CN101581484B - Duel cold sources airplane ground energy-conserving and environment-protective air-conditioning system - Google Patents
Duel cold sources airplane ground energy-conserving and environment-protective air-conditioning system Download PDFInfo
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- CN101581484B CN101581484B CN200910059575XA CN200910059575A CN101581484B CN 101581484 B CN101581484 B CN 101581484B CN 200910059575X A CN200910059575X A CN 200910059575XA CN 200910059575 A CN200910059575 A CN 200910059575A CN 101581484 B CN101581484 B CN 101581484B
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- 238000004378 air conditioning Methods 0.000 title claims abstract description 52
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 59
- 230000006835 compression Effects 0.000 claims abstract description 8
- 238000007906 compression Methods 0.000 claims abstract description 8
- 238000005057 refrigeration Methods 0.000 claims abstract description 7
- 238000007664 blowing Methods 0.000 claims description 5
- 238000001035 drying Methods 0.000 claims description 4
- 238000001914 filtration Methods 0.000 claims description 4
- 238000009413 insulation Methods 0.000 claims description 4
- 238000002156 mixing Methods 0.000 claims description 2
- 230000007306 turnover Effects 0.000 claims description 2
- 238000005265 energy consumption Methods 0.000 abstract description 5
- 239000003507 refrigerant Substances 0.000 abstract description 5
- 230000009977 dual effect Effects 0.000 abstract 1
- 238000001816 cooling Methods 0.000 description 8
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- 229910000831 Steel Inorganic materials 0.000 description 3
- 230000002950 deficient Effects 0.000 description 3
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- 230000005611 electricity Effects 0.000 description 1
- 238000004134 energy conservation Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
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- 238000002309 gasification Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000036541 health Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 229940074869 marquis Drugs 0.000 description 1
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Abstract
The invention relates to a dual cold sources airplane ground energy-conserving and environment-protective air-conditioning system, which solves the problems of high energy consumption, parking apron occupation and high operating cost in prior airplane ground air-conditioning unit. The system consists of a first air processing system and a second air processing system in compression refrigeration type; wherein, the first air processing system takes water supplied by a central air conditioner as heat transferring medium; the second air processing system in compression refrigeration type takes refrigerant as heat transferring medium. In the first processing system, a water-through heat exchanger (7) is injected with water from the central air conditioner of airport lounges by a pump (8) to carry out heat exchange with air from airport lounges or gallery bridge channel; the cooled air is transmitted into an engine room parked in the airport driven by a centrifugal fan (6) through a evaporator, an air outlet hood (1) and a underground passage; water after heat exchange by the water-through heat exchanger (7) is directly or through a double pipes heat exchanger to discharge into a water-storing system of the central air conditioner in airport lounges. The first processing system and the second processing system are located in the airport lounges. An underground passage system comprises an air supply duct with an insulating layer (22) buried under landing field outdoor, one end of the air supply duct is connected with the air supply tube (1), and the other end thereof is connectedwith a tube (23).
Description
Technical field:
The present invention is relevant with Air Ground Equipment, and especially the air-conditioning system of using on the ground with aircraft is relevant.
Background technology:
Bridge hanging type, fixed or movable air conditioner system are all adopted to the air-treatment of ground interior of aircraft in each big airport now.The bridge hanging type air-conditioning system is lifted under the connecting bridge, and unit and air supplying hose move with connecting bridge and move.Fixed air-conditioning system is installed on by the connecting bridge vertical columns, and the movable air conditioner system is movable to the aircraft stop position.
1. the defective that exists of bridge hanging type air-conditioning system and mounting means:
A. be hung under the connecting bridge because of this unit, limited by the water source, can not make the water-cooled unit, can only be forced air-cooled air-conditioning, 3～5 tons of the unit weight of different colds, therefore require connecting bridge should have higher structural strength, bearing capacity and good anti-shake performance, must increase steel plate thickness, high-caliber welding procedure.
