CN205378482U - Punching press liquid cold die piece - Google Patents
Punching press liquid cold die piece Download PDFInfo
- Publication number
- CN205378482U CN205378482U CN201620126362.XU CN201620126362U CN205378482U CN 205378482 U CN205378482 U CN 205378482U CN 201620126362 U CN201620126362 U CN 201620126362U CN 205378482 U CN205378482 U CN 205378482U
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- gas
- liquid heat
- exchange
- water tank
- electronic equipment
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Abstract
The utility model relates to a punching press liquid cold die piece, electronic equipment cold drawing export in proper order through draw together water tank, water pump, flow switch, gas -liquid heat exchanger, pressure sensor, that temperature sensor connects back the electronic equipment cold drawing is imported, its characterized in that: the gas -liquid heat exchanger sets up in the covering is personally experienced sth. Part of the body to the aircraft cabin, sets up the ram air import and the ram air export of an intercommunication gas -liquid heat exchanger hot journey on the gas -liquid heat exchanger fore -and -after aircraft cabin body covering, another the hot journey connection flow sensor and the pressure sensor of gas -liquid heat exchanger, water pump, flow sensor, pressure sensor and temperature sensor are connected to the controller. Its simple structure need not to be equipped with the refrigeration compression, reduces design -manufacturing costs.
Description
Technical field
This utility model relates to a kind of liquid cooling apparatus, specifically a kind of punching press liquid cooled module.
Background technology
Along with the increase day by day that aviation requires, set electronic equipment in it and get more and more, necessarily cause improving constantly of its thermic load, in order to ensure safe handling and the life-span of electronic equipment, it is necessary to electronic equipment is cooled down.As adopted aircraft self air conditioning system to cool down, increase the weight of the load of aircraft self air conditioning system undoubtedly, affected air conditioning comfortableness in aircraft cabin.Air environment is cooled down by the independent refrigerant compression cooling system of existing employing, requires very strict to the restriction of the volume of cooling system, weight, electrical power, adds airplane design, manufacturing cost.
Summary of the invention
For deficiency of the prior art, this utility model provides a kind of simple in construction, it is not necessary to be equipped with refrigerant compression, reduces the punching press liquid cooled module of design and manufacture cost.
The technical solution adopted in the utility model is: a kind of punching press liquid cooled module, including water tank, water pump, flow switch, gas-liquid heat-exchange, pressure transducer, temperature sensor and controller, electronic equipment cold drawing exports successively through water tank, water pump, flow switch, gas-liquid heat-exchange, pressure transducer, temperature sensor connects back to electronic equipment cold drawing import, it is characterized in that: described gas-liquid heat-exchange is arranged in aircraft nacelle eyelid covering, aircraft nacelle eyelid covering before and after gas-liquid heat-exchange offers ram air inlet and the ram-air outlet of the connection hot journey of gas-liquid heat-exchange one, another hot journey connection traffic sensor and pressure transducer of gas-liquid heat-exchange, described controller connects water pump, flow transducer, pressure transducer and temperature sensor.
Further, it is provided with bleeding point between the outlet of described electronic equipment cold drawing and water tank.
Further, safety valve is set in described water tank.
Yet further, described water tank is provided with filling opening and tap hole.
Adopting above technical scheme, the beneficial effects of the utility model are: in aircraft flight, after ram-air is passed into a hot journey of gas-liquid heat-exchange by the ram air inlet of aircraft nacelle eyelid covering out of my cabin, discharge from ram-air outlet；After in electronic equipment cold drawing, refrigerating medium absorbs electronic equipment heat, refrigerating medium is delivered to water tank successively by the outlet of electronic equipment cold drawing, water pump is controlled by flow switch, refrigerating medium in water tank is delivered to another hot journey of gas-liquid heat-exchange by controller, with ram-air flow through one hot Cheng Huanre lower the temperature refrigerating medium, refrigerating medium sends electronic equipment cold drawing import back to through pressure transducer and temperature sensor, repeats to absorb electronic equipment heat in electronic equipment cold drawing；Deliver to the unlatching of the refrigerating medium flow of gas-liquid heat-exchange, pressure and temperature signal delivery controller control water pump, to guarantee that the enough cold of electronic equipment cold drawing carries out heat absorption cooling, effectively guarantee the heating cooling of electronic equipment, make full use of the outer ram-air of aircraft cabin, without refrigeration compressor set, reduce design and manufacture cost；Additionally set configuration safety valve, filling opening, tap hole on bleeding point and water tank before water tank, improve the delivery safety of refrigerating medium further, stablize.
