SHELL AND TUBE HEAT EXCHANGER
A heat exchanger is provided that includes a shell defining a first fluid space and one or more tubes within the first fluid space having interiors fluidly isolated therefrom. The tubes define a second fluid space and are configured to permit thermal energy transfer between the first fluid space and the second fluid space. One or more heat pipes are disposed within one of the first fluid space and the second fluid space and are configured to transfer thermal energy within the respective fluid space.
The embodiments herein generally relate to heat exchangers and more particularly to shell and tube heat exchangers.
Numerous heat exchangers have been devised for transferring heat stored in a first medium or fluid to a second medium or fluid. One example of a heat exchanger for high temperature/high pressure applications is a shell and tube heat exchanger. Several features are essential for efficient heat transfer in shell and tube type heat exchangers.
A large tube surface area is necessary for effective heat transfer, wherein the surface area increases with tube length and tube diameter. However, the advantage gained from a larger tube diameter is offset by a decreased thermal energy exchange which results from the medium inside of the large tubes tending to flow through the middle area of the tube where thermal energy transfer is lowest rather than adjacent the peripheral tube wall where thermal energy exchange is greatest. Further, a long tube length poses a problem with longitudinal expansion. When a high temperature shell fluid is employed, the tube temperature increases resulting in thermal expansion of the tubes, which can lead to damage and/or leaks between the mediums. Thus, there are size constraints that impact the efficiency of tube and shell heat exchangers, resulting in smaller heat exchangers.
Another factor affecting the thermal energy transfer between mediums is the flow of the fluids in relation to each other. Optimum thermal energy transfer is achieved when the shell fluid and tube fluid are in a contraflow, or counter-flow, configuration allowing for small heat exchangers that are efficient. However, in extreme temperature conditions, a counter-flow configuration may not be sufficient to warm a cold fluid at the point where the cold fluid enters the heat exchanger. If the cold fluid is not warmed sufficiently, icing or other impacts on fluid flow may occur.
BRIEF DESCRIPTION OF THE INVENTIONAccording to one embodiment, a heat exchanger is provided that includes a shell defining a first fluid space and one or more tubes within the first fluid space having interiors fluidly isolated therefrom. The tubes define a second fluid space and are configured to permit thermal energy transfer between the first fluid space and the second fluid space. One or more heat pipes are disposed within one of the first fluid space and the second fluid space and are configured to transfer thermal energy within the respective fluid space.
According to another embodiment, a method of transferring thermal energy between two mediums is provided. The method includes providing a heat exchanger defining a first fluid space and a second fluid space that is fluidly isolated from the first fluid space, the heat exchanger configured to allow thermal energy transfer between the first fluid space and the second fluid space, and providing one or more heat pipes within one of the first fluid space and the second fluid space, the heat pipes configured to transfer thermal energy within the respective first fluid space or second fluid space.
Technical effects of embodiments of the invention include providing an improved heat exchanger that enables efficient thermal energy transfer between mediums, or fluids, in a shell and tube heat exchanger that is configured for high pressure applications. Further, thermal energy transfer for a given heat exchanger size can be optimized in accordance with embodiments disclosed herein.
The subject matter which is regarded as the invention 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 invention are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:
Referring to
The cylindrical body 106 defines a first fluid space, labeled as interior shell space 112, located in the center of the shell 102 and bounded at a first end by a first tube sheet 114 and at a second end by a second tube sheet 116. The first end tube sheet 114 and the second end tube sheet 116 fluidly isolate the shell space 112 from a first end cavity 128 and a second end cavity 130. The first end cavity 128 and the second end cavity 130 are fluidly connected by the interior(s) of the one or more tubes 104. A second fluid space may be defined as the volume within the tubes 104, and may further include the first and second end cavities 128, 130. It shall be understood that in order for the first and second end cavities 128, 130 to fluid connect to the tubes 104, at least one tube 104 may pass completely through each tube sheet 114, 116.
A first medium 101, such as a fluid, flows through the shell space 112 by entering the shell space 112 at a point 103 through first port 118 and exiting the shell space 112 at a point 105 through second port 120. The first medium in the shell space 112 is in contact with the exterior surfaces of the tubes 104. This allows for thermal energy transfer between a medium within the shell space 112 (first medium 101) and a medium within the tubes 104 (second medium 107), without mixing of the two mediums. The flow path of the first fluid within the shell space 112 can be controlled or directed by the inclusion of one or more baffles 122, 124. As shown in
A second medium 107 flows through the heat exchanger 100 along a second fluid path. The second medium 107 enters the heat exchanger 100 at point 109 through a third port 126 and enters the first end cavity 128. The second medium 107 then flows through the tubes 104 and into the second end cavity 130. The second medium 107 will then exit the heat exchanger 100 at point 111 by way of a fourth port 132. Similar to the first medium 101, the second medium 107 also flows generally from left to right through heat exchanger 100 in
As noted, the first tube sheet 114, the second tube sheet 116, and the tubes 104 fluidly isolate the first medium 101 and the second medium 107 from each other to prevent mixing. This allows for the first medium 101 and the second medium 107 to be of different compositions and, more importantly, of different temperatures. The tubes 104 are formed from thermally conductive material(s) in order to transfer thermal energy from the first medium 101 to the second medium 107, or vice versa. For example, thermal energy from a relatively warm or hot medium can be transferred to a relatively cool or cold medium when passing through the heat exchanger 100.