B. unit is installed under the movable bridge, requires lifting column should have sufficiently high hydraulic-driven and just can make connecting bridge move to the aircraft stop position.
C. unit blasting air flexible pipe folding and unfolding inconvenience, wearing and tearing are big, fed distance far away, temperature rise, take machine level ground area, are unfavorable for vehicle dealing process, have certain unsafe factor.
More than several point defects cause the airport construction cost to increase by 300,000～600,000 yuan, the annual 100000 yuan/platform of operating cost that increases is higher than the air-conditioning cost of investment far away.
2. the defective that exists of the fixed air-conditioning system in ground:
A. the same with the bridge hanging type unit, limited by the water source, can only be forced air-cooled air-conditioning, volume is big, is installed in connecting bridge vertical columns next door, takies the machine level ground than large tracts of land.
B. occupy the stand of aircraft draw bar and various dollies, the machine level ground is more crowded, causes unsafe factor also for simultaneously the various vehicles of being to and under the connecting bridge, against the important caution of airport " safety first ".
C. install on ground, and the air supplying hose fed distance is far away, and wearing and tearing are big, temperature rise, and the unit power consumption increases by 10%, and annual operating cost increases about 100,000 yuan.
3. the defective that exists of movable air conditioner system:
Limited by the water source, unit is forced air-cooled air-conditioning, and volume is big, and weight is generally at 5～8 tons, and selected carrying capacity of chassis is also bigger, increases the unit cost.
B. because unit volume is bigger, take the certain area of aircraft anchor point, and cause unsafe factor can for aircraft and other supply vehicle.
C. if unit for carrying generating set, then can cause machine level ground noise big, the waste gas that generating set is discharged causes airport environment to pollute, and influences the Normal Take-Off And Landing of aircraft when serious.
D. if unit does not carry generating set, then need external power supply, longer according to the required cable of aircraft stop position, twisted and released of the cable is extremely inconvenient, and causes certain obstruction and unsafe factor to vehicular traffic.
E. unit energy consumption height, air supplying hose is longer, 5～7 ℃ of temperature rises, noise is big, and the condensed water discharging is inconvenient, causes the environmental pollution of machine level ground.
Summary of the invention:
The purpose of this invention is to provide a kind of energy savings, reduce to pollute, use and construction cost low, do not take the airport area, safe in utilization, Duel cold sources airplane ground energy-conserving and environment-protective air-conditioning system easily.
The present invention is achieved in that
Duel cold sources airplane ground energy-conserving and environment-protective air-conditioning system of the present invention; be water-cooled first air treatment system of heat transferring medium and be that compression refrigeration formula second air treatment system of heat transferring medium is formed with the cold-producing medium by the cold water that provides with central air-conditioning; air-conditioning system first air treatment system has channelling water heat exchanger 7 to inject from terminal central air-conditioning cold water and air from terminal or shelter bridge passage through water pump 8 to carry out heat exchange; the evaporimeter that cooled air is driven through second air treatment system by centrifugal blower 6; outlet housing 2; air supplying hose 1 and underpass system send in the aircraft storehouse; water after 7 heat exchange of channelling water heat exchanger directly or through double pipe heat exchanger 10 drains into terminal central air-conditioning water retention system; first; two air treatment systems are positioned at terminal; the underpass system comprises the band heat-insulation layer air supply duct 22 that is embedded in outdoor airplane parking area; air supply duct one end links to each other with air supplying hose 1, and the other end of air supply duct 22 links to each other with flexible pipe 23.
Channelling water heat exchanger 7 is in parallel two, and the air inlet evaporimeter outer and that the centrifugal blower air outlet is outer that lays respectively at centrifugal blower 6 both sides is arranged in a triangle.
Between outlet housing 2 and the evaporimeter 4 electric heater 3 is arranged, after the channelling water heat exchanger heats outside air, provide hot-air by flexible pipe for aircraft through fan housing 2 through evaporimeter 4 and electric heater heating again.