Accompanying drawing explanation
Fig. 1 is this utility model structural representation.
In figure: electronic equipment cold drawing 1, cold drawing outlet 2, bleeding point 3, water tank 4, filling opening 5, tap hole 6, water pump 7, flow switch 8, controller 9, gas-liquid heat-exchange 10, pressure transducer 11, temperature sensor 12, cold drawing import 13, aircraft nacelle eyelid covering 14, ram air inlet 15, ram-air outlet 16.
Detailed description of the invention
Below in conjunction with drawings and Examples, the utility model is described in further detail.
Shown in Fig. 1: a kind of punching press liquid cooled module includes water tank 4, water pump 7, flow switch 8, gas-liquid heat-exchange 10, pressure transducer 9 and temperature sensor 11, gas-liquid heat-exchange 10 is arranged in aircraft nacelle eyelid covering 14, aircraft nacelle eyelid covering 14 before and after gas-liquid heat-exchange 10 offers ram air inlet 15 and the ram-air outlet 16 of the connection hot journey of gas-liquid heat-exchange 10 1, another hot journey input of gas-liquid heat-exchange 10 is through flow switch 8, water pump 7 and water tank 4 are connected to the cold drawing outlet 2 of electronic equipment cold drawing 1, another hot journey outfan of gas-liquid heat-exchange 9 is connected to the cold drawing import 13 of electronic equipment cold drawing 1 through pressure transducer 11 and temperature sensor 12, controller 9 connects water pump, flow transducer, pressure transducer and temperature sensor.It is provided with bleeding point 3 between electronic equipment cold drawing 1 cold drawing outlet 2 and water tank 4.Setting safety valve in water tank 4, water tank 4 is provided with filling opening 5 and tap hole 6.
Claims (4)
1. a punching press liquid cooled module, including water tank, water pump, flow switch, gas-liquid heat-exchange, pressure transducer, temperature sensor and controller, electronic equipment cold drawing exports successively through water tank, water pump, flow switch, gas-liquid heat-exchange, pressure transducer, temperature sensor connects back to electronic equipment cold drawing import, it is characterized in that: described gas-liquid heat-exchange is arranged in aircraft nacelle eyelid covering, aircraft nacelle eyelid covering before and after gas-liquid heat-exchange offers ram air inlet and the ram-air outlet of the connection hot journey of gas-liquid heat-exchange one, another hot journey connection traffic sensor and pressure transducer of gas-liquid heat-exchange, described controller connects water pump, flow transducer, pressure transducer and temperature sensor.
2. a kind of punching press liquid cooled module according to claim 1, is characterized in that: be provided with bleeding point between the outlet of described electronic equipment cold drawing and water tank.
3. a kind of punching press liquid cooled module according to claim 1 and 2, is characterized in that: set safety valve in described water tank.
4. a kind of punching press liquid cooled module according to claim 1 and 2, is characterized in that: described water tank is provided with filling opening and tap hole.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2015205667613 | 2015-07-31 | ||
| CN201520566761 | 2015-07-31 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205378482U true CN205378482U (en) | 2016-07-06 |
Family
ID=56270682
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620126362.XU Active CN205378482U (en) | 2015-07-31 | 2016-02-18 | Punching press liquid cold die piece |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205378482U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105007708A (en) * | 2015-07-31 | 2015-10-28 | 江苏宏基环电有限公司 | Pressing liquid cooling module |
| CN112078806A (en) * | 2020-09-25 | 2020-12-15 | 中国直升机设计研究所 | Helicopter liquid cooling integrated control system |
-
2016
- 2016-02-18 CN CN201620126362.XU patent/CN205378482U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105007708A (en) * | 2015-07-31 | 2015-10-28 | 江苏宏基环电有限公司 | Pressing liquid cooling module |
| CN112078806A (en) * | 2020-09-25 | 2020-12-15 | 中国直升机设计研究所 | Helicopter liquid cooling integrated control system |
| CN112078806B (en) * | 2020-09-25 | 2022-12-30 | 中国直升机设计研究所 | Helicopter liquid cooling integrated control system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 225400 Taizhou City, Taixing Province Economic Development Zone, Jiangxi Road, No. 1, Patentee after: Jiangsu Acer electric ring Limited by Share Ltd Address before: 225400 Taizhou City, Taixing Province Economic Development Zone, Jiangxi Road, No. 1, Patentee before: JIANGSU ACER RING ELECTRIC COMPANY LIMITED |