Conduit for improved fluid flow and heat transfer
09845902 · 2017-12-19
Assignee
Inventors
Cpc classification
F16L9/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F13/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F1/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16L9/006
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F28F13/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F1/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F1/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The present disclosure provides conduits with modified interior surfaces that increase the surface area of the interior surface of the conduit to provide the conduit with improved thermal energy exchange with the wall of the conduit. The modified interior surfaces can also be configured to reduce friction flow on the fluid passing therethrough.
Claims
1. A method comprising: providing a conduit having a direction of flow, a length parallel to the direction of flow, an interior surface, and an exterior surface; providing, within the interior of the conduit, modified surface features selected from the group consisting of dimples and gouge-like shapes, wherein the modified surface features have a length, width, and depth, and wherein the length of the modified surface features is parallel to the direction of flow and less than the length of the conduit, wherein the modified surface features are configured to increase the surface area of the conduit and to increase thermal transfer between liquid flowing through the conduit and a wall of the conduit, wherein the modified surface features are disposed on the interior surface of the conduit, and wherein the exterior surface comprises no modified surface features; placing the conduit in a geothermal well; and flowing liquid through the conduit, wherein the thermal transfer occurs between the liquid and the wall of the conduit.
2. The method of claim 1, wherein the modified surface features are cylindrical.
3. The method of claim 1, wherein the length of the modified surface features is greater than the width of the modified surface features.
4. The method of claim 1, wherein the depth of the modified surface features slopes up at one end of the length.
5. The method of claim 1, wherein the modified surface features have a ratio of length to width of about 5:3.
6. The method of claim 1, wherein the modified surface features are configured to form eddies characteristic of turbulent flow.
7. The method of claim 1, wherein the modified surface features are configured to generate vortices within a boundary layer between turbulent and laminar flow.
8. The method of claim 1, wherein the modified surface features are configured to create a region of circulation adjacent to the interior surface.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The following drawings illustrate by way of example and not limitation. For the sake of brevity and clarity, every feature of a given structure is not always labeled in every figure in which that structure appears. Identical reference numbers do not necessarily indicate an identical structure. Rather, the same reference number may be used to indicate a similar feature or a feature with similar functionality, as may non-identical reference numbers. The figures are drawn to scale for certain embodiments (unless otherwise noted), meaning the sizes of the depicted elements are accurate relative to each other for at least the depicted embodiment:
(2)
(3)
(4)
(5)
(6)
(7)
(8) It should be understood that the drawings are not necessarily to scale and that the disclosed embodiments are sometimes illustrated diagrammatically and in partial views. In certain instances, details which are not necessary for an understanding of the disclosed methods and apparatuses or which render other details difficult to perceive may have been omitted. It should be understood, of course, that this disclosure is not limited to the particular embodiments illustrated herein
DETAILED DESCRIPTION OF THE DISCLOSURE
(9) As used herein, “a” and “an” means one or more than one unless otherwise stated.
(10) As recited herein, the present disclosure provides conduits with modified internal surfaces particularized to either reduce internal friction imparted on the fluid flowing through the conduit, increase heat transfer between the surface material of the conduit and the fluid moving through the conduit, or both. The modified interior surfaces of the present disclosure improve the heat transfer characteristics of the conduits of the present disclosure over a standard conduit. The modified interior surfaces comprise a series of modified surface features such as indentations, cuts, scraps, gouges, or grinding into the interior surface of a conduit. The modified interior surfaces of the present disclosure also improve the flow characteristics of the conduit by reducing drag or friction acting on the fluid as it flows through the conduit.
(11) In one embodiment, the modified interior surfaces comprise a regular pattern of indentations to give the fluid a flow direction. In another embodiment, the modified interior surfaces comprise an irregular pattern of indentations to cause or increase the turbulence of fluid flow, thereby allowing the fluid to mix. The increase in turbulence improves heat transfer from the environment exterior to the conduit through convection and conduction. In addition to or as an alternative, changing the shape of the modified surface features of the present disclosure may reduce friction by giving the turbulence of the fluid flow directionality. For instance, offsetting and elongation of the indentions or modified surface features create small vortices giving the fluid turbulence a uniform direction that reduces the friction in the flow.
(12) The reduction of the friction provided by the modified interior surfaces also reduces the power required to move the fluid through the conduit. In addition, the friction reduction also increases the fluid velocity, and thus improves the throughput of the fluid that moves through the conduit.
