US20140060090A1 - Method of servicing an aircraft cooling system and aircraft cooling system - Google Patents

Method of servicing an aircraft cooling system and aircraft cooling system Download PDF

Info

Publication number
US20140060090A1
US20140060090A1 US13/974,373 US201313974373A US2014060090A1 US 20140060090 A1 US20140060090 A1 US 20140060090A1 US 201313974373 A US201313974373 A US 201313974373A US 2014060090 A1 US2014060090 A1 US 2014060090A1
Authority
US
United States
Prior art keywords
refrigerant
cooling circuit
cooling
cooling system
circuit
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US13/974,373
Other languages
English (en)
Inventor
Markus Piesker
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations GmbH
Original Assignee
Airbus Operations GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Priority to US13/974,373 priority Critical patent/US20140060090A1/en
Publication of US20140060090A1 publication Critical patent/US20140060090A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B45/00—Arrangements for charging or discharging refrigerant
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/28—Liquid-handling installations specially adapted for fuelling stationary aircraft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B41/00—Fluid-circulation arrangements
    • F25B41/30—Expansion means; Dispositions thereof
    • F25B41/385—Dispositions with two or more expansion means arranged in parallel on a refrigerant line leading to the same evaporator
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B49/00—Arrangement or mounting of control or safety devices
    • F25B49/02—Arrangement or mounting of control or safety devices for compression type machines, plants or systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B49/00—Arrangement or mounting of control or safety devices
    • F25B49/02—Arrangement or mounting of control or safety devices for compression type machines, plants or systems
    • F25B49/022—Compressor control arrangements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/0674—Environmental Control Systems comprising liquid subsystems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2345/00—Details for charging or discharging refrigerants; Service stations therefor
    • F25B2345/001—Charging refrigerant to a cycle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2345/00—Details for charging or discharging refrigerants; Service stations therefor
    • F25B2345/005—Service stations therefor
    • F25B2345/0052—Service stations therefor having wheels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2400/00—General features or devices for refrigeration machines, plants or systems, combined heating and refrigeration systems or heat-pump systems, i.e. not limited to a particular subgroup of F25B
    • F25B2400/06—Several compression cycles arranged in parallel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B40/00—Subcoolers, desuperheaters or superheaters
    • F25B40/02—Subcoolers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B5/00—Compression machines, plants or systems, with several evaporator circuits, e.g. for varying refrigerating capacity
    • F25B5/02—Compression machines, plants or systems, with several evaporator circuits, e.g. for varying refrigerating capacity arranged in parallel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B7/00—Compression machines, plants or systems, with cascade operation, i.e. with two or more circuits, the heat from the condenser of one circuit being absorbed by the evaporator of the next circuit

