US2809872A - Lubricating bearings of refrigerator compressor - Google Patents
Lubricating bearings of refrigerator compressor Download PDFInfo
- Publication number
- US2809872A US2809872A US479803A US47980354A US2809872A US 2809872 A US2809872 A US 2809872A US 479803 A US479803 A US 479803A US 47980354 A US47980354 A US 47980354A US 2809872 A US2809872 A US 2809872A
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- United States
- Prior art keywords
- thrust plate
- impeller
- plate facing
- hole
- oil
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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- 230000001050 lubricating effect Effects 0.000 title description 6
- 239000003921 oil Substances 0.000 description 36
- 238000005461 lubrication Methods 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 4
- 238000005266 casting Methods 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 239000003507 refrigerant Substances 0.000 description 3
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical group [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000010687 lubricating oil Substances 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 238000005057 refrigeration Methods 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- 239000000725 suspension Substances 0.000 description 2
- 101150006573 PAN1 gene Proteins 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B31/00—Compressor arrangements
- F25B31/002—Lubrication
Definitions
- This invention relates generally to lubricating bearings of motor-compressor units, and more specifically to an improved hermetic motor-compressor unit for use in a refrigeration system wherein the motor is of the axial air-gap type.
- This application is a division of an original application by the same inventor, filed July 16, 1953, Serial No. 368,293, and entitled Refrigerator Compressor.
- One of the objects of the invention is the provision of improved structure for the lubrication of the bearings of motor compressor unit.
- Fig. 1 is a cross sectional view taken through the motor compressor on a plane passing through the axis of its shaft.
- Fig. 2 is an exploded view of the parts of a combