Electronics enclosure with heat-transfer element

Abstract

A compressor may include a compressor shell, a motor, a compression mechanism, and an assembly that houses an electronic component. The electronic component may control operation of the compressor and/or diagnose compressor faults. The assembly may include a shell, an electronic component, a fan, and an airflow deflector. The shell member may define an enclosure having an internal cavity. The fan and the electronic component may be disposed within the internal cavity. The airflow deflector may include a base portion, a first leg, and a second leg. The first and second legs may be spaced apart from each other and extend from the base portion. The fan may force air against the base portion. A first portion of the air may flow from the base portion along the first leg. A second portion of the air may flow from the base portion along the second leg.

Description

FIELD

The present disclosure relates to an electronics enclosure with a heat-transfer element.

BACKGROUND

This section provides background information related to the present disclosure and is not necessarily prior art.

Electronic components, such as control modules for a compressor, for example, generate heat during operation. Such electronic components are often housed in sealed enclosures that protect the electronic components from exposure to moisture, dirt, and debris. A fan can be provided within the enclosure to facilitate heat transfer between the electronic components and air within the enclosure. Heat can then be transferred from the air to the walls of the enclosure, and subsequently to the ambient atmosphere, for example. The present disclosure provides an enclosure for electronic components and includes features for improving airflow within the enclosure to improve cooling of the electronic components.

SUMMARY

This section provides a general summary of the disclosure, and is not a comprehensive disclosure of its full scope or all of its features.

In one form, the present disclosure provides a compressor that may include a compressor shell, a compression mechanism disposed within the compressor shell, a motor disposed within the shell and driving the compression mechanism, and a control module in communication with the motor and configured to control operation of the motor. An enclosure may be mounted to the compressor shell and may define an internal cavity in which the control module may be disposed. A fan may be disposed within the internal cavity. The enclosure may include an airflow deflector having a base portion, a first leg, and a second leg. The first and second legs may be spaced apart from each other and extend from the base portion. The fan may force air against the base portion. A first portion of the air may flow from the base portion along the first leg. A second portion of the air may flow from the base portion along the second leg.

In some configurations of the compressor of the above paragraph, the airflow deflector is integrally formed with a shell member that defines the enclosure. In some configurations, the airflow deflector is a recess formed in the shell member.

In some configurations of the compressor, the airflow deflector is formed separately from a shell member that defines the enclosure. In some configurations, the airflow deflector is mounted to the shell member.

In some configurations of the compressor of any of the above paragraphs, the base portion and the first and second legs cooperate to form a U-shape.

In some configurations of the compressor of any of the above paragraphs, the fan is aligned with the base portion such that a rotational axis of the fan extends through the base portion.

In some configurations of the compressor of any of the above paragraphs, the first and second legs include curved surfaces.

In some configurations of the compressor of any of the above paragraphs, air flows from the fan toward the base portion in a first direction.

In some configurations of the compressor of any of the above paragraphs, the curved surfaces of the first and second legs curve in a second direction as the curved surfaces extend away from the base portion.

In some configurations of the compressor of any of the above paragraphs, the second direction is opposite the first direction.

In another form, the present disclosure provides an assembly that may include a shell, an electronic component, a fan, and an airflow deflector. The shell member may at least partially define an enclosure having an internal cavity. The electronic component may be disposed within the internal cavity. The fan may be disposed within the internal cavity. The airflow deflector may include a base portion, a first leg, and a second leg. The first and second legs may be spaced apart from each other and extend from the base portion. The fan may force air against the base portion. A first portion of the air may flow from the base portion along the first leg. A second portion of the air may flow from the base portion along the second leg.

In some configurations of the assembly of the above paragraph, the airflow deflector is integrally formed with the shell member.

In some configurations of the assembly of either of the above paragraphs, the airflow deflector is a recess formed in the shell member.

In some configurations, the airflow deflector is formed separately from the shell member and is mounted to the shell member.

In some configurations of the assembly of any of the above paragraphs, the base portion and the first and second legs cooperate to form a U-shape.

In some configurations of the assembly of any of the above paragraphs, the fan is aligned with the base portion such that a rotational axis of the fan extends through the base portion.

In some configurations of the assembly of any of the above paragraphs, the first and second legs include curved surfaces.

In some configurations of the assembly of any of the above paragraphs, air flows from the fan toward the base portion in a first direction.