Below the ambient temperature value of setting, the first air treatment system work, the ambient temperature value of setting and more than, first and second air treatment system is all worked.
The fixing card 25 of joint under the cover plate of the exposed junction of described flexible pipe 23 and bounce device 24 is connected; when not blowing; depress the cover plate of bounce device 24, flexible pipe is contracted in the vertical shaft 26, during air-supply; carry on the cover plate of bounce device 24; retaining bar 29 fork manually is connected joint 30 with joint on the aircraft, it is underground that drip pipe road 28 is embedded in the airplane parking area; one end is connected with silo bottom, and an end has magnetic valve 27 and is connected with the central air-conditioning water retention system.
Evaporimeter one end low-pressure filter 20 is connected with compressor 14, or/and double pipe heat exchanger 10 is connected with compressor 14, perhaps the other end of evaporimeter is connected with compressor 14 through expansion valve 21, second magnetic valve 17 other end through expansion valve 21, first magnetic valve 17, hand valve 16, device for drying and filtering 15, reservoir 13.
The present invention is applicable to that the airport connecting bridge can be light bridge, and is less demanding to bearing capacity and structural strength, do not take the confined space of machine level ground and connecting bridge, energy-conservation environmental protection again.
The present invention has following characteristics:
1. energy consumption is low, the refrigerating efficiency height.Energy Efficiency Ratio was about 1.0 when traditional forced air-cooled air-conditioning system was used the R134a cold-producing medium, when using the R22 cold-producing medium Energy Efficiency Ratio between 1.5～2.2, the energy consumption height, refrigerating efficiency is low.And this unit (ADW) Energy Efficiency Ratio can reach more than 3.5.
2. build, operating cost is low, appearance and size is little, in light weight, energy-saving and environmental protection, noise are low.Only need when this unit (ADW) is installed that two water pipes advance with the terminal central air-conditioning, return water system is connected, installation simply, and is easy to operate.Compare with traditional forced air-cooled air-conditioning system, the unit of identical refrigerating capacity can use environment friendly refrigerating fluid R134a to replace R22 fully, and the unit cost reduces by 35%, and appearance and size reduces 20%, and the same terms is saved operating cost 40% down.
3. this unit (ADW) can be installed in the less place, position, angle of terminal, and it is little to take up room, and noise is about 60dB (A) during operation.Therefore the user can replace heavy connecting bridge with light-duty connecting bridge fully, and cost of investment saves about 30%, improves the security of connecting bridge.
4. when adopting the cold-storage technology as if the terminal central air-conditioning, can avoid electrical network on daytime " peak phase " load, utilize electrical network at night " paddy phase " load, make full use of the different electrovalence policies of peak valley phase that government is just implementing.According to statistics, the valley period power valency only is equivalent to 1/2 even 1/5 of peak phase electricity price.To make the user save operating cost about 50% like this.
5. because of this unit is installed in the terminal, new wind comes from terminal, can effectively reduce unit load, energy efficient 20%.
6. underpass system (GSS) is connected with the air-conditioning unit for aircraft provides through cooling, dehumidifying, fresh, comfortable air duct, and air supply duct is embedded in subterranean layer.One of this system is connected with ADW, and the other end then is placed in machine level ground aircraft stop position, and the aircraft joint stretches out by bounce device or the terrace of withdrawing, and bounce device is return the back and flushed fully with the airplane parking area, ensures that the airplane parking area use is unblocked.Structural representation is as figure (two).
7. do not take the airplane parking area area, can effectively solve the airplane parking area congested problem, aircraft is stopped convenient, does not have any unsafe factor and exists.
8. air supplying hose is easy to operate, acts freely, and it is little to wear and tear.
9. passage good heat insulating, its temperature rise is put aerial air supplying hose temperature rise far below dew, energy efficient about 10%.
