CN211019719U - Integrated automatic temperature control equipment cabin - Google Patents
Integrated automatic temperature control equipment cabin Download PDFInfo
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- CN211019719U CN211019719U CN201921162237.4U CN201921162237U CN211019719U CN 211019719 U CN211019719 U CN 211019719U CN 201921162237 U CN201921162237 U CN 201921162237U CN 211019719 U CN211019719 U CN 211019719U
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Abstract
An integrated automatic temperature control equipment cabin relates to the design field of equipment cabins of mobile missile launching platforms; the heat preservation cabin comprises a heat preservation cabin body, 4 open type cabinets, 3 door plates, a ventilation heating device, 2 temperature sensors and 2 shutters; wherein, the heat-insulating cabin body is a hollow cuboid structure which is horizontally arranged; 4 open cabinets are fixedly arranged in the inner cavity of the heat-insulating cabin body at intervals along the horizontal direction; a door plate is fixedly arranged between every two adjacent open type cabinets; the ventilation heating device is fixedly arranged at the top of the heat-insulation cabin body; the 2 temperature sensors are respectively and fixedly arranged on the top of the 2-side open type cabinet; 2 shutters are fixedly arranged on the rear side wall of the heat preservation cabin body; the utility model provides a big problem of the little space installation degree of difficulty of a plurality of equipment, set up automatic temperature control system simultaneously, provide reliable operational environment for electronic equipment.
Description
Technical Field
The utility model relates to a remove guided missile launching platform equipment cabin design field, especially an automatic temperature control equipment cabin integrates.
Background
Along with the upgrading and upgrading of missile launching equipment, the modern mobile missile launching platform is more and more integrated and miniaturized. The measurement and launch control system is used as a control system of a missile launching platform, two vehicles are arranged in original launching equipment, and the two vehicles are integrated into a skirt edge equipment cabin of the launching platform. The measuring, transmitting and controlling equipment cabin is small in size and high in power density, and in order to meet the low-temperature transmitting requirement, the equipment cabin is a heat-insulating cabin which can insulate heat at low temperature so as to meet the transmitting environment requirement. However, the heat insulation material is filled in the heat insulation cabin, so that the equipment cabin can not effectively dissipate heat in a high-temperature environment, the temperature in the equipment cabin is rapidly increased, and the environmental requirement required by the work of the measurement, control and control equipment is difficult to meet.
SUMMERY OF THE UTILITY MODEL
The utility model discloses an overcome prior art's the aforesaid not enough, provide and integrate automatic temperature control equipment cabin, solved the big problem of the little space installation degree of difficulty of a plurality of equipment, set up automatic temperature control system simultaneously, provide reliable operational environment for electronic equipment.
The above object of the present invention is achieved by the following technical solutions:
the integrated automatic temperature control equipment cabin comprises a heat insulation cabin body, 4 open type cabinets, 3 door plates, a ventilation heating device, 2 temperature sensors and 2 shutters; wherein, the heat-insulating cabin body is a hollow cuboid structure which is horizontally arranged; 4 open cabinets are fixedly arranged in the inner cavity of the heat-insulating cabin body at intervals along the horizontal direction; a door plate is fixedly arranged between every two adjacent open type cabinets; the ventilation heating device is fixedly arranged at the top of the heat-insulation cabin body; the 2 temperature sensors are respectively and fixedly arranged on the top of the 2-side open type cabinet; 2 shutters are fixedly arranged on the rear side wall of the heat preservation cabin body.
In the integrated automatic temperature control equipment cabin, the distance between the temperature sensor and the inner wall of the heat insulation cabin body is 350-360 mm.
In the integrated automatic temperature control equipment cabin, the temperature measured by the temperature sensor ranges from minus 45 ℃ to 80 ℃; the measurement accuracy is +/-1 ℃.
In the integrated automatic temperature control equipment cabin, the shutter is of a rectangular structure; the louver size is 275mm by 410 mm; the distance between the fixed position of the louver and the inner wall of the heat-insulating cabin body is 360-370 mm; the height from the bottom of the heat-insulating cabin body is 330 mm and 340 mm.
In the integrated automatic temperature control equipment cabin, when the internal temperature of the heat insulation cabin body is lower than a threshold value a, 2 shutters are closed; the ventilation heating device realizes heating of the interior of the heat-insulation cabin body; stopping the ventilation heating device until the temperature rises to a threshold value b;
when the internal temperature of the heat-insulating cabin body is higher than a threshold value c, 2 shutters are opened; the ventilation heating device realizes air exhaust, and performs air exchange between the inside and the outside of the heat-insulation cabin body to realize heat dissipation; until the temperature drops to a threshold d; the ventilation heating device stops working.
In the integrated automatic temperature control equipment cabin, a is-25 ℃; b is-15 ℃.
In the integrated automatic temperature control equipment cabin, the total power consumption of the ventilation heating device is more than 500W. And less than 1300W.
In the integrated automatic temperature control equipment cabin, the c is 35 ℃; d is 30 ℃.
