The subject matter disclosed herein relates to refrigeration systems. More specifically, the subject matter disclosed herein relates to refrigeration of cargo compartments of trucks or trailers.
A typical refrigerated truck or truck trailer, such as those utilized to transport a cargo, includes a refrigeration unit located at one end of the cargo compartment. The refrigeration unit includes a compressor, condenser, expansion valve and evaporator serially connected by refrigerant lines in a closed refrigerant circuit in accord with known refrigerant vapor compression cycles. The evaporator is located in a compartment that requires cooling, such as a cargo compartment of the truck or trailer. The condenser and compressor are located outside of the compartment. Cargo compartment air is passed over the coils of the evaporator, boiling the refrigerant flowing through the evaporator coil, thus heat is absorbed from the air in the conditioned compartment to cool the conditioned compartment. The gaseous refrigerant is then flowed to the compressor for compression thereat. A power unit, including an engine, drives the compressor of the refrigeration unit, and is typically diesel powered, or in other applications natural gas powered. In many truck/trailer transport refrigeration systems, the compressor is driven by the engine shaft either through a belt drive or by a mechanical shaft-to-shaft link. In other systems, so-called “electrically driven” systems, the engine drives a generator that generates electrical power, which in turn drives the compressor.
Exhaust gas from the engine is directed outwardly to ambient via an exhaust pipe. The exhaust gas temperature from the engine can be quite high, especially from natural gas powered engines, where the exhaust gas temperature can exceed 1000° Fahrenheit. This is problematic when the exhaust is directed toward, for example, foliage or sidewalks, nearby vehicles or the like and may result in fire or damage.
In one embodiment, a transportation refrigeration unit includes an evaporator circulating a flow of refrigerant therethrough to cool a flow of supply air flowing over the evaporator, a compressor in fluid communication with the evaporator to compress the flow of refrigerant, and an engine operably connected to the compressor to drive operation of the compressor. The engine includes an exhaust pathway to direct an exhaust gas flow from the transportation refrigeration unit, and a nozzle extending circumferentially around the exhaust pathway defining a nozzle flowpath between the exhaust pathway and the nozzle, the nozzle configured to flow a cooling airflow along the nozzle flowpath to reduce a temperature of the exhaust gas flow.
Additionally or alternatively, in this or other embodiments the nozzle includes a nozzle inlet upstream of an exhaust pathway exit, relative to a direction of flow of the exhaust gas flow through the exhaust pathway.
Additionally or alternatively, in this or other embodiments the nozzle includes a nozzle outlet downstream of an exhaust pathway exit, relative to a direction of flow of the exhaust gas flow through the exhaust pathway.
Additionally or alternatively, in this or other embodiments a mixing area is located in the nozzle downstream of the exhaust pathway exit, and is configured to allow for mixing of the exhaust gas flow with the cooling airflow to further reduce the temperature of the exhaust gas flow.
Additionally or alternatively, in this or other embodiments the nozzle is positioned at the exhaust pathway via one or more ribs extending between the nozzle and the exhaust pathway.
Additionally or alternatively, in this or other embodiments a nozzle inlet is positioned in a path of a condenser fan airflow exiting a condenser fan of the transportation refrigeration unit.
Additionally or alternatively, in this or other embodiments the engine utilizes natural gas as a fuel.
In another embodiment, a method of operating a transportation refrigeration unit includes operating a compressor to compress a flow of refrigerant in the transportation refrigeration unit and operating an engine operably connected to the compressor to drive the compressor. A flow of exhaust gas is directed away from the engine via an exhaust pathway, and a cooling airflow is flowed through a nozzle flowpath defined between the exhaust pathway and a nozzle disposed circumferentially around the exhaust pathway, thereby reducing a temperature of the flow of exhaust gas exiting the exhaust pathway.
Additionally or alternatively, in this or other embodiments the cooling airflow is flowed into the nozzle through a nozzle inlet located upstream of an exhaust pathway exit, relative to a direction of flow of the exhaust gas flow through the exhaust pathway.
