CN207985214U - Atmosphere control system for aircraft - Google Patents

Abstract

The air of processing is supplied to the cabin of aircraft using it by a kind of atmosphere control system for aircraft using an at least flexible conduit for when the aircraft is on the ground, being temporarily connected to an at least airplane from least one air conditioner unit.Air conditioner unit is made of at least one heating and cooling packaging part, and air for being supplied to the cabin is heated or cooled using it；And the atmosphere control system includes transfer device, and air conditioner unit can be moved relative to aircraft using it.Transfer device is made of retractable boarding bridge.The atmosphere control system includes for heating network (alternatively in the heating of the combination and cooling packaging part and region, network for region cooling) between conveying heating or cooling fluid subsystem, its subsystem includes an at least flexible conduit, which includes at least one conduit and at least one conduit for returning to fluid from air conditioner unit for fluid to be input to air conditioner unit.

Description

Atmosphere control system for aircraft

Technical field

The utility model is related to a kind of modifications of the atmosphere control system for aircraft etc..

Background technology

In today's society, flight has become the usual way of the rapid journey between different location.Air travel and boat Air transport is defeated to bring many great possibilities, but also results in some problems.It is with the relevant problem of air travel, when Aircraft parks shorter or longer time, and when waiting for flight next time, the indoor air of aircraft cabin can become between flying twice Cold or heating.It is generally necessary to cabin atmosphere be heated or cooled, especially during parking for a long time.Cabin atmosphere is heated or cooled Needs, with weather, temperature, aircraft stand and it is different.In the case where outdoor temperature is especially high or especially low, These problems become very challenging.It is relevant with cabin air temperature under especially hot or cold weather conditions Problem may become very serious, and in the worst case, the health of possible entail dangers to passenger.

It is with the relevant problem of air in cooling or heating aircraft cabin, it is often necessary to run starting for aircraft Machine could obtain satisfactory weather in aircraft.Engine long-play is kept before taking off, and can lead to fuel Cost increases and environmental pressure increases.Since flight (air travel) can adversely affect environment, so, It is influenced caused by flight and its auxiliary facility it is necessary to reduce.One of relevant maximum environmental problem is aircraft with flying The discharge of the fuel of burning.In addition, operating the related all devices with flight in a manner of more environmentally-friendly, become more to aggravate It wants.Therefore, the target on airport is powered for necessary corollary equipment using the energy of alternative energy source, such as, such as weather intelligence The systems such as air-conditioning system can preferably reduce the influence to environment compared with the existing energy using these energy.Be parked in ground Another relevant problem of aircraft on face is, corrodes as caused by the moisture in air.It is parked on ground longer Among the aircraft of time, this problem is especially prominent.

Another problem of the existing design of aircraft climate control systems is that these atmosphere control systems are generally positioned at On ground, such as on lorry (cart) or other kinds of vehicle.Atmosphere control system is placed on lorry on the ground, Lorry can give the aircraft vicinity parked carry out work inter-related task vehicle and employee bring the risk that is in the way.By these lorries It is moved to another position from a position, can also involve a large amount of work.During use, there is also soft for atmosphere control system Pipe, rope etc. are placed in the problem on ground.For example, conduit, hose and rope may hinder vehicle and personnel, and even can Increase injured risk.

One problem of existing design is that existing design is substantially only used for an application, and wherein each product is suitable For specifically applying.Therefore, these expections can use or be expected on lorry to be stored, and be not suitable for two kinds and answer With.Another related problem is with going on or off the plane, the climate controlling of the inner space in so-called " connecting bridge " etc..For Existing connecting bridge design, it is difficult to be heated and cooled down in an efficient way.

Another problem for being related to the aircraft parked on the ground is, efficiently melts around and under the aircraft parked It avenges (ice).Currently, such as using power driven system snow melt is carried out, this generates the need to more cost effective snow melt type It wants.

One problem of aircraft air-conditioning system existing design is, existing design by air cooling to freezing point temperature hereinafter, Such as down to -25 degrees Celsius, and in extreme circumstances then down to -40 degrees Celsius.This may will produce the needs to defrosting instead, To remove frosting etc. as caused by the cold air of pole.

Another problem of existing system is that existing system uses power supply.Currently, flight (air travel) row Industry is largely highly desirable to selection than more environmentally friendly alternative solution used at present.

When aircraft ground or it is aerial when, there is also ice formation issues in the engine of aircraft.When precipitation or the like is being sent out In motivation when glaciation, can occur engine icing phenomenon on the ground.It also occur that with knot in the relevant engine that flies Ice, for example, it is related with aircraft decline when landing.There are in the case of ice, need to carry out new fly taking off in engine By ice thaw before row.

The prior art

It is previously known have several different equipment (device, system) modification, it is parked on the ground for heating and/or cooling The cabin and analog of aircraft.For example, US4632019 describes a kind of machine when aircraft is parked on the ground for cooling down aircraft The system in cabin.Its design is significantly different with the utility model.According to its description, which is for example not intended to heat by region And/or region cools down to provide power (operation).In addition, the air that the system is only used for the cabin to being supplied to aircraft carries out It is cooling.

RE32687 describes a kind of modification of the atmosphere control system for aircraft, according to its description comprising to weather Cooling and heating the fluid of control system supply.For heating or cooling fluid extraction and importing (return) conduit The design of (pipeline) and the utility model is significantly different.For example, weather aspect is to deposit in winter for extraction and the design of importing conduit In problem.Further, which is located at structural top, causes to visit such as with relevant repair, inspection Ask sex chromosome mosaicism.

EP 1951573 even disclose it is a kind of for aircraft supply electric power and to the air in the cabin of aircraft into The cooling system of row.The design is largely different from the utility model.For example, according to its description, which is not purport Power is being provided by region heating and region cooling.US7651052 discloses a kind of for supplying electric power and sky to aircraft The component of gas.The system is intended for the air in cooling aircraft cabin.The design is different from the utility model.For example, according to It is described, which is not intended to provide power by region heating and region cooling.

US6637215 discloses a kind of system and method for cooling down the cabin atmosphere in aircraft.The design and this reality It is different with novel design.For example, according to its description, which is not intended to cool down by region heating and region dynamic to provide Power.

EP1951573B1 even discloses a kind of modification for cooling down the system of the cabin atmosphere in aircraft.The design It is different from the design of the utility model.For example, according to its description, the design be not intended to by region heating and region cooling come Power is provided.US3399545 discloses a kind of modification of aircraft air-conditioning system.According to its description, the design and according to this patent The design of application is significantly different.For example, according to its description, which will produce energy expenditure more higher than the utility model.It is empty The length of airway can cause system to occur heating and ventilation loss.

On Helsinborg/airports peace Ge Heermu, develops and test a kind of original of the atmosphere control system of simple version Type.However, the design is largely different from according to the design of present patent application.

Utility model content

The main purpose of the utility model is to create a kind of climate controlling system solving or reduce at least one above problem System.Another purpose of the utility model is to create a kind of atmosphere control system, can be to the air in aircraft cabin using it It heated, cooled down and is dehumidified.Another purpose of the utility model is to create a kind of atmosphere control system, and region is used to add Heat carrys out the warm air supplied to aircraft.The further object of the utility model is to create a kind of atmosphere control system, is utilized Region cools down to cool down the cold air of aircraft supply.The further object of the utility model is to create a kind of climate controlling system System, can be placed on the connecting bridge on airport.In an alternative embodiment, another purpose of the utility model is to create one kind Atmosphere control system can be used for the space in warm or cooling connecting bridge or the like.In an alternative embodiment, can think To the utility model is used for warm at least one other space, object or the like, such as, in the position for the aircraft parked Set the ground of nearby (surrounding).In an alternative embodiment, the further object of the utility model is to create one kind by module The system of composition.At least one above-mentioned purpose pointed out is to utilize to be realized according to the atmosphere control system of claim.

