CN2572261Y - Ground air condition vehicle for airplane - Google Patents
Ground air condition vehicle for airplane Download PDFInfo
- Publication number
- CN2572261Y CN2572261Y CN02280429U CN02280429U CN2572261Y CN 2572261 Y CN2572261 Y CN 2572261Y CN 02280429 U CN02280429 U CN 02280429U CN 02280429 U CN02280429 U CN 02280429U CN 2572261 Y CN2572261 Y CN 2572261Y
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- automobile
- dehydrater
- radiator
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Abstract
The utility model relates to a ground air conditioning automobile for an airplane which comprises a box type specially loaded portion and a second category chassis of an automobile. The specially loaded portion of the utility model is mainly composed of an air conditioning device, an operating device of a device, an electric control device, a power device, a driving device, a control device of a skylight and an automobile body. The automobile body which comprises an automobile frame and door windows makes the specially loaded portion surrounded and concentratedly arranged on the second category automobile chassis or a non-motor automobile chassis with metal casings, and the internal part of the automobile body is provided with a ventilating pipeline, a refrigerating essential element, a heating essential element, a dehumidifying and pressurizing essential element, etc. The air conditioning automobile uses structural forms of air cooling and air compression heating. The utility model can provide dry and clean air with specified index requirements to equipment cabins of an airplane, a control cabin, or a passenger cabin. The utility model has functions of ventilation, refrigeration, heating, dehumidification, etc.
Description
Technical field: the utility model relates to a kind of aircraft ground air-conditioning car, is the ground handling equipment supporting with aircraft.
Background technology: aircraft ground air-conditioning car of the prior art adopts air cooling formula and two kinds of versions of sweat cooling formula.The sweat cooling formula adopts freon refrigerant, has the technical barrier of seepage.Have to annually to replenish cold-producing medium in order addressing this problem, but to keep in repair, dose the operation more complicated of cold-producing medium in the open air.Also exist maximum potential safety hazard in the above-mentioned technology, adopt the resistance wire heating exactly, belong to naked light and heat, poor stability.Though the air cooling formula can be avoided the generation of the problems referred to above, it is used for the little occasion of gas supply flow always.
Summary of the invention: the purpose of this utility model is at above-mentioned technical deficiency, and a kind of new equipment of design.It is a kind ofly can provide the drying that set quota requires, clean air to airplane equipment cabin, driving cabin or main cabin, the version that aircraft ground air-conditioning car with functions such as ventilation, refrigeration, heating, dehumidifying, this air-conditioned coach adopt air cooling and air compression to heat.For achieving the above object, the utility model adopts following technical proposals: aircraft ground air-conditioning car mainly comprises special dress part of van-type and body with frame (7) two large divisions.Its chassis can be body with frame (constituting the self-propelled air-conditioned coach), also can be non-motor chassis (constituting the pull-type air-conditioned coach), its special dress part mainly is made up of aircondition (6), instrument manipulation device (5), electrical control gear (4), power set (2), transmission device (3), scuttle control device (1) and car body (8).Car body (8) comprises vehicle frame, door and window, and it is adorned the part enclosure aggregate with metal shell with the spy and is installed in two class automobile chassises (7) and goes up and constitute.Parts such as installing air pipeline, refrigeration, heating, dehumidifying in the car body (8), concrete structure and annexation are: described aircondition (6) comprises assemblies such as charging turbine cooler, air radiator, low pressure dehydrater and high pressure water separation regenerative air cycle cooling system device, and the annexation of its structure and air feed part is: air intake communicates with air filter (43), inlet flexible pipe (39), air compressor (42), filter (41) successively.Pipeline divides two-way, one the tunnel joins through motorized adjustment butterfly valve (38) and air radiator assembly one-level radiator (37), the blast pipe that is provided with the one-level radiator (37) of draining valve (45) connects with the compressor (51) of booster-type cooling turbine unit (47), and join by the heat radiator assembly secondary radiator (36) that pipeline and bottom are provided with draining valve (46), secondary radiator (36) joins by pipeline assembly and heat exchanger (48), high pressure water separation regenerative air cycle cooling system device (52), and the turbine arrival end by blast pipe and booster-type cooling turbine unit links.Turbine outlet communicates with heat exchanger (48), junction station (49) and low pressure dehydrater (53), the bottom of dehydrater (53) is provided with draining valve (54), dehydrater (53) links with ventilation duct interface (55), and links by the interface on vent hose (50), Ground Service Plug (57) and the aircraft machine.Another road motorized adjustment butterfly valve (44) joins by pipeline and junction station (49), and joins with low pressure dehydrater (53), connects with interface on the aircraft machine by ventilation duct interface (55), vent hose (50), Ground Service Plug (57).