Definitions

  • the invention relates to a method of servicing an aircraft cooling system for operation with a two-phase refrigerant, an aircraft cooling system for operation with a two-phase refrigerant and an arrangement comprising the aircraft cooling system as well as a servicing unit for servicing the aircraft cooling system.
  • Cooling systems for operation with a two-phase refrigerant are known from DE 10 2006 005 035 B3, WO 2007/088012 A1, DE 10 2009 011 797 A1 and US 2010/0251737 A1 and may be used to cool various cooling energy consumers present on board an aircraft such as, for example, food that is intended to be supplied to the passengers or heat generating components such as electric or electronic components.
  • the cooling systems known from DE 10 2006 005 035 B3, WO 2007/088012 A1, DE 10 2009 011 797 A1 and US 2010/0251737 A1 the phase transitions of the refrigerant flowing through the circuit that occur during operation of the system allow the latent heat consumption that then occurs to be utilized for cooling purposes.
  • the refrigerant mass flow needed to provide a desired cooling capacity is therefore markedly lower than for example in a liquid cooling system, in which a one-phase liquid refrigerant is used.
  • the cooling systems described in DE 10 2006 005 035 B3, WO 2007/088012 A1, DE 10 2009 011 797 A1 and US 2010/0251737 A1 may have lower tubing cross sections than a liquid cooling system with a comparable cooling capacity and hence provide the advantages of a lower installation volume and a lower weight.
  • the reduction of the refrigerant mass flow makes it possible to reduce the conveying capacity needed to convey the refrigerant through the cooling circuit of the cooling system. This leads to an increased efficiency of the system because less energy is needed to operate a corresponding conveying device, such as for example a pump, and moreover less additional heat generated by the conveying device during operation of the conveying device has to be removed from the cooling system.
  • the invention is directed to the object to provide a reliable and efficient method of servicing an aircraft cooling system for operation with a two-phase refrigerant. Further, the invention is directed to the object to provide an aircraft cooling system for operation with a two-phase refrigerant which can be serviced in a reliable and efficient manner. Finally, the invention is directed to the object to provide an arrangement comprising the aircraft cooling system and a servicing unit for servicing the aircraft cooling system in a reliable and efficient manner.
  • a refilling container containing a two-phase refrigerant is connected to a refrigerant connection provided in a cooling circuit of the cooling system.
  • the refilling container is connected to the refrigerant connection of the cooling system in a sealed manner via a preferably flexible line and a first refrigerant connection adaptor.
  • the refilling container, the flexible line and the first refrigerant connection adaptor may be integrated into a preferably mobile servicing unit which may be formed separate of the aircraft and be adapted for connection to the aircraft cooling system exclusively for servicing purposes.
  • the aircraft cooling system may, for example, be a cooling system which is in particular suitable for cooling heat generating components or food on board the aircraft and comprises a cooling circuit allowing circulation of a two-phase refrigerant therethrough.
  • the two-phase refrigerant which circulates in the cooling circuit of the cooling system is a refrigerant, which upon releasing cooling energy to a cooling energy consumer is converted from the liquid to the gaseous state of aggregation and is then converted back to the liquid state of aggregation.
  • the two-phase refrigerant may, for example, be R134A (CH2F-CF3).
  • Electric or electronic systems, such as avionic systems or fuel cell systems usually have to be cooled at a higher temperature level than food.
  • Galden® can be used as a two-phase refrigerant.
  • CO2 is employed as the two-phase refrigerant, since CO2 is at least substantially environment-neutral.
  • the cooling system is operated with a predetermined operating amount of refrigerant circulating in the cooling circuit which is defined by an amount of refrigerant which is necessarily required to properly operate the cooling system, and an additional amount of refrigerant to compensate for leakages of the system and system tolerances.
  • a predetermined operating amount of refrigerant circulating in the cooling circuit should be as low as possible.
  • Small leakages present in the system or service work involving dismounting of components from the cooling system or replacing components of the cooling system may, however, cause the amount of refrigerant circulating in the cooling circuit to fall below a predetermined minimum value which may, for example, be defined by the amount of refrigerant which is necessarily required to properly operate the cooling system.
  • the servicing method according to the invention therefore comprises the step of supplying the refrigerant contained in the refilling container from the refilling container into the cooling circuit of the cooling system.
  • the refrigerant contained in the refilling container is supplied into the cooling circuit of the cooling system while there is still a considerable amount of refrigerant present in the cooling circuit of the cooling system which might, however, not be sufficient to properly operate the cooling system.
  • a condenser disposed in the cooling circuit is operated so as to liquefy gaseous refrigerant flowing through the cooling circuit. Operation of the condenser causes a decrease of the temperature and hence the pressure of the refrigerant in the cooling circuit of the cooling system. As a result, refrigerant may be conveyed from the refilling container into the cooling circuit of the cooling system in a fast and efficient manner. Further, operation of the condenser ensures that refrigerant supplied from the refilling container into the cooling circuit of the cooling system is liquefied immediately upon entering the cooling circuit.
  • the method according to the invention thus allows a cooling system operated with a two-phase refrigerant to be serviced in a reliable, time-saving and cost-effective manner.
  • operation of the condenser is controlled such that the pressure of the refrigerant in the cooling circuit of the cooling system is decreased below the pressure of the refrigerant in the refilling container.
  • the refrigerant may be conveyed from the refilling container into the cooling circuit of the cooling system driven by the pressure difference between the refilling container and the cooling circuit, i.e., the difference between the pressure of the refrigerant in the refilling container and the pressure of the refrigerant in the cooling circuit.
  • the use of an additional conveying device for conveying the refrigerant from the refilling container into the cooling circuit thus can be limited or even dispensed with.
  • the reflow of refrigerant from the cooling circuit into the refilling container may be prevented, independent of the pressure conditions in the refilling container and the cooling circuit, for example, by means of a check valve which may be integrated into the refrigerant connection of the cooling circuit or the first refrigerant connection adaptor of the servicing unit.
  • the pressure difference driven supply of refrigerant from the filling container into the cooling circuit of the cooling system may slow down or even be interrupted due to a decrease of the temperature and hence the pressure of the refrigerant in the refilling container which may result from a large amount of refrigerant being discharged from the refilling container in a short period of time.
  • the refrigerant contained in the refilling container then may be liquefied, for example by means of a condenser of the servicing unit, prior to being supplied into the cooling circuit of the cooling system.
  • the liquid refrigerant may be conveyed into the cooling circuit of the cooling system by means of a suitable conveying device, such as a pump of the servicing unit.
  • a pressure difference driven supply of liquid refrigerant from the refilling container into the cooling circuit of the cooling system is conceivable.
  • liquid refrigerant contained in a lower region of the refilling container is supplied into the cooling circuit, wherein the pressure in the refilling container is built up due to the presence of a gas layer in an upper region of the refilling container.
  • a servicing unit to be connected to the cooling system for servicing the cooling system may be or a particularly simply design and may comprise only one refilling container.
  • operation of the condenser is ceased when an amount of refrigerant in the cooling circuit has reached a predetermined maximum value.
  • residual refrigerant is supplied from the refilling container into the cooling circuit only until pressure equalization takes place between the refilling container and the cooling circuit, i.e., until the pressure of the refrigerant in the refilling container corresponds to the pressure of the refrigerant in the cooling circuit.
  • Ceasing operation of the condenser may be achieved by shutting-down the condenser, for example under the control of a suitable control unit.
  • a storage volume of the condenser such that it is capable of receiving an amount of liquefied refrigerant which corresponds to the predetermined maximum amount of refrigerant in the cooling circuit.