The utility model provides a kind of atmosphere control system, for when the aircraft is on the ground, being temporarily connected at least The air of processing is supplied to institute by one airplane using an at least flexible conduit using it from least one air conditioner unit State the cabin of aircraft；The air conditioner unit is made of at least one heating and cooling packaging part, using it to being supplied to The air for stating cabin is heated or cooled；And the atmosphere control system includes transfer device, can be relative to using it The aircraft and the transfer device move the air conditioner unit；And the atmosphere control system includes for described Heating or cooling fluid is conveyed between heating and cooling packaging part and region heating network or the network cooled down for region Subsystem, subsystem includes an at least flexible conduit, and the flexible conduit includes at least one for by the fluid Be input to the air conditioner unit conduit and at least one for the fluid to be returned from the air conditioner unit Conduit；It is characterized in that, the atmosphere control system is used to air returning to institute from the cabin of the aircraft by least one State the discharge duct composition of air conditioner unit, and the atmosphere control system includes at least one for thawing aircraft engine The module of machine.

Description of the drawings

It, will with reference to the following drawings below in the detailed description of the utility model.Each in these attached drawings exists It is briefly described in the following drawings list.Exemplary embodiment in attached drawing is not intended to limit the protection domain of present patent application. It note that attached drawing is schematic diagram, it is thus possible to details therein can be omitted.

Fig. 1 schematically shows this atmosphere control system for being attached to connecting bridge.

Fig. 2 shows the connections of the network with the network of region heating and/or for region cooling.

Fig. 3 schematically shows the exemplary embodiment of the function of atmosphere control system.

Fig. 4 A to Fig. 4 D show the alternative embodiment of the utility model.

Fig. 5 A to Fig. 5 C show the aircraft for being equipped at least one engine defrosting module with inlet duct.

Fig. 6 A to Fig. 6 C show the aircraft for being equipped at least one engine defrosting module with inlet duct.

Fig. 7 shows the exemplary air distributor of the engine for channel to be connected to aircraft from steam line.

Specific implementation mode

With reference to attached drawing, a kind of atmosphere control system 1 according to present patent application is shown, such as to standing on ground On the supply heating of an at least airplane 2 or cooling air.

Atmosphere control system 1 is made of at least one air conditioner unit 3, and (warm) or cooling supply are heated using it To the air of aircraft.Atmosphere control system 1 to the supply of air conditioner unit 3 further from least one for heating or cooling Liquid subsystem 4 form.Atmosphere control system 1 further by least one for air that is will heat or cooling down from sky The subsystem 5 that gas disposal unit 3 is transferred to the cabin of aircraft 2 forms.Subsystem 5 can also include it is a kind of for by air from The cabin of aircraft returns to the function of atmosphere control system, is intended to recover energy.

Referring to Fig.1 with Fig. 4 A to Fig. 4 D, the air conditioner unit 3 being placed on transfer device 6 is shown, utilize this turn Moving device 6 can move air conditioner unit 3 relative to aircraft 2.In Fig. 1, transfer device 6 by least one connecting bridge 7 or The structure of similar type is constituted.In an alternative embodiment, as shown in Fig. 4 A to Fig. 4 D, transfer device 6 is applicable in by another purpose Transfer device composition, such as, such as vehicle 8, lorry (bracket, cart) or the like.

Referring to Fig.1, how illustrate in greater detail transfer device 6 is by adjacent with building 9 (such as departure hall) " connecting bridge " (causeway, slope) 7 or similar structures composition.The design of connecting bridge 7 can be in the range of present patent application It changes.It is preferable, however, that one end 10 of connecting bridge is pivotably connected to building 9.The second end of connecting bridge 7 11 for being connected to aircraft.It preferably, can be by the size operation of connecting bridge 7 at can be shortened or be extended.Connecting bridge 7 Shortening or elongation can be realized in a telescopic manner, or be realized using the applicable technology of another purpose.In alternative embodiment In, it is contemplated that the length of connecting bridge is nonadjustable.

