HEAT EXCHANGER WITH CROSSING HEAT EXCHANGE TUBES

Abstract

A heat exchanger is provided that a flowpath extending longitudinally through a duct. The flowpath extends laterally within the duct between a first sidewall and a second sidewall. The flowpath extends vertically within the duct between a first manifold wall and a second manifold wall. The first manifold wall is configured to form a peripheral boundary of a first manifold plenum outside of the duct. The second manifold wall is configured to form a peripheral boundary of a second manifold plenum outside of the duct. A plurality of tubes extend vertically across the flowpath and are connected to the first manifold wall and the second manifold wall. Each of the tubes has a bore configured to fluidly couple the first manifold plenum to the second manifold plenum. The tubes include a first tube and a second tube. The first tube is adjacent and angularly offset from the second tube.

Description

BACKGROUND OF THE DISCLOSURE

1. Technical Field

This disclosure relates generally to a heat exchange system and, more particularly, to a heat exchanger with multiple heat exchange tubes crossing a flowpath.

2. Background Information

Various types and configurations of heat exchangers are known in the art. While these known heat exchangers have various benefits, there is still room in the art for improvement. In particular, there is a need in the art for a heat exchanger which can reduce vibratory responses induced by a cross flow of fluid through the heat exchanger.

SUMMARY OF THE DISCLOSURE

According to an aspect of the present disclosure, a heat exchanger is provided that includes a duct and a plurality of tubes. The duct includes a flowpath, a first sidewall, a second sidewall, a first manifold wall and a second manifold wall. The flowpath extends longitudinally through the duct. The flowpath extends laterally within the duct between the first sidewall and the second sidewall. The flowpath extends vertically within the duct between the first manifold wall and the second manifold wall. The first manifold wall is configured to form a peripheral boundary of a first manifold plenum outside of the duct. The second manifold wall is configured to form a peripheral boundary of a second manifold plenum outside of the duct. The tubes extend vertically across the flowpath and are connected to the first manifold wall and the second manifold wall. Each of the tubes has a bore configured to fluidly couple the first manifold plenum to the second manifold plenum. The tubes include a first tube and a second tube. The first tube is adjacent and angularly offset from the second tube.

According to another aspect of the present disclosure, another heat exchanger is provided that includes a first manifold, a second manifold and a plurality of tubes. The first manifold includes a first manifold wall and a first manifold plenum. The first manifold wall is between and partially forms the first manifold plenum and a flowpath. The second manifold includes a second manifold wall and a second manifold plenum. The second manifold wall is between and partially forms the second manifold plenum and the flowpath. The tubes extend vertically across the flowpath and are connected to the first manifold wall and the second manifold wall. Each of the tubes has an internal passage fluidly coupling the first manifold plenum to the second manifold plenum. The tubes include a first tube and a second tube that is angularly offset from the first tube within the flowpath. The first tube extends along a straight first trajectory out from the first manifold wall, through the flowpath and to the second manifold wall. The second tube extends along a straight second trajectory out from the first manifold wall, through the flowpath and to the second manifold wall.

According to still another aspect of the present disclosure, another heat exchanger is provided that includes a first manifold, a second manifold and a plurality of tubes. The first manifold includes a first manifold wall and a first manifold plenum. The first manifold wall is between and partially forms the first manifold plenum and a flowpath. The second manifold includes a second manifold wall and a second manifold plenum. The second manifold wall is between and partially forms the second manifold plenum and the flowpath. The tubes extend vertically across the flowpath and are connected to the first manifold wall and the second manifold wall. Each of the tubes has an internal passage fluidly coupling the first manifold plenum to the second manifold plenum. The tubes include a first tube and a second tube. The first tube is angularly offset from the second tube at a first location vertically between the first manifold wall and the second manifold wall. The first tube is attached to the second tube at the first location. The internal passage of the first tube is fluidly uncoupled from the internal passage of the second tube vertically between the first manifold wall and the second manifold wall.

The first tube may extend along a straight first trajectory out from the first manifold wall, through the flowpath and to the second manifold wall. In addition or alternatively, the second tube may extend along a straight second trajectory out from the first manifold wall, through the flowpath and to the second manifold wall.

The first tube may extend along the straight first trajectory through the first manifold wall and/or the second manifold wall. In addition or alternatively, the second tube may extend along the straight second trajectory through the first manifold wall and/or the second manifold wall.

The first tube may be angularly offset from the first manifold wall and/or the second manifold wall by a first acute angle. In addition or alternatively, the second tube may be angularly offset from the first manifold wall and/or the second manifold wall by a second acute angle.

The heat exchanger may also include a heat exchanger housing including the first manifold wall and the second manifold wall. The flowpath may extend longitudinally through the heat exchanger housing.

At least one of the tubes may be configured according to a heat exchange tube crossover parameter between 0.75 inches/crossover and 4.0 inches/crossover.

The first tube may be laterally adjacent the second tube.

The first tube may engage the second tube.

The first tube may be connected to the second tube at a first location within the flowpath vertically between the first manifold wall and the second manifold wall.

The tubes may also include a third tube. The first tube may be adjacent and angularly offset from the third tube. The first tube may be connected to the third tube at a second location within the flowpath vertically between the first location and the second manifold wall. A connection between the first tube and the second tube at the first location may

be a rigid connection.

A connection between the first tube and the second tube at the first location may be a compliant connection.

The bore of the first tube may be fluidly discrete from the bore of the second tube within the flowpath.

The first tube may be angularly offset from the second tube by a first acute angle.

The first tube may be angularly offset from the first manifold wall by a second acute angle.

The second acute angle may be greater than the first acute angle.

The first tube may also be angularly offset from the second manifold wall by the second acute angle.

The first tube may extend along a straight first trajectory out of a first aperture in the first manifold wall, through the flowpath and into a first aperture in the second manifold wall.

The second tube may extend along a straight second trajectory out of a second aperture in the first manifold wall, through the flowpath and into a second aperture in the second manifold wall.

The tubes may be arranged into a plurality of first arrays and a plurality of second arrays that are laterally interposed with the first arrays. The tubes arranged in the first arrays may be parallel with one another. The tubes arranged in the second arrays may be parallel with one another. One of the first arrays may include the first tube. One of the second arrays may include the second tube.

The duct may be configured as part of a monolithic body.

The present disclosure may include any one or more of the individual features disclosed above and/or below alone or in any combination thereof.

The foregoing features and the operation of the invention will become more apparent in light of the following description and the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a sectional illustration of a heat exchanger for a heat exchange system.

FIG. 2 is another sectional illustration of the heat exchanger for the heat exchange system.

FIG. 3 is a perspective illustration of a portion of the heat exchanger.

FIG. 4 is a perspective cutaway illustration of a portion of the heat exchanger.

FIG. 5 is a partial sectional illustration of a first heat exchange tube extending between and connected to a pair of manifold walls.

FIG. 6 is a partial sectional illustration of a second heat exchange tube extending between and connected to the manifold walls.

FIG. 7A is a cross-sectional illustration of a heat exchange tube in a plane perpendicular to a centerline axis of the heat exchanger tube; e.g., see line 7A-7A in FIG. 5 or 6.

FIG. 7B is a cross-sectional illustration of the heat exchange tube of FIG. 7A in an x-z plane; e.g., see line 7B-7B in FIG. 5 or 6.

FIG. 8A is partial illustration of a pair of laterally adjacent heat exchange tubes laterally engaged at a point of crossover.

FIG. 8B is a partial illustration of a pair of laterally adjacent heat exchange tubes laterally spaced at a point of crossover.

FIG. 9 is a sectional illustration of the heat exchanger where laterally adjacent heat exchange tubes are connected to one another at one or more vertical locations.

FIG. 10 is a side cutaway illustration of a turbine engine which may include the heat exchange system.

DETAILED DESCRIPTION

FIGS. 1 and 2 illustrate a heat exchanger 20 (e.g., a microtube heat exchanger) for a heat exchange system 22. The heat exchange system 22 may be a cooling system or a heating system for a gas turbine engine. The present disclosure, however, is not limited to turbine engine applications. The heat exchanger 20 of FIGS. 1 and 2 includes a heat exchanger (HX) housing 24 and a plurality of heat exchange (HX) tubes 26A and 26B (generally referred to as “26”).

The HX housing 24 of FIG. 1 extends laterally (e.g., along an x-axis) between and to opposing lateral sides 28 and 30 of the heat exchanger 20 and its HX housing 24. The HX housing 24 extends vertically (e.g., along a y-axis) between and to opposing vertical sides 32 and 34 of the heat exchanger 20 and its HX housing 24. Note, the term “vertical” is used herein to describe a depthwise direction and is not limited to a gravitational up/down direction. The HX housing 24 of FIG. 2 extends longitudinally (e.g., along a z-axis) between and to opposing longitudinal ends 36 and 38 of the heat exchanger 20 and its HX housing 24.

The HX housing 24 of FIGS. 1 and 2 includes a heat exchanger (HX) duct 40, a first manifold 42 and a second manifold 44. Referring to FIG. 1, the HX duct 40 includes a duct first sidewall 46, a duct second sidewall 47, a duct first manifold wall 48 and a duct second manifold wall 49. These duct walls 46-49 are arranged together to provide the HX duct 40 with an internal duct flowpath 52; see also FIG. 2.

The duct sidewalls 46 and 47 of FIG. 1 are respectively disposed at (e.g., on, adjacent or proximate) or towards the lateral sides 28 and 30. Each of these duct sidewalls 46 and 47 extends vertically between and to the duct manifold walls 48 and 49. Each of the duct sidewalls 46 and 47 of FIG. 1 is also connected to (e.g., formed integral with or otherwise attached to) the duct manifold walls 48 and 49. Each of the duct sidewalls 46 and 47 of FIGS. 2 and 3 extends longitudinally between and to the longitudinal ends 36 and 38. Each of the duct sidewalls 46 and 47 of FIG. 1 extends laterally between and to an interior side 54, 56 of the respective duct sidewall 46, 47 and an exterior side 58, 60 of the respective duct sidewall 46, 47. The interior side 54 of the first sidewall 46 forms a first lateral peripheral boundary of the duct flowpath 52 within the HX duct 40. The interior side 56 of the second sidewall 47 forms a second lateral peripheral boundary of the duct flowpath 52 within the HX duct 40, where the second lateral peripheral boundary is laterally opposite the first lateral peripheral boundary.