  • the predetermined maximum value of the amount of refrigerant in the cooling circuit may correspond to the predetermined operating amount of refrigerant or be slightly higher than the predetermined operating amount of refrigerant, but still low enough to prevent an undesired pressure increase in the cooling circuit, for example at high ambient temperatures.
  • the amount of liquid refrigerant in the cooling circuit may be detected by at least one fill level sensor which may be disposed in an accumulator and/or a storage container of the cooling system. Further, by measuring the temperature and the pressure of the refrigerant in the cooling circuit, the amount of gaseous refrigerant in the cooling circuit may be derived allowing the total amount of refrigerant present in the cooling circuit of the cooling system to be determined.
  • the supply of residual refrigerant from the refilling container into the cooling circuit until pressure equalization takes place between the refilling container and the cooling circuit may cause an undesired pressure increase in the cooling circuit, for example when the refrigerant in the refilling container has a high temperature due to high ambient temperatures. Therefore, the supply of refrigerant from the refilling container into the cooling circuit may be interrupted when a pressure in the cooling circuit has reached a predetermined value. An interruption of the supply of refrigerant from the refilling container into the cooling circuit in dependence of the pressure in the cooling circuit may be achieved, for example, by means of a pressure regulator which may be incorporated in the refrigerant connection of the cooling system or the first refrigerant connection adaptor of the servicing unit.
  • a first warning signal indicating a required supply of refrigerant into the cooling circuit may be output when an amount of refrigerant in the cooling circuit falls below a predetermined warning value.
  • the predetermined warning value may be lower than the predetermined maximum value and the predetermined operating value of the amount of refrigerant in the cooling circuit, but still higher than the predetermined minimum value of the amount of refrigerant in the cooling circuit.
  • the first warning signal may be a visual signal or an audible signal which may indicate to the aircraft crew and/or the aircraft service crew that servicing of the cooling system including refilling of refrigerant into the cooling circuit of the cooling system will be required in the near future, but that the cooling system still is ready to operate.
  • a second warning signal indicating a required supply of refrigerant into the cooling circuit may be output when an amount of refrigerant in the cooling circuit falls below the predetermined minimum value.
  • the second warning signal may be a visual signal or an audible signal which may indicate to the aircraft crew and/or the aircraft service crew that servicing of the cooling system including refilling of refrigerant into the cooling circuit of the cooling system is required and that the cooling system is no longer ready to operate.
  • operation of the cooling system may be ceased, for example under the control of a suitable control unit, when an amount of refrigerant in the cooling circuit falls below the predetermined minimum value.
  • start-up of the cooling system may be prevented, for example under the control of a suitable control unit, when the amount of refrigerant in the cooling circuit is below the predetermined minimum value. Ceasing operation and/or preventing start-up of the cooling system when the amount of refrigerant in the cooling circuit is below the predetermined minimum value protects the components of the cooling system, in particular a conveying device for conveying the refrigerant through the cooling circuit of the cooling system, from damages caused by dry operation of these components.
  • self-sealing couplings connecting the component to the cooling circuit may prevent refrigerant from exiting the cooling circuit.
  • a chiller and/or the conveying device for conveying the refrigerant through the cooling circuit of the cooling system may be connected to the cooling circuit via self-sealing couplings and thus may be dismounted from the cooling circuit, for example for servicing purposes, in a particularly safe, easy and time-saving manner without an excessive amount of refrigerant leaking from the cooling circuit.
  • Self-sealing couplings add to the costs and the weight of the cooling system and also may not be actuatable at high refrigerant pressures in the cooling circuit of the cooling system.
  • refrigerant may be discharged from the cooling circuit or conveyed into a hermetically sealable accumulator disposed in the cooling circuit.
  • Refrigerant discharged from the cooling circuit may either be released to the ambient or collected in a storage container.
  • a second refrigerant connection adaptor may be connected to the refrigerant connection of the cooling system.
  • the second refrigerant connection adaptor may comprise a nozzle which is adapted to control the flow of refrigerant from the cooling circuit such that freezing of the refrigerant and hence icing of the nozzle and/or further components of the cooling system and/or the servicing unit is reliably prevented.
  • the refrigerant is discharged from the cooling circuit of the cooling system in its liquid state of aggregation.
  • the storage container may be incorporated in a servicing unit in a releasable manner and be connected to the refrigerant connection of the cooling system via the second refrigerant connection adaptor and a preferably flexible line.
  • the refrigerant discharged from the cooling circuit of the cooling system is stored in the storage container in its liquid state of aggregation and hence at a relatively low pressure. If necessary, the refrigerant may be liquefied by means of a condenser of the servicing unit prior to being received in the storage container.
  • the cooling circuit After discharging refrigerant from the cooling circuit and prior to reintroducing refrigerant into the cooling circuit, the cooling circuit preferably is evacuated.
  • the cooling circuit may be evacuated by means of an evacuation device such as, for example, a vacuum pump of the servicing unit. Evacuation of the cooling circuit allows residual air and humidity, which may affect operation of the cooling system, to be removed from the cooling system before refrigerant is reintroduced into the cooling circuit.
  • the refrigerant reintroduced into the cooling circuit may be the refrigerant which is discharged from the cooling circuit and received in the storage container. It is, however, also conceivable to supply the cooling system entirely or partially with “fresh” refrigerant which may be supplied to the storage container of the servicing unit.
  • the condenser of the cooling system may be operated so as to evaporate the refrigerant prior to entering the cooling circuit and to liquefy the gaseous refrigerant upon circulating through the cooling circuit.
  • a condenser of the servicing unit preferably is not operated so as to ensure unhindered evaporation of the refrigerant which, for example, is contained in the storage container of the servicing unit.
  • the storage container is heated so as to support evaporation of the refrigerant in the storage container.
  • An aircraft cooling system comprises a cooling circuit allowing circulation of a two-phase refrigerant therethrough.
  • a refrigerant connection is provided in the cooling circuit which, for servicing of the aircraft cooling system, is adapted to be connected to a refilling container containing the two-phase refrigerant.
  • the cooling system further comprises a control unit, for example an electronic control unit, which is adapted to operate a condenser disposed in the cooling circuit so as to liquefy gaseous refrigerant flowing through the cooling circuit during the supply of refrigerant from the refilling container into the cooling circuit.
  • the refrigerant connection of the cooling system may be designed so as to allow a flow of refrigerant from the refilling container into the cooling circuit, but to prevent a flow of refrigerant from the cooling circuit into the refilling container.
  • a check valve may be integrated into the refrigerant connection.
  • the control unit may further be adapted to cease operation of the condenser when an amount of refrigerant in the cooling circuit has reached a predetermined maximum value.
  • a storage volume of the condenser may be designed such that it is capable of receiving an amount of liquefied refrigerant which corresponds to the predetermined maximum amount of refrigerant in the cooling circuit.
  • the control unit may further be adapted to interrupt the supply of refrigerant from the refilling container into the cooling circuit of the cooling system when an amount of refrigerant in the cooling circuit has reached a predetermined maximum value.
  • the control unit may be adapted to control a suitable valve of the cooling system into a closed position wherein the valve interrupts the flow of refrigerant from the refilling container into the cooling circuit of the cooling system.
  • the control unit of the cooling system and/or a control unit of a servicing unit may be adapted to control a suitable valve of the servicing unit into a closed position wherein the valve interrupts the flow of refrigerant from the refilling container into the cooling circuit of the cooling system.
  • the control unit of the cooling system and/or the control unit of a servicing unit may be adapted to cease operation of the servicing unit to interrupt the supply of refrigerant from the refilling container into the cooling circuit of the cooling system.