In the exemplary embodiment, air conditioner unit 3 is connected to the downside 12 of connecting bridge 7.Preferably, air-treatment list Member 3 is as close to the second end 11 (free end) for being connected to connecting bridge 7.Air conditioner unit is to the downside 12 of connecting bridge 7 Connection is to realize that here it is the originals not being described in more detail in the present patent application using previously known technology Cause.Second end 11 due to air conditioner unit 3 as close to connecting bridge 7 is placed, so, reduce by heating or cold But loss when air is transferred to the cabin of aircraft 2 from air conditioner unit 3 in subsystem 5.It in an alternative embodiment, can be with It is contemplated that air conditioner unit 3 is connected to connecting bridge 7 at the position that another purpose is applicable in.By relative to aircraft and Building moves connecting bridge 7, and air conditioner unit 3 can be moved relative to aircraft 2 and building 9.Referring again to Fig. 1, show Atmosphere control system 1 includes at least one subsystem for supplying relatively hot liquid or relatively cold liquid 4, which is used for heating and the air in cooling air processing unit.

Relatively hot fluid or relatively cold can be realized in several of different ways and using different technologies Fluid is to the input in air conditioner unit 3.In the preferred embodiment shown in figure 2, this is individually closed using at least one What road 13 was realized, this closed circuit 13 is connected at least one district heating network 15 via at least one first heat exchanger 14, and And at least one second heat exchanger 16 is connected to the network 17 cooled down for region.

Via the equal realizations connection of an at least flexible conduit (hose, pipe) 18.Flexible conduit 18 is used for including at least one To the conduit of 3 supply fluid of air conditioner unit and at least one for the conduit from air conditioner unit Returning fluid.Standby It selects in embodiment, can respectively realize and supplied to the fluid of air conditioner unit 3 and from sky via individual flexible conduit etc. The fluid of gas disposal unit 3 returns.Via at least one tie point 19 or several tie points 19, realization flexible conduit (or it is more A flexible conduit) arrive the connection for being used for the network 15 that region is heated and the network 17 for region cooling.In the utility model In range, the position of tie point 19 or several tie points 19 position may great changes will take place.For will heating or The subsystem 4 that cooling fluid is supplied to air conditioner unit 3 is made of at least one devices for taking-up 20, (multiple) flexible conduit 18/from devices for taking-up 20 roll and be unfolded.During the elongation of connecting bridge 7, flexible conduit 18 is opened up from devices for taking-up 20 It opens, and during the retraction of connecting bridge 7, flexible conduit 18 is rolls-up onto on devices for taking-up.Preferably, devices for taking-up 20 connects To the top side 21 of connecting bridge 7.In a preferred embodiment, it is preferable that flexible conduit is not heat-insulated, to allow thereon any Snow and ice melts under weather conditions in winter.Since flexible conduit is not heat-insulated, so ensure that devices for taking-up gas in winter Function under the conditions of time.In turn, in an alternative embodiment, this will not exclude heat-insulated flexible conduit.

In an alternative embodiment, devices for taking-up 20 may be coupled to the different location on connecting bridge.Further, weather control The alternative embodiment of system processed may include at least one first devices for taking-up 20 and at least one second devices for taking-up 20.It uses At least two devices for taking-ups allow to use the system on relatively long connecting bridge.Preferably, devices for taking-up 20 is bullet Spring loaded type.Preferably, flexible conduit etc. is connected to building via at least one strain relief means etc..

Between devices for taking-up 20 and air conditioner unit 3, pass through at least a conduit (pipe, hose) 22 or similar company Connect conveying cooling or heating fluid.

With reference to Fig. 2, supply system 4 is shown with flow and is arrived for region heating and the connection of the network of region cooling Exemplary embodiment.In a preferred embodiment, which shunts (bypass) valve 23 and one second shunting by least one first Valve 24 forms.Flow divider 23 controls fluid and heats transfer of the network to first heat exchanger from region, and flow divider 24 controls Transfer of the fluid from the network cooled down for region to second heat exchanger.Via at least one steam line 25, heating is realized Or cooling air from atmosphere control system 3 to the transfer of the cabin of aircraft 2.Preferably, steam line is suitable for the purpose Flexible type.The length of flexible duct can change in the range of present patent application.

Flexible duct 25 can be connected to the cabin of aircraft in various ways.In the preferred embodiment of present patent application, Steam line 25 (or in the appropriate case, multiple pipelines) is connected to one in the Inlet gas connector (adapter) 26 of aircraft It is a or multiple.The advantages of being connected to connector 26 is that it includes the existing connection with aircraft cabin.

Air-flow to aircraft cabin can cause the air in cabin to be gradually replaced, and preferably via the ventilation of aircraft Device 27 is discharged.By this method, the air themperature in cabin can be increased or reduce, this depends on heating or cold Whether air but is supplied to cabin.In addition, the reduction of air humidity in cabin is realized, by the quilt in air conditioner unit Dehumidifying and caused by earlier stage is provided to the air of cabin.

With reference to Fig. 3, show how air conditioner unit 3 including at least one can be increased using it is transported to cabin The device 28 of air themperature.Therefore, which can increase by 29 groups of the heating packaging part of air themperature by least one using it At.Preferably, this atmosphere control system 1 further includes second device 30, and can cool down (dehumidifying) using it will enter aircraft cabin Air.Therefore, air conditioner unit 3 is made of at least one cooling packaging part 31, can be reduced using it and is supplied to cabin Air temperature.In the preferred embodiment of this atmosphere control system 1, heating packaging part 29 and cooling packaging part 31 can collect At in the heating and cooling packaging part 32 to combination.Heating by this combination and cooling packaging part, atmosphere control system can To be cooled and heated to aircraft cabin.With reference to Fig. 3, that schematically shows in the exemplary embodiment how in weather Air-treatment is realized in control system.Air-flow in atmosphere control system is generated by an at least desk fan 33 Deng.Untreated sky Gas is introduced into atmosphere control system at least one first fine filter 34, and deliver air to combination later adds hot and cold But packaging part (coil pipe heating/cooling) 32.After air is by the heating of the combination and cooling packaging part 32, in exemplary reality It applies in example, air is transported at least one filter 35.Preferably, which is made of at least one electrostatic filter. In an alternative embodiment, the design can not include filter 35 or the filter can be by least one carbon filter group At.It is had many advantages using electrostatic filter.Electrostatic filter for example have the advantages that it is more relatively smaller than carbon filter, and With pressure drop more lower than carbon filter.In a manner of similar with carbon filter, electrostatic filter also has need not periodically more The advantages of changing.Filter 35 makes such as removing smell from smoke evacuation, aircraft fuel, (may be toxin) culinary art smell The cabin atmosphere that must be introduced there is no smell.In the exemplary embodiment, which further includes at least one prevent finally The fire resisting damper 36 that fire is spread in system or system.After fire resisting damper 36, via an at least air inlet for being connected to aircraft Mouthful or suitably connected via purpose or connector be connected in another way aircraft cabin conduit, will be processed Air supply to aircraft cabin.

In an alternative embodiment, it is further contemplated that, which includes at least one device for ionization. In the alternative embodiment of this system, the air removed from cabin returns to air-treatment list via at least one discharge duct 38 Member.Preferably, discharge duct 38 is made of flexible duct.The length in flexible venting tube road 38 can be in the range of present patent application Inside change.

