The present invention generally relates to apparatus and methods for the treatment of airstreams in an environmental control system (ECS) and, more particularly, to remove humidity from airstreams using an integrated heat exchanger system having a water extraction device.
In an aircraft environmental control system, humidity must be removed from the air prior to delivery to the pressurized cabin or equipment/electronics. The humidity can be removed by cooling the air below the water saturation temperature in reheater and condenser heat exchangers thus condensing most of the water vapor in the air into droplets. The droplets must then be separated from the air before the air is recuperatively heated in the reheater, and expanded and cooled in the cooling turbine.
Past high pressure water extraction loop designs include a condenser, a reheater, and a water extractor. However, the designs can be large, heavy, have many parts and components, and typically provide an installation challenge in many ECS applications. It is difficult to package the length required for current water extractor designs.
As can be seen, there is a need for an improved heat exchanger system that includes water extraction.
In one aspect of the present invention, a heat exchange system comprises a reheater; a condenser that is downstream of and directly interfaces the reheater; a first water extractor that is downstream of and directly interfaces the condenser, wherein the first water extractor includes: a group of low pressure chambers; wherein at least one channel is configured to promote a high pressure flow to enter at least one chamber; and a second water extractor that is downstream of and directly interfaces the condenser, and is upstream of and directly interfaces the reheater.
In another aspect of the present invention, a water extractor comprises a plurality of layers of low pressure zones; a plurality of channels of high pressure zones; wherein the low pressure zone layers alternate, in a radial direction, with the high pressure zone channels; and wherein at least one of the low pressure zones is configured to enable air/water flow to enter, from at least one high pressure zone, to at least one low pressure zone.
In yet another aspect of the present invention, a water extractor a plurality of layers of chamber inlets; a plurality of channels of flow paths; wherein the chamber inlet layers alternate, in a radial direction, with the flow path channels; and wherein at least one of the chamber inlets is configured to promote a flow to enter, from at least one flow path, to at least one chamber inlet,
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. However, any single inventive feature may not address any of the problems discussed above or may only address one of the problems discussed above. Further, one or more of the problems discussed above may not be fully addressed by any of the features described below.
As used herein, the term “air” is intended to encompass the broader term “fluid”. Thus, the term “air” and “fluid” are intended to be interchangeable.
The present invention generally provides an integrated heat exchange system whereby a core of cross-flow heat exchange passages are shared by a reheater and a condenser. A first water extractor is directly downstream of a first pass of the condenser and directly interfaces the condenser so that fluid lines are eliminated between the condenser and the first water extractor. The first water extractor extracts humidity in the fluid (i.e., air) from the condenser. Concurrently, the first water extractor turns the humidified fluid back towards and into a second pass of the condenser. A second water extractor is directly downstream of the condenser and further extracts humidity in the fluid from the condenser. The second water extractor turns the further dehumidified fluid towards and into the reheater.
As a result of the integration of the components herein, space requirements for a heat exchange system can be reduced by about 30% to about 50% of the volume of space otherwise required by past heat exchange system designs. The number of parts is reduced by about 40% to about 70%. The number of connections is reduced by about 25% to about 50%.
In
The core 11 may include cross flow heat exchange passages. The core 11 can include common fins, bars, tube sheets and separator plates as known in the art.
In
In an embodiment, the shared portion 11a may include the reheater 14 and the condenser 15, each of which are in defined portions of the core 11 but share some of the same heat exchange passages. In other words, one or more heat exchange passages may extend through the reheater 14 and the condenser 15, wherein each of the passages may have two operational segments (though not physically segmented). One operational segment may function as part of a reheater and another operational segment may function as part of a condenser.
As shown in
The humidified air inlet face 14a may connect to an air inlet or manifold 22 which may receive a humidified inlet air 17, such as air from a secondary heat exchanger of an aircraft ECS. Upon the humidified air 17 in the reheater 14 undergoing heat exchange, the humidified air outlet face 14b may pass reheater humidified air into the condenser 15.
At the same time, the dehumidified air inlet face 14c of the reheater 14 may receive further dehumidified air from the second water extractor 19 described below. The reheater 14 can heat the dehumidified air and pass it through the dehumidified air outlet face 14d. Heated, dehumidified air 13 may flow into an air outlet or manifold 21, and then to a turbine, for example, of an ECS of an aircraft.
The condenser 15 can operate on a cross flow of fluids in the heat exchange passages as in known in the art. The condenser 15 may be directly downstream of the reheater, and may include a reheater air inlet face 15a, a condensed air outlet face 15b, a dehumidified air inlet face 15c, and a dehumidified air outlet face 15d (
The reheated air inlet face 15a of the condenser 15 may directly interface the humidified air outlet face 14b of the reheater 14. In other words, 15a is directly face-to-face with 14b in the absence of fluid connection lines otherwise used when a reheater and condenser are not integrated as a single component as in past designs. The reheated air inlet face 15a of the condenser 15 may receive humidified air from the reheater 14.
The condenser 15 may condense the humidified air from the reheater 14. This may occur via heat exchange with an inlet air 12, such as from a turbine of an aircraft ECS. The inlet air 12 may pass into an air inlet or manifold 20 that is connected to the condenser 15. Condensed air may then exit from the condenser 15, via the condensed air outlet face 15b.
As mentioned above, the condenser 15 can share heat exchange passages with the reheater 14. As depicted in
The first water extractor 16, of the heat exchange system 10, may be directly downstream of the condenser 15, and may include a condensed air inlet face 16a and a dehumidified air outlet face 16b (
The condensed air inlet face 16a of the water extractor 16 may directly interface the condensed air outlet face 15b of the condenser 15. In other words, 16a is directly face-to-face with 15b in the absence of fluid connection lines between them. The condensed air inlet face 16a of the water extractor 16 may receive condensed water and air from the condenser 15.
In an exemplary embodiment, the first water extractor 40 may include a first outside wall 40c. The first water extractor 40 may also include a plurality of first interior walls 40d that are radially inward of the first outside wall 40c. The first interior walls 40d may be curved and/or semi-circular, and may be concentric to one another in a radial direction. In various embodiments, the first interior walls 40d may or may not be equally spaced, radially, from one another.
In
The chambers 40m may be arranged in one or more groups 40k (i.e., low pressure zones) of chambers 40m. The number of chambers 40m in each chamber group 40k may be the same or some/all may differ from one another.
In embodiments, one or more of the chamber groups 40k may be configured in one or more chamber layers 40n (i.e., low pressure zones) that may be positioned concentric to one another in a radial direction. Each chamber layer 40n may have a curved or semi-circular configuration. However, the chamber layers 40n may or may not have different configurations.
In embodiments, the chambers 40m, in one or more of the chamber groups 40k, may be positioned in an end-to-end relationship. However, the present invention contemplates that the chambers can be positioned in a side-by-side relationship or in other orientations.
In
In embodiments, one or more chambers 40m may be configured with a respective chamber inlet 40i (i.e., low pressure zone). Accordingly, the inlets 40i may be arranged in and be part of the chamber layers 40n.
One or more of the chamber inlets 40i can be positioned along a side (or both opposing sides) of a respective flow channel 40p described below, thus providing an inlet layer. In embodiments, the chamber inlets 40i can be equally or unequally spaced from one another along the respective flow channel 40p. Thereby, the chamber inlets 40i can enable and promote the flow of humid air into one or more chambers 40m, as further described below.
The one or more chamber inlets 40i may be parts of one or more interior walls 40d. In embodiments, a respective chamber inlet 40i may be on opposite lateral sides of a single chamber 40m. In embodiments, one or more of the chamber inlets 40i may include two interior wall portions 40h, 40j. The wall portions 40h, 40j may be parallel to one another in certain embodiments.