  • the aircraft cooling system may further comprise means for interrupting the supply of refrigerant from the refilling container into the cooling circuit of the cooling system when a pressure in the cooling circuit has reached a predetermined value.
  • An interruption of the supply of refrigerant from the refilling container into the cooling circuit in dependence of the pressure in the cooling circuit may be achieved, for example, by means of a pressure regulator incorporated in the refrigerant connection of the cooling system.
  • the aircraft cooling system may further comprise a warning signal output device which is adapted to output a first warning signal indicating a required supply of refrigerant into the cooling circuit when an amount of refrigerant in the cooling circuit falls below a predetermined warning value, and/or to output a second warning signal indicating a required supply of refrigerant into the cooling circuit when an amount of refrigerant in the cooling circuit falls below a predetermined minimum value.
  • a warning signal output device which is adapted to output a first warning signal indicating a required supply of refrigerant into the cooling circuit when an amount of refrigerant in the cooling circuit falls below a predetermined warning value, and/or to output a second warning signal indicating a required supply of refrigerant into the cooling circuit when an amount of refrigerant in the cooling circuit falls below a predetermined minimum value.
  • control unit may be adapted to cease operation of the cooling system when an amount of refrigerant in the cooling circuit falls below the predetermined minimum value.
  • control unit may be adapted to prevent start-up of the cooling system when the amount of refrigerant in the cooling circuit is below the predetermined minimum value.
  • a component disposed in the cooling circuit such as, for example, a chiller or a conveying device, may be connected to the cooling circuit via self-sealing couplings which, upon dismounting the component from the cooling circuit, are adapted to prevent refrigerant from exiting the cooling circuit.
  • the aircraft cooling system may comprise a hermetically sealable accumulator disposed in the cooling circuit.
  • the control unit of the aircraft cooling system upon reintroducing refrigerant into the cooling circuit when the cooling circuit, after discharging refrigerant from the cooling circuit, is evacuated, may be adapted to operate the condenser of the cooling system so as to evaporate the refrigerant prior to entering the cooling circuit and to liquefy the gaseous refrigerant upon circulating through the cooling circuit.
  • An arrangement according to the invention comprises an above described aircraft cooling system and a servicing unit for servicing the aircraft cooling system.
  • the servicing unit comprises a first refrigerant connection adaptor adapted to be connected to the refrigerant connection of the cooling system so as to connect a refilling container containing a two-phase refrigerant to a cooling circuit of the cooling system.
  • the servicing unit preferably is formed separate from the aircraft and may be designed as a movable device which, for example, comprises a carriage onto which the components of servicing unit are mounted.
  • the servicing unit preferably further comprises a condenser.
  • the condenser may be used for liquefying refrigerant contained in a refilling container prior to being supplied into the cooling circuit of the cooling system, for liquefying refrigerant discharged from the cooling circuit of the cooling system prior to being received in a storage container and/or for liquefying refrigerant prior to being reintroduced into the cooling circuit when the cooling circuit, after discharging refrigerant from the cooling circuit, is evacuated.
  • the servicing unit may further comprise a conveying device which may be used for conveying refrigerant from the refilling container into the cooling circuit of the cooling system and/or for conveying refrigerant from the cooling circuit of the cooling system into the storage container.
  • a conveying device which may be used for conveying refrigerant from the refilling container into the cooling circuit of the cooling system and/or for conveying refrigerant from the cooling circuit of the cooling system into the storage container.
  • the conveying device of the servicing unit is designed in the form of a pump and hence should be operated with refrigerant in its liquid state of aggregation.
  • the servicing unit may further comprise means for interrupting the supply of refrigerant from the refilling container into the cooling circuit of the cooling system, when a pressure in the cooling circuit has reached a predetermined value.
  • a suitable pressure regulator may be incorporated in the first refrigerant connection adaptor of the servicing unit.
  • the servicing unit may comprise means for interrupting the supply of refrigerant from the refilling container into the cooling circuit of the cooling system, when an amount of refrigerant in the cooling circuit has reached a predetermined value.
  • a second refrigerant connection adaptor of the servicing unit may be adapted to be connected to the refrigerant connection of the cooling system so as to discharge refrigerant from the cooling circuit of the cooling system.
  • the second refrigerant connection adaptor may comprise a nozzle which is adapted to control the flow of refrigerant from the cooling circuit such that freezing of the refrigerant and hence icing of the nozzle and/or further components of the cooling system and/or the servicing unit is reliably prevented.
  • the servicing unit may further comprise an evacuation device such as, for example, a vacuum pump which may be adapted to evacuate the cooling circuit of the cooling system after discharging refrigerant from the cooling circuit and prior to reintroducing refrigerant into the cooling circuit.
  • an evacuation device such as, for example, a vacuum pump which may be adapted to evacuate the cooling circuit of the cooling system after discharging refrigerant from the cooling circuit and prior to reintroducing refrigerant into the cooling circuit.
  • the servicing unit may also comprise a heater which is adapted to heat the storage container of the servicing unit so as to support evaporation of the refrigerant in the storage container.
  • the arrangement 100 depicted in FIG. 1 comprises a cooling system 10 which on board an aircraft, for example, may be employed to cool food provided for supplying to the passengers.
  • the cooling system 10 comprises a cooling circuit 12 allowing circulation of a two-phase refrigerant therethrough.
  • the two-phase refrigerant may for example be CO2 or R134A.
  • Four evaporators 14 a , 14 b , 14 c , 14 d are disposed in the cooling circuit 12 .
  • Each evaporator 14 a , 14 b , 14 c , 14 d comprises a refrigerant inlet 16 a , 16 b , 16 c , 16 d and a refrigerant outlet 18 a , 18 b , 18 c , 18 d .
  • the refrigerant flowing through the cooling circuit 12 is supplied to the refrigerant inlets 16 a , 16 b , 16 c , 16 d of the evaporators 14 a , 14 b , 14 c , 14 d in its liquid state of aggregation.
  • the refrigerant Upon flowing through the evaporators 14 a , 14 b , 14 c , 14 d the refrigerant releases its cooling energy to a cooling energy consumer which in the embodiment of a cooling system 10 depicted in FIG. 1 is formed by the food to be cooled.
  • the refrigerant Upon releasing its cooling energy, the refrigerant is evaporated and hence exits the evaporators 14 a , 14 b , 14 c , 14 d at the refrigerant outlets 18 a , 18 b , 18 c , 18 d of the evaporators 14 a , 14 b , 14 c , 14 d in its gaseous state of aggregation.
  • the supply of refrigerant to the evaporators 14 a , 14 b , 14 c , 14 d is controlled by respective valves 20 a , 20 b , 20 c , 20 d which are disposed in the cooling circuit 12 upstream of the evaporators 14 a , 14 b , 14 c , 14 d , respectively.
  • the cooling system 10 comprises a first, a second and a third condenser 22 a , 22 b , 22 c .
  • Each condenser 22 a , 22 b , 22 c has two refrigerant inlets 24 a , 24 a ′, 24 b , 24 b ′, 24 c , 24 c ′ and two refrigerant outlets 26 a , 26 a ′, 26 b , 26 b ′, 26 c , 26 c ′.
  • the condensers 22 a , 22 b , 22 c are thermally coupled to respective chillers 27 a , 27 b , 27 c which are connected to the cooling circuit 12 of the cooling system 10 via self-sealing couplings.
  • the condensers 22 a , 22 b , 22 c also may be coupled to a different cold source such as, for example, an outer skin heat exchanger of the aircraft.
  • the cooling energy provided by the chillers 27 a , 27 b , 27 c in the condensers 22 a , 22 b , 22 c is used to condense the refrigerant.
  • the refrigerant exits the condensers 22 a , 22 b , 22 c at the refrigerant outlets 26 a , 26 a ′, 26 b , 26 b ′, 26 c , 26 c ′ of the condensers 22 a , 22 b , 22 c in its liquid state of aggregation.
  • the refrigerant outlets 26 a , 26 a ′, 26 b , 26 b ′, 26 c , 26 c ′ of the condensers 22 a , 22 b , 22 c each are connected to a storage container 28 a , 28 a ′, 28 b , 28 b ′, 28 c , 28 c ′, 28 d , 28 d ′ which is arranged downstream and below each one of the condensers 22 a , 22 b , 22 c .
  • the storage containers 28 a , 28 a ′, 28 b , 28 b ′, 28 c , 28 c ′, 28 d , 28 d ′ which may also be formed integral with the condensers 22 a , 22 b , 22 c , are connected to supercoolers 30 a , 30 b , 30 c which are arranged downstream and below the storage containers 28 a , 28 a ′, 28 b , 28 b ′, 28 c , 28 c ′, 28 d , 28 d ′.
  • Liquid refrigerant may be conveyed gravity-driven from the condensers 22 a , 22 b , 22 c into the storage containers 28 a , 28 a ′, 28 b , 28 b ′, 28 c , 28 c ′, 28 d , 28 d ′ and further into the supercoolers 30 a , 30 b , 30 c .
