The present invention generally relates to refrigeration systems. More particularly, the invention relates to a compact refrigeration system which may be advantageously employed in a vehicle.
In some vehicles such as aircraft, refrigeration systems may be employed to perform various cooling functions. In a typical aircraft, where space is limited, it is advantageous to construct on-board refrigeration systems that occupy as little volume as possible. At the same time, it is advantageous to construct aircraft refrigeration systems with low weight and high efficiency.
It is known that incorporating suction line heat exchangers in refrigeration systems may increase temperature of refrigerant vapor at a compressor inlet. The increased temperature may reduce the amount of refrigerant that can be absorbed into lubricating oil and thereby may result in an increase of viscosity of the oil. Higher viscosity oil-refrigerant mixture may provide improved lubrication and longer life for various compressor components. Additionally, the suction line heat exchanger may minimize the amount of liquid refrigerant that enters the compressor thus adding further to higher oil viscosity.
While suction line heat exchangers are a desirable feature for refrigeration systems, their use has heretofore added substantial volume to a refrigeration system. Typically, effective suction line heat exchangers may have a volume that is about equal to the volume of a receiver of the system.
As can be seen, there is a need for an aircraft refrigeration system system in which a suction line heat exchanger may be employed and in which the suction line heat exchanger adds only minimal volume to the system.
In one aspect of the present invention, a distributed cooling system for an aircraft may comprise an evaporator; a compressor; a condenser; and a receiver interposed between the condenser and the evaporator for receiving liquid refrigerant from the condenser, the receiver comprising a heat exchanger; and the heat exchanger interposed between the evaporator and the compressor and configured to transfer heat from the liquid refrigerant in the receiver to refrigerant vapor emerging from the evaporator.
In another aspect of the present invention, a receiver for a refrigeration system may comprise an enclosure with an inlet for liquid refrigerant at a first end and an outlet for the liquid refrigerant at a second end; and a heat exchanger with an inlet and an outlet for refrigerant vapor; and wherein the heat exchanger is surrounded by the enclosure.
In still another aspect of the present invention, a method for improving operation of a refrigeration system may comprise passing a vapor and liquid mixture emerging from an evaporator through a heat exchanger incorporated in a receiver; passing heated liquid refrigerant into the receiver and into contact with the heat exchanger; transferring heat from the liquid refrigerant to the vapor; and passing the heated mixture to an inlet of a compressor.
These and other features, aspects and advantages of the present invention will become better understood with reference to the following drawings, description and claims.
The following detailed description is of the best currently contemplated modes of carrying out the invention. The description is not to be taken in a limiting sense, but is made merely for the purpose of illustrating the general principles of the invention, since the scope of the invention is best defined by the appended claims.
Various inventive features are described below that can each be used independently of one another or in combination with other features.
The present invention generally provides a cooling system that uses a space-saving receiver and an integral suction-line heat exchanger incorporated into a single enclosure.
Referring now to
A refrigerant circuit 20 may interconnect the evaporator 16 to a compressor 22 at an inlet side 22-1. In an exemplary embodiment of the invention, the compressor 22 may be a scroll compressor. The compressor 22 may be driven by an AC motor 24 which may be provided with electrical power through a dedicated inverter 26 which may be connected to a DC bus 28 of the aircraft. The compressor 22 may be interconnected, at an outlet side 22-2, to the evaporator 16 through a condenser 30. A receiver 31 may be interposed between the condenser 30 and the evaporator 16.
Referring now to
Referring now to
In an exemplary embodiment, the heat exchanger 32 may comprise a serpentine tube 32-2 and a plurality of baffles 32-4. The heat exchanger 32 may be positioned within the enclosure 31-2. The heat exchanger 32 may be interposed between the evaporator 16 and the inlet 22-1 of the compressor 22 on a suction line 20-1. Refrigerant vapor may be comingled with lubricating oil and liquid refrigerant as it emerges from the evaporator 16. This mixture of lubricating oil, refrigerant vapor and liquid refrigerant may be referred as a suction-line mixture 50. The mixture 50 from the evaporator 16 may enter the heat exchanger 32 at an inlet 32-6 and may exit at an outlet 32-8. The mixture 50 may pass through the tube 32-2 and the liquid refrigerant 40 may pass over the baffles 32-4. The liquid refrigerant 40 may transfer heat to the baffles 32-4 and the tube 32-2 and the mixture 50. This transfer of heat may raise the temperature of the mixture 50 as it passes through the heat exchanger 32 and into the compressor 20.
The heat exchanger 32 may advantageously heat the mixture 50 sufficiently to vaporize any liquid refrigerant that may be contained in the mixture 50 so that any refrigerant emerging from the heat exchanger may be in a vapor state. Additionally, because the heat exchanger 32 may advantageously raise the temperature of the mixture 50, viscosity of an oil-refrigerant component of the mixture may be increased. This may occur because the oil-refrigerant component may become modified to have a higher fraction of oil. Higher viscosity oil-refrigerant may provide improved lubrication and longer life for various compressor components. It may also be noted that because the heat exchanger 32 may minimize the amount of liquid refrigerant that enters the compressor 22, resultant oil viscosity may be increased.
Referring now to
Referring particularly to
Referring now to
It should be understood, of course, that the foregoing relates to exemplary embodiments of the invention and that modifications may be made without departing from the spirit and scope of the invention as set forth in the following claims.
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Number | Date | Country | |
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20160091232 A1 | Mar 2016 | US |
Number | Date | Country | |
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Parent | 12912965 | Oct 2010 | US |
Child | 14921260 | US |