In some configurations of the assembly of any of the above paragraphs, the curved surfaces of the first and second legs may curve in a second direction as the curved surfaces extend away from the base portion.

In some configurations of the assembly of any of the above paragraphs, the second direction is opposite the first direction.

In some configurations of the assembly of any of the above paragraphs, the electronic component is disposed adjacent the base portion and between the first and second legs.

In some configurations of the assembly of any of the above paragraphs, the electronic component is, includes or is a part of a control module configured to control operation of a compressor.

In some configurations of the assembly of any of the above paragraphs, the enclosure is mounted to a shell of the compressor.

In some configurations of the assembly of any of the above paragraphs, a depth of the airflow deflector and an angle of attack of the first and second legs are configured to optimize airflow within the enclosure.

In some configurations of the assembly of any of the above paragraphs, the cavity is sealed such that air does not flow into or out of the cavity.

In some configurations of the assembly of any of the above paragraphs, the shell member may include heat sink fins. The fins may be formed on an exterior surface of the shell member.

Further areas of applicability will become apparent from the description provided herein. The description and specific examples in this summary are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.

DRAWINGS

The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.

FIG. 1 is a perspective view of a compressor including a control module and an enclosure in which the control module is housed;

FIG. 2 is a perspective view of the enclosure;

FIG. 3 is a cross-sectional view of the enclosure and control module taken along line 3-3 of FIG. 2;

FIG. 4 is a partial perspective view of an interior of a shell member of the enclosure;

FIG. 5 is a plan view of an exterior of the shell member;

FIG. 6 is a perspective view of an alternative enclosure for housing the control module;

FIG. 7 is a cross-sectional view of the enclosure and control module taken along line 7-7 of FIG. 6;

FIG. 8 is a perspective view of an airflow deflector and fan of the enclosure of FIG. 6;

FIG. 9 is an exploded perspective view of the airflow deflector and fan; and

FIG. 10 is a plan view of the enclosure of FIG. 6.

Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.

DETAILED DESCRIPTION

Example embodiments will now be described more fully with reference to the accompanying drawings.

Example embodiments are provided so that this disclosure will be thorough, and will fully convey the scope to those who are skilled in the art. Numerous specific details are set forth such as examples of specific components, devices, and methods, to provide a thorough understanding of embodiments of the present disclosure. It will be apparent to those skilled in the art that specific details need not be employed, that example embodiments may be embodied in many different forms and that neither should be construed to limit the scope of the disclosure. In some example embodiments, well-known processes, well-known device structures, and well-known technologies are not described in detail.

The terminology used herein is for the purpose of describing particular example embodiments only and is not intended to be limiting. As used herein, the singular forms “a,” “an,” and “the” may be intended to include the plural forms as well, unless the context clearly indicates otherwise. The terms “comprises,” “comprising,” “including,” and “having,” are inclusive and therefore specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof. The method steps, processes, and operations described herein are not to be construed as necessarily requiring their performance in the particular order discussed or illustrated, unless specifically identified as an order of performance. It is also to be understood that additional or alternative steps may be employed.

When an element or layer is referred to as being “on,” “engaged to,” “connected to,” or “coupled to” another element or layer, it may be directly on, engaged, connected or coupled to the other element or layer, or intervening elements or layers may be present. In contrast, when an element is referred to as being “directly on,” “directly engaged to,” “directly connected to,” or “directly coupled to” another element or layer, there may be no intervening elements or layers present. Other words used to describe the relationship between elements should be interpreted in a like fashion (e.g., “between” versus “directly between,” “adjacent” versus “directly adjacent,” etc.). As used herein, the term “and/or” includes any and all combinations of one or more of the associated listed items.

Although the terms first, second, third, etc. may be used herein to describe various elements, components, regions, layers and/or sections, these elements, components, regions, layers and/or sections should not be limited by these terms. These terms may be only used to distinguish one element, component, region, layer or section from another region, layer or section. Terms such as “first,” “second,” and other numerical terms when used herein do not imply a sequence or order unless clearly indicated by the context. Thus, a first element, component, region, layer or section discussed below could be termed a second element, component, region, layer or section without departing from the teachings of the example embodiments.

Spatially relative terms, such as “inner,” “outer,” “beneath,” “below,” “lower,” “above,” “upper,” and the like, may be used herein for ease of description to describe one element or feature's relationship to another element(s) or feature(s) as illustrated in the figures. Spatially relative terms may be intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, elements described as “below” or “beneath” other elements or features would then be oriented “above” the other elements or features. Thus, the example term “below” can encompass both an orientation of above and below. The device may be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.