In embodiments, one or more of the wall portions 40h may have a step configuration. One or more of the wall portions 40h may extend into a respective flow channel 40p. A distal end of the wall portion 40h that is in a flow channel may be described as a “shave off edge.”
Still referring to
In one or more of the flow paths (high pressure zones) 26b and/or flow channels 40p (high pressure zones), the humid air may be at a pressure higher than the pressure in one or more of the chambers (low pressure zones) 40m and/or chamber layers 40n (low pressure zones). This pressure differential may be particularly present between a chamber 40m and an immediately adjacent flow path 26b. In other words, the pressure differential may be particularly present between a chamber layer 40n and an immediately adjacent flow channel 40p. The pressure differential may enable and promote the humid air in a flow path 26b to enter one or more of the adjacent chamber inlets 40i.
One or more chamber inlets 50i enable and promote a portion of the flow to enter one or more chambers 50m of one or more chamber layers 50n. In a chamber 50m, humid air may accumulate within the chamber. Water may tend to accumulate at a downstream end of the chamber 50m. Between the two ends of the chamber 50m, a mixture of humid air and water droplets are relatively randomly mixed.
Though not depicted in
Also, in this embodiment, one or more interior chambers 60m-2 may have a chamber inlet 60i-1 formed by a wall portion 60h-1, but only on one lateral side of the chamber 60m-2 so that humid air and water, from a flow channel, may flow into the chamber 60m-2 from only one lateral side. On an opposite lateral side of that chamber 60m-2, a wall portion or ramp 60h-2 may form an inlet or pocket 60i-2 but it may be closed to the chamber 60m-2 so that humid air and water may not flow into the chamber 60m-2 from that one side. Thus, in embodiments, along any one flow channel 60p that extends between two chamber layers 60n, open inlets 60i-1 may be located along one side of the flow channel, while closed inlets 60i-2 may be located along an opposite side the flow channel. That is in contrast to the embodiment of
In any of the embodiments herein, the number and configuration of chambers, inlets, flow channels and flow layers may be different.
Turning back to
In the condenser 15, the dehumidified air may undergo heat exchange with the inlet air 12, and exit as outlet air 18, via an air outlet or manifold 23. The outlet air 18 may flow to a mixer, for example, of an ECS of an aircraft. The dehumidified air may exit the condenser 15 as condensed, dehumidified air, via the dehumidified air outlet face 15d.
A second water extractor 19 can be directly downstream of and directly interfacing the condenser 15. A condensed air inlet face 19a of the water extractor 19 may be directly face-to-face with the dehumidified air outlet face 15d of the condenser 15. Thereby, flow lines are eliminated between the water extractor 19 and the condenser 15.
The second water extractor 19 can be similar in design and function to the first water extractor 16. Upon receiving the dehumidified, condensed water and air from the condenser 15, the second water extractor 19 can turn the condensed water and air which, in this case, is towards the reheater 14. In this exemplary embodiment, the condensed air can be turned 90°, or substantially about 90°. Concurrently as the condensed water and air is turned, the water extractor 19 can remove water from the condensed water and air, via inertia.
From the second water extractor 19, further dehumidified condensed air may exit, via the dehumidified outlet face 19b, and enter the reheater 14, via the dehumidified air inlet face 14c. In the reheater 14, the further dehumidified condensed air may undergo heat exchange with the inlet air 17 and exit as the outlet air 13.
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.
This application is a divisional of U.S. patent application Ser. No. 15/728,316, filed Oct. 9, 2017, and entitled, “HIGH PRESSURE WATER EXTRACTION DEVICE WITH SHAVE OFF EDGE THAT FEEDS A LOW PRESSURE CHAMBER AND INTERNAL HELIX FEATURE TO IMPROVE WATER COLLECTION AND DRAINAGE,” the entire content of which is incorporated herein by reference.
Number | Date | Country | |
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Parent | 15728316 | Oct 2017 | US |
Child | 17301049 | US |