CN103851729A - Aviation air conditioning vehicle system for ship - Google Patents
Aviation air conditioning vehicle system for ship Download PDFInfo
- Publication number
- CN103851729A CN103851729A CN201410046419.0A CN201410046419A CN103851729A CN 103851729 A CN103851729 A CN 103851729A CN 201410046419 A CN201410046419 A CN 201410046419A CN 103851729 A CN103851729 A CN 103851729A
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- air
- conditioning system
- evaporimeter
- aviation
- air conditioning
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- 238000004378 air conditioning Methods 0.000 title claims abstract description 59
- 238000001816 cooling Methods 0.000 claims abstract description 25
- 239000007788 liquid Substances 0.000 claims description 8
- 238000010438 heat treatment Methods 0.000 claims description 5
- 238000001035 drying Methods 0.000 claims description 4
- 238000001914 filtration Methods 0.000 claims description 4
- 238000005057 refrigeration Methods 0.000 abstract description 8
- 230000000694 effects Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000009897 systematic effect Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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- Air Conditioning Control Device (AREA)
Abstract
The invention relates to an aviation air conditioning vehicle system for a ship. The aviation air conditioning vehicle system comprises an air supply system, a cooling system and an electric control system, wherein the air supply system comprises an air inlet, a plate type filter, a first-stage air conditioning system and a Roots blower, the cooling system comprises a second-stage air conditioning system, a third-stage air conditioning system and an air outlet pipeline, the electric control system comprises an electric control box, a humidity sensor and a temperature sensor, the plate type filter and the first-stage air conditioning system are adopted for realizing the pretreatment on the air in the environment, the treated air is blown into the cooling system through the Roots blower, the refrigeration effect of the equipment is improved through the multi-stage air conditioning system, and finally, the work mode of each stage of air conditioning system is controlled according to the refrigeration requirements by the temperature and humidity sensors in the air outlet pipeline via the electric control system. The aviation air conditioning vehicle system for the ship has the advantages that the air supply pressure is high, the refrigeration effect is good, the energy sources are saved, the temperature and humidity control is precise, and the work reliability is high.
Description
Technical field
The present invention relates to field of air conditioning, be specifically related to a kind of naval vessel aviation air-conditioned coach system.
Background technology
On naval vessel, be the equipment of fixed bit for aircraft provides low-temperature receiver at present, get new wind from environment, after aviation aircondition is processed, deliver to the position that needs dehumidifying or temperature adjustment on aircraft.When aircraft on deck some specific region or or the aviation aircondition of fixed bit while breaking down, the aviation aircondition of fixed bit can not provide the dehumidifying of needs or the air of temperature adjustment for aircraft, just need to, by air-conditioned coach traction to specific position, come for aircraft service.The pressure of the cold air that existing all kinds of aviation air-conditioned coaches provide is at present lower, can only pass into enough wind to conventional aircraft, just cannot provide to blower fan inside enough cold air, or the air themperature providing does not reach requirement once run into the air pipeline that flow resistance is large.
Summary of the invention
The object of the present invention is to provide a kind of naval vessel aviation air-conditioned coach system.
The technical scheme that the present invention takes is:
Aviation air-conditioned coach system for a kind of naval vessel, comprise air feed system, cooling system and electric control system, it is characterized in that: described air feed system comprises air inlet, leaf filter, first order air-conditioning system and roots blower, described air inlet connects the air inlet of roots blower successively through the evaporimeter of leaf filter, first order air-conditioning system;
Described cooling system comprises second level air-conditioning system, third level air-conditioning system and wind pipe, and the air outlet of roots blower is communicated with wind pipe through the evaporimeter of second level air-conditioning system, the evaporimeter of third level air-conditioning system successively;
Described electric control system comprises electric control box, humidity sensor and temperature sensor, in connecting pipe in connecting pipe between the evaporimeter of described first order air-conditioning system and roots blower air inlet, between air outlet and the cooling system of Roots's wind, between the evaporimeter of second level air-conditioning system and the evaporimeter of third level air-conditioning system, between the evaporimeter and wind pipe of third level air-conditioning system, be equipped with temperature sensor on cooling system wind pipe, described cooling system wind pipe is also provided with humidity sensor.