The duct manifold walls 48 and 49 of FIG. 1 are respectively disposed at or towards the vertical sides 32 and 34. Each of these duct manifold walls 48 and 49 extends laterally between and to the lateral sides 28 and 30. Each of the duct manifold walls 48 and 49 of FIG. 2 extends longitudinally between and to the longitudinal ends 36 and 38. Each of the duct manifold walls 48 and 49 of FIG. 1 extends vertically between and to an interior side 62, 64 of the respective duct manifold wall 48, 49 and an exterior side 66, 68 of the respective duct manifold wall 48, 49. The interior side 62 of the first manifold wall 48 forms a first vertical peripheral boundary of the duct flowpath 52 within the HX duct 40. The interior side 64 of the second manifold wall 49 forms a second vertical peripheral boundary of the duct flowpath 52 within the HX duct 40, where the second vertical peripheral boundary is vertically opposite the first vertical peripheral boundary. A surface at the exterior side 66 of the first manifold wall 48 may form a vertical peripheral boundary of a first manifold plenum 70 within the first manifold 42. A surface at the exterior side 68 of the second manifold wall 49 may form a vertical peripheral boundary of a second manifold plenum 72 within the second manifold 44.

Referring to FIG. 2, the first manifold wall 48 includes a plurality of first apertures 74; e.g., through-holes. Each of these first apertures 74 projects vertically through the first manifold wall 48.

The second manifold wall 49 includes a plurality of second apertures 76; e.g., through-holes. Each of these second apertures 76 projects vertically through the second manifold wall 49.

The duct flowpath 52 of FIG. 1 extends laterally within the HX duct 40 between and to the duct sidewalls 46 and 47. The duct flowpath 52 of FIG. 1 extends vertically within the HX duct 40 between and to the duct manifold walls 48 and 49. The duct flowpath 52 of FIG. 2 extends longitudinally through the heat exchanger 20 and its HX duct 40 between the longitudinal ends 36 and 38.

Referring to FIG. 1, the first manifold 42 is configured to form the first manifold plenum 70 vertically adjacent the HX duct 40. The first manifold 42 of FIG. 1 includes the first manifold wall 48 and a first manifold structure 78; e.g., a cover, a cap, a fitting, etc. The first manifold structure 78 is connected (e.g., attached) to the first manifold wall 48. The first manifold plenum 70 is disposed vertically between and formed by the first manifold wall 48 and the first manifold structure 78. The first manifold structure 78 of FIG. 1 includes a first port 80. This first port 80 is configured to fluidly couple the first manifold plenum 70 to a first conduit 82 of the heat exchange system 22. For ease of description, the first port 80 may be described below as an inlet into the first manifold 42, and the first manifold plenum 70 may be described below as an inlet plenum. The present disclosure, however, is not limited to such an exemplary arrangement.

The second manifold 44 is configured to form the second manifold plenum 72 vertically adjacent the HX duct 40. The second manifold 44 of FIG. 1 includes the second manifold wall 49 and a second manifold structure 84; e.g., a cover, a cap, a fitting, etc. The second manifold structure 84 is connected (e.g., attached) to the second manifold wall 49. The second manifold plenum 72 is disposed vertically between and formed by the second manifold wall 49 and the second manifold structure 84. The second manifold structure 84 of FIG. 1 includes a second port 86. This second port 86 is configured to fluidly couple the second manifold plenum 72 to a second conduit 88 of the heat exchange system 22. For ease of description, the second port 86 may be described below as an outlet into the second manifold 44, and the second manifold plenum 72 may be described below as an outlet plenum. The present disclosure, however, is not limited to such an exemplary arrangement.

Referring to FIGS. 3 and 4, the HX tubes 26A and 26B are divided into a plurality of longitudinally extending arrays 90A and 90B (generally referred to as “90”). Each tube array 90A, 90B includes a set of the HX tubes 26A, 26B. The HX tubes 26A, 26B in each tube array 90A, 90B may be laterally aligned, and longitudinally spaced apart from one another in the respective tube array 90A, 90B within the duct flowpath 52. The HX tubes 26A, 26B in each tube array 90A, 90B may be parallel with one another. The first tube arrays 90A of FIGS. 3 and 4 are laterally interposed with the second tube arrays 90B. Each interior first tube array 90A, for example, may be arranged laterally between a respective laterally neighboring (e.g., adjacent) pair of the second tube arrays 90B. Similarly, each interior second tube array 90B may be arranged laterally between a respective laterally neighboring pair of the first tube arrays 90A.

