The following description relates to heat exchangers and, more specifically, to an outlet manifold of a heat exchanger.
Heat exchangers are typically devices that bring two physical elements, such as hot and cold fluids, into thermal communication with each other. In a heat exchanger in a duct, the hot and cold fluids can be air where the cold air is flown through tubes extending throughout the heat exchanger and the hot air is directed toward fins of the heat exchanger which are thermally communicative with the tubes. In this way, heat is removed from the hot air and transferred to the material of the fins, from the fins to the tubes and from the tubes to the cold air. The temperature of the cold air is thus increased as the cold air proceeds through the heat exchanger.
According to an aspect of the disclosure, an outlet manifold is provided and includes an outlet portion having first and second sides and an inlet portion to which the outlet portion is fluidly coupled. The inlet portion has first and second sides corresponding to the first and second sides of the outlet portion. Each of the first and second sides of the inlet portion includes one or more tubular members connectable with corresponding tube joints and a mixing chamber fluidly interposed between each of the one or more tubular members and the outlet portion.
In accordance with additional or alternative embodiments, the outlet portion has an annular shape defining the first and second sides.
In accordance with additional or alternative embodiments, the mixing chambers are adjacent to the outlet portion and the one or more tubular members of each of the first and second sides of the inlet portion extend laterally outwardly from the respective mixing chambers.
In accordance with additional or alternative embodiments, each tubular member includes a tubular member end, a bushing, which is fittable onto the tubular member end and a tube seal, which is fittable in an interior of the bushing.
In accordance with additional or alternative embodiments, for each tubular member for which the tubular member end is offset from a center of the mixing chamber, the tubular member includes a curved section.
In accordance with additional or alternative embodiments, the mixing chambers of the first and second sides of the inlet portion include curved surfaces leading to the outlet portion.
In accordance with additional or alternative embodiments, the mixing chambers of the first and second sides of the inlet portion are fluidly communicative through a common orifice.
In accordance with additional or alternative embodiments, the one or more tubular members of each of the first and second sides of the inlet portion are symmetric about an axis bifurcating the respective first and second sides of the outlet and inlet portions.
According to another aspect of the disclosure, a heat exchanger assembly is provided and includes a backplane, an inlet manifold configured to direct fluid from a first backplane side to a second backplane side, first heat exchangers supported on the second backplane side and configured to direct the fluid in opposite outward directions, second heat exchangers and an outlet manifold. The second heat exchangers are supported on the first backplane side, include one or more tube joints and are configured to direct the fluid in opposite inward directions toward the tube joints. The outlet manifold includes, at opposite sides thereof, one or more tubular members configured to respectively connect with corresponding ones of each of the one or more tube joints of each of the second heat exchangers.
In accordance with additional or alternative embodiments, the backplane is curved and the opposite outward and inward directions are oriented circumferentially.
In accordance with additional or alternative embodiments, the outlet manifold is coupled to an engine duct.
In accordance with additional or alternative embodiments, the outlet manifold includes an outlet portion having first and second circumferential sides and an inlet portion to which the outlet portion is fluidly coupled. The inlet portion has first and second circumferential sides corresponding to the first and second circumferential sides of the outlet portion and each of the first and second circumferential sides of the inlet portion includes the one or more tubular members and a mixing chamber fluidly interposed between each of the one or more tubular members and the outlet portion.
In accordance with additional or alternative embodiments, the outlet portion has an annular shape defining the first and second circumferential sides.
In accordance with additional or alternative embodiments, the mixing chambers are adjacent to the outlet portion and the one or more tubular members extend laterally outwardly from the respective mixing chambers.
In accordance with additional or alternative embodiments, each tubular member includes a tubular member end, a bushing, which is fittable onto the tubular member end and a tube seal, which is fittable in an interior of the bushing.
In accordance with additional or alternative embodiments, for each tubular member for which the tubular member end is offset from a center of the mixing chamber, the tubular member includes a curved section.
In accordance with additional or alternative embodiments, the mixing chambers of the first and second circumferential sides of the inlet portion include curved surfaces leading to the outlet portion.
In accordance with additional or alternative embodiments, the mixing chambers of the first and second circumferential sides of the inlet portion are fluidly communicative through a common orifice.