With reference to FIG. 1, a compressor 10 is provided that may be operable to compress a working fluid (e.g., a refrigerant) and circulate the working fluid throughout a vapor compression circuit of a climate-control system (e.g., a refrigeration or air conditioning system). The compressor 10 includes a control module 12 disposed within an enclosure 14. The control module 12 may include processing circuitry (e.g., a circuit board) and other electronic components and may be operable to control operation of the compressor 10 and/or diagnose compressor faults. For example, the control module 12 may be a variable-speed drive for controlling a motor 13 of a variable-speed compressor. The motor 13 may drive a compression mechanism 15 of the compressor 10 (e.g., via a driveshaft). For example, the compression mechanism 15 may be a scroll compression mechanism (including a pair of interleaving scrolls), a reciprocating compression mechanism (including one or more pistons and cylinders), a rotary vane compression mechanism (including a rotor and cylinder), or any other type of compression mechanism. The enclosure 14 may house the control module 12 and can be mounted to a shell 16 of the compressor 10.

Referring now to FIGS. 2-5, the enclosure 14 will be described in detail. The enclosure 14 may include a first shell member 18 (FIGS. 2-5) and a second shell member 20 (FIG. 3) that cooperate to define a sealed internal cavity 22 (FIG. 3) in which the control module 12 is disposed. The first and second shell members 18, 20 can be fixed to each other by bolts or other fasteners, for example.

A fan 24 may be disposed within the cavity 22 and is operable to circulate air around the cavity 22 to convectively cool the control module 12. The fan 24 may be attached to or mounted proximate an airflow deflector (or airfoil) 26. In the particular example shown in FIGS. 2-5, the airflow deflector 26 is integrally formed in the first shell member 18. In some configurations, heat sink fins may be formed on exterior surfaces of the first shell member 18 and/or the second shell member 20.

As shown in FIG. 4, the airflow deflector 26 may be a generally U-shaped scoop or recess formed in an interior surface 28 of the first shell member 18. The airflow deflector 26 may include a base portion 30, a first leg 34, and a second leg 36. The first and second legs 34, 36 may be spaced apart from each other and may extend from the base portion 30. The first and second legs 34, 36 may define first and second airflow paths, respectively. That is, the fan 24 may force air against the base portion 30 between the first and second legs 34, 36, and a first portion of that air may flow through the first airflow path along the first leg 34 and a second portion of the air may flow through the second airflow path along the second leg 36. From the first and second legs 34, 36, the air may flow throughout the internal cavity 22 of the enclosure 14 to cool the control module 12.

As shown in FIG. 3, the base portion 30 of the airflow deflector 26 may have a depth D. The depth D may be a distance (measured along or parallel to a rotational axis R of the fan 24) between the fan 24 and a base portion 30 of the airflow deflector 26. A base surface 32 of each of the first and second legs 34, 36 may be disposed at an angle of attack A (e.g., an angle between the base surface 32 and the rotational axis R). The base surfaces 32 of the first and second legs 34, 36 can be curved or sloped. The depth D, angle of attack A, and any curve of slope of the base surfaces 32 may be selected to maximize airflow velocity through the airflow deflector 26 and minimize a pressure drop of air flowing through the airflow deflector 26.

As shown in FIG. 5, one or more electronic components 40 of the control module 12 may be positioned between the first and second legs 34, 36 and adjacent the base portion 30. Such positioning may enhance the cooling of the components 40. For this reason, in some configurations, the component(s) 40 selected to be positioned between first and second legs 34, 36 may be components that tend to generate the most heat and/or need the most cooling.

Referring now to FIGS. 6-10, an alternative enclosure 114 is provided that can house the control module 12. The enclosure 114 may include a first shell member 118, a second shell member 120, and a fan 124. The first and second shell members 118, 120 and fan 124 be similar or identical to the shell members 18, 20 and fan 24 described above, except that the first shell member 118 does not include an integrally formed airflow deflector. Instead, the enclosure 114 includes a separate airflow deflector (or airfoil) 126 that may be mounted to the first shell member 118.