Referring to FIG. 2, each of the first tubes 26A is canted in a first direction and each of the second tubes 26B is canted in an opposite second direction when viewed, for example, in a first reference plane; e.g., a y-z plane. With this arrangement, each of the first tubes 26A may longitudinally and/or vertically cross over one or more of the (e.g., laterally adjacent) second tubes 26B within the duct flowpath 52. Similarly, each of the second tubes 26B may longitudinally and/or vertically cross over one or more of the (e.g., laterally adjacent) first tubes 26A within the duct flowpath 52. Each of the first tubes 26A is thereby angularly offset from each respective second tube 26B by an inter-tube angle 92A, 92B (generally referred to as “92”). This inter-tube angle 92 is a non-zero acute angle. The inter-tube angle 92, for example, may be greater than zero degrees (0°) and equal to or less than forty-five degrees (45°); e.g., between five degrees (5°) and fifteen degrees (15°), between fifteen degrees (15°) and thirty degrees (30°), or between thirty degrees (30°) and forty-five degrees (45°).

The first tubes 26A and the second tubes 26B may be configured according to a heat exchange (HX) tube crossover parameter. This HX tube crossover parameter may be defined as a ratio of a longitudinal length of a HX tube to a number of times that HX tube crosses one or more other HX tubes. For example, referring to FIG. 2, the first tube 26AA has a first longitudinal length 93A (see FIG. 5) measured between the interior sides 62 and 64. This first tube 26AA of FIG. 2 crosses over two other second tubes 26B at two locations when viewed, for example, in the reference plane of FIG. 2. Thus, the HX tube crossover parameter for the first tube 26AA is equal to first longitudinal length 93A (see FIG. 5) divided by two. Similarly, the second tube 26BB has a second longitudinal length 93B (see FIG. 5) measured between the interior sides 62 and 64. This second tube 26BB of FIG. 2 crosses over two other first tubes 26A at two locations when viewed, for example, in the reference plane of FIG. 2. Thus, the HX tube crossover parameter for the second tube 26BB is equal to second longitudinal length 93B (see FIG. 5) divided by two. The HX tube crossover parameter for one or more of the HX tubes 26A and/or 26B may be between 0.75 inches/crossover and 4.0 inches/crossover; e.g., between 0.75 inches/crossover and 1.5 inches/crossover, between 1.5 inches/crossover and 3.0 inches/crossover, or between 3.0 inches/crossover and 4.0 inches/crossover.

Each of the first tubes 26A of FIG. 2 (see also FIG. 5) is angularly offset from the first manifold wall 48 and its interior side 62 by a first tube-first manifold wall offset angle 94 (e.g., a non-zero acute angle) when viewed, for example, in the first reference plane. Each of the first tubes 26A of FIG. 2 is angularly offset from the second manifold wall 49 and its interior side 64 by a first tube-second manifold wall offset angle 96 (e.g., a non-zero acute angle) when viewed, for example, in the first reference plane. The first tube-second manifold wall offset angle 96 may be equal to the first tube-first manifold wall offset angle 94. However, these offset angles 94 and 96 may be different than the inter-tube angle 92. The first tube-second manifold wall offset angle 96 and the first tube-first manifold wall offset angle 94, for example, may each be greater than the inter-tube angle 92. Each offset angle 94, 96, for example, may be equal to or greater than forty-five degrees (45°) and less than ninety)(90°; e.g., between forty-five degrees (45°) and sixty degrees (60°), between sixty degrees (60°) and seventy-five degrees (75°), or between seventy-five degrees (75°) and eighty-five degrees (85°).

Referring to FIG. 1, each of the first tubes 26A may be angularly offset from the first manifold wall 48 and its interior side 62 by another first tube-first manifold wall offset angle 98 when viewed, for example, in a second reference plane; e.g., a x-z plane. Each of the first tubes 26A may be angularly offset from the second manifold wall 49 and its interior side 64 by another first tube-second manifold wall offset angle 100 when viewed, for example, in the second reference plane. The first tube-second manifold wall offset angle 100 may be equal to the first tube-first manifold wall offset angle 98. In the embodiment of FIG. 1, each offset angle 98, 100 is a right (90°) angle. The present disclosure, however, is not limited to such an exemplary arrangement.

Referring to FIG. 5, each of the first tubes 26A extends axially along a first centerline axis 102 of the respective first tube 26A between and to a first end 104 of the respective first tube 26A and a second end 106 of the respective first tube 26A. Each first tube 26A has a tubular sidewall 108 that forms an internal first passageway 110 (e.g., a bore, a channel, etc.) within the respective first tube 26A. This first passageway 110 extends axially along the first centerline axis 102 through respective first tube 26A from an inlet 112 into the first passageway 110 and an outlet 114 from the first passageway 110. The inlet 112 may be disposed at the first end 104. The outlet 114 may be disposed at the second end 106. Each first tube 26A extends vertically across the duct flowpath 52 between the first manifold 42 and its first manifold wall 48 and the second manifold 44 and its second manifold wall 49. Each first tube 26A is mated with (e.g., projects into or through) a respective one of the first apertures 74. Each first tube 26A is further mated with (e.g., projects into or through) a respective one of the second apertures 76. With this arrangement, each inlet 112 is fluidly coupled with the first manifold plenum 70 and each outlet 114 is fluidly coupled with the second manifold plenum 72. Each first tube 26A and its first passageway 110 thereby fluidly couples the first manifold plenum 70 to the second manifold plenum 72. Here, each first passageway 110 may form a fluidly discrete pathway from the first manifold plenum 70 to the second manifold plenum 72.