In an alternative embodiment, the returning air from aircraft cabin is transported to via at least one aircraft door and is connected to In the inner space of the connecting bridge of aircraft.By conveying returning air by door (or multiple doors), reduce from aircraft machine The resistance of air is discharged in cabin.At at least one position along connecting bridge length, at least one opening will by the opening Exhaust from connecting bridge inner space is transported to atmosphere control system by least one discharge duct 38.In air conditioner unit In, recycle all or part of air as gas supply (air inlet) from cabin to air conditioner unit.In alternative embodiment In, it is contemplated that the heat exchange being vented is intended to recover energy from exhaust.If such as relatively warm Air, such as+16 degrees Celsius of air is recycled from cabin and is heated again and returns to the cabin of aircraft, then It can be substantially energy saving.This is compared with -20 degrees Celsius of cold air for for example direct supplying to aircraft.The sky recycled Gas ratio may be different.For example, can be with from 2/3rds in the air that aircraft cabin is removed by discharge duct 38 It is recycled.

In an alternative embodiment, it is contemplated that the temperature at least one sensor sensing aircraft cabin.Sensor By in relation to cabin temperature data/information and possible other parameters be sent to the control system of atmosphere control system.Logical When crossing electric wire transmission information, the sensor of associated connector can be for example connected to via ventilation device or the like Aircraft cabin.The transmission of data or information from sensor to control system, can also wirelessly realize.

In an alternative embodiment, it is contemplated that come using the fluid in the return line of atmosphere control system The inner space of connecting bridge is heated or cooled.In warm climates, the inner space of connecting bridge is cooled.In cold weather Under, the air inside connecting bridge is heated.For example, this is to be connected to connecting bridge from atmosphere control system by least one Independent pipeline realize.

In the other embodiments of the utility model, neighbouring boarding is heated using the Returning fluid from atmosphere control system The surface on the ground of the ground (snow melt) of bridge and/or the position of the neighbouring aircraft parked.This is for example, by coming from air-treatment What the Returning fluid of unit used at least one earth-return circuit 39 for snow melt was realized.

With reference to Fig. 4 A to Fig. 4 D, the alternative embodiment of transfer device 6 is shown, wherein transfer device 6 is by structures such as vehicles 8 At.Fig. 4 A and Fig. 4 B show a kind of atmosphere control system, are intended to air supply will heat or cooling to an at least frame At least one of aircraft cabin.Fig. 4 C and Fig. 4 D show a kind of atmosphere control system, and it will be will heating or cooling to be intended to Air supply is at least at least one of airplane cabin and at least one for recycling the air from cabin In energy a part return line.Vehicle 8 can be equipped with its own driving unit, but can also be by utilizing external drive Unit operation or the cart (bracket, lorry) 40 or vehicle that move manually are constituted.The design of cart 40 may be in this patent Occurs prodigious variation in the range of application.Preferably, it is realized to region via one or more flexible conduit 41 and heats network With the connection of the network cooled down for region.Preferably, by the system for being connected to Zone heating, system and cooling down for region Flexible conduit 41 is rolled on all at least one devices for taking-ups 42 as shown in drawings.In an alternative embodiment, it is contemplated that It is that when without using conduit, conduit is stored at least one of atmosphere control system storeroom in another way. In alternative embodiment, the storage of conduit when not in use can be realized in another appropriate manner, for example, conduit can be opposite In atmosphere control system from external storage.Preferably, it will be connected using one or more quick connectors (connector) 43 flexible The network that conduit is connected to Zone heating, system or is cooled down for region.Quick connector 43 includes at least one check-valves, The check-valves of the type provides minimum leakage or does not leak substantially completely.For example, with the valve of trade mark Drylok sale Door can be preferably used as Quick coupling part, connect the conduit to Zone heating, system.In an alternative embodiment, it can use other The suitable connector of purpose, the system that flexible conduit is connected to Zone heating, system and is cooled down for region.It is led by flexibility It, can using it, it is preferable to use at least one shut-off valve during pipe is connected to region heating network and the network that is cooled down for region To execute the closing of each corresponding flexible conduit.

