CN210822777U - Heat dissipation assembly for aircraft environment control system - Google Patents
Heat dissipation assembly for aircraft environment control system Download PDFInfo
- Publication number
- CN210822777U CN210822777U CN201921721370.9U CN201921721370U CN210822777U CN 210822777 U CN210822777 U CN 210822777U CN 201921721370 U CN201921721370 U CN 201921721370U CN 210822777 U CN210822777 U CN 210822777U
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- CN
- China
- Prior art keywords
- fixed mounting
- control system
- thick bamboo
- heat dissipation
- installation section
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 230000017525 heat dissipation Effects 0.000 title claims abstract description 17
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 57
- 238000009434 installation Methods 0.000 claims abstract description 44
- 230000007613 environmental effect Effects 0.000 claims abstract description 17
- 238000001816 cooling Methods 0.000 claims abstract description 16
- 239000000428 dust Substances 0.000 claims description 15
- 235000017166 Bambusa arundinacea Nutrition 0.000 abstract description 26
- 235000017491 Bambusa tulda Nutrition 0.000 abstract description 26
- 241001330002 Bambuseae Species 0.000 abstract description 26
- 235000015334 Phyllostachys viridis Nutrition 0.000 abstract description 26
- 239000011425 bamboo Substances 0.000 abstract description 26
- 241000883990 Flabellum Species 0.000 description 5
- 238000005265 energy consumption Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
Images
Classifications
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Abstract
The utility model belongs to the technical field of the aircraft, especially, be a radiator unit for aircraft environmental control system, including switch board, cooling body, pipeline and a plurality of air outlet nozzle, cooling body fixed mounting be in one side of switch board, pipeline fixed mounting be in on one side inner wall of switch board, it is a plurality of air outlet nozzle fixed mounting be in on the pipeline, cooling body includes fixed mounting and is in the installation section of thick bamboo of switch board one side, be equipped with the circulating pipe in the installation section of thick bamboo, the top fixed mounting of installation section of thick bamboo has the water tank, the top fixed mounting of installation section of thick bamboo has the suction pump, the one end of circulating pipe run through the installation section of thick bamboo and with suction pump fixed connection, fixed mounting has the inlet tube on the water tank, the one end of circulating pipe run through the installation section of thick bamboo. The utility model discloses simple structure is convenient for carry out high-efficient heat dissipation to the switch board, simultaneously through controller and temperature sensor, is convenient for reduce energy resource consumption.
Description
Technical Field
The utility model relates to an aircraft technical field especially relates to a radiator unit for aircraft environmental control system.
Background
An aircraft environmental control system, namely an aircraft environmental control system, is one of important airborne systems and takes on the task of providing a comfortable air environment for onboard personnel, and the environmental control system provides a sufficient comfortable survival and working environment for the aircrew and passengers by controlling parameters such as temperature, humidity, flow rate, pressure and the like of air in an aircraft cabin.
In the aircraft environmental control system, the switch board has played centralized control's effect, however the radiating mechanism of the switch board among the current aircraft environmental control system adopts cooling fan heat dissipation mostly, and the radiating effect is poor, and mostly for cooling fan rotates always to reach radiating purpose, this kind of heat dissipation mode is extravagant power relatively, for this reason, provides a radiator unit who is used for aircraft environmental control system.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcomings existing in the prior art, and providing a heat radiation component for an aircraft environmental control system.
In order to achieve the above purpose, the utility model adopts the following technical scheme: a heat dissipation assembly for an aircraft environmental control system comprises a control cabinet, a cooling mechanism, a pipeline and a plurality of air outlet nozzles, wherein the cooling mechanism is fixedly arranged on one side of the control cabinet, the pipeline is fixedly arranged on the inner wall of one side of the control cabinet, and the air outlet nozzles are fixedly arranged on the pipeline;
cooling body includes fixed mounting and is in the installation section of thick bamboo of switch board one side, be equipped with the circulating pipe in the installation section of thick bamboo, the top fixed mounting of installation section of thick bamboo has the water tank, the top fixed mounting of installation section of thick bamboo has the suction pump, the one end of circulating pipe run through the installation section of thick bamboo and with suction pump fixed connection, fixed mounting has the inlet tube on the water tank, the one end of circulating pipe run through the installation section of thick bamboo and with inlet tube fixed connection, be equipped with the motor in the installation section of thick bamboo, fixed mounting has the flabellum on the output shaft of motor, be equipped with the dust screen in the installation section of thick bamboo.
Preferably, an air inlet is formed in one side of the control cabinet, and the air inlet is matched with the mounting cylinder.
Preferably, a controller is fixedly mounted on one side of the control cabinet, and a temperature sensor is arranged on the inner wall of the top of the control cabinet.
Preferably, the water tank is provided with an installation pipe, and one end of the installation pipe is fixedly connected with the water suction pump.
Preferably, a water filling port is arranged on the water tank.
Preferably, the inner wall of the bottom of the installation cylinder is fixedly provided with a support seat, and the motor is fixedly arranged on the support seat.
Compared with the prior art, the beneficial effects of the utility model are that: firstly, a control cabinet, an installation barrel, a circulating pipe, a water tank, a water pump, a water inlet pipe, a motor, fan blades, a dust screen, a pipeline, air outlet nozzles, air inlet holes, a controller and a temperature sensor are matched, when the temperature sensor detects that the temperature exceeds a specified value, the controller controls the water pump and the motor to be started, the water pump pumps water in the water tank into the circulating pipe, air in the installation barrel is cooled through the circulating pipe, the water with heat flows back into the water tank through the water pump to be cooled, the water circulation is realized through the continuous work of the water pump, the air enters the installation barrel through the dust screen, the dust screen filters dust in the air, the motor is started, an output shaft of the motor drives the fan blades to rotate, the cooled air flows out of the pipeline through the air inlet holes on the pipeline, and dissipates heat of the control cabinet, the air flows out from the heat dissipation holes in the control cabinet, and when the temperature sensor detects that the temperature is lower than a specified value, the controller controls the water suction pump and the motor to be closed, so that energy consumption is saved.
The utility model discloses simple structure is convenient for carry out high-efficient heat dissipation to the switch board, simultaneously through controller and temperature sensor, is convenient for reduce energy resource consumption.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is an enlarged schematic view of a portion a of fig. 1.
In the figure: 1. a control cabinet; 2. mounting the cylinder; 3. a circulation pipe; 4. a water tank; 5. a water pump; 6. a water inlet pipe; 7. a motor; 8. a fan blade; 9. a dust screen; 10. a pipeline; 11. an air outlet nozzle; 12. an air inlet; 13. a controller; 14. a temperature sensor.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-2, the present invention provides a technical solution: a heat dissipation assembly for an aircraft environmental control system comprises a control cabinet 1, a cooling mechanism, a pipeline 10 and a plurality of air outlet nozzles 11, wherein the cooling mechanism is fixedly installed on one side of the control cabinet 1, the pipeline 10 is fixedly installed on the inner wall of one side of the control cabinet 1, and the air outlet nozzles 11 are fixedly installed on the pipeline 10;
cooling body includes fixed mounting and is in the installation section of thick bamboo 2 of 1 one side of switch board, be equipped with circulating pipe 3 in the installation section of thick bamboo 2, the top fixed mounting of installation section of thick bamboo 2 has water tank 4, the top fixed mounting of installation section of thick bamboo 2 has suction pump 5, the one end of circulating pipe 3 run through installation section of thick bamboo 2 and with suction pump 5 fixed connection, fixed mounting has inlet tube 6 on the water tank 4, the one end of circulating pipe 3 run through installation section of thick bamboo 2 and with inlet tube 6 fixed connection, be equipped with motor 7 in the installation section of thick bamboo 2, fixed mounting has flabellum 8 on the output shaft of motor 7, be equipped with dust screen 9 in the installation section of thick bamboo 2, dust screen 9 is located motor 7 and keeps.
The air inlet has been seted up to one side of switch board, the inlet port and installation section of thick bamboo looks adaptation, one side fixed mounting of switch board has the controller, be equipped with temperature sensor on the top inner wall of switch board, be equipped with the installation pipe on the water tank, the one end and the suction pump fixed connection of installation pipe, be equipped with the filler on the water tank, fixed mounting has the supporting seat on the bottom inner wall of installation section of thick bamboo, motor fixed mounting is on the supporting seat, and through the device's switch board 1, installation section of thick bamboo 2, circulating pipe 3, water tank 4, suction pump 5, inlet tube 6, motor 7, flabellum 8, dust screen 9, pipeline 10, air outlet 11, inlet port 12, controller 13 and temperature sensor 14 cooperate, when temperature sensor 14 detected the temperature and exceeded appointed value, controller 13 will control suction pump 5 and motor 7 and start, and suction pump 5 takes the water in the water tank 4 out to the circulating pipe 3 in, the air in the installation cylinder 2 is cooled through the circulating pipe 3, the water with heat flows back to the water tank 4 through the water suction pump 5 to be cooled, the water circulation is realized through the continuous work of the water suction pump 5, the air enters the installation cylinder 2 through the dustproof net 9, the dust in the air is filtered by the dustproof net 9, the motor 7 is started, the output shaft of the motor 7 drives the fan blade 8 to rotate, the cooled air is carried into the pipeline 10 through the air inlet hole 12 by the fan blade 8, the air flows out from the air outlet nozzles 11 on the pipeline 10 to dissipate the heat of the control cabinet 1, the air flows out from the heat dissipation holes on the control cabinet 1, when the temperature sensor 14 detects that the temperature is lower than a specified value, the controller 13 controls the water suction pump 5 and the motor 7 to be closed, thereby saving the energy consumption, the utility model discloses has simple structure, is convenient for carrying out high-efficiency heat dissipation on the control, is convenient for reducing energy consumption.
The working principle is as follows: the control cabinet 1 is provided with heat dissipation holes, a temperature sensor 14, a controller 13, a water pump 5, a motor 7 and an external power supply which are electrically connected through leads to form a closed loop;
when the temperature sensor 14 detects that the temperature exceeds a specified value, the controller 13 controls the water suction pump 5 and the motor 7 to be started, the water suction pump 5 pumps water in the water tank 4 into the circulating pipe 3, the air in the installation cylinder 2 is cooled through the circulating pipe 3, the water with heat flows back into the water tank 4 through the water suction pump 5 to be cooled, and the water suction pump 5 continuously works, so that water circulation is realized, and the air in the installation cylinder 2 is continuously cooled;
the air passes through dust screen 9 and gets into installation section of thick bamboo 2, dust screen 9 filters the dust in the air, then motor 7 starts, motor 7's output shaft drives flabellum 8 and rotates, flabellum 8 blows the air after the cooling to pipeline 10 in through inlet port 12, at last through a plurality of air outlet nozzle 11 on the pipeline 10 outflow, thereby dispel the heat to switch board 1, the air is flowed by the louvre on the switch board 1 at last, when temperature sensor 14 detects that the temperature is less than appointed value, controller 13 control suction pump 5 and motor 7 are closed, thereby practice thrift the energy consumption.
Above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the design of the present invention, equivalent replacement or change should be covered within the protection scope of the present invention.
Claims (6)
1. The utility model provides a radiator unit for aircraft environmental control system which characterized in that: the cooling device comprises a control cabinet (1), a cooling mechanism, a pipeline (10) and a plurality of air outlet nozzles (11), wherein the cooling mechanism is fixedly arranged on one side of the control cabinet (1), the pipeline (10) is fixedly arranged on the inner wall of one side of the control cabinet (1), and the air outlet nozzles (11) are fixedly arranged on the pipeline (10);
the cooling mechanism comprises an installation cylinder (2) fixedly installed on one side of the control cabinet (1), a circulating pipe (3) is arranged in the mounting cylinder (2), a water tank (4) is fixedly mounted at the top of the mounting cylinder (2), a water suction pump (5) is fixedly installed at the top of the installation cylinder (2), one end of the circulating pipe (3) penetrates through the installation cylinder (2) and is fixedly connected with the water suction pump (5), a water inlet pipe (6) is fixedly arranged on the water tank (4), one end of the circulating pipe (3) penetrates through the mounting cylinder (2) and is fixedly connected with the water inlet pipe (6), a motor (7) is arranged in the mounting cylinder (2), the output shaft of the motor (7) is fixedly provided with fan blades (8), and a dust screen (9) is arranged in the mounting cylinder (2), and the dust screen (9) is positioned on one side of the motor (7) far away from the circulating pipe (3).
2. The heat dissipation assembly for an aircraft environmental control system according to claim 1, wherein: an air inlet (12) is formed in one side of the control cabinet (1), and the air inlet is matched with the mounting cylinder (2).
3. The heat dissipation assembly for an aircraft environmental control system according to claim 1, wherein: one side fixed mounting of switch board (1) has controller (13), be equipped with temperature sensor (14) on the top inner wall of switch board (1).
4. The heat dissipation assembly for an aircraft environmental control system according to claim 1, wherein: the water tank (4) is provided with an installation pipe, and one end of the installation pipe is fixedly connected with the water suction pump (5).
5. The heat dissipation assembly for an aircraft environmental control system according to claim 1, wherein: and a water filling port is arranged on the water tank (4).
6. The heat dissipation assembly for an aircraft environmental control system according to claim 1, wherein: the inner wall of the bottom of the installation cylinder (2) is fixedly provided with a supporting seat, and the motor (7) is fixedly arranged on the supporting seat.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921721370.9U CN210822777U (en) | 2019-10-15 | 2019-10-15 | Heat dissipation assembly for aircraft environment control system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921721370.9U CN210822777U (en) | 2019-10-15 | 2019-10-15 | Heat dissipation assembly for aircraft environment control system |
Publications (1)
Publication Number | Publication Date |
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CN210822777U true CN210822777U (en) | 2020-06-23 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201921721370.9U Expired - Fee Related CN210822777U (en) | 2019-10-15 | 2019-10-15 | Heat dissipation assembly for aircraft environment control system |
Country Status (1)
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CN (1) | CN210822777U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112218487A (en) * | 2020-09-10 | 2021-01-12 | 济南职业学院 | Energy-saving electrical automation control system |
CN112804844A (en) * | 2021-02-08 | 2021-05-14 | 石家庄邮电职业技术学院 | Heat radiation communication cabinet |
-
2019
- 2019-10-15 CN CN201921721370.9U patent/CN210822777U/en not_active Expired - Fee Related
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112218487A (en) * | 2020-09-10 | 2021-01-12 | 济南职业学院 | Energy-saving electrical automation control system |
CN112804844A (en) * | 2021-02-08 | 2021-05-14 | 石家庄邮电职业技术学院 | Heat radiation communication cabinet |
CN112804844B (en) * | 2021-02-08 | 2022-03-29 | 石家庄邮电职业技术学院 | Heat radiation communication cabinet |
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200623 |
|
CF01 | Termination of patent right due to non-payment of annual fee |