An entirety of first centerline axis 102 may follow a straight trajectory. Each first tube 26A may thereby also follow a straight trajectory. Each first tube 26A, more particularly, may be configured as a straight tube; e.g., a tube without any bends, kinks or the like. Providing each first tube 26A with such a straight-line geometry may facilitate mating the respective first tube 26A with the apertures 74 and 76 in the manifold walls 48 and 49 by inserting the first tube 26A into the HX housing 24 along its respective first centerline axis 102. Following the inserting of the first tubes 26A, each of the first tubes 26A may be attached to the manifold walls 48 and 49 via bonding (e.g., welding, brazing, adhering, etc.) and/or via a mechanical connection (e.g., a press fit). With this arrangement, an annular interface (e.g., a seam) between each first tube 26A and the respective manifold wall 48, 49 may be sealed to prevent fluid leakage thereacross. Of course, a seal element and/or potting may also or alternatively be provided at the annular interface to prevent fluid leaks.

Each of the second tubes 26B of FIG. 2 (see also FIG. 6) is angularly offset from the first manifold wall 48 and its interior side 62 by a second tube-first manifold wall offset angle 116 (e.g., a non-zero acute angle) when viewed, for example, in the first reference plane. Each of the second tubes 26B of FIG. 2 is angularly offset from the second manifold wall 49 and its interior side 64 by a second tube-second manifold wall offset angle 118 (e.g., a non-zero acute angle) when viewed, for example, in the first reference plane. The second tube-second manifold wall offset angle 118 may be equal to the second tube-first manifold wall offset angle 116 and/or the offset angles 94 and/or 96. However, these offset angles 116 and 118 may be different than the inter-tube angle 92. The second tube-second manifold wall offset angle 118 and the second tube-first manifold wall offset angle 116, for example, may each be greater than the inter-tube angle 92. Each offset angle 116, 118, for example, may be equal to or greater than forty-five degrees (45°) and less than ninety (90°); e.g., between forty-five degrees (45°) and sixty degrees (60°), between sixty degrees (60°) and seventy-five degrees (75°), or between seventy-five degrees (75°) and eighty-five degrees (85°).

Referring to FIG. 1, each of the second tubes 26B may be angularly offset from the first manifold wall 48 and its interior side 62 by another second tube-first manifold wall offset angle 120 when viewed, for example, in the second reference plane. Each of the second tubes 26B may be angularly offset from the second manifold wall 49 and its interior side 64 by another second tube-second manifold wall offset angle 122 when viewed, for example, in the second reference plane. The second tube-second manifold wall offset angle 122 may be equal to the second tube-first manifold wall offset angle 120. In the embodiment of FIG. 1, each offset angle is a right (90°) angle. The present disclosure, however, is not limited to such an exemplary arrangement.

Referring to FIG. 6, each of the second tubes 26B extends axially along a second centerline axis 124 of the respective second tube 26B between and to a first end 126 of the respective second tube 26B and a second end 128 of the respective second tube 26B. Each second tube 26B has a tubular sidewall 130 that forms an internal second passageway 132 (e.g., a bore, a channel, etc.) within the respective second tube 26B. This second passageway 132 extends axially along the second centerline axis 124 through respective second tube 26B from an inlet 134 into the second passageway 132 and an outlet 136 from the second passageway 132. The inlet 134 may be disposed at the first end 126. The outlet 136 may be disposed at the second end 128. Each second tube 26B extends vertically across the duct flowpath 52 between the first manifold 42 and its first manifold wall 48 and the second manifold 44 and its second manifold wall 49. Each second tube 26B is mated with (e.g., projects into or through) a respective one of the first apertures 74. Each second tube 26B is further mated with (e.g., projects into or through) a respective one of the second apertures 76. With this arrangement, each inlet 134 is fluidly coupled with the first manifold plenum 70 and each outlet 136 is fluidly coupled with the second manifold plenum 72. Each second tube 26B and its second passageway 132 thereby fluidly couples the first manifold plenum 70 to the second manifold plenum 72. Here, each second passageway 132 may form a fluidly discrete pathway from the first manifold plenum 70 to the second manifold plenum 72.