When not in use, the storage of flexible conduit can be realized via devices for taking-up.In an alternative embodiment, without using When, the storage of flexible conduit can be realized in such a way that another purpose is suitable.For example, flexible conduit can be to be not attached to gas The mode for waiting control system is stored in exterior space.Preferably, atmosphere control system includes at least one (going out with main power source Mouthful) connection.This can be realized by electric wire 44 etc..In the exemplary embodiment, which includes at least one for electricity The devices for taking-up 45 of line.

In the alternative embodiment of this atmosphere control system, by least two and preferably several modules form.Example Such as, a module can be made of the regulating device of air, that is, cool down packaging part, heating packaging part or combination adds hot and cold But packaging part.It is further contemplated that various types of filters are by one or more module compositions.By using module Change design, one or more filters module corresponding with specific application requirement can be selected.It is further contemplated that One or more filters module adaptive is in main season (temperature change etc.).

The idea of modularized design behind is that air conditioner unit should can both be suspended on connecting bridge 7 and use, The upper use of cart (lorry) 8 or the like can also be connected to.Therefore, module can have suitable design so that at air Reason unit can be suspended on connecting bridge.Another module is made of the wheel application with or without driving unit, is connected It is connected to air conditioner unit so that it can be moved on the ground.Add-on module includes cold for region heating network and region But the connector of network.The design can also include at least one module, (such as supplied and arranged by being used for aircraft ventilation system Gas) connector composition.In an alternative embodiment, module can also include the module for ground heating (melting snow and ice), And the module for handling the air for being supplied to connecting bridge.

With reference to Fig. 5 A to Fig. 5 C, it includes at least one for the aircraft engine that thaws that atmosphere control system, which is shown, Module 46.The module includes at least one of Fig. 5 A to Fig. 5 C air distributors 47, adapter etc., the air for that will heat It is assigned to aircraft engine from steam line 25.Pipeline is connected to air conditioner unit 3, is not shown in figure air conditioner unit. In the exemplary embodiment of Fig. 6 A to Fig. 6 C, module 46 includes at least one the first engine 49 for being connected to aircraft First passage 48 and it is at least one for be connected to aircraft the second engine 51 second channel 50.Have when being connected to When the aircraft of more than two engines, number of channels is adjusted according to the quantity of engine.

Each channel is connected to one of the engine of aircraft using at least one connector 52.In the exemplary embodiment, Connector 52 is made of the deformation of at least one sheath 53, helmet, material piece etc..Sheath 53, helmet etc. are connected to motor Front and the entrance for covering engine.

With reference to Fig. 6 A to Fig. 6 C, the alternative embodiment of module 46 is shown.In this embodiment, it is not distributed using air Device 47.Supply of the heating air to aircraft engine is carried out via two or more steam lines 25.

With reference to Fig. 7, shows exemplary air distributor 47, air stream of steam line 25 is divided at least one using it A first pipe 48 and at least one second pipe 50.In the exemplary embodiment, air distributor 47, air manifold etc. include The first pontes 54 and tube portion for being connected to steam line 25, for be connected to first passage 48 it is at least one Second connecting portion point 55 and tube portion, and it is connected at least one third coupling part 56 and the tube portion of second channel 50.

In the detailed description of the utility model, may omit for the professional in the utility model field show and The design details being clear to.Include these apparent design details in necessary degree, to realize the suitable of the present apparatus and method When and comprehensive performance.Even if some preferred embodiments are described in detail, but for the expert in the utility model field For, the change and modification of this method and design may become apparent.All such modifications and modification are regarded as falling into Within scope of the appended claims.

In an alternative embodiment, atmosphere control system includes a kind of function, using the function, can be adjusted from climate controlling The air humidity (moisture) of system discharge being supplied in the processing air of aircraft cabin.In an alternative embodiment, climate controlling The supply of electric power of system can be completed by the technology that another purpose is applicable in.For example, can be applicable in via another purpose Conduit, hose, pipe etc. complete energy supply.Thus it is conceivable that via hybrid combining (including internal combustion engine, power generation Machine and battery) solar panel, small-scale wind turbines or the other energy for being suitable for the purpose, generate the system of being supplied to Energy.It is further contemplated that this atmosphere control system can be defined as it is a kind of in the further of present patent application The system and or method used during processing.

Utility model advantage

The utility model realizes several advantages.Most apparent advantage is that, obtains elimination or reduce at least one described The system of technical problem.Another advantage is to obtain a kind of atmosphere control system for aircraft, substantially by coming from The energy of region heating provides power, this is advantageous in terms of environment.Another advantage of the utility model is that this practicality is new Type can be used for cooling and heating aircraft cabin.Another advantage of the utility model is can to connect the cooling unit of device It is connected to the system cooled down for region.Another advantage is that the present apparatus can be for example for heating/cooling down so-called connecting bridge Space system a part.Another advantage of this system is that the utility model can be used for warm ground to be melted in Snow and ice near the position for the aircraft parked.

Claims (10)

1. a kind of atmosphere control system (1) utilizes for when the aircraft is on the ground, being temporarily connected to an at least airplane (2) The air of processing is supplied to the aircraft by it using an at least flexible conduit (18) from least one air conditioner unit (3) Cabin；The air conditioner unit (3) is made of at least one heating and cooling packaging part (29), using it to being supplied to The air for stating cabin is heated or cooled；And the atmosphere control system includes transfer device (6), can be opposite using it In the aircraft and the mobile air conditioner unit of the transfer device (6)；And the atmosphere control system (1) includes using In in the heating and cooling packaging part (29) and region heating network or for conveying heating between the network of region cooling Or the subsystem of cooling fluid, subsystem include an at least flexible conduit (18), the flexible conduit (18) includes extremely Few one conduit for the fluid to be input to the air conditioner unit and at least one are used for the fluid from institute State the conduit of air conditioner unit return；It is characterized in that, the atmosphere control system by least one for by air from institute The discharge duct (38) for stating cabin back to the air conditioner unit (3) of aircraft forms, and the atmosphere control system Including at least one module (46) for the aircraft engine that thaws, the module (46) includes at least one air distributor (47), adapter, for the air of heating to be assigned to the aircraft engine from steam line (25).

2. atmosphere control system (1) according to claim 1, which is characterized in that the module (46) includes at least one The first passage (48) of the first engine (49) for being connected to the aircraft and at least one for being connected to the aircraft The second engine (51) second channel (50)；And each channel (48,50) are connected using at least one connector (52) One be connected in the engine of the aircraft.

3. atmosphere control system (1) according to claim 2, which is characterized in that the connector (52) is by least one It is connected to motor front and covers the modification composition of the sheath (53) of the entrance of the engine, helmet, material piece.

4. atmosphere control system (1) according to any one of claim 1 to 3, which is characterized in that the transfer device (6) it is made of retractable boarding bridge (7).

5. atmosphere control system (1) according to any one of claims 1 to 3, which is characterized in that the transfer device (6) it is made of lorry.

6. atmosphere control system (1) according to claim 4, which is characterized in that described to be used for the air-treatment list The subsystem of first (3) supply cold fluid and hot fluid includes at least one devices for taking-up (20), described soft using the devices for taking-up (20) Property conduit (18) the connecting bridge length variation during be rolled-up and be unfolded respectively.

7. atmosphere control system (1) according to claim 4, which is characterized in that the atmosphere control system is by least one It is a for air supply will heat or alternatively cooling to the inner space of connecting bridge, module including at least one from Independent conduit of the atmosphere control system to the connecting bridge.

8. atmosphere control system (1) according to any one of claim 1 to 3, which is characterized in that the climate controlling system System includes at least one sensor for sensing the temperature in aircraft cabin.

9. atmosphere control system (1) according to any one of claim 1 to 3, which is characterized in that the air-treatment list First (3) are at least one for cooling or heating battery module and at least one filter module by least one carbon filter It constitutes.

10. atmosphere control system (1) according to claim 4, which is characterized in that the atmosphere control system includes at least One sensor for sensing the temperature in aircraft cabin.