The present disclosure relates to a screw compressor for a heating, ventilation, and air conditioning system (HVAC), such as a vehicle HVAC.
This section provides background information related to the present disclosure, which is not necessarily prior art.
While current heating, ventilation, and air conditioning (HVAC) system compressors are suitable for their intended use, they are subject to improvement. For example, there is a need for a compressor which, when compressing refrigerant: does not increase the temperature of the refrigerant as much as a piston compressor does; reduces pulsation and spill-back of refrigerant as compared to a piston compressor; and has a lower level of overload requirements as compared to a piston compressor. The present disclosure advantageously provides for compressors that address these needs in the art, as well as numerous others as described herein and as one skilled in the art will appreciate.
This section provides a general summary of the disclosure, and is not a comprehensive disclosure of its full scope or all of its features.
The present disclosure includes a screw compressor for a heating, ventilation, and air conditioning (HVAC) system. The screw compressor includes a housing having an inlet end and an outlet end for refrigerant to pass into and out of the housing. A motor is within the housing. A plurality of screw sets are arranged about the motor. The screw sets receive refrigerant entering through the inlet, compress the refrigerant between meshed rotors of the plurality of screw sets, and direct refrigerant out of the housing through the outlet end of the housing.
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.
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.
Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
Example embodiments will now be described more fully with reference to the accompanying drawings.
The exemplary HVAC system 10 includes an evaporator 12, a condenser 14, a dryer 16, and a thermal expansion valve 18. Any suitable refrigerant is circulated through the HVAC system 10 by way of a refrigerant line 20. From the evaporator 12, the refrigerant line 20 delivers refrigerant to an inlet 112 of the compressor 110. The inlet 112 is included with a rotatable inlet cylinder 114. The refrigerant enters the compressor 110 as a low pressure gas, which is compressed by the compressor 110 into a high pressure gas. The high pressure gas refrigerant exits the compressor 110 through an outlet 116 of a rotatable outlet cylinder 118. Advantageously, the inlet cylinder 114 and the outlet cylinder 118 are each rotatable, which allows the inlet 112 and the outlet 116 to be arranged at any suitable rotational position about the compressor 110 to facilitate connection of the refrigerant lines 20 to the inlet 112 and the outlet 116, and thus generally facilitate installation of the compressor 110 in the HVAC system 10.
The high pressure gas refrigerant flows from the compressor 110 to the condenser 14, where heat is radiated out from the refrigerant. At the condenser 14, the high pressure gas refrigerant condenses to a high pressure liquid refrigerant, which is dried at the dryer 16. From the dryer 16 the liquid refrigerant flows through the refrigerant line 20 to the thermal expansion valve 18, and back to the evaporator 12 as a low pressure liquid that absorbs heat from a vehicle passenger cabin, for example.
With reference to
The inlet 112, which provides a refrigerant passageway into the rotatable inlet cylinder 114, is defined by a coupling member 112′. The coupling member 112′ is rotatable independent of the rotatable inlet cylinder 114 (such as along an axis perpendicular to the longitudinal axis A) to provide further adjustability of the inlet 112 and further facilitate coupling of the refrigerant line 20 to the inlet 112 and the coupling member 112′. Similarly, the outlet 116 is defined by a coupling member 116′. The coupling member 116′ is rotatable independent of the rotatable outlet cylinder 118 (such as along an axis perpendicular to the longitudinal axis A) to provide further adjustability of the outlet 116 and further facilitate coupling of the refrigerant line 20 to the outlet 116 and the coupling member 116′.