(13)
(14) Laminar flow within pipe is characterized by fluid flowing in a smooth line, parallel to each layer of itself. This means that the layer defined within the center of the conduit would have the same flow and direction—though not necessarily velocity—as the layer at the edge of the pipe. Laminar flow tends to operate in the lower velocity regime, where friction of the pipe wall has not yet impacted the connection between the layers. Turbulent flow, however, is characterized by less organized flow in perpendicular directions to the laminar flow of the fluid. These swirls, or eddies, inhibit the smooth nature of laminar flow, causing lateral mixing, and in particularly violent turbulence and increased friction.
(15) The introduction of turbulence to a fluid system, however, does not always result in higher friction. Boundary layer transition, where a laminar flow transitions to one of turbulence is well known in the art of aircraft design. As air flows over an airfoil, it is separated into a laminar regime within the boundary layer and a turbulent one outside. While the laminar flow results in low skin friction, the system is characterized by adverse pressure gradients which can cause flow reversal within the boundary layer, and result in subsequent boundary layer separation. Consequential flow separation negatively affects the pressure distribution along the airfoil resulting in lower lift and higher drag.
(16) In certain situations, it is advantageous to prematurely trigger a boundary layer transition, thereby reducing the pressure gradient problem. This is generally done with vortex generators—small external vanes or bumps perpendicular to the flow. Vortex generators are generally 80% as tall as the expected boundary layer.
(17) Fluid flow within a pipe is different, and thus requires a novel solution. In accordance with the present disclosure, fluid flow within conduit is improved through the presence of dimples 110 in the interior surface of the conduit.
(18) The vortices generated by dimples 110 and cavities 120 create a region of circulation adjacent to the pipe wall, encouraging a laminar flow regime in a larger cross-sectional area of the pipe than would exist if the dimples were not present. This directionality imparted on the turbulent layer thereby organizes it. See
(19) Flow friction is decreased as the organized turbulent layer acts as a lubricating layer for the main centerline flow. The organized layer is fashioned according to the size, shape, and depth of the cavities in the interior surface of the conduit. In some embodiments, the organized turbulent layer expands in depth. The use of dimples or other surface area enhancing surface features, in this case results in efficient thermal mixing of the working fluid through the turbulence that results when the working fluid meets the interior surface features 110 or 410. Thermal mixing may be controlled by the expansion of the organized turbulent layer. In some cases, decreased friction is traded off for increased thermal mixing, though in certain designs, both are concurrently achievable.
(20) Referring to
(21) Referring to
(22) In one specific exemplary embodiment, the preferred dimple or modified surface feature for improved heat transfer for a given pipe or conduit with a 3″ inner diameter (ID) a circular modified surface feature with a ⅜″ diameter and a ⅛″ depth. This specific exemplary embodiment provides a 100% increase in surface area over a pipe or conduit without the modified surface feature of the present disclosure. An example of the circular modified surface feature is shown in
(23) Referring to
(24) It is contemplated that the two-dimensional front view of the modified surface feature of the present disclosure can have any regular or irregular geometric shapes. Regular geometric shapes include any polygon with three or more sides such as triangle, rectangle, pentagon, etc. Regular geometric shapes also include circular shapes such as elliptical, oval, etc. Irregular shapes can be based on any regular geometric shapes where the sides and corners may not be straight and can take on various irregularities such as askew, bent, fluctuating, jagged, serrated, sinuous, snaking, tortuous, or undulating lines.
(25) It is also contemplated that the depth of the modified surface features of the present disclosure can be but need not be uniform across a single modified surface feature or between a plurality of modified surface features. A single conduit can have different sized and shaped modified surface features. For instance a conduit can have a region with modified surface features that are configured to increase the surface area for improved thermal transfer and another region with modified surface features that are configured to improve flow, or a region with modified surface features that do both. The modified surface features can be added to a particular conduit depending on the desired application.
(26) Modified surface features are affirmatively etched into the interior surface of the modified conduit. Random discontinuities such as pipe fitting seams, defects in the conduit, or inherent roughness in the interior surface do not qualify as modified surface features according to the disclosure herein.
(27) Although the present invention and its advantages have been described in detail, it should be understood that various changes, substitutions and alterations can be made herein without departing from the spirit and scope of the invention as defined by the appended claims. Moreover, the scope of the present application is not intended to be limited to the particular embodiments of the process, machine, manufacture, composition of matter, means, methods and steps described in the specification. As one of ordinary skill in the art will readily appreciate from the disclosure of the present invention, processes, machines, manufacture, compositions of matter, means, methods, or steps, presently existing or later to be developed that perform substantially the same function or achieve substantially the same result as the corresponding embodiments described herein may be utilized according to the present invention. Accordingly, the appended claims are intended to include within their scope such processes, machines, manufacture, compositions of matter, means, methods, or steps.