In order to facilitate heating of a cold medium (or cooling of a hot medium), the cold medium is passed through the heat exchanger 100 in one of the shell space 112 and the tubes 104, such as shown in
As shown in
In an alternative configuration, one of the mediums flows from right to left in
Turning to
A relative temperature gradient representative of the first and second mediums 201, 207 passing through the parallel-flow heat exchanger 200 is shown in
Turning now to
A relative temperature gradient representative of the first and second mediums passing through the counter-flow heat exchanger 300 is shown in
Regardless of the type of heat exchanger, the principle of operation is to have two mediums of different temperatures brought into close contact but prevent the mediums from mixing. This allows for cold mediums to be warmed and warm mediums to be cooled without energy being added or removed from the system; it is merely an exchange of thermal energy between the mediums. Further, there is also a change in pressure in the mediums, as the temperature changes, which transfers energy, e.g., a pressure drop occurs as each fluid moves from the entrance of the heat exchanger to the exit of the heat exchanger, transferring energy. In the example of heat exchangers employed in aircraft, size and weight constraints apply, in additional to the requirement of providing a vessel for high pressure mediums. Due to the size and weight constraints, a counter-flow shell and tube heat exchanger provides the best advantage, but due to icing problems during flight, parallel flow may be preferred.
Turning now to
The addition of heat pipes 450, 452 allows for a parallel-flow heat exchanger to include the benefits of a counter-flow heat exchanger, i.e., optimization of thermal energy transfer efficiency, and thus the size of the heat exchanger can be optimized with the benefits/advantages of both parallel-flow and counter-flow heat exchanger configurations. The materials and mediums of the heat pipes are configured such that the mediums of the heat exchanger will cause a phase transition of the heat pipe medium, thus enabling efficient intra-medium thermal transfer.
As shown in
In operation, in the parallel-flow heat exchanger 400 of
As shown in
Advantageously, embodiments of the invention provide maximum thermal energy transfer and maximum absolute pressure capability for a given volume. Furthermore, advantageously, icing within a fuel line, such as on an aircraft, can be efficiently prevented. Moreover, heat pipes added to a shell and tube heat exchanger provide a uniform temperature gradient and thermal energy transfer throughout the heat exchanger while maintaining the benefit of icing prevention and optimizing the heat exchanger size.
While the invention has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the invention is not limited to such disclosed embodiments. Rather, the invention can be modified to incorporate any number of variations, alterations, substitutions, combination, sub-combination, or equivalent arrangements not heretofore described, but which are commensurate with the spirit and scope of the invention. Additionally, while various embodiments of the invention have been described, it is to be understood that aspects of the invention may include only some of the described embodiments.
For example, although described herein as a particular shell and tube heat exchanger in each of the embodiments, other types of shell and tube heat exchangers may employ heat pipes without departing from the scope of the invention. One such alternative configuration is a U-shaped shell and tube heat exchanger, with heat pipes located within the U-shaped tubes and within the shell space of the heat exchanger. Furthermore, variations of shell and tube heat exchangers may include any number of tubes, shapes, sizes, and/or configurations without departing from the scope of the invention. Moreover, although described above in
Accordingly, the invention is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.
Claims
1. A heat exchanger comprising:
- a shell defining a first fluid space;
- one or more tubes within the first fluid space having interiors fluidly isolated therefrom, the tubes defining a second fluid space and configured to permit thermal energy transfer between the first fluid space and the second fluid space; and
- one or more heat pipes disposed within one of the first fluid space and the second fluid space and configured to transfer thermal energy within the respective fluid space.
2. The heat exchanger of claim 1, further comprising a first medium configured to flow through the first fluid space, and a second medium configured to flow through the second fluid space.
3. The heat exchanger of claim 2, wherein the first medium is a relatively hot oil and the second medium is a relatively cold fuel.
4. The heat exchanger of claim 2, wherein the first medium and the second medium flow in generally parallel directions through the respective fluid spaces.
5. The heat exchanger of claim 2, wherein the first medium and the second medium flow in generally opposite directions through the respective fluid spaces.
6. The heat exchanger of claim 1, wherein the one or more heat pipes define at least one first heat pipe disposed within the first fluid space, the heat exchanger further comprising at least one second heat pipe disposed within the second fluid space.
7. The heat exchanger of claim 1, configured to be installed on an aircraft.
8. A method of transferring thermal energy between two mediums, the method comprising:
- providing a heat exchanger defining a first fluid space and a second fluid space that is fluidly isolated from the first fluid space, the heat exchanger configured to allow thermal energy transfer between the first fluid space and the second fluid space; and
- providing one or more heat pipes within one of the first fluid space and the second fluid space, the heat pipes configured to transfer thermal energy within the respective first fluid space or second fluid space.
9. The method of claim 8, further comprising providing one or more additional heat pipes within the other of the first fluid space and the second fluid space, the one or more additional heat pipes configured to transfer thermal energy within the respective first fluid space or second fluid space.
10. The method of claim 8, wherein the first fluid space is defined by a shell and the second fluid space is defined by one or more tubes that pass through the shell.
11. The method of claim 8, further comprising providing a first medium within the first fluid space and a second medium within the second fluid space.
12. The method of claim 11, wherein the first medium is a relatively hot oil and the second medium is a relatively cold fuel.
13. The method of claim 11, wherein the first fluid and the second fluid flow in generally parallel directions through the respective fluid spaces.
14. The method of claim 11, wherein the first fluid and the second fluid flow in generally opposite directions through the respective fluid spaces.
Type: Application
Filed: Nov 25, 2014
Publication Date: May 26, 2016
Inventor: Leo J. Veilleux, JR. (Wethersfield, CT)
Application Number: 14/552,748