Like the airflow deflector 26, the airflow deflector 126 may be generally U-shaped and may include a base portion 130, a first leg 134, and a second leg 136. As shown in FIG. 7, the base portion 130 of the airflow deflector 126 may have a depth D. The depth D may be a distance (measured along or parallel to a rotational axis R of the fan 124) between the fan 124 and a base portion 130 of the airflow deflector 126. A base surface 132 of each of the first and second legs 134, 136 may be disposed at an angle of attack A (e.g., an angle between the base surface 132 and the rotational axis R). The base surfaces 132 of the first and second legs 134, 136 can be curved or sloped. The depth D, angle of attack A, and any curve of slope of the base surfaces 132 may be selected to maximize airflow velocity through the airflow deflector 126 and minimize a pressure drop of air flowing through the airflow deflector 126.

The airflow deflectors 26, 126 of the enclosures 14, 114 may improve airflow throughout the interior of the enclosures 14, 114 and around the control module 12. Furthermore, the airflow deflectors 26, 126 may reduce or eliminate turbulence in the airflow, which improves heat transfer between the control module 12 and the air within the enclosure 14, 114.

The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.

Claims

1. A compressor comprising: a compressor shell;a compression mechanism disposed within the compressor shell;a motor disposed within the shell and driving the compressor mechanism;a control module in communication with the motor and configured to control operation of the motor;an enclosure mounted to the compressor shell and defining an internal cavity, wherein the control module is disposed within the internal cavity;a fan disposed within the internal cavity; andan airflow deflector having a base portion, a first leg, and a second leg, wherein the first and second legs are spaced apart from each other and extend from the base portion,wherein the fan forces air against the base portion, wherein a first portion of the air flows from the base portion along the first leg, and wherein a second portion of the air flows from the base portion along the second leg.

2. The compressor of claim 1, wherein the airflow deflector is integrally formed with a shell member that defines the enclosure, and wherein the airflow deflector is a recess formed in the shell member.

3. The compressor of claim 1, wherein the airflow deflector is formed separately from a shell member that defines the enclosure, wherein the airflow deflector is mounted to the shell member.

4. The compressor of claim 1, wherein the base portion and the first and second legs cooperate to form a U-shape, and wherein the fan is aligned with the base portion such that a rotational axis of the fan extends through the base portion.

5. The compressor of claim 1, wherein the first and second legs include curved surfaces, wherein the air flows from the fan toward the base portion in a first direction, wherein the curved surfaces of the first and second legs curve in a second direction as the curved surfaces extend away from the base portion, and wherein the second direction is opposite the first direction.

6. An assembly comprising: a compressor including a compressor shell;a shell member at least partially defining an enclosure having an internal cavity, wherein the shell member is coupled to the compressor shell;an electronic component disposed within the internal cavity;a fan disposed within the internal cavity; andan airflow deflector having a base portion, a first leg, and a second leg, wherein the first and second legs are spaced apart from each other and extend from the base portion,wherein the fan forces air against the base portion, wherein a first portion of the air flows from the base portion along the first leg, and wherein a second portion of the air flows from the base portion along the second leg.

7. The assembly of claim 6, wherein the airflow deflector is integrally formed with the shell member.

8. The assembly of claim 7, wherein the airflow deflector is a recess formed in the shell member.

9. The assembly of claim 6, wherein the airflow deflector is formed separately from the shell member and is mounted to the shell member.

10. The assembly of claim 6, wherein the base portion and the first and second legs cooperate to form a U-shape.

11. The assembly of claim 10, wherein the fan is aligned with the base portion such that a rotational axis of the fan extends through the base portion.

12. The assembly of claim 6, wherein the first and second legs include curved surfaces.

13. The assembly of claim 12, wherein the air flows from the fan toward the base portion in a first direction.

14. The assembly of claim 13, wherein the curved surfaces of the first and second legs curve in a second direction as the curved surfaces extend away from the base portion.

15. The assembly of claim 14, wherein the second direction is opposite the first direction.

16. The assembly of claim 6, wherein the electronic component is disposed adjacent the base portion and between the first and second legs.

17. The assembly of claim 6, wherein the electronic component is configured to control operation of the compressor.

18. The assembly of claim 17, wherein the enclosure is mounted to shell the compressor.

19. The assembly of claim 6, wherein a depth of the airflow deflector and an angle of attack of the first and second legs are configured to optimize airflow within the enclosure.

20. The assembly of claim 6, wherein the internal cavity is a sealed cavity.