Further, described air-conditioning system comprises the compressor, condenser, liquid reservoir, device for drying and filtering, expansion valve, evaporimeter and the gas-liquid separator that are connected to successively loop through pipeline.
Further, the condenser of described air-conditioning system outside is provided with more than one axial flow blower.
Further, described wind pipe is divided into two, between the evaporimeter of any or two and third level air-conditioning system, is provided with heater.Any one or two wind pipes are provided with electrical heating.
Further, on described wind pipe, be also provided with the flow sensor, pressure sensor and the volume damper that all connect electric control box.
Again further, described roots blower and cooling system connecting pipe are provided with check valve.
Take after above technical scheme, beneficial effect of the present invention is:
(1) for the air quality the present invention who ensures air feed takes leaf filter and one-level air-conditioning system to carry out pretreatment to the air in environment, air after treatment blasts cooling system through roots blower, use roots blower can guarantee cooling time the cold air of high pressure, large flow can be provided, for aircraft provides enough cold air.
(2) naval vessel is provided with three grades of air-conditioning systems by aviation air-conditioned coach system, improve the refrigeration of equipment, the air outlet of air-conditioning systems at different levels is provided with temperature sensor, under the control of electric control system, need to control the working method of air-conditioning systems at different levels according to refrigeration, save the energy, avoided waste; The condenser outside of air-conditioning systems at different levels is provided with many group axial flow blowers, can adjust according to demand the quantity of axial flow operation, and condenser is fully dispelled the heat, and improves refrigeration.
(3) between the evaporimeter of third level air-conditioning system and wind pipe, be provided with heater, heater is finely tuned the temperature and humidity of the air after refrigeration under the control of electric control system, ensures the quality of system cooling; Coordinate on arbitrary wind pipe, electrical heating to be set and to finely tune on wind pipe, further guarantee quality.
(4) naval vessel is provided with humidity sensor, flow sensor and pressure sensor with the wind pipe that aviation air-conditioned coach system is provided with three grades of air-conditioning systems, can regulate the flow of cooling-air and pressure, humidity sensor feeds back to electric control system by the humidity of cooling-air and regulates.
Naval vessel provided by the invention possesses for wind pressure large by aviation air-conditioned coach system, good refrigeration effect, and temperature humidity control is accurate, and functional reliability is high.
Brief description of the drawings
Fig. 1 is the schematic diagram of air-conditioning system;
Fig. 2 is systematic schematic diagram of the present invention.
In Fig. 1: compressor 41, condenser 42, liquid reservoir 43, device for drying and filtering 44, expansion valve 45, evaporimeter 46, gas-liquid separator 47, axial flow blower 48.
In Fig. 2: leaf filter 1, first evaporator 2, roots blower 3, first order air-conditioning system 4, second level air-conditioning system 5, third level air-conditioning system 6, second level evaporimeter 7, third evaporator 8, heater 9, electrical control cabinet 10, temperature sensor 11, flow sensor 12, electrical heating 13, humidity sensor 14, pressure sensor 15, volume damper 16, wind pipe 17.
Detailed description of the invention
Below in conjunction with accompanying drawing, the specific embodiment of the present invention is further described:
As shown in Figure 1-2, a kind of naval vessel comprises air feed system, cooling system and electric control system by aviation air-conditioned coach system, described air feed system comprises leaf filter 1, first evaporator 2, roots blower 3 and first order air-conditioning system 4, outdoor air is serially connected with first order air-conditioning system 4 evaporimeters 2 from air inlet after leaf filter 1 filters, cooling blasts cooling system by roots blower 3 after processing, and the connecting pipe between roots blower 3 and cooling system is provided with check valve.