Additionally or alternatively, in this or other embodiments the cooling airflow is flowed toward a nozzle outlet located downstream of an exhaust pathway exit, relative to a direction of flow of the exhaust gas flow through the exhaust pathway.
Additionally or alternatively, in this or other embodiments the cooling airflow is mixed with the flow of exhaust gas flow in a mixing area in the nozzle downstream of the exhaust pathway exit to further reduce the temperature of the flow of exhaust gas.
Additionally or alternatively, in this or other embodiments the nozzle is positioned at the exhaust pathway via one or more ribs extending between the nozzle and the exhaust pathway.
Additionally or alternatively, in this or other embodiments a nozzle inlet is positioned in a path of a condenser fan airflow exiting a condenser fan of the transportation refrigeration unit.
Additionally or alternatively, in this or other embodiments at least a portion of the condenser fan airflow is flowed into the nozzle inlet.
Additionally or alternatively, in this or other embodiments the engine utilizes natural gas as a fuel.
These and other advantages and features will become more apparent from the following description taken in conjunction with the drawings.
The subject matter is particularly pointed out and distinctly claimed at the conclusion of the specification. The foregoing and other features, and advantages of the present disclosure are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:
The detailed description explains embodiments, together with advantages and features, by way of example with reference to the drawings.
Shown in
Referring now to
As stated above, the compressor 36 compresses a vapor refrigerant flow 50, and the refrigerant flow 50 changes phase into liquid at the condenser 44. The condenser 44 is fluidly connected to an expansion device 48. The expansion device 48 is fluidly connected to the evaporator 32, where the airflow 34 is cooled and the refrigerant flow 50 is boiled through thermal energy exchange at the evaporator 32. The vaporized refrigerant flow 50 is then returned to compressor inlet 52 of compressor 36.
Referring now to
Referring to the cross-sectional view of
The exhaust gas flow 56 flows along the exhaust pipe 54 in a flow direction 64 toward an exhaust pipe exit 66. The nozzle 58 has a nozzle inlet 68 upstream of the exhaust pipe exit 66 and a nozzle outlet 70 downstream of the exhaust pipe exit 66, relative to the flow direction 64. The nozzle configuration draws a cooling airflow 72 into the nozzle 58 via the nozzle inlet 68 and through the nozzle 58 toward a mixing area 74 inside of the nozzle 58, downstream of the exhaust pipe exit 66. The cooling airflow 72 mixes with the exhaust gas flow 56 reducing a temperature of the exhaust gas flow 56 before the exhaust gas flow 56 exits the nozzle 58 via the nozzle outlet 70. In the embodiment of
In some embodiments, the nozzle 58 is located to take advantage of a condenser fan airflow 76 exiting a condenser fan 78 of the refrigeration unit 24. The nozzle inlet 70 is positioned in a path of the condenser fan airflow 76 such that at least a portion of the condenser fan airflow 76, accelerated by the condenser fan 78, into the nozzle inlet 70. This increased velocity airflow into the nozzle 58 increases the cooling of the exhaust gas flow 56.
The disclosed nozzle 58 exhibits a temperature reduction of exiting exhaust gas temperature when measured 6 inches from the nozzle outlet 70, when compared to exhaust gas temperature when measured 6 inches from an exit of a typical exhaust pipe. In some cases, the exhaust gas temperature reduction is in the range of 50-60%.
While the present disclosure has been described in detail in connection with only a limited number of embodiments, it should be readily understood that the present disclosure is not limited to such disclosed embodiments. Rather, the present disclosure can be modified to incorporate any number of variations, alterations, substitutions or equivalent arrangements not heretofore described, but which are commensurate in scope. Additionally, while various embodiments have been described, it is to be understood that aspects of the present disclosure may include only some of the described embodiments. Accordingly, the present disclosure is not to be seen as limited by the foregoing description, but is only limited by the scope of the appended claims.
This application is a National Stage application of PCT/US2016/059658, filed Oct. 31, 2016, which claims the benefit of U.S. Provisional Application No. 62/256,493, filed Nov. 17, 2015, both of which are incorporated by reference in their entirety herein.
