The embodiments described herein relate to an apparatus and method for converting rotational motion into linear motion and evacuating non-compressible gases of a compressor.
A general hermetic compressor includes a motor portion and compressor portion sealed in a hermetic container. A compressor may be classified as reciprocating, rotary, or any other type where a refrigerant is compressed. In general, a hermetic compressor has a crank shaft coupled to a rotor of the motor part that transfers power to reciprocating pistons. The reciprocating pistons compress the compressible gas within a cylinder. Reciprocating pistons may be arranged in offset horizontal planes that cause unwanted forces on the crankpin and crankshaft. In order to compensate for the unwanted forces, larger crankshaft bearings may be required.
A lower part of the hermetic container may be filled with oil or a condensed fluid. An oil path is formed in an axial direction of the crank shaft, and an oil feeder is installed at a lower end of the oil path so as to be immersed in oil. As the crank shaft rotates, oil is pumped along the oil path to be fed, supplying the required components with lubrication. The hermetic container may be filled at the factory to properly seal the container. A factory fill may require additional transportation and installation costs.
A hermetic compressor may include a hermetic shell having a shell and a base which collectively define an enclosed cavity. The hermetic shell may define a discharge port and a suction port. The hermitic compressor may include an electric motor having a stator disposed within the enclosed cavity on the base. The motor may have a rotary output. The compressor may be made of a cast-iron block and include a head assembly. The cast-iron block and head assembly may define a crankshaft axis. The cast-iron block may include a pair of directly opposed cylinders oriented perpendicular to the crankshaft axis, each having an inlet and an outlet port.
The compressor may include a crankshaft having an input shaft rotatably supported on the cast-iron block along the crankshaft axis and connected to the electric motor rotary output, and an eccentric crankpin orbitally rotating about the axis as the crankshaft is rotated. A pair of opposed pistons may lie on the common plane. Each piston may be pivotably connected to one of the connecting rod piston ends to drive the pistons in an oscillatory manner within the cylinders as the crankshaft rotates. The piston and cylinder pairs may cause fluid to be pumped from the inlet port to the outlet port as the piston oscillates varying the volume of the enclosed space bound by the piston and the cylinder pairs.
A pair of connecting rods may have a crankshaft end with a bearing opening surrounding the eccentric crankpin, a spaced apart piston end and a rod portion there between. The connecting rods may generally lie in a common plane perpendicular to the input shaft axis with each of the first ends axially offset from one another in a dogleg manner lying on opposite side of the common plane to surround the crankpin.
The connecting rod assembly may include a friction reduction element disposed between the connecting rod crankshaft ends and a plurality of spring feet mounted on the hermetic shell base in spaced apart relation for supporting the compressor on a support surface.
A pipe may connect the outlet port of a first cylinder to the inlet port of the other second cylinder in a serial fashion with the first cylinder inlet port coupled to the hermetic shell and the second cylinder outlet port discharging to the discharge port exiting the hermetic shell. In at least one other embodiment, a pair of outlet pipes connect the pair of outlet ports to the discharge port exiting the hermetic shell.
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The preferred embodiment improves on previous methods to evacuate trapped gases that are undesirable. Prior to the preferred embodiment, these trapped gases were evacuated at the site of manufacture by vacuum suction. The preferred embodiment includes a vent port 26 to release trapped air at the installation site. The vent port 26 is disposed above the seam 13 to prevent oil leakage during gas evacuation.
The vent port 26 provides an effective way to remove trapped gases that are undesirable at the installation site. The method for removing undesirable gases primarily uses the vent port 26 and the refill port 28. Initially, the vent port 26 is closed. Trapped moisture is then removed from the system by drawing a vacuum on the refill port 28. The hermetic shell 10 is then pressurized using the refill port 28 and refrigerant or inert gas. The internal pressure of the hermetic shell may be raised to any level sufficient to promote the release of undesirable gases. Typically, the hermetic shell 10 pressure is raised more than one quarter of the normal working pressure, but less than the full normal working pressure of the compressor.
The heavier air is then allowed to settle to the bottom of the hermetic shell, but above the level of the resting oil, which is generally located at the seam 13. The opening of the vent port 26 then releases undesirable gases from the hermetic shell, which leaves only oil and refrigerant gas retained in the shell.