  • the supercoolers 30 a , 30 b , 30 c may also be formed integral with the condensers 22 a , 22 b , 22 c.
  • the cooling circuit 12 of the cooling system 10 comprises two loops 12 a , 12 a ′ which are hermetically sealed from each other.
  • Two evaporators 14 a , 14 b are disposed in the first cooling circuit loop 12 a
  • two evaporators 14 c , 14 d are disposed in the second cooling circuit loop 12 a ′.
  • a first conveying device 32 a designed in the form of a pump serves to convey refrigerant through the first cooling circuit loop 12 a
  • a second conveying device 32 b also designed in the form of a pump serves to convey refrigerant through the second cooling circuit loop 12 a ′.
  • the conveying devices 32 a , 32 b are connected to the cooling circuit 12 of the cooling system 10 via self-sealing couplings.
  • Each one of the condensers 22 a , 22 b , 22 c is connected to first and the second conveying device 32 a , 32 b and hence to the first and the second cooling circuit loop 12 a , 12 a ′ so as to provide for redundancy in the event of a malfunctioning of one of the condensers 22 a , 22 b , 22 c.
  • a first accumulator 34 a is connected to the refrigerant inlet 24 a of the condenser 22 a , wherein the supply of refrigerant from the first accumulator 34 a to the condenser 22 a is controlled by means of a valve 36 a .
  • a valve 36 b controls the supply of refrigerant from a second accumulator 34 b to the refrigerant inlet 24 c ′ of the condenser 22 c .
  • valve 36 a provided in the first cooling circuit loop 12 a merely serves to control the flow of refrigerant between the first accumulator 34 a and the condenser 22 a
  • the valve 36 b disposed in the second cooling circuit loop 12 a ′ is designed in the form of a 3/2 control valve which may either allow refrigerant to be conveyed into the second accumulator 34 a or the condenser 22 c by the second conveying device 32 b or allow refrigerant to flow from the second accumulator 34 a to the refrigerant inlet 24 c ′ of the condenser 22 c .
  • a pressure regulating valve 37 is disposed upstream of the valve 36 b and downstream of the second conveying device 32 b .
  • the pressure regulating valve 37 is adapted to open or close in dependence on a pressure difference acting on the valve 37 .
  • the supply of refrigerant from the first conveying device 32 a to the first accumulator 34 a is controlled by means of a valve 38 .
  • the accumulators 34 a , 34 b may simply be designed as an “additional volume” which at a predetermined temperature limits the pressure in the cooling circuit 12 .
  • the accumulators 34 a , 34 b then may be connected to only a single line which opens into the accumulators 34 a , 34 b in a lower region, preferably at the lowest point of the accumulators 34 a , 34 b and connects the accumulators 34 a , 34 b to the condensers 22 a , 22 b , 22 c.
  • Cooling circuit control valves 40 a , 40 b are disposed in the first and the second cooling circuit loop 12 a , 12 a ′ downstream of the evaporators 14 a , 14 b , 14 c , 14 d and upstream of the condensers 22 a , 22 b , 22 c .
  • Further cooling circuit control valves 42 a , 42 b are disposed in the first and the second cooling circuit loop 12 a , 12 a ′ upstream of the evaporators 14 a , 14 b , 14 c , 14 d and downstream of the condensers 22 a , 22 b , 22 c .
  • cooling circuit control valves 40 a , 40 b , 42 a , 42 b seal a high pressure section of the cooling circuit loops 12 a , 12 a ′ from a low pressure section of the cooling circuit loops 12 a , 12 a ′.
  • cooling circuit control valves 43 a , 43 b are disposed in the first and the second cooling circuit loop 12 a , 12 a ′ upstream of the accumulators 34 a , 34 b .
  • the accumulators 34 a , 34 b may be hermetically sealed.
  • the accumulators 34 a , 34 b are connected to the cooling circuit 12 via self-sealing couplings.
  • the valves 36 a , 36 b , 38 , 43 a , 43 b may be closed and the accumulators 34 a , 34 b may be released from the cooling circuit 12 without considerable amounts of refrigerant exiting the cooling system 10 by simply actuating the self-sealing couplings.
  • the accumulators 34 a , 34 b may be released from the cooling circuit 12 in an empty state or also with refrigerant received therein.
  • an accumulator 34 a , 34 b which is filled with the refrigerant present in the cooling circuit 12 of the cooling system 10 may be replaced by a replacement accumulator 34 a , 34 b which is filled with a desired amount of “fresh” refrigerant.
  • a replacement accumulator 34 a , 34 b which is filled with a desired amount of “fresh” refrigerant.
  • valves 36 a , 36 b , 38 , 43 a , 43 b are automatically actuatable valves. It is, however, also conceivable to design the valves 36 a , 36 b , 38 , 43 a , 43 b as manually actuatable valves.
  • An actuating lever for actuating manually actuatable valves 36 a , 36 b , 38 , 43 a , 43 b then, however, should be designed in such a manner that unintended misuse of the lever is prevented.
  • the actuating lever of a valve 36 a , 36 b , 38 , 43 a , 43 b could be designed such that the lever, for actuating the valve 36 a , 36 b , 38 , 43 a , 43 b , has be pressed into the valve 36 a , 36 b , 38 , 43 a , 43 b and, after the actuation of the valve 36 a , 36 b , 38 , 43 a , 43 b , automatically falls out of the valve 36 a , 36 b , 38 , 43 a , 43 b or latches in an idle position.
  • the cooling system 10 further comprises pressure relief valves 44 a , 44 b which are connected to a respective one of the cooling circuit loops 12 a , 12 a ′ downstream of a respective one of the cooling circuit control valves 42 a , 42 b .
  • Pressure relief valves 46 a , 46 b are connected to a respective one of the cooling circuit loops 12 a , 12 a ′ upstream of a respective one of the cooling circuit control valves 40 a , 40 b .
  • Pressure relief valves 48 a , 48 b are connected to a respective one of the cooling circuit loops 12 a , 12 a ′ downstream of a respective one of the cooling circuit control valves 40 a , 40 b .
  • pressure relief valves 49 a , 49 b are connected to the accumulators 34 a , 34 b .
  • the pressure relief valves 44 a , 44 b , 46 a , 46 b , 48 a , 48 b , 49 a , 49 b are designed as mechanically actuatable valves which automatically open in case a pressure difference acting on the valves 44 a , 44 b , 46 a , 46 b , 48 a , 48 b , 49 a , 49 b exceeds a threshold value which is determined by the design of the valves 44 a , 44 b , 46 a , 46 b , 48 a , 48 b , 49 a , 49 b .
  • the pressure relief valves 44 a , 44 b , 46 a , 46 b , 48 a , 48 b , 49 a , 49 b in the form of burst discs or bust discs may be provided in addition to the pressure relief valves 44 a , 44 b , 46 a , 46 b , 48 a , 48 b , 49 a , 49 b.
  • the cooling system 10 further is provided with refrigerant connections 50 a , 50 b .
  • the refrigerant connection 50 a associated with the first cooling circuit loop 12 a is connected to the first accumulator 34 a
  • the refrigerant connection 50 a associated with the second cooling circuit loop 12 a is connected to the second accumulator 34 b .
  • the refrigerant connection 50 a associated with the first cooling circuit loop 12 a is connected to an outlet side of the first conveying device 32 a , wherein a valve 51 a serves to control the supply of refrigerant from the outlet side of the first conveying device 32 a to the refrigerant connection 50 a .
  • the refrigerant connection 50 b associated with the second cooling circuit loop 12 b is connected to an outlet side of the second conveying device 32 b , wherein a valve 51 b serves to control the supply of refrigerant from the outlet side of the second conveying device 32 b to the refrigerant connection 50 b .
  • Each one of the refrigerant connections 50 a , 50 b comprises an integrated check valve and an integrated pressure regulator (not shown in the drawing). Operation of the cooling system 10 is controlled by means of an electronic control unit 52 .
  • the electronic control unit 52 controls operation of the evaporators 14 a , 14 b , 14 c , 14 d , the condensers 22 a , 22 b and the various valves employed in the cooling circuit 12 .
  • Fill level sensors are provided in the accumulators 34 a , 34 b and/or the storage containers 28 a , 28 a ′, 28 b , 28 b ′, 28 c , 28 c ′.
  • the fill level sensors serve to detect the amount of liquid refrigerant present in the cooling circuit 12 .
  • the cooling system 10 comprises sensors (also not shown in the drawing) which serve to detect the temperature and the pressure of the refrigerant in the cooling circuit 12 and hence allow the amount of gaseous refrigerant present in the cooling circuit 12 to be determined.
  • suitable sensors are provided which detect the operating state of the valves 36 a , 36 b , 38 , 43 a , 43 b , i.e., detect whether the accumulators 34 a , 34 b are hermetically sealed or connected to the cooling circuit 12 .
  • the signals of all sensors are transmitted to the control unit 52 .
  • a warning signal output device 54 a , 54 b is associated with each one of the first and the second cooling circuit loop 12 a , 12 a′.
  • the arrangement 100 further comprises a servicing unit 56 for servicing the aircraft cooling system 10 .
  • the servicing unit 56 is designed as a movable device which comprises a carriage 57 onto which the components of servicing unit 100 are mounted.
  • the servicing unit 56 comprises a first refrigerant connection adaptor 58 adapted to be connected to a refrigerant connection 50 a , 50 b of the cooling system 10 so as to connect a refilling container 60 containing a two-phase refrigerant to the cooling circuit 12 of the cooling system 10 .