The rotatable inlet cylinder 114 is rotatable about the longitudinal axis A to allow the inlet 112 to be arranged at any suitable rotatable position about the longitudinal axis A to facilitate coupling of the refrigerant line 20 to the inlet 112. The rotatable inlet cylinder 114 is between the inlet end 122 of the housing 120 and an inverter 130. The inverter 130 is any suitable power inverter for changing direct current to alternating current for powering a motor 150. The inverter 130 is mounted at the housing 120 in any suitable manner to compress the rotatable inlet cylinder 114 between the inverter 130 and the housing 120. When the connection between the inverter 130 and the housing 120 is loosened (e.g., fasteners coupling the inverter 130 to the housing 120 are loosened) the inverter 130 does not apply compression force against the rotatable inlet cylinder 114, and thus the rotatable inlet cylinder 114 is free to rotate about the longitudinal axis A. When the connection between the inverter 130 and the housing 120 is tightened, the inverter 130 is drawn towards the housing 120 along the longitudinal axis A to apply compression force against the rotatable inlet cylinder 114 thereby preventing the rotatable inlet cylinder 114 from rotating.
With reference to
With renewed reference to
With additional reference to
With renewed reference to
The screw set 160A is merely an exemplary screw set, and thus any other suitable screw sets may be included. For example and as illustrated in
The present disclosure thus provides numerous advantages over prior HVAC compressors. For example, the rotation of the screw sets 160A, 160B, 160C by the motor 150 is quieter than other types of compressors, such as reciprocal compressors. Furthermore, the temperature increase of the refrigerant during the compression by the helical screw sets 160A, 160B, 160C is far less than the temperature increase caused by piston reciprocal compressors. Because the compression process of the rotary screw sets 160A, 160B, 160C is a continuous sweeping motion, there is very little pulsation or spill-back, which is in contrast to current piston compressors. Still further, there is no source of friction or large inertia to overcome, so the rotary screw sets 160A, 160B, 160C do not have a high level of overload requirements. Also, by arranging the motor 150 along the longitudinal axis A and the screw sets 160A, 160B, 160C about the motor 150, the compressor 110 can advantageously be made shorter, thereby saving valuable vehicle space.
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.
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.
Number | Name | Date | Kind |
---|---|---|---|
2575154 | Zoll | Nov 1951 | A |
2693762 | Sennet | Nov 1954 | A |
4220197 | Schaefer et al. | Sep 1980 | A |
5533887 | Maruyama | Jul 1996 | A |
5979168 | Beekman | Nov 1999 | A |
6003324 | Shaw | Dec 1999 | A |
6217304 | Shaw | Apr 2001 | B1 |
6478560 | Bowman | Nov 2002 | B1 |
7178352 | Lifson | Feb 2007 | B2 |
7980836 | Shaw | Jul 2011 | B2 |
8205469 | Tsuboi | Jun 2012 | B2 |
20180363650 | Kikuchi | Dec 2018 | A1 |
Number | Date | Country |
---|---|---|
101605073 | Mar 2016 | KR |
Entry |
---|
“One Female More Change the World of Screw Compressors for Oil and Water Injected Screw Compressors” by Guenter Kirsten (COO at UNO International Inventments INC), Published on Mar. 5, 2017, https://www.linkedin.com/pulse/one-female-more-change-world-screw-compressors-oil-water-kirsten/. |
“New Development for an Three Rotor Screw Compressor with Poly-Ceramic Rotors” by Guenter Kirsten (COO at UNO International Investments INC), Published on Mar. 9, 2016, https://www.linkedin.com/pulse/new-development-three-rotor-screw-compressor-rotors-guenter-kirsten/. |
“Small Screw Compressors for Automobile Air Conditioning Systems” by Y. Fukazawa and U. Ozawa, Published in 1980, https://docs.lib.purdue.edu/cgi/viewcontent.cgi?referer=https://www.google.com/&httpsredir=1&article=1350&context=icec. |
“Variable Speed Tri-Rotor Screw Compression Technology” by Ko Young Ye, Published in 2006, https://docs.lib.purdue.edu/cgi/viewcontent.cgi?article=2824&context=icec. |
Number | Date | Country | |
---|---|---|---|
20200096235 A1 | Mar 2020 | US |