10. this system is of a specified duration service life, can save material consumption about 10%.
Two refrigeration source airplane ground energy-conserving and environment-protective air-conditioning systems are used for big airport, have the following advantages:
A. effectively save airport construction and operating cost, make full use of terminal or shelter bridge return air, and central air-conditioning cold water, reduce the unit energy consumption greatly, solve the not enough problem of airport supply of electric power.Every equal cold unit uses this system will save construction cost 50～800,000 yuan, saves operating cost and material and consumes 150,000 yuan/year.
B. save and built machine level ground, airport area, reduce machine level ground congested problem, for parking of other vehicle provides the space.
The existence of unsafe factor when c. having avoided takeoff and landing improves the passing security of other vehicle simultaneously.
D. operation, convenience easy to maintenance are increased work efficiency greatly, save human resources.
E. reduce environmental pollution, improve human health.
Therefore, two refrigeration source airplane ground energy-conserving and environment-protective air-conditioning systems are truly efficient, energy-saving and environmental protection, air-conditioning system easily and efficiently.
Description of drawings:
Fig. 1 is air treatment system figure of the present invention.
Fig. 2 is a underpass system schematic of the present invention.
Fig. 3 is the bounce device structure chart.
The specific embodiment:
The present invention is made up of two parts: 1. Duel cold sources airplane ground energy-conserving and environment-protective air-conditioning unit (ADM); 2. underpass system (GSS).
1. Duel cold sources airplane ground energy-conserving and environment-protective air-conditioning system (ADW) is to utilize departure hall central air-conditioning cold water (the certain density ethylene glycol-aqueous solution or the NaCl-aqueous solution) to regulate air themperature by channelling water heat exchanger and evaporimeter, for aircraft provides aircondition comfortable, fresh air.
This unit is by cold water is provided with central air-conditioning is the multi-level water cooling formula air treatment system of heat transferring medium and be that the steam compression type air treatment system of heat transferring medium is formed with the cold-producing medium.Two systems comprise as lower member:
The 1-air supplying hose; The 2-outlet housing; The 3-heater; 4,5-steam compression type evaporimeter; The 6-centrifugal blower; 7-channelling water heat exchanger; The 8-water pump; The 9-magnetic valve; The 10-double pipe heat exchanger; 11,18-shock-absorbing pipe; 12-high and low pressure force controller; The 13-reservoir; The 14-compressor; The 15-device for drying and filtering; The 16-ball valve; The 17-magnetic valve; The 19-liquid-sighting glass; The 20-filter; The 21-expansion valve
Operation principle: when environment temperature is higher than more than 30 ℃, outside air is the cooling for the first time of process channelling water heat exchanger 7 surfaces, dehumidifying earlier under the effect of centrifugal blower 6, air after the cooling is again through steam compression type evaporimeter 4,5 cooling for the second time, further the cooling air reaches the requirement of wind pushing temperature at last.Be pressed into channelling water heat exchanger 7 from terminal central air-conditioning cold water by water pump 8, carry out with outside air that leaving water temperature raises after the heat exchange, enter double pipe heat exchanger 10 and carry out heat exchange with the high-temperature high-pressure refrigerant steam, water temperature further raises, and is extracted out by water pump at last to drain in the terminal central air-conditioning return water system.When ambient temperature was lower than 30 ℃, outside air only needed to carry out the requirement that heat exchange just can reach the unit blasting air temperature with channelling water heat exchanger 7, and this moment, vapor compression type refrigerating system did not participate in the air cooling.