An entirety of second centerline axis 124 may follow a straight trajectory. Each second tube 26B may thereby also follow a straight trajectory. Each second tube 26B, more particularly, may be configured as a straight tube; e.g., a tube without any bends, kinks or the like. Providing each second tube 26B with such a straight-line geometry may facilitate mating the respective second tube 26B with the apertures 74 and 76 in the manifold walls 48 and 49 by inserting the second tube 26B into the HX housing 24 along its respective second centerline axis 124. Following the inserting of the second tubes 26B, each of the second tubes 26B may be attached to the manifold walls 48 and 49 via bonding (e.g., welding, brazing, adhering, etc.) and/or via a mechanical connection (e.g., a press fit). With this arrangement, an annular interface (e.g., a seam) between each second tube 26B and the respective manifold wall 48, 49 may be sealed to prevent fluid leakage thereacross. Of course, a seal element and/or potting may also or alternatively be provided at the annular interface to prevent fluid leaks.

With the foregoing arrangement, referring to FIGS. 1 and 2, the HX tubes 26 form a second flowpath vertically across the HX duct 40 and between the first manifold 42 and the second manifold 44. This second flowpath is transverse to the duct flowpath 52.

During operation of the heat exchanger 20 of FIGS. 1 and 2, a first fluid (e.g., a gas and/or a liquid) is directed into the duct flowpath 52 and a second fluid (e.g., a gas and/or a liquid) is directed into the second flowpath. As the first fluid flows within the HX duct 40 and the second fluid flows within the HX tubes 26, each HX tube 26 may transfer heat energy between the first fluid and the second fluid. The heat exchanger 20 may thereby heat the first fluid and cool the second fluid where the second fluid is warmer than the first fluid. Alternatively, the heat exchanger 20 may cool the first fluid and heat the second fluid where the first fluid is warmer than the second fluid. Examples of the heat exchange fluids include, but are not limited to, ambient air, compressed air, fuel, coolant and lubricant.

The flow of the first fluid through the duct flowpath 52 may excite vibrations in the HX tubes 26. The excitation of these vibrations, however, can be reduced by canting the HX tubes 26 relative to the flow of the first fluid; e.g., the z-axis direction. In particular, by canting the HX tubes 26 as described above, an effective cross-section of each HX tube 26 may be changed from, for example, a circular geometry of FIG. 7A to an elongated geometry (e.g., an oval geometry) of FIG. 7B. Note, the circular geometry of FIG. 7A is shown in a plane perpendicular to the HX tube centerline axis 102, 124. The elongated geometry of FIG. 7B is shown in a third reference plane (e.g., a y-z plane) which is angularly offset from the plane of FIG. 7A. Provision of the elongated geometry may facilitate a reduction in vortex shedding at a trailing edge 138 of the respective HX tube 26. Furthermore, canting the HX tubes 26 within the duct flowpath 52 increases available surface area for heat transfer between the first fluid and the second fluid. The present disclosure, however, is not limited to the exemplary cross-sectional geometries shown in FIGS. 7A and 7B.

Referring to FIG. 8A, at each location 140A, 140B (generally referred to as “140”) (see also FIG. 9) where one of the HX tubes (e.g., 26A or 26B) crosses over another one of the HX tubes (e.g., 26B or 26A), those HX tubes 26 may laterally engage (e.g., contact) one another. Providing engagement between the HX tubes 26 may effectively fix those HX tubes 26 to one another at the crossover locations 140. The engagement may thereby stiffen the HX tubes 26 and reduce an effective unsupported length of the HX tube 26 within the duct flowpath 52. Reducing the effective unsupported length may increase a natural resonant frequency of the of the respective HX tube 26. It is contemplated however, referring to FIG. 8B, the crossing HX tubes 26 may alternatively be laterally spaced from one another in other embodiments.

Referring to FIG. 9, two or more of the crossing HX tubes 26A and 26B may be laterally connected to one another. The HX tubes 26, for example, at any one or more or all of the crossover locations 140 may be connected (e.g., tied) to one another. Each of the connections between the HX tubes 26 may be a rigid connection. The respective HX tubes 26, for example, may be bonded (e.g., brazed, welded or adhered) to one another, wire tied to one another, engage one another through a mechanical interference fit, etc. Alternatively, any one or more or each of the connections between the HX tubes 26 may each be a compliant connection. The respective HX tubes 26, for example, may be connected through a damper such as, but not limited to, a rubber band or strap. Similar to providing engagement between the HX tubes 26 as discussed above, the connections between the respective HX tubes 26 may stiffen the HX tubes 26 and/or shorten the effective unsupported length of the HX tube 26 within the duct flowpath 52.

The connections at the crossover locations 140 of FIG. 9 are located vertically between the first manifold wall 48 and the second manifold wall 49. The connections at the first crossover locations 140A are located vertically between the first manifold wall 48 and the second crossover locations 140B. The connections at the second crossover locations 140B are located vertically between the first crossover locations 140A and the second manifold wall 49.

Referring to FIGS. 3 and 4, in some embodiments, the HX duct 40 and its members 46-49 may be configured together is a monolithic body. The duct members 46-49, for example, may be cast, machined and/or otherwise formed as a single unitary body.