Cooling system comprises second level air-conditioning system 5, third level air-conditioning system 6, second level evaporimeter 7, third evaporator 8 and heater 9, described second level evaporimeter 7 is serially connected with second level air-conditioning system 5, third evaporator 8 is serially connected with third level air-conditioning system 6, second level air-conditioning system 5 and third level air-conditioning system 6 are arranged in parallel, roots blower 3 blast through pretreated air successively by cabin being lowered the temperature through two wind pipe 17 air-out respectively after second level evaporimeter 7, third evaporator 8 and heater 9, another root wind pipe is provided with electrical heating 13.
Described three grades of air-conditioning systems are for being arranged in parallel, it is compressor 41, condenser 42, liquid reservoir 43, device for drying and filtering 44, expansion valve 45, evaporimeter 46 and the gas-liquid separator 47 in loop that air-conditioning systems at different levels include serial connection successively, and the outside of condenser is provided with the axial flow blower 48 of two groups of parallel connections.
Electric control system comprises electrical control cabinet 10, temperature sensor 11, flow sensor 12, humidity sensor 14 and pressure sensor 15, the outside of leaf filter 1 is provided with humidity sensor 14, in connecting pipe between first evaporator 2 and roots blower 3 air inlets, be provided with temperature sensor 11, connecting pipe between roots blower 3 and cooling system is provided with temperature sensor 11, between described second level evaporimeter 7 and third evaporator 8, be provided with temperature sensor 11, between described third evaporator and electric heater, be provided with temperature sensor 11.Described cooling system wind pipe 17 is provided with flow sensor 12, humidity sensor 14, pressure sensor 15 and volume damper 16, and electric control system is by the quantity of the work of three grades of air-conditioning systems of FEEDBACK CONTROL, volume damper, heater, electrically heated duty and the axial flow blower of temperature, humidity, flow or pressure to each sensor.
Claims (7)
1. an aviation air-conditioned coach system for naval vessel, comprises air feed system, cooling system and electric control system, it is characterized in that:
Described air feed system comprises air inlet, leaf filter, first order air-conditioning system and roots blower, and described air inlet connects the air inlet of roots blower successively through the evaporimeter of leaf filter, first order air-conditioning system;
Described cooling system comprises second level air-conditioning system, third level air-conditioning system and wind pipe, and the air outlet of roots blower is communicated with wind pipe through the evaporimeter of second level air-conditioning system, the evaporimeter of third level air-conditioning system successively;
Described electric control system comprises electric control box, humidity sensor and temperature sensor, in connecting pipe in connecting pipe between the evaporimeter of described first order air-conditioning system and roots blower air inlet, between air outlet and the cooling system of Roots's wind, between the evaporimeter of second level air-conditioning system and the evaporimeter of third level air-conditioning system, between the evaporimeter and wind pipe of third level air-conditioning system, be equipped with temperature sensor on cooling system wind pipe, described cooling system wind pipe is also provided with humidity sensor.
2. aviation air-conditioned coach system for a kind of naval vessel according to claim 1, is characterized in that, described air-conditioning system comprises the compressor, condenser, liquid reservoir, device for drying and filtering, expansion valve, evaporimeter and the gas-liquid separator that are connected to successively loop through pipeline.
3. aviation air-conditioned coach system for a kind of naval vessel according to claim 2, is characterized in that, the condenser outside of described air-conditioning system is provided with more than one axial flow blower.
4. aviation air-conditioned coach system for a kind of naval vessel according to claim 1, is characterized in that, described wind pipe is divided into two, between the evaporimeter of any or two and third level air-conditioning system, is provided with heater.
5. aviation air-conditioned coach system for a kind of naval vessel according to claim 4, is characterized in that, any one or two wind pipes are provided with electrical heating.
6. according to aviation air-conditioned coach system for a kind of naval vessel described in claim 1 or 4 or 5, it is characterized in that, on described wind pipe, be also provided with the flow sensor, pressure sensor and the volume damper that all connect electric control box.