The low-temperature low-pressure refrigerant steam that comes out from evaporimeter passes through suction line, the filter 20 of flowing through, wall shake pipe 18 is inhaled into compressor 14, be compressed into high temperature and high pressure gas by compressor again, high-temperature high-pressure refrigerant enters double pipe heat exchanger 10 by discharge duct, the cold water that liberated heat is flowed through is wherein taken away, cold-producing medium is cooled into liquid, through liquid line, reservoir 13, device for drying and filtering 15, ball valve 16, magnetic valve 17 arrives expansion valve 21 places, liquid refrigerant is become the gas-liquid mixture of low temperature and pressure by the throttling step-down, enter evaporimeter 4 and carry out heat exchange with the surperficial air of flowing through, air is cooled and reaches wind pushing temperature, cold-producing medium is heated gasification, enters compressor by the suction line too small multiplexer 20 of flowing through once more.Enter next circulation once more, go round and begin again like this in the water of airborne transfer of heat central air-conditioning, to realize providing dehumidifying, fresh cold air to aircraft.
The two refrigeration source airplane ground energy-conserving and environment-protective air-conditioning units (ADW) of 1-; 28-drip pipe road; 22-band heat-insulation layer air feed steel pipe; The 23-wired hose of blowing; The 24-bounce device; The 27-magnetic valve.
Principle: when aircraft has been stopped, the wired hose 23 of will blowing is pulled out and is connected to the aircraft air inlet, press bounce device 24 " startup " button, the air-conditioning system that is placed in marquis's machine building starts motion, unit is sent through cooling, except that warm cold air enters aircraft cabin inside by the air feed steel pipe 22 of band heat-insulation layer and the wired hose 23 of blowing, and air conditioning is carried out in the cabin handled.Air supply duct outer surface condensate water flows in the water leg, and when water level reach a certain height, magnetic valve 27 was opened, and condensed water is drawn in the central air-conditioning water retention system by discharge tube 28 in the water leg.
After the engine room inside air themperature reaches requirement, press and " stop " button on the bounce device 24, the motion of air-conditioning system unit, air-supply finishes.Treat in the air supplying hose after the air release wired hose to be folded in the underground piping, the aircraft joint is fixed on the bounce device, depresses bounce device at last, guarantees that bounce device 24 flushes with ground and solid and reliable by specific retaining mechanism.
Claims (6)
1. Duel cold sources airplane ground energy-conserving and environment-protective air-conditioning system; it is characterized in that being water-cooled first air treatment system of heat transferring medium and being that compression refrigeration formula second air treatment system of heat transferring medium is formed with the cold-producing medium by the cold water that provides with central air-conditioning; air-conditioning system first air treatment system has channelling water heat exchanger (7) to inject from terminal central air-conditioning cold water and air from terminal or shelter bridge passage through water pump (8) to carry out heat exchange; cooled air is by the evaporimeter of centrifugal blower (6) driving through second air treatment system; outlet housing (2); air supplying hose (1) and underpass system send in the aircraft storehouse; water after channelling water heat exchanger (7) heat exchange directly or through double pipe heat exchanger (10) drains into terminal central air-conditioning water retention system; first; two air treatment systems are positioned at terminal; the underpass system comprises the band heat-insulation layer air supply duct (22) that is embedded in outdoor airplane parking area; air supply duct one end links to each other with air supplying hose (1), and the other end of air supply duct (22) links to each other with flexible pipe (23).
2. air-conditioning system according to claim 1 is characterized in that channelling water heat exchanger (7) two for parallel connection, and the air inlet evaporimeter outer and that the centrifugal blower air outlet is outer that lays respectively at centrifugal blower (6) both sides is arranged in a triangle.
3. air-conditioning system according to claim 1, it is characterized in that compressor (14) is parallel with high and low pressure force controller (12), respectively there is a shock-absorbing pipe at the medium turnover two ends of compressor, the water inlet pipe and water outlet pipe of channelling water heat exchanger (7) is after magnetic valve (9) is communicated with, and the mixing water of water inlet pipe and water outlet pipe enters double pipe heat exchanger (10) together.
4. air-conditioning system according to claim 1 is characterized in that below the ambient temperature value of setting, the first air treatment system work, the ambient temperature value of setting and more than, first and second air treatment system is all worked.