In some embodiments, each of the HX tubes 26 is formed discrete from the monolithic body. The HX tubes 26 may then be assembled with the HX duct 40, for example, as described above. With such an arrangement, each of the HX tubes 26 may be a wrought tube. The present disclosure, however, is not limited to such an exemplary heat exchanger construction.

FIG. 10 illustrates an exemplary embodiment of a gas turbine engine 142 with which the heat exchanger 20 may be included or may otherwise service. This turbine engine 142 extends along an axial centerline 144 between an upstream airflow inlet 146 and a downstream airflow exhaust 148. The turbine engine 142 includes a fan section 150, a compressor section 151, a combustor section 152 and a turbine section 153. The compressor section 151 includes a low pressure compressor (LPC) section 151A and a high pressure compressor (HPC) section 151B. The turbine section 153 includes a high pressure turbine (HPT) section 153A and a low pressure turbine (LPT) section 153B.

The engine sections 150-153B are arranged sequentially along the axial centerline 144 within an engine housing 156. This engine housing 156 includes an inner case 158 (e.g., a core case) and an outer case 160 (e.g., a fan case). The inner case 158 may house one or more of the engine sections 151A-153B; e.g., an engine core. The outer case 160 may house at least the fan section 150.

Each of the engine sections 150, 151A, 151B, 153A and 153B includes a respective bladed rotor 162-166. Each of these bladed rotors 162-166 includes a plurality of rotor blades arranged circumferentially around and connected to one or more respective rotor disks. The rotor blades, for example, may be formed integral with or mechanically fastened, welded, brazed, adhered and/or otherwise attached to the respective rotor disk(s).

The fan rotor 162 is connected to a geartrain 168, for example, through a fan shaft 170. The geartrain 168 and the LPC rotor 163 are connected to and driven by the LPT rotor 166 through a low speed shaft 171. The HPC rotor 164 is connected to and driven by the HPT rotor 165 through a high speed shaft 172. The shafts 170-172 are rotatably supported by a plurality of bearings 174; e.g., rolling element and/or thrust bearings. Each of these bearings 174 is connected to the engine housing 156 by at least one stationary structure such as, for example, an annular support strut.

During operation, air enters the turbine engine 142 through the airflow inlet 146. This air is directed through the fan section 150 and into a core flowpath 176 and a bypass flowpath 178. The core flowpath 176 extends sequentially through the engine sections 151A-153B; e.g., the engine core. The air within the core flowpath 176 may be referred to as “core air”. The bypass flowpath 178 extends through a bypass duct, which bypasses the engine core. The air within the bypass flowpath 178 may be referred to as “bypass air”.

The core air is compressed by the LPC rotor 163 and the HPC rotor 164 and directed into a combustion chamber 180 of a combustor in the combustor section 152. Fuel is injected into the combustion chamber 180 and mixed with the compressed core air to provide a fuel-air mixture. This fuel-air mixture is ignited and combustion products thereof flow through and sequentially cause the HPT rotor 165 and the LPT rotor 166 to rotate. The rotation of the HPT rotor 165 and the LPT rotor 166 respectively drive rotation of the HPC rotor 164 and the LPC rotor 163 and, thus, compression of the air received from a core airflow inlet. The rotation of the LPT rotor 166 also drives rotation of the fan rotor 162, which propels the bypass air through and out of the bypass flowpath 178. The propulsion of the bypass air may account for a majority of thrust generated by the turbine engine 142.

The heat exchanger 20 may be included in various turbine engines other than the one described above as well as in other types of equipment. The heat exchanger 20, for example, may be included in a geared turbine engine where a geartrain connects one or more shafts to one or more rotors in a fan section, a compressor section and/or any other engine section.

Alternatively, the heat exchanger 20 may be included in a turbine engine configured without a geartrain; e.g., a direct drive turbine engine. The heat exchanger 20 may be included in a turbine engine configured with a single spool, with two spools (e.g., see FIG. 10), or with more than two spools. The turbine engine may be configured as a turbofan engine, a turbojet engine, a turboprop engine, a turboshaft engine, a propfan engine, a pusher fan engine or any other type of turbine engine. The turbine engine may alternatively be configured as an auxiliary power unit (APU) or an industrial gas turbine engine. The present disclosure therefore is not limited to any particular types or configurations of turbine engines.

While various embodiments of the present disclosure have been described, it will be apparent to those of ordinary skill in the art that many more embodiments and implementations are possible within the scope of the disclosure. For example, the present disclosure as described herein includes several aspects and embodiments that include particular features. Although these features may be described individually, it is within the scope of the present disclosure that some or all of these features may be combined with any one of the aspects and remain within the scope of the disclosure. Accordingly, the present disclosure is not to be restricted except in light of the attached claims and their equivalents.