In the above cabin, the air pumping amount of the ventilation heating device is not less than 50m3/h。
In the above cabin, the electromagnetic shielding sum of the 2 louver windows and the ventilation and heating device is not more than 40 dB.
Compared with the prior art, the utility model have following advantage:
(1) the utility model adopts an integrated design, which solves the problem of difficulty in installation of a plurality of devices in small space;
(2) the utility model adopts an open frame cabinet to ensure the heat dissipation of the electronic equipment;
(3) the utility model is provided with an automatic temperature control system, which can cool when the temperature is high and heat when the temperature is low, thus providing a reliable working environment for the electronic equipment;
(4) the utility model discloses under the circumstances of guaranteeing to integrate, leave sufficient space between rack and the rack, the cable arrangement between the equipment heat dissipation of being convenient for and the under-deck equipment.
Drawings
Fig. 1 is a front view of the temperature control device cabin of the present invention;
fig. 2 is a rear view of the temperature control device cabin of the present invention.
Detailed Description
The invention will be described in further detail with reference to the following figures and specific embodiments:
the utility model provides an integrated automatic temperature control equipment cabin, which adopts integrated design and solves the problem of large difficulty in installation of a plurality of equipment in small space; the equipment in the cabinet 2 and the equipment in the cabinet 2 in the heat-insulating cabin 1 adopt a modular installation mode, so that the equipment is convenient to install and maintain; the cabinet 2 adopts an open type frame cabinet, so that the heat dissipation of the electronic equipment is ensured; the automatic ventilation heating device 9 is arranged in the equipment cabin, so that a reliable working environment is provided for the electronic equipment; in order to facilitate the electrical connection between the electronic equipment inside the equipment cabin and the equipment outside the equipment cabin, a switching component is designed outside the equipment cabin, so that the connection test is convenient and quick; under the condition of ensuring integration, a sufficient space is reserved between the cabinet and the cabinet, so that heat dissipation of equipment and cable arrangement between equipment in the cabin are facilitated.
Fig. 1 is a front view of the temperature control equipment compartment, fig. 2 is a rear view of the temperature control equipment compartment, and it can be seen that the temperature control equipment compartment comprises a heat-insulating compartment body 1, 4 open type cabinets 2, 3 door panels 3, a ventilation and heating device 9, 2 temperature sensors 10 and 2 shutters 12; wherein, the heat-insulating cabin body 1 is a hollow cuboid structure which is horizontally arranged; the 4 open cabinets 2 are fixedly arranged in the inner cavity of the heat-insulating cabin 1 at intervals along the horizontal direction; sufficient space is left between the machine cabinet 2 and the machine cabinet 2, so that heat dissipation of equipment and cable arrangement between equipment in the cabin are facilitated. The cabinet 2 adopts an open type frame cabinet to ensure the heat dissipation of the electronic equipment, and a door plate 3 is fixedly arranged between every two adjacent open type cabinets 2; the ventilation heating device 9 is fixedly arranged at the top of the heat-insulation cabin body 1; the 2 temperature sensors 10 are respectively and fixedly installed at the top of the 2-side open type cabinet 2; 2 shutters 12 are fixedly arranged on the rear side wall of the heat preservation cabin 1.
The distance between the temperature sensor 10 and the inner wall of the heat-insulating cabin 1 is 350-360 mm. The temperature measuring range of the temperature sensor 10 is-45-80 ℃; the measurement accuracy is +/-1 ℃.
The louver 12 is of a rectangular structure; the louver 12 size is 275mm 410 mm; the distance between the fixed position of the louver 12 and the inner wall of the heat-insulating cabin 1 is 360-370 mm; the height from the bottom of the heat-insulating cabin body 1 is 330 mm and 340 mm.
When the internal temperature of the heat-insulating cabin body 1 is lower than minus 25 ℃, 2 shutters 12 are closed; the ventilation heating device 9 realizes the heating of the interior of the heat-insulation cabin body 1; the ventilation heating device 9 stops working until the temperature rises to-15 ℃; the total power consumption of the ventilation heating device 9 is more than 500W. And less than 1300W.
When the internal temperature of the heat-insulating cabin body 1 is higher than 35 ℃, 2 shutters 12 are opened; the ventilation heating device 9 realizes air exhaust, and performs air exchange between the inside and the outside of the heat-insulation cabin body 1 to realize heat dissipation; until the temperature is reduced to 30 ℃; the ventilation heating apparatus 9 stops operating. The air suction amount of the ventilation heating device 9 is not less than 50m3H is used as the reference value. The air exchange between the inside of the heat-insulating cabin body 1 and the outside of the heat-insulating cabin body 1 is forced through 2 shutters 12 and a ventilation heating device 9, so that the heat dissipation inside the equipment cabin is realized.
In the working process, the sum of electromagnetic shielding of the 2 windows of the louver 12 and the ventilation opening of the ventilation heating device 9 is not more than 40 dB.