5. air-conditioning system according to claim 1; the exposed junction that it is characterized in that described flexible pipe (23) is connected with the fixing card of joint (25) under the cover plate of bounce device (24); when not blowing; depress the cover plate of bounce device (24); flexible pipe is contracted in the vertical shaft (26); during air-supply; carry on the cover plate of bounce device (24); retaining bar (29) fork; manually joint (30) is connected with joint on the aircraft; drip pipe road (28) is embedded in that the airplane parking area is underground, and an end is connected with silo bottom, and an end has magnetic valve (27) and is connected with the central air-conditioning water retention system.
6. air-conditioning system according to claim 1, it is characterized in that evaporimeter one end low-pressure filter (20) is connected with compressor (14), or/and double pipe heat exchanger (10) is connected with compressor (14), perhaps the other end of evaporimeter is connected with compressor (14) through expansion valve (21), second magnetic valve (17) other end through expansion valve (21), first magnetic valve (17), hand valve (16), device for drying and filtering (15), reservoir (13).
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| Application Number | Priority Date | Filing Date | Title |
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| CN200910059575XA CN101581484B (en) | 2009-06-12 | 2009-06-12 | Duel cold sources airplane ground energy-conserving and environment-protective air-conditioning system |
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| CN200910059575XA CN101581484B (en) | 2009-06-12 | 2009-06-12 | Duel cold sources airplane ground energy-conserving and environment-protective air-conditioning system |
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| CN101581484A CN101581484A (en) | 2009-11-18 |
| CN101581484B true CN101581484B (en) | 2011-01-26 |
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Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8767400B2 (en) * | 2011-06-27 | 2014-07-01 | The Bergquist Torrington Company | Cooling module with parallel blowers |
| CN104235961B (en) * | 2014-07-22 | 2017-01-11 | 江苏兆胜空调有限公司 | High-pressure low-humidity air conditioner device for cooling aircraft for boat |
| CN108167968A (en) * | 2018-02-02 | 2018-06-15 | 无锡雪鸥移动空调有限公司 | Full liquid cooling aircraft ground well ground air conditioner unit |
| CN110966703A (en) * | 2019-12-13 | 2020-04-07 | 江苏风神空调集团股份有限公司 | Aircraft ground fresh air ventilation system |
| CN111578553A (en) * | 2020-05-25 | 2020-08-25 | 中国建筑西北设计研究院有限公司 | Aircraft ground air conditioning system |
| CN111591457B (en) * | 2020-05-27 | 2021-06-15 | 珠海方博科技有限公司 | Airport ground vehicle-free service system |
| CN113405194B (en) * | 2021-06-03 | 2022-08-19 | 广东省建筑设计研究院有限公司 | Mixed ventilation and air-conditioning combined operation system for boarding bridge |
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Denomination of invention: Duel cold sources airplane ground energy-conserving and environment-protective air-conditioning system Effective date of registration: 20120510 Granted publication date: 20110126 Pledgee: Chengdu Productivity Promotion Center Pledgor: Sichuan Huashengqiang Aviation Equipment Co., Ltd. Registration number: 2012990000198 |
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Denomination of invention: Duel cold sources airplane ground energy-conserving and environment-protective air-conditioning system Effective date of registration: 20140404 Granted publication date: 20110126 Pledgee: Chengdu rural commercial bank Limited by Share Ltd Jin Dong branch Pledgor: Sichuan Huashengqiang Aviation Equipment Co., Ltd. Registration number: 2014510000007 |
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Denomination of invention: Duel cold sources airplane ground energy-conserving and environment-protective air-conditioning system Effective date of registration: 20150508 Granted publication date: 20110126 Pledgee: Chengdu rural commercial bank Limited by Share Ltd Jin Dong branch Pledgor: Sichuan Huashengqiang Aviation Equipment Co., Ltd. Registration number: 2015510000019 |
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