece 6 of during operation, semiconductor refrigeration piece 6 cools down the environment in the cabin formula laser radar 1, after the heat dissipation, close fan 4, semiconductor refrigeration piece 6 and electric fan 63 can.
The foregoing has shown and described the basic principles and main features of the present utility model and the advantages of the present utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present utility model, and various changes and modifications may be made without departing from the spirit and scope of the utility model, which is defined in the appended claims. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (6)
1. The utility model provides a cabin formula is heat dissipation and protector for laser radar, includes cabin formula laser radar (1), its characterized in that, the upper end block of cabin formula laser radar (1) has apron (2), the lower extreme fixedly connected with filter frame (3) of apron (2), the left end of cabin formula laser radar (1) is provided with fan (4), buffer unit (5) and semiconductor refrigeration piece (6).
2. The heat dissipation and protection device for the cabin laser radar according to claim 1, wherein a vent (11) is reserved on the right end wall of the cabin laser radar (1), a mounting groove (12), a through hole (13) and a sliding groove (14) are reserved on the left end wall of the cabin laser radar (1), and the fan (4) is located in the mounting groove (12).
3. The heat dissipation and protection device for cabin lidar according to claim 1, wherein a sealing ring (21) is fixedly connected to the outer side of the cover plate (2).
4. The heat dissipation and protection device for cabin-type lidar according to claim 1, wherein a filter screen (31) is fixedly connected to the filter frame (3), a rubber ring (32) is fixedly connected to the lower end of the filter frame (3), and the lower end of the rubber ring (32) is in contact with the bottom wall of the cabin-type lidar (1).
5. The cabin type laser radar heat dissipation and protection device according to claim 2, wherein the buffer assembly (5) comprises a connecting block (51) fixed on the fan (4), the connecting block (51) penetrates through the through hole (13), the other end of the connecting block (51) is fixedly connected with a sliding block (52), the other end of the sliding block (52) is fixedly connected with a spring (53), the other end of the spring (53) is fixedly connected with the sliding groove (14), the sliding block (52) is in sliding connection with the sliding groove (14), and one end of the mounting groove (12) close to the fan (4) is fixedly connected with a rubber block (54).
6. The cabin type heat radiation and protection device for the laser radar according to claim 1, wherein the left end of the semiconductor refrigerating sheet (6) is fixedly connected with a mounting plate (61), a ventilation opening (62) is reserved on the mounting plate (61), and the left end of the mounting plate (61) is fixedly connected with an electric fan (63).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321261161.7U CN219799774U (en) | 2023-05-23 | 2023-05-23 | Cabin formula is heat dissipation and protector for laser radar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321261161.7U CN219799774U (en) | 2023-05-23 | 2023-05-23 | Cabin formula is heat dissipation and protector for laser radar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219799774U true CN219799774U (en) | 2023-10-03 |
Family
ID=88186695
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321261161.7U Active CN219799774U (en) | 2023-05-23 | 2023-05-23 | Cabin formula is heat dissipation and protector for laser radar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219799774U (en) |
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2023
- 2023-05-23 CN CN202321261161.7U patent/CN219799774U/en active Active
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