Design feature of the present utility model is: a, employing body with frame have independent transportation transition ability; B, employing combined metal sealing van-type structure, maintainability is good, and is rainproof, dustproof; C, power source adopt diesel engine, are furnished with independent water radiator, with a shared electricity of driving engine and a shared fuel tank; The instrument actuating element enters the left side of direction, independent operation in garage; The two sides of tail of d, car respectively has a storage bobbin carriage, is provided with ventilation interface in the case, has special-purpose vent hose and quick-release coupling, can give two airplane air feeds simultaneously, also can use separately for an airplane; E, have mark, lighting apparatus, can or not have under the light condition and use for night; F, have extinguishing device, safe and reliable.This car cooling is fast, and flow is big, and Operation and Maintenance is simple; Without cold-producing medium, non-environmental-pollution; With the heating of air compress technique, safe and reliable; Be provided with high and low pressure two-stage dehydrater, the efficient that dewaters height.
Description of drawings:
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is the vertical view of Fig. 1.
Fig. 3 is the utility model aircondition structural representation.
Fig. 4 is the vertical view of Fig. 3.
Fig. 5 is the connection diagram of the utility model aircondition air feed part.
Fig. 6 is the structural representation of the utility model low pressure dehydrater.
Specific embodiment:
With reference to Fig. 1,2, aircraft ground air-conditioning car mainly comprises special dress part of van-type and body with frame 7 two large divisions.Its special dress part mainly is made up of aircondition 6, instrument manipulation device 5, electrical control gear 4, power set 2, transmission device 3, scuttle control device 1 and car body 8.Car body 8 comprises vehicle frame, door and window, and it is adorned the part enclosure aggregate with metal shell with the spy and is installed on the two class automobile chassises 7 and constitutes.
With reference to Fig. 3,4,5, described aircondition 6 comprises charging turbine cooler, air radiator assembly, low pressure dehydrater assembly and high pressure water separation regenerative air cycle cooling system device assembly, and the annexation of its structure and air feed part is: air intake communicates with air filter 43, inlet flexible pipe 39, air compressor 42, filter 41 successively.Pipeline divides two-way, one the tunnel joins through motorized adjustment butterfly valve 38 and air radiator assembly one-level radiator 37, the blast pipe that is provided with the one-level radiator 37 of draining valve 45 connects with the turbocompressor 51 of booster-type cooling turbine unit 47, and join by the heat radiator assembly secondary radiator 36 that pipeline and bottom are provided with draining valve 46, secondary radiator 36 joins by pipeline assembly and heat exchanger 48, high pressure water separation regenerative air cycle cooling system device 52, and the turbine inlet by blast pipe and booster-type cooling turbine unit links.Turbine outlet communicates with heat exchanger 48, junction station 49 and low pressure dehydrater 53, and the bottom of dehydrater 53 is provided with draining valve 54, and dehydrater 53 links with ventilation duct interface 55, and links by the interface on vent hose 50, Ground Service Plug 57 and the aircraft machine.Another road motorized adjustment butterfly valve 44 joins by pipeline and junction station 49, and junction station 49 joins with low pressure dehydrater 53, connects with interface on the aircraft machine by ventilation duct interface 55, vent hose 50, Ground Service Plug 57.Air feed principle of the present utility model is: air enters air radiator assembly one-level radiator 37 through the pressure-air that air filter 43, air compressor 42 and filter 41 produce through thermometer, Pressure gauge and motorized adjustment butterfly valve 38, the pressure-air of process cooling enters booster-type cooling turbine unit 47 by the blast pipe of one-level radiator 37, air is supercharging once more, high-temperature gas communicates with heat radiator assembly secondary radiator 36 by pipeline, air is lowered the temperature once more, and gas enters heat exchanger 48, high pressure water separation regenerative air cycle cooling system device 52 by secondary radiator blast pipe.At this moment, air and moisture are discharged by draining valve 46 from, water; Air enters cooling turbine unit 47 coolings, Cryogenic air through blast pipe enter heat exchanger 48 once more, junction station 49 enters low pressure dehydrater 53, air separates once more with water, water is discharged through draining valve 54, and dry air links by the air inlet on vent hose, air-conditioned coach Ground Service Plug and the aircraft machine of special use by the road.