An important requirement prior to the use of the hermetic compressor system is to ensure the proper amount of refrigerant is present in the system prior to use. Verification of adequate refrigerant may be performed numerous ways, but the following are example methods used to verify adequate refrigerant in the system.
The preferred method to ensure the compressor is adequately filled with refrigerant is to measure the weight and volume of the amount of air removed from the system through the vent port 26. This method is well known to those skilled in the art. The installer would then add refrigerant as necessary.
The second method to ensure the proper amount of refrigerant is to measure the internal pressure of the hermetic shell 10 and adjust the amount of refrigerant as necessary. This method is well known to those skilled in the art. The new process for high-efficiency cooling, described as putting gas in the sealed refrigeration systems free from any contamination, caters to all types of gas (e.g. R134 or R600).
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The L-shaped connecting rod 110 as described above has a symmetric companion L-shaped connecting rod 112. The companion L-shaped connecting rod 112 defines a hole 123 on crankpin end 120 of the connecting rod 112. The hole 123 may be used for a pin to connect the crankpin end 120 and piston end 124. The crankpin end 120 of the connecting rod 112 is rotationally attached to the crankpin 108 with a bearing sized to receive the crankpin 108. The crankpin end 120 can then orbit about the crankshaft 106 along with the crankpin 108. The orbiting motion of the crankpin end 120 causes the attached piston end 124 to reciprocate. The reciprocating motion of the piston end 124 causes the piston 128 to similarly reciprocate. The reciprocating motion of the piston 126 compresses the compressible gas of the cylinder.
The companion L-shaped connecting rod 112 is flipped about a horizontal plane 111, which is perpendicular to the eccentric axis or crankpin axis 109, such that the piston ends 122, 124 of both connecting rods 110, 112 are aligned along a common horizontal plane 111. The piston end 124 of the companion L-shaped connecting rod 112 is oriented in the opposite direction of the piston end 122 of the L-shaped connecting rod 110. Further, the connecting rods 110, 112 interleave with each other. Specifically, crankpin end 118 of connecting rod 110 has a semicircular portion 132 opposite the crankpin 108 from the side of crankpin end 118 that joins to the piston end 122. Similarly, crankpin end 120 of connecting rod 112 has a semicircular portion 134 opposite the crankpin 108 from the side of crankpin end 120 that joins to piston end 124. Semicircular portion 132 of crankpin end 118 lies entirely on one side of the horizontal plane 111, and semicircular portion 134 of crankpin end 120 lies entirely on the opposite side of horizontal plane 111 from semicircular portion 132. The side of crankpin end 120 that connects to piston end 124 has a portion 138 that extends across the horizontal plane 111, and has an arcuate recess 140 in which semicircular portion 132 of crankpin end 118 partially sits. Likewise, crankpin end 118, at the end of crankpin end 118 that connects to piston end 122, has a portion 136 that extends across the horizontal plane 111, in which semicircular portion 134 of crankpin end 120 partially sits in a similar arcuate recess. Further, both piston end 122 of connecting rod 110 and piston end 124 of connecting rod 112 each have a longitudinal axis, from their respective crankpin end 118, 120 to their respective pistons 126, 128 that is entirely on the horizontal plane 111.
The orientation of the companion L-shaped connecting rod 112 to the L-shaped connecting rod 110 is one of the novel aspects of the embodiment because the piston ends 122, 124 of the connecting rods 110, 112 operate on the same horizontal plane 111. This provides enhanced symmetry for the compressor because each of the pistons 126, 128 are disposed on the same plane and create opposing forces. This configuration allows reciprocating movement of the pistons 126, 128 in the same plane without undesirable stresses.
Conflicting rotation of the connecting rods 110, 112 may cause unwanted friction and restricted movement. A thin washer 130 may be disposed between the L-shaped connecting rods 110, 112 may have a thickness between 0.1 mm and 0.3 mm. The washer may relieve mechanical friction, which tends to create counter force to the rotation of the bearing with respect to each other.
The connecting rods 110, 112 form a tear shape truncated toward the piston ends 122, 124. Each of the connecting rods 110, 112 define a bearing opening 125, 127 on respective connecting rod crankpin ends 118, 120. The connecting rod crankpin ends 118, 120 also define a cleft for receiving the piston ends 122, 124 of the connecting rods 110, 112. The pistons 126, 128 are connected on the distal end of the connecting rod piston ends 122, 124. The compressor pistons 126, 128 reciprocate within the cylinders (not shown).