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/US2016/059658 | 10/31/2016 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2017/087144 | 5/26/2017 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
877431 | Jones | Jan 1908 | A |
2886121 | Welbourn | May 1959 | A |
2913871 | Bradwhaw | Nov 1959 | A |
3045421 | Pagliuca | Jul 1962 | A |
3543510 | Kaufmann, Jr. | Dec 1970 | A |
4313523 | Copen | Feb 1982 | A |
5014512 | Kakuta | May 1991 | A |
5962822 | May | Oct 1999 | A |
7051524 | Kraft | May 2006 | B1 |
7461506 | McNally et al. | Dec 2008 | B2 |
7487633 | Popik et al. | Feb 2009 | B2 |
7637099 | Ranganathan et al. | Dec 2009 | B2 |
7645432 | Solomon | Jan 2010 | B1 |
7669411 | Mallampalli et al. | Mar 2010 | B2 |
7757482 | Li et al. | Jul 2010 | B2 |
7762064 | Tennison | Jul 2010 | B2 |
7793495 | Bradley et al. | Sep 2010 | B2 |
7833301 | Schindler et al. | Nov 2010 | B2 |
7845465 | Baumgartner | Dec 2010 | B2 |
7913489 | Angoshtari et al. | Mar 2011 | B2 |
7987666 | Branning et al. | Aug 2011 | B2 |
8001775 | Krajewski et al. | Aug 2011 | B2 |
8056327 | Brown et al. | Nov 2011 | B2 |
8109083 | Gibson et al. | Feb 2012 | B2 |
8166752 | Garcia et al. | May 2012 | B2 |
8181453 | Goplen et al. | May 2012 | B2 |
8341948 | Freese | Jan 2013 | B2 |
8429896 | Pekrul et al. | Apr 2013 | B2 |
8479501 | McCarthy, Jr. | Jul 2013 | B2 |
8549850 | Janakiraman et al. | Oct 2013 | B2 |
8661798 | Prather | Mar 2014 | B2 |
8720195 | Gardner et al. | May 2014 | B2 |
8794300 | Irmler et al. | Aug 2014 | B2 |
9822690 | Gao | Nov 2017 | B2 |
9995249 | Takahashi | Jun 2018 | B2 |
20060123818 | Kim | Jun 2006 | A1 |
20090139217 | Eifert et al. | Jun 2009 | A1 |
20100000205 | Freese | Jan 2010 | A1 |
20100126155 | Garcia | May 2010 | A1 |
20110192153 | Schmidt | Aug 2011 | A1 |
20120102919 | Smith et al. | May 2012 | A1 |
20120272640 | Mungas et al. | Nov 2012 | A1 |
20120318602 | Bada Ghar Wala | Dec 2012 | A1 |
20130327417 | Gardner | Dec 2013 | A1 |
20140174087 | Mizoguchi | Jun 2014 | A1 |
20140216370 | Ichihashi | Aug 2014 | A1 |
20140223933 | Steele et al. | Aug 2014 | A1 |
20140250941 | Steele | Sep 2014 | A1 |
20150128578 | Helferich | May 2015 | A1 |
20150128921 | Paull | May 2015 | A1 |
Number | Date | Country |
---|---|---|
102146828 | Aug 2011 | CN |
3735059 | Apr 1989 | DE |
102012012007 | Dec 2012 | DE |
1607597 | Dec 2005 | EP |
2211038 | Jul 2010 | EP |
2008030259 | Mar 2008 | WO |
2009099399 | Aug 2009 | WO |
2013043389 | Mar 2013 | WO |
Entry |
---|
International Search Report for International Application No. PCT/US2016/059658; International Filing Date Oct. 31, 2016; dated Dec. 19, 2016; 6 Pages. |
Written Opinion for International Application No. PCT/US2016/059658; International Filing Date Oct. 31, 2016; dated Dec. 19, 2016; 6 Pages. |
Number | Date | Country | |
---|---|---|---|
20180355775 A1 | Dec 2018 | US |
Number | Date | Country | |
---|---|---|---|
62256493 | Nov 2015 | US |