With reference to Fig. 6, the low pressure dehydrater comprises cover assembly 59, following cap assemblies 81, establishes supporting network assembly 64 in the cover assembly 59, and supporting network assembly 64 is provided with wire mesh demister 60, wire mesh demister 60 joins with water conservancy diversion rod 61,63 respectively, and wire mesh demister 60 is divided into water receiving umbrella shade assembly 62.Gripper shoe 65 is tightened up by bolt 66, packing ring 67, spring washer 68 and is fixed on cylindrical shell 80 by gasket seal 69, bolt 70, packing ring 71, spring washer 72, nut 73.Gripper shoe 65 is provided with water collection sheet 77, ceramic element 76, ceramic element 76 is fixed on gripper shoe 65 by the collar 75, cushion 74, and install water collection sheet 77 at interval with ceramic element 76, establish the center collar 78 on the central tube assembly 79 and be connected with gripper shoe 65, following cap assemblies 81 is fixed on the cylinder assembly 80.
Claims (2)
1, a kind of aircraft ground air-conditioning car, mainly comprise special dress part of van-type and chassis (7) two large divisions, its chassis can be body with frame, also can be non-motor chassis, its special dress part is mainly by aircondition (6), instrument manipulation device (5), electrical control gear (4), power set (2), transmission device (3), scuttle control device (1) and car body (8) are formed, car body (8) comprises vehicle frame, door and window, it is adorned the part enclosure aggregate with metal shell with the spy and is installed in two class automobile chassises (7) and goes up and constitute, installing air pipeline in the car body (8), source of the gas, refrigeration, supercharging, heating, the dehumidifying critical piece, it is characterized in that: described aircondition (6) comprises the charging turbine cooler, the air radiator assembly, low pressure dehydrater and high pressure water separation regenerative air cycle cooling system device assembly, the annexation of its structure and air feed part is: air intake successively with air filter (43), inlet flexible pipe (39), air compressor (42), filter (41) communicates, pipeline divides two-way, one the tunnel joins through motorized adjustment butterfly valve (38) and air radiator assembly one-level radiator (37), the blast pipe that is provided with the one-level radiator (37) of draining valve (45) connects with the turbocompressor (51) of booster-type cooling turbine unit (47), and join by the heat radiator assembly secondary radiator (36) that pipeline and bottom are provided with draining valve (46), secondary radiator (36) is by pipeline assembly and heat exchanger (48), high pressure water separation regenerative air cycle cooling system device (52) joins, turbine inlet by blast pipe and booster-type cooling turbine unit links, turbine outlet and heat exchanger (48), junction station (49) and low pressure dehydrater (53) communicate, the bottom of dehydrater (53) is provided with draining valve (54), dehydrater (53) links with ventilation duct interface (55), and by vent hose (50), interface on Ground Service Plug (57) and the aircraft machine links; Another road motorized adjustment butterfly valve (44) joins by pipeline and junction station (49), and junction station (49) joins with low pressure dehydrater (53), connects with interface on the aircraft machine by ventilation duct interface (55), vent hose (50), Ground Service Plug (57).