Claims

1. A heat exchanger, comprising:

a duct including a flowpath, a first sidewall, a second sidewall, a first manifold wall and a second manifold wall, the flowpath extending longitudinally through the duct, the flowpath extending laterally within the duct between the first sidewall and the second sidewall, the flowpath extending vertically within the duct between the first manifold wall and the second manifold wall, the first manifold wall configured to form a peripheral boundary of a first manifold plenum outside of the duct, and the second manifold wall configured to form a peripheral boundary of a second manifold plenum outside of the duct; and

a plurality of tubes extending vertically across the flowpath and connected to the first manifold wall and the second manifold wall, each of the plurality of tubes having a bore configured to fluidly couple the first manifold plenum to the second manifold plenum, the plurality of tubes including a first tube and a second tube, and the first tube adjacent and angularly offset from the second tube.

2. The heat exchanger of claim 1, wherein at least one of the plurality of tubes is configured according to a heat exchange tube crossover parameter between 0.75 inches/crossover and 4.0 inches/crossover.

3. The heat exchanger of claim 1, wherein the first tube is laterally adjacent the second tube.

4. The heat exchanger of claim 1, wherein the first tube engages the second tube.

5. The heat exchanger of claim 1, wherein the first tube is connected to the second tube at a first location within the flowpath vertically between the first manifold wall and the second manifold wall.

6. The heat exchanger of claim 5, wherein

the plurality of tubes further includes a third tube;

the first tube is adjacent and angularly offset from the third tube; and

the first tube is connected to the third tube at a second location within the flowpath vertically between the first location and the second manifold wall.

7. The heat exchanger of claim 5, wherein a connection between the first tube and the second tube at the first location is a rigid connection.

8. The heat exchanger of claim 5, wherein a connection between the first tube and the second tube at the first location is a compliant connection.

9. The heat exchanger of claim 1, wherein the bore of the first tube is fluidly discrete from the bore of the second tube within the flowpath.

10. The heat exchanger of claim 1, wherein the first tube is angularly offset from the second tube by a first acute angle.

11. The heat exchanger of claim 10, wherein the first tube is angularly offset from the first manifold wall by a second acute angle.

12. The heat exchanger of claim 11, wherein the second acute angle is greater than the first acute angle.

13. The heat exchanger of claim 1, wherein the first tube extends along a straight first trajectory out of a first aperture in the first manifold wall, through the flowpath and into a first aperture in the second manifold wall.

14. The heat exchanger of claim 1, wherein the second tube extends along a straight second trajectory out of a second aperture in the first manifold wall, through the flowpath and into a second aperture in the second manifold wall.

15. The heat exchanger of claim 1, wherein

the plurality of tubes are arranged into a plurality of first arrays and a plurality of second arrays that are laterally interposed with the plurality of first arrays;

the plurality of tubes arranged in the plurality of first arrays are parallel with one another;

the plurality of tubes arranged in the plurality of second arrays are parallel with one another;

one of the plurality of first arrays includes the first tube; and

one of the plurality of second arrays includes the second tube.

16. A heat exchanger, comprising:

a first manifold including a first manifold wall and a first manifold plenum, the first manifold wall between and partially forming the first manifold plenum and a flowpath;

a second manifold including a second manifold wall and a second manifold plenum, the second manifold wall between and partially forming the second manifold plenum and the flowpath; and

a plurality of tubes extending vertically across the flowpath and connected to the first manifold wall and the second manifold wall, each of the plurality of tubes having an internal passage fluidly coupling the first manifold plenum to the second manifold plenum, and the plurality of tubes including a first tube and a second tube that is angularly offset from the first tube within the flowpath;

the first tube extending along a straight first trajectory out from the first manifold wall, through the flowpath and to the second manifold wall; and

the second tube extending along a straight second trajectory out from the first manifold wall, through the flowpath and to the second manifold wall.

17. The heat exchanger of claim 16, wherein at least one of

the first tube extends along the straight first trajectory through at least one of the first manifold wall or the second manifold wall; or

the second tube extends along the straight second trajectory through at least one of the first manifold wall or the second manifold wall.

18. The heat exchanger of claim 16, further comprising:

a heat exchanger housing including the first manifold wall and the second manifold wall;

the flowpath extending longitudinally through the heat exchanger housing.

19. A heat exchanger, comprising:

a first manifold including a first manifold wall and a first manifold plenum, the first manifold wall between and partially forming the first manifold plenum and a flowpath;

a second manifold including a second manifold wall and a second manifold plenum, the second manifold wall between and partially forming the second manifold plenum and the flowpath; and

a plurality of tubes extending vertically across the flowpath and connected to the first manifold wall and the second manifold wall, each of the plurality of tubes having an internal passage fluidly coupling the first manifold plenum to the second manifold plenum, and the plurality of tubes including a first tube and a second tube;

the first tube angularly offset from the second tube at a first location vertically between the first manifold wall and the second manifold wall;

the first tube attached to the second tube at the first location; and

the internal passage of the first tube fluidly uncoupled from the internal passage of the second tube vertically between the first manifold wall and the second manifold wall.

20. The heat exchanger of claim 19, wherein at least one of

the first tube extends along a straight first trajectory out from the first manifold wall, through the flowpath and to the second manifold wall; or

the second tube extends along a straight second trajectory out from the first manifold wall, through the flowpath and to the second manifold wall.