7. aviation air-conditioned coach system for a kind of naval vessel according to claim 1, is characterized in that, described roots blower and cooling system connecting pipe are provided with check valve.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410046419.0A CN103851729A (en) | 2014-02-10 | 2014-02-10 | Aviation air conditioning vehicle system for ship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410046419.0A CN103851729A (en) | 2014-02-10 | 2014-02-10 | Aviation air conditioning vehicle system for ship |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103851729A true CN103851729A (en) | 2014-06-11 |
Family
ID=50859692
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410046419.0A Pending CN103851729A (en) | 2014-02-10 | 2014-02-10 | Aviation air conditioning vehicle system for ship |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103851729A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113280521A (en) * | 2021-04-22 | 2021-08-20 | 北京航天发射技术研究所 | Movable full fresh air conditioner |
| CN114709514A (en) * | 2022-04-01 | 2022-07-05 | 广船国际有限公司 | Ship power battery ventilation system and ship |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1776308A (en) * | 2005-11-29 | 2006-05-24 | 广东省吉荣空调设备公司 | Aircraft floor air conditioner set |
| JP2009537779A (en) * | 2006-05-19 | 2009-10-29 | ルブラン−ニミ アン アブレジェ ルブラン ソシエテ アノニム | Air conditioning unit and air conditioning method |
| CN202244116U (en) * | 2011-09-10 | 2012-05-30 | 西安飞豹科技发展公司 | Pull-type aircraft air-conditioning vehicle |
| CN202244115U (en) * | 2011-09-10 | 2012-05-30 | 西安飞豹科技发展公司 | High-pressure air cycle machine |
| CN103332298A (en) * | 2013-06-27 | 2013-10-02 | 广东申菱空调设备有限公司 | Variable frequency high-precision aircraft ground air conditioning unit and control method thereof |
| CN103407578A (en) * | 2013-08-09 | 2013-11-27 | 广东申菱空调设备有限公司 | Ground air conditioner vehicle of frequency conversion plane |
| CN203687263U (en) * | 2014-02-10 | 2014-07-02 | 中船重工天禾船舶设备江苏有限公司 | Aviation air conditioning vehicle system for ships |
-
2014
- 2014-02-10 CN CN201410046419.0A patent/CN103851729A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1776308A (en) * | 2005-11-29 | 2006-05-24 | 广东省吉荣空调设备公司 | Aircraft floor air conditioner set |
| JP2009537779A (en) * | 2006-05-19 | 2009-10-29 | ルブラン−ニミ アン アブレジェ ルブラン ソシエテ アノニム | Air conditioning unit and air conditioning method |
| CN202244116U (en) * | 2011-09-10 | 2012-05-30 | 西安飞豹科技发展公司 | Pull-type aircraft air-conditioning vehicle |
| CN202244115U (en) * | 2011-09-10 | 2012-05-30 | 西安飞豹科技发展公司 | High-pressure air cycle machine |
| CN103332298A (en) * | 2013-06-27 | 2013-10-02 | 广东申菱空调设备有限公司 | Variable frequency high-precision aircraft ground air conditioning unit and control method thereof |
| CN103407578A (en) * | 2013-08-09 | 2013-11-27 | 广东申菱空调设备有限公司 | Ground air conditioner vehicle of frequency conversion plane |
| CN203687263U (en) * | 2014-02-10 | 2014-07-02 | 中船重工天禾船舶设备江苏有限公司 | Aviation air conditioning vehicle system for ships |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113280521A (en) * | 2021-04-22 | 2021-08-20 | 北京航天发射技术研究所 | Movable full fresh air conditioner |
| CN114709514A (en) * | 2022-04-01 | 2022-07-05 | 广船国际有限公司 | Ship power battery ventilation system and ship |
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| PB01 | Publication | ||
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| RJ01 | Rejection of invention patent application after publication | ||
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Application publication date: 20140611 |