Number | Date | Country | Kind |
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0903956 | Jan 2009 | BR | national |
This application is a continuation-in-part of U.S. application Ser. No. 13/143,869 filed on Sep. 28, 2011, which is the U.S. national phase of PCT Appln. No. PCT/BR2010/000008 filed Jan. 8, 2010 which claims priority to Brazilian application PI 0903956-2 filed Jan. 9, 2009, the disclosures of which are incorporated in their entirety by reference herein.
Number | Name | Date | Kind |
---|---|---|---|
1329348 | Copeland | Jan 1920 | A |
1747457 | Putnam | Feb 1930 | A |
1820883 | Hueber | Aug 1931 | A |
2179268 | Neeson | Nov 1939 | A |
2225228 | Neeson | Dec 1940 | A |
2323068 | Maniscalco | Jun 1943 | A |
2483007 | Higham | Sep 1949 | A |
2965289 | Weibel, Jr. | Dec 1960 | A |
3162360 | Privon | Dec 1964 | A |
3401873 | Privon | Sep 1968 | A |
3692434 | Schnear | Sep 1972 | A |
3757581 | Mankin | Sep 1973 | A |
3762837 | Ellis | Oct 1973 | A |
3763659 | Hover | Oct 1973 | A |
3785453 | Buonocore | Jan 1974 | A |
3817661 | Ingalls | Jun 1974 | A |
3857652 | Thayer | Dec 1974 | A |
4236874 | Sisk | Dec 1980 | A |
4494447 | Sisk | Jan 1985 | A |
4573880 | Hirano | Mar 1986 | A |
4850313 | Gibbons | Jul 1989 | A |
4873951 | Garthwaite | Oct 1989 | A |
4988269 | Blass | Jan 1991 | A |
5152677 | Bauer | Oct 1992 | A |
5203228 | Miyawaki | Apr 1993 | A |
5326231 | Pandeya | Jul 1994 | A |
5328338 | Hirano | Jul 1994 | A |
5733108 | Rifle | Mar 1998 | A |
5762479 | Baars et al. | Jun 1998 | A |
5846059 | Mizuno | Dec 1998 | A |
5881631 | Ryu | Mar 1999 | A |
5950579 | Ott | Sep 1999 | A |
5957667 | Epp | Sep 1999 | A |
6190137 | Robbins | Feb 2001 | B1 |
6409481 | Brabek | Jun 2002 | B1 |
6641374 | Kim | Nov 2003 | B2 |
6684755 | Boyd | Feb 2004 | B2 |
6692239 | Nishikawa | Feb 2004 | B2 |
6832900 | Leu | Dec 2004 | B2 |
7210912 | Tomell | May 2007 | B2 |
7396219 | Berwanger | Jul 2008 | B2 |
7422423 | Kawabata | Sep 2008 | B2 |
8113797 | Valbjoern | Feb 2012 | B2 |
8435013 | Kondou | May 2013 | B2 |
8800306 | Schoenoff et al. | Aug 2014 | B2 |
9097249 | Petersen | Aug 2015 | B2 |
20040026201 | Imasaka et al. | Feb 2004 | A1 |
20040156731 | Bond et al. | Aug 2004 | A1 |
20040191094 | Kojima | Sep 2004 | A1 |
20050069431 | Leu | Mar 2005 | A1 |
20050106037 | Kim et al. | May 2005 | A1 |
20070098580 | Petersen | May 2007 | A1 |
20090174741 | Nagata et al. | Jul 2009 | A1 |
20100034676 | Kang et al. | Feb 2010 | A1 |
20120023973 | Mayorca | Feb 2012 | A1 |
Number | Date | Country |
---|---|---|
9600527 | Dec 1997 | BR |
2431298 | Dec 2003 | CA |
1769674 | May 2006 | CN |
2007135152 | Nov 2007 | NO |
Entry |
---|
International Search Report for PCT/BR2010/000008, English Translation and original attached together, Completed by the Brazilian Patent Office dated Apr. 16, 2010, 8 Pages all together. |
Number | Date | Country | |
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20160281701 A1 | Sep 2016 | US |
Number | Date | Country | |
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Parent | 13143869 | US | |
Child | 15174573 | US |