The rear wall of the heat-insulation cabin body 1 is provided with a patch panel, the patch panel is provided with an electrical connector, and the electrical connection between the equipment in the equipment cabin and an external system is realized through the connector.
The details of the present invention not described in detail in the specification are well known to those skilled in the art.
Claims (10)
1. Integrated automatic temperature control equipment cabin, its characterized in that: comprises a heat-insulating cabin body (1), 4 open type cabinets (2), 3 door plates (3), a ventilation heating device (9), 2 temperature sensors (10) and 2 shutters (12); wherein, the heat-insulating cabin body (1) is a hollow cuboid structure which is horizontally arranged; 4 open cabinets (2) are fixedly arranged in the inner cavity of the heat-insulating cabin body (1) at intervals along the horizontal direction; a door panel (3) is fixedly arranged between every two adjacent open type cabinets (2); the ventilation heating device (9) is fixedly arranged at the top of the heat-insulation cabin body (1); the 2 temperature sensors (10) are respectively and fixedly installed at the top of the 2-side open type cabinet (2); 2 shutters (12) are fixedly arranged on the rear side wall of the heat preservation cabin body (1).
2. The compartment of claim 1, wherein: the distance between the temperature sensor (10) and the inner wall of the heat-insulating cabin body (1) is 350-360 mm.
3. The compartment of claim 2, wherein: the temperature measuring range of the temperature sensor (10) is-45-80 ℃; the measurement accuracy is +/-1 ℃.
4. The compartment of claim 3, wherein: the louver (12) is of a rectangular structure; the size of the louver (12) is 275mm x 410 mm; the distance between the fixed position of the shutter (12) and the inner wall of the heat-insulating cabin body (1) is 360-370 mm; the height from the bottom of the heat-insulating cabin body (1) is 330 mm and 340 mm.
5. The compartment of claim 4, wherein: when the internal temperature of the heat-insulating cabin body (1) is lower than a threshold value a, 2 shutters (12) are closed; the ventilation heating device (9) realizes the heating of the interior of the heat-insulating cabin body (1); until the temperature rises to a threshold value b, the ventilation heating device (9) stops working;
when the internal temperature of the heat-insulating cabin body (1) is higher than a threshold value c, 2 shutters (12) are opened; the ventilation heating device (9) realizes air suction, and exchanges air between the inside and the outside of the heat-insulation cabin body (1) to realize heat dissipation; until the temperature drops to a threshold d; the ventilation heating device (9) stops working.
6. The compartment of claim 5, wherein: the a is-25 ℃; b is-15 ℃.
7. The compartment of claim 6, wherein: the total power consumption of the ventilation heating device (9) is more than 500W; and less than 1300W.
8. The compartment of claim 7, wherein: the c is 35 ℃; d is 30 ℃.
9. The compartment of claim 8, wherein: the air extraction amount of the ventilation heating device (9) is not less than 50m3/h。
10. The compartment of claim 9, wherein: the electromagnetic shielding sum of the 2 louver (12) windows and the ventilation opening of the ventilation heating device (9) is not more than 40 dB.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921162237.4U CN211019719U (en) | 2019-07-23 | 2019-07-23 | Integrated automatic temperature control equipment cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921162237.4U CN211019719U (en) | 2019-07-23 | 2019-07-23 | Integrated automatic temperature control equipment cabin |
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| Publication Number | Publication Date |
|---|---|
| CN211019719U true CN211019719U (en) | 2020-07-14 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921162237.4U Active CN211019719U (en) | 2019-07-23 | 2019-07-23 | Integrated automatic temperature control equipment cabin |
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| CN (1) | CN211019719U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112833707A (en) * | 2021-01-04 | 2021-05-25 | 中国人民解放军海军航空大学岸防兵学院 | Missile launching box |
| CN113467547A (en) * | 2021-07-12 | 2021-10-01 | 哈尔滨工业大学 | Constant-temperature self-adaptive temperature control system for hot breaking of adhesive film |
| CN114312214A (en) * | 2021-12-16 | 2022-04-12 | 贵州航天电子科技有限公司 | Miniaturized integrated ventilation unit for equipment compartment |
-
2019
- 2019-07-23 CN CN201921162237.4U patent/CN211019719U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112833707A (en) * | 2021-01-04 | 2021-05-25 | 中国人民解放军海军航空大学岸防兵学院 | Missile launching box |
| CN112833707B (en) * | 2021-01-04 | 2023-09-08 | 中国人民解放军海军航空大学岸防兵学院 | Missile launching box |
| CN113467547A (en) * | 2021-07-12 | 2021-10-01 | 哈尔滨工业大学 | Constant-temperature self-adaptive temperature control system for hot breaking of adhesive film |
| CN114312214A (en) * | 2021-12-16 | 2022-04-12 | 贵州航天电子科技有限公司 | Miniaturized integrated ventilation unit for equipment compartment |
| CN114312214B (en) * | 2021-12-16 | 2024-03-12 | 贵州航天电子科技有限公司 | Ventilating device for small integrated equipment cabin |
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