  • the servicing unit 56 further comprises a condenser 62 which is provided with cooling energy from a chiller 64 and a conveying device 66 which is designed in the form of a pump.
  • a second refrigerant connection adaptor 68 of the servicing unit 56 is adapted to be connected to a refrigerant connection 50 a , 50 b of the cooling system 10 so as to discharge refrigerant from the cooling circuit 12 of the cooling system 10 .
  • the second refrigerant connection adaptor 68 comprises a nozzle (not shown in the drawing) which is adapted to control the flow of refrigerant from the cooling circuit 12 such that freezing of the refrigerant and hence icing of the nozzle and/or further components of the cooling system 10 and/or the servicing unit 56 is prevented.
  • the first and/or the second refrigerant connection adaptor 58 , 68 of the servicing unit 56 may comprise an integrated check valve and an integrated pressure regulator (not shown in the drawing).
  • the refrigerant connections 50 a , 50 b of the cooling system 10 are adapted to be connected to either the first or the second refrigerant connection adaptor 58 , 68 of the servicing unit 56 .
  • a mechanical or electrical mechanism of the refrigerant connections 50 a , 50 b (not shown in the drawing), which is actuated upon connecting the first refrigerant connection adaptor 58 to the refrigerant connections 50 a , 50 b , provides for an activation of the check valve and the pressure regulator integrated in the refrigerant connections 50 a , 50 b .
  • refrigerant is prevented to flow from the cooling circuit 12 in the direction of the servicing unit.
  • built-up of excessive pressure in the cooling circuit 12 is prevented.
  • the mechanical or electrical mechanism of the refrigerant connections 50 a , 50 b which is actuated upon connecting the second refrigerant connection adaptor 68 to the refrigerant connections 50 a , 50 b , provides for a deactivation of the check valve and the pressure regulator integrated in the refrigerant connections 50 a , 50 b .
  • a flow of refrigerant from the cooling circuit 12 in the direction of the servicing unit is enabled.
  • An undesired flow of refrigerant from the servicing unit 56 into the cooling circuit 12 and/or the built-up of excessive pressure in the servicing unit 56 are prevented when the second refrigerant connection adaptor 68 comprises an integrated check valve and/or an integrated pressure regulator.
  • the servicing unit 56 further comprises an evacuation device 70 in the form of a vacuum pump. Finally, the servicing unit 56 comprises a heater 72 which is adapted to heat a storage container 74 of the servicing unit 56 .
  • the control unit 52 controls the operation of the cooling system 10 such that the chillers 27 a , 27 b , 27 c are operated and refrigerant is liquefied in the condensers 22 a , 22 b , 22 c and supercooled in the supercoolers 30 a , 30 b , 30 c . Due to the conveying devices 32 a , 32 b being arranged below the condensers 22 a , 22 b , 22 c the conveying devices 32 a , 32 b are flooded by the refrigerant liquefied in the condensers 22 a , 22 b , 22 c .
  • conveying devices 32 a , 32 b are flooded before operation of the conveying devices 32 a , 32 b is started, it is not necessary that the conveying devices 32 a , 32 b are designed in the form of a self-sucking pump.
  • the conveying devices 32 a , 32 b convey refrigerant liquefied in the condensers 22 a , 22 b , 22 c into the accumulators 34 a , 34 b via valves 36 a , 36 b .
  • the valves 42 a , 42 b are closed so as to prevent refrigerant to be conveyed to the evaporators 14 a , 14 b , 14 c , 14 d .
  • An operating state of the cooling system 10 wherein the condensers 22 a , 22 b , 22 c are operated so as liquefy refrigerant, although the amount of liquid refrigerant present in the cooling circuit 12 is already sufficient to allow the desired flooding of cooling system components, while the supply of refrigerant to the evaporators 14 a , 14 b , 14 c , 14 d , however, still is interrupted is designated as a stand-by operational state of the cooling system 10 .
  • the control device 52 of the cooling system 10 controls the operation of the cooling system 10 in such a way that the cooling system 10 is operated in its stand-by operational state as long as possible.
  • the stand-by operational state of the cooling system 10 is terminated and normal operation of the cooling system 10 is initiated when cooling energy has to be supplied to cooling energy consumers.
  • the valves 42 a , 42 b are opened such that liquid refrigerant may be conveyed to the evaporators 14 a , 14 b , 14 c , 14 d by the conveying devices 32 a , 32 b.
  • the supply of refrigerant to the evaporators 14 a , 14 b , 14 c , 14 d is controlled by opening the valves 20 a , 20 b , 20 c , 20 d .
  • the valves 20 a , 20 b , 20 c , 20 d are open, the valves 36 a , 36 b interrupt the supply of refrigerant to the accumulators 34 a , 34 b such that the refrigerant exiting the condensers 22 a , 22 b , 22 c is exclusively conveyed to the evaporators 14 a , 14 b , 14 c , 14 d.
  • valves 42 a , 42 b may, however, again be partially closed or entirely closed so as to control the pressure of the refrigerant within the cooling circuit 12 in dependence on the operating state of the evaporators 14 a , 14 b , 14 c , 14 d , i.e., in dependence on the cooling energy demand of the cooling energy consumers supplied with cooling energy by the cooling system 10 .
  • the pressure of the refrigerant within the cooling circuit 12 and the supply of refrigerant to the evaporators 14 a , 14 b , 14 c , 14 d is controlled by appropriately controlling the speed of the conveying devices 32 a , 32 b .
  • the operating speed of the conveying devices 32 a , 32 b is increased when the cooling requirement of the cooling energy consumers supplied with cooling energy by the evaporators 14 a , 14 b , 14 c , 14 d increases.
  • the control unit 52 controls the valves 40 a , 40 b such that the pressure in the cooling circuit 12 downstream of the evaporators 14 a , 14 b , 14 c , 14 d and upstream of the condensers 22 a , 22 b , 22 c is higher than downstream of the condensers 22 a , 22 b , 22 c and upstream of the evaporators 14 a , 14 b , 14 c , 14 d .
  • valves 40 a , 40 b are operated so as to increase or decrease a flow cross-section of the cooling circuit 12 between the evaporators 14 a , 14 b , 14 c , 14 d and the condensers 22 a , 22 b , 22 c.
  • the control device 52 during normal operation of the cooling system 10 controls the supply of refrigerant to the evaporators 14 a , 14 b , 14 c , 14 d in dependence on the operational state of the evaporators 14 a , 14 b , 14 c , 14 d , i.e., the cooling energy requirement of the cooling energy consumers coupled to the evaporators 14 a , 14 b , 14 c , 14 d such that a dry evaporation of the refrigerant occurs in the evaporators 14 a , 14 b , 14 c , 14 d .
  • the supply of refrigerant to the individual evaporators 14 a , 14 b , 14 c , 14 d is controlled by suitably controlling the respective valves 20 a , 20 b , 20 c , 20 d.
  • the cooling system 10 is operated with a predetermined operating amount of refrigerant circulating in the cooling circuit 12 which is defined by an amount of refrigerant which is necessarily required to properly operate the cooling system 10 , and an additional amount of refrigerant to compensate for leakages of the system 10 and system tolerances. Small leakages present in the system 10 or service work involving dismounting of components from the cooling system 10 or replacing components of the cooling system 10 may, however, cause the amount of refrigerant circulating in the cooling circuit 12 to fall below a predetermined minimum value which may, for example, be defined by the amount of refrigerant which is necessarily required to properly operate the cooling system 10 .
  • the warning signal output units 54 a , 54 b of the cooling system 10 output a first warning signal indicating a required supply of refrigerant into the cooling circuit 12 when an amount of refrigerant in the cooling circuit 12 , which is measured by means of the fill level sensors, the pressure sensors and the temperature sensors of the cooling system 10 , falls below a predetermined warning value.
  • the predetermined warning value is lower than the predetermined operating value of the amount of refrigerant in the cooling circuit 12 , but still higher than the predetermined minimum value of the amount of refrigerant in the cooling circuit 12 .
  • the first warning signal may be a visual signal or an audible signal which indicates to an aircraft crew or a service crew that servicing of the cooling system 10 including refilling of refrigerant into the cooling circuit 12 of the cooling system 10 will be required in the near future, but that the cooling system 10 still is ready to operate.
  • the warning signal output units 54 a , 54 b of the cooling system 10 output a second warning signal indicating a required supply of refrigerant into the cooling circuit 12 when an amount of refrigerant in the cooling circuit 12 , which is measured by means of the fill level sensors, the pressure sensors and the temperature sensors of the cooling system 10 , falls below the predetermined minimum value.
  • the second warning signal may be a visual signal or an audible signal which indicates to an aircraft crew or a service crew that servicing of the cooling system 10 including refilling of refrigerant into the cooling circuit 12 of the cooling system 10 is required and that the cooling system 10 is no longer ready to operate.
  • control unit 52 ceases operation of the cooling system 10 when an amount of refrigerant in the cooling circuit, which is measured by means of the fill level sensors, the pressure sensors and the temperature sensors of the cooling system 10 , falls below the predetermined minimum value.
  • start-up of the cooling system 10 is prevented by the control unit 52 when the amount of refrigerant in the cooling circuit 12 is below the predetermined minimum value. Ceasing operation and/or preventing start-up of the cooling system 10 when the amount of refrigerant in the cooling circuit 10 is below the predetermined minimum value protects the components of the cooling system 10 , in particular the conveying devices 32 a , 32 b from damages caused by dry operation.
  • the residual refrigerant present in the cooling circuit 12 may be conveyed into the accumulators 34 a , 34 b . Thereafter, the accumulators 34 a , 34 b may be sealed by closing the valves 36 a , 36 b , 38 , 43 a , 43 b .
  • the accumulators 34 a , 34 b may be dismounted from the cooling circuit and replaced by replacement accumulators 34 a , 34 b filled with a desired amount of “fresh” refrigerant, wherein the self-sealing couplings via which the accumulators 34 a , 34 b are connected to the cooling circuit 12 prevent refrigerant from leaking from the cooling circuit 12 upon dismounting the accumulators 34 a , 34 b .
  • simple couplings may be used for connecting the accumulators 34 a , 34 b to the cooling circuit 12 .
  • refrigerant may be discharged from the cooling circuit 12 by means of the servicing unit 56 as discussed in detail below.
  • the refrigerant is environment-neutral, it is, however, also conceivable to release the refrigerant from the cooling circuit 12 to the ambient.
  • the refilling container 60 of the servicing unit 56 which contains a two-phase refrigerant of the same type as the refrigerant circulating in the cooling circuit 12 of the cooling system 10 , is connected to a refrigerant connection 50 a , 50 b of the cooling system 10 in a sealed manner via the first refrigerant connection adaptor 58 and a flexible line.
  • the refrigerant contained in the refilling container 60 is supplied from the refilling container 60 into the cooling circuit 12 of the cooling system 10 while at least one of the condensers 22 a , 22 b , 22 c disposed in the cooling circuit 12 of the cooling system 10 , under the control of the control unit 52 , is operated so as to liquefy gaseous refrigerant flowing through the cooling circuit 12 .
  • the at least one of the condensers 22 a , 22 b , 22 c is operated only in case the sensors for detecting the operating state of the valves 36 a , 36 b , 38 , 43 a , 43 b detect that the accumulators 34 a , 34 b are connected to the cooling circuit 12 and hence can receive refrigerant supplied into the cooling circuit 12 from the refilling container 60 .
  • Operation of the condenser 22 a , 22 b , 22 c causes a decrease of the temperature and hence the pressure of the refrigerant in the cooling circuit 12 of the cooling system 10 .
  • refrigerant may be conveyed from the refilling container 60 into the cooling circuit 12 of the cooling system 10 in a fast and efficient manner.
  • operation of the condenser 22 a , 22 b , 22 c ensures that refrigerant supplied from the refilling container 60 into the cooling circuit 12 of the cooling system 10 is liquefied immediately upon entering the cooling circuit 12 .
  • the period of time which is necessary to bring the cooling system 10 into a state ready to operate after servicing is minimized.
  • operation of the at least one of the condensers 22 a , 22 b , 22 c is controlled such that the pressure of the refrigerant in the cooling circuit 12 of the cooling system 10 is decreased below the pressure of the refrigerant in the refilling container 60 .
  • the refrigerant may be conveyed from the refilling container 60 into the cooling circuit 12 of the cooling system 10 driven by the pressure difference between the refilling container 60 and the cooling circuit 12 , i.e., the difference between the pressure of the refrigerant in the refilling container 60 and the pressure of the refrigerant in the cooling circuit 12 .
  • the check valve integrated into the refrigerant connection 50 a , 50 b which is connected to the first refrigerant connection adaptor 58 of the servicing unit 52 ensures that refrigerant may flow of from the refilling container 60 into the cooling circuit 12 , but that a reflow of refrigerant from the cooling circuit 12 into the refilling container 60 is prevented.
  • the refrigerant contained in the refilling container 60 is liquefied by means of the condenser 62 of the servicing unit 52 and thereafter conveyed into the cooling circuit 12 of the cooling system 10 by means of the conveying device 66 of the servicing unit 52 in its liquid state of aggregation.
  • operation of the at least one of the condensers 22 a , 22 b , 22 c of the cooling system 10 is ceased when an amount of refrigerant in the cooling circuit 12 , which is measured by means of the fill level sensors, the pressure sensors and the temperature sensors of the cooling system 10 , has reached a predetermined maximum value.
  • the predetermined maximum value of the amount of refrigerant in the cooling circuit 12 corresponds to the predetermined operating amount of refrigerant in the cooling circuit 12 .
  • the supply of refrigerant from the refilling container 60 into the cooling circuit 12 is interrupted when a pressure in the cooling circuit 12 , which is measured by means of the pressure sensors of the cooling system 10 has reached a predetermined value.
  • the interruption of the supply of refrigerant from the refilling container 60 into the cooling circuit 12 in dependence of the pressure in the cooling circuit 12 is achieved by means of a pressure regulator incorporated in the refrigerant connection 50 a , 50 b of the cooling system 10 .
  • the self-sealing couplings connecting these components to the cooling circuit 12 prevent refrigerant from exiting the cooling circuit 12 . If, however, a component of the cooling system 10 , which is not connected to the cooling circuit 12 via self-sealing couplings, should be dismounted from the cooling system 10 , refrigerant is discharged from the cooling circuit 12 or conveyed into one or both of the hermetically sealable accumulators 34 a , 34 b . Refrigerant received in the accumulators 34 a , 34 b does not have to be replaced, but simply is maintained in the cooling circuit 12 of the cooling system 10 .
  • the refrigerant may either be released to the ambient or collected in the storage container 74 of the servicing unit 52 .
  • the second refrigerant connection adaptor 68 is connected to a refrigerant connection 50 a , 50 b of the cooling system 10 .
  • the nozzle of the second refrigerant connection adaptor 68 controls the flow of refrigerant from the cooling circuit 12 such that freezing of the refrigerant and hence icing of the nozzle and/or further components of the cooling system 10 and/or the servicing unit 52 is prevented.
  • the refrigerant is discharged from the cooling circuit 12 of the cooling system 10 in its liquid state of aggregation.
  • the refrigerant after being liquefied, may be conveyed from the storage containers 28 a , 28 a ′, 28 b , 28 b ′, 28 c , 28 c ′, 28 d , 28 d ′ to the refrigerant connections 50 a , 50 b of the cooling system 10 by means of the conveying devices 32 a , 32 b .
  • respective valves 37 , 38 , 42 a , 42 b , 51 a , 51 b are suitably controlled, i.e., valves 37 , 38 , 42 a , 42 b , are closed, whereas valves 51 a , 51 b are opened.
  • the refrigerant discharged from the cooling circuit 12 of the cooling system 10 is stored in the storage container 74 of the servicing unit 52 in it liquid state of aggregation and hence at a relatively low pressure. If necessary, the refrigerant may be liquefied by means of a condenser 64 of the servicing unit 52 prior to being received in the storage container 74 . Discharging the refrigerant from the cooling circuit 12 of the cooling system 10 in its liquid state of aggregation allows to compensate for pressure differences between the cooling circuit 12 , in particular the accumulators 34 a , 34 b and the storage container 74 of the servicing unit 52 . In addition, the refrigerant experiences only a small temperature decrease.
  • the cooling circuit 12 After discharging refrigerant from the cooling circuit 12 and prior to reintroducing refrigerant into the cooling circuit 12 so as to return the cooling system to a ready to operate state, the cooling circuit 12 is evacuated by means of the evacuation device 70 of the servicing unit 60 . Evacuation of the cooling circuit 12 allows residual air and humidity, which may affect operation of the cooling system 10 , to be removed from the cooling system 10 before refrigerant is reintroduced into the cooling circuit 12 .
  • the refrigerant reintroduced into the cooling circuit 12 may be the refrigerant which is discharged from the cooling circuit 12 and received in the storage container 74 . It is, however, also conceivable to supply the cooling system 10 entirely or partially with “fresh” refrigerant which may be supplied to the storage container 74 of the servicing unit.
  • At least one of the condensers 22 a , 22 b , 22 c of the cooling system 10 is operated under the control of the control unit 52 so as to evaporate the refrigerant prior to entering the cooling circuit 12 and to liquefy the gaseous refrigerant upon circulating through the cooling circuit 12 .
  • the condenser 62 of the servicing unit 52 is not operated so as to ensure unhindered evaporation of the refrigerant contained in the storage container 74 of the servicing unit 52 . If necessary, the storage container 74 is heated by means of the heating device 72 so as to support evaporation of the refrigerant in the storage container 74 .

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
US13/974,373 2012-08-31 2013-08-23 Method of servicing an aircraft cooling system and aircraft cooling system Abandoned US20140060090A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US13/974,373 US20140060090A1 (en) 2012-08-31 2013-08-23 Method of servicing an aircraft cooling system and aircraft cooling system

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US201261695312P 2012-08-31 2012-08-31
EP12006183.3 2012-08-31
EP12006183.3A EP2703752A1 (de) 2012-08-31 2012-08-31 Verfahren zur Wartung eines Flugzeugkühlsystems, und Flugzeugkühlsystem
US13/974,373 US20140060090A1 (en) 2012-08-31 2013-08-23 Method of servicing an aircraft cooling system and aircraft cooling system

Publications (1)

Publication Number Publication Date
US20140060090A1 true US20140060090A1 (en) 2014-03-06

Family

ID=46924197

Family Applications (2)

Application Number Title Priority Date Filing Date
US13/974,373 Abandoned US20140060090A1 (en) 2012-08-31 2013-08-23 Method of servicing an aircraft cooling system and aircraft cooling system
US14/012,587 Abandoned US20140060091A1 (en) 2012-08-31 2013-08-28 Method of servicing an aircraft cooling system and aircraft cooling system

Family Applications After (1)

Application Number Title Priority Date Filing Date
US14/012,587 Abandoned US20140060091A1 (en) 2012-08-31 2013-08-28 Method of servicing an aircraft cooling system and aircraft cooling system

Country Status (3)

Country Link
US (2) US20140060090A1 (de)
EP (1) EP2703752A1 (de)
CN (1) CN103661954A (de)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109367791B (zh) * 2018-10-18 2022-05-13 中国航空工业集团公司金城南京机电液压工程研究中心 一种多电飞机电动环境控制系统
US20230382536A1 (en) * 2022-05-26 2023-11-30 Hamilton Sundstrand Corporation Vapor cycle liquid cabin cooling system
CN117262220B (zh) * 2023-09-18 2024-08-20 清华大学 飞行器舱段热防护结构系统

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3232070A (en) * 1963-05-17 1966-02-01 Spormac Sales Company Refrigerant saver
US3785163A (en) * 1971-09-13 1974-01-15 Watsco Inc Refrigerant charging means and method
CA1088183A (en) * 1976-06-24 1980-10-21 Trane Company Of Canada Limited Refrigerant charge adjuster apparatus
US4098303A (en) * 1976-09-17 1978-07-04 Robert Brown Associates Vapor recovery system for loading backs and storage tanks
US4612775A (en) * 1984-05-04 1986-09-23 Kysor Industrial Corporation Refrigeration monitor and alarm system
US4688388A (en) * 1985-04-29 1987-08-25 Kent-Moore Corporation Service station for refrigeration equipment
US4624112A (en) * 1985-08-26 1986-11-25 Murray Corporation Automotive air conditioner charging station with over-ride controls
US4646527A (en) * 1985-10-22 1987-03-03 Taylor Shelton E Refrigerant recovery and purification system
US4766733A (en) * 1987-10-19 1988-08-30 Scuderi Carmelo J Refrigerant reclamation and charging unit
US5031068A (en) * 1987-11-06 1991-07-09 Hansen Technologies Corporation Liquid level control system for refrigeration apparatus
US5005375A (en) * 1989-04-06 1991-04-09 Kent-Moore Corporation Refrigeration equipment service apparatus with quick-disconnect couplings
US5024061A (en) * 1989-12-12 1991-06-18 Terrestrial Engineering Corporation Recovery processing and storage unit
US5101637A (en) * 1991-02-06 1992-04-07 Cfc Solutions Corp. Refrigerant recovery device
US5293902A (en) * 1993-06-07 1994-03-15 Tif Instruments, Inc. Quick-disconnect fluid coupling
US6101988A (en) * 1996-11-13 2000-08-15 Evans Cooling Systems, Inc. Hermetically-sealed engine cooling system and related method of cooling
US6619057B2 (en) * 2001-12-13 2003-09-16 Carrier Corporation System and method for low side pump down in mobile refrigeration unit
DE102006005035B3 (de) 2006-02-03 2007-09-27 Airbus Deutschland Gmbh Kühlsystem
JP4225357B2 (ja) * 2007-04-13 2009-02-18 ダイキン工業株式会社 冷媒充填装置、冷凍装置及び冷媒充填方法
DE102009011797B4 (de) 2009-03-05 2014-06-26 Airbus Operations Gmbh Verfahren zum Betreiben eines Kühlsystems sowie Kühlsystem
DE102009054436A1 (de) * 2009-11-25 2011-05-26 Dometic Waeco International Gmbh Verfahren zum Warten einer mit geschlossenem Kältemittel-Kreislaufsystem betriebenen Fahrzeugklimaanlage und Service-Gerät hierfür

Also Published As

Publication number Publication date
EP2703752A1 (de) 2014-03-05
US20140060091A1 (en) 2014-03-06
CN103661954A (zh) 2014-03-26

Similar Documents

Publication Publication Date Title
EP3551926B1 (de) Wasserstoff tankstelle
US9603380B2 (en) Multifunctional refrigerant container and method of operating such a refrigerant container
CN112154287B (zh) 气体填充装置
US11415084B2 (en) Storage tank for cryogenic liquid gas
US20130233003A1 (en) Reliable cooling system for operation with a two-phase refrigerant
US20140060090A1 (en) Method of servicing an aircraft cooling system and aircraft cooling system
US20200224824A1 (en) Device and process for filling a mobile refrigerant tank with a cryogenic refrigerant
US9188374B2 (en) Cooling system and method for operating a cooling system
US20130340470A1 (en) Aircraft comprising a cooling system for operation with a two-phase refrigerant
EP2503265B1 (de) Verfahren für den Betrieb eines Kühlsystems
US9726404B2 (en) Cooling system with a plurality of subcoolers
US9719706B2 (en) Accumulator arrangement with an integrated subcooler
US9861844B2 (en) Method and system for fire prevention and/or fire fighting
DK181417B1 (en) A hydrogen refueling station with a solid phase cooling bank
US9322584B2 (en) Cooling system for operation with a two-phase refrigerant
CN118251577A (zh) 制冷系统和确定所述制冷系统中制冷剂的装填状态的方法
US20220238896A1 (en) Cooling system for two-phase refrigerant
CN116937018A (zh) 一种储能电池的控温设备
JPS6239319B2 (de)

Legal Events

Date Code Title Description
STCB Information on status: application discontinuation

Free format text: EXPRESSLY ABANDONED -- DURING EXAMINATION