2, aircraft ground air-conditioning car according to claim 1, it is characterized in that: described low pressure dehydrater (53) comprises cover assembly (59), following cap assemblies (81), establish supporting network assembly (64) in the cover assembly (59), supporting network assembly (64) is provided with wire mesh demister (60), wire mesh demister (60) respectively with water conservancy diversion rod (61), (63) join, wire mesh demister (60) is divided into water receiving umbrella shade assembly (62), gripper shoe (65) is by bolt (66), packing ring (67), spring washer (68) tightens up and by gasket seal (69), bolt (70), packing ring (71), spring washer (72), nut (73) is fixed on cylindrical shell (80), gripper shoe (65) is provided with water collection sheet (77), ceramic element (76), ceramic element (76) is by the collar (75), cushion (74) is fixed on gripper shoe (65), and install at interval water collection sheet (77) with ceramic element (76), establish the center collar (78) on the central tube assembly (79) and link with gripper shoe (65), following cap assemblies (81) is fixed on the cylinder assembly (80).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN02280429U CN2572261Y (en) | 2002-10-10 | 2002-10-10 | Ground air condition vehicle for airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN02280429U CN2572261Y (en) | 2002-10-10 | 2002-10-10 | Ground air condition vehicle for airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2572261Y true CN2572261Y (en) | 2003-09-10 |
Family
ID=33743159
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN02280429U Expired - Fee Related CN2572261Y (en) | 2002-10-10 | 2002-10-10 | Ground air condition vehicle for airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2572261Y (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100339648C (en) * | 2005-11-29 | 2007-09-26 | 广东省吉荣空调设备公司 | Aircraft floor air conditioner set |
| CN101817296A (en) * | 2010-04-15 | 2010-09-01 | 上海理工大学 | Airplane ground air-conditioning vehicle utilizing exhaust waste heat of diesel engine |
| CN102390542A (en) * | 2011-09-10 | 2012-03-28 | 西安飞豹科技发展公司 | Pull type aircraft cooling air vehicle |
| CN102914111A (en) * | 2012-10-24 | 2013-02-06 | 中国航空工业集团公司北京航空材料研究院 | Aircraft surface skin cooling device |
| CN102112373B (en) * | 2008-06-26 | 2013-12-25 | 空中客车作业有限公司 | Auxiliary cooling device for connection to aircraft liquid cooling system |
| WO2015149289A1 (en) * | 2014-04-01 | 2015-10-08 | 深圳市智轮电动车驱动技术有限公司 | Air supply system for whole vehicle |
| CN112623251A (en) * | 2020-12-18 | 2021-04-09 | 中国民航大学 | Movable microenvironment adjusting device for airport corridor bridge berth area |
-
2002
- 2002-10-10 CN CN02280429U patent/CN2572261Y/en not_active Expired - Fee Related
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100339648C (en) * | 2005-11-29 | 2007-09-26 | 广东省吉荣空调设备公司 | Aircraft floor air conditioner set |
| CN102112373B (en) * | 2008-06-26 | 2013-12-25 | 空中客车作业有限公司 | Auxiliary cooling device for connection to aircraft liquid cooling system |
| CN101817296A (en) * | 2010-04-15 | 2010-09-01 | 上海理工大学 | Airplane ground air-conditioning vehicle utilizing exhaust waste heat of diesel engine |
| CN101817296B (en) * | 2010-04-15 | 2011-11-09 | 上海理工大学 | Airplane ground air-conditioning vehicle utilizing exhaust waste heat of diesel engine |
| CN102390542B (en) * | 2011-09-10 | 2014-06-04 | 西安飞豹科技发展公司 | Pull type aircraft cooling air vehicle |
| CN102390542A (en) * | 2011-09-10 | 2012-03-28 | 西安飞豹科技发展公司 | Pull type aircraft cooling air vehicle |
| CN102914111A (en) * | 2012-10-24 | 2013-02-06 | 中国航空工业集团公司北京航空材料研究院 | Aircraft surface skin cooling device |
| CN102914111B (en) * | 2012-10-24 | 2014-11-26 | 中国航空工业集团公司北京航空材料研究院 | Aircraft surface skin cooling device |
| WO2015149289A1 (en) * | 2014-04-01 | 2015-10-08 | 深圳市智轮电动车驱动技术有限公司 | Air supply system for whole vehicle |
| CN106103148A (en) * | 2014-04-01 | 2016-11-09 | 深圳市智轮电动车驱动技术有限公司 | Car load air feed system |
| CN106103148B (en) * | 2014-04-01 | 2018-03-30 | 深圳市智轮电动车驱动技术有限公司 | Vehicle air feed system |
| US10906588B2 (en) | 2014-04-01 | 2021-02-02 | Guangdong Hua'chan Research Institute Of Intelligent Transportation System Co., Ltd. | Air supply system for whole vehicle |
| CN112623251A (en) * | 2020-12-18 | 2021-04-09 | 中国民航大学 | Movable microenvironment adjusting device for airport corridor bridge berth area |
| CN112623251B (en) * | 2020-12-18 | 2022-07-29 | 中国民航大学 | Portable microenvironment adjusting device of airport corridor bridge berth area |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20030910 Termination date: 20101010 |