In accordance with additional or alternative embodiments, the one or more tubular members of each of the first and second circumferential sides of the inlet portion are symmetric about an axis bifurcating the respective first and second circumferential sides of the outlet and inlet portions.
According to yet another aspect of the disclosure, a heat exchanger assembly is provided and includes a backplane, an inlet manifold configured to direct fluid from a first backplane side to a second backplane side, first heat exchangers supported on the second backplane side and configured to direct the fluid in opposite outward directions, second heat exchangers and an outlet manifold. The second heat exchangers are supported on the first backplane side, include a linear array of tube joints and are configured to direct the fluid in opposite inward directions toward the tube joints. The outlet manifold includes, at opposite sides thereof, a linear array of tubular members configured to respectively connect with corresponding ones of each of the tube joints of each of the second heat exchangers.
These and other advantages and features will become more apparent from the following description taken in conjunction with the drawings.
The subject matter, which is regarded as the disclosure, is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The foregoing and other features and advantages of the disclosure are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:
These and other advantages and features will become more apparent from the following description taken in conjunction with the drawings.
Some current heat exchanger assemblies require a component that will direct bleed air from heat exchangers to engine external ducting efficiently and with minimal disruptions. Thus, as will be described below, an outlet manifold is provided with a chamber that accepts discharged air from two heat exchanger cores and guides that discharged air to engine discharge ducting. More particularly, the outlet manifold can serve as an interface between stream heat exchangers and the engine ducting via tube seals and allows for excessive axial, lateral and radial tolerances during installation. The outlet manifold includes internal surfaces and curvatures that efficiently accept inlet air flows from up to six or more equal flow paths and minimizes air flow pressure drops. The outlet manifold is designed to work with various operating pressures, temperatures and ducting to enhance system performance in various applications.
With reference to
As shown in
In addition, it is to be understood that the numbers of the one or more tube joints 131 for each of the second heat exchangers 1301 and 1302 are variable and need not be the same. However, for the purposes of clarity and brevity and unless otherwise stipulated, the following description will generally relate to the case that is illustrated in
With continued reference to
As shown in
The inlet portion 142 has first and second circumferential sides 1421 and 1422 that correspond to the first and second circumferential sides 1411 and 1412 of the outlet portion 141. The first circumferential side 1421 of the inlet portion 142 includes the three tubular members 150 of the first linear array and a mixing chamber 160. The mixing chamber 160 is generally disposed adjacent to the first circumferential side 1411 of the outlet portion 141. The mixing chamber 160 is thus fluidly interposed between each of the three tubular members 150 and at least the first circumferential side 1411 of the outlet portion 141. The tubular members 150 extend laterally or circumferentially outwardly from the mixing chamber 160. The second circumferential side 1422 of the inlet portion 142 includes the three tubular members 151 of the second linear array and a mixing chamber 161. The mixing chamber 161 is generally disposed adjacent to the second circumferential side 1411 of the outlet portion 141. The mixing chamber 161 is thus fluidly interposed between each of the three tubular members 151 and at least the second circumferential side 1412 of the outlet portion 141. The tubular members 151 extend laterally or circumferentially outwardly from the mixing chamber 161.
As shown in
In addition, as shown in
With continued reference to
Technical effects and benefits of the present disclosure are the provision of an outlet manifold that is small enough to fit within restrictive spatial envelopes and can withstand high temperatures and pressures without creating substantial pressure drops.
While the disclosure is provided in detail in connection with only a limited number of embodiments, it should be readily understood that the disclosure is not limited to such disclosed embodiments. Rather, the disclosure can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate with the spirit and scope of the disclosure. Additionally, while various embodiments of the disclosure have been described, it is to be understood that the exemplary embodiment(s) may include only some of the described exemplary aspects. Accordingly, the disclosure is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.
This invention was made with government support under D6305-ATPC-28-F1-410X420 awarded by the United States Air Force. The government has certain rights to the invention.
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Entry |
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European Search Report Application No. 19185337.3; dated Jun. 15, 2020; pp. 7. |
Number | Date | Country | |
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20200088478 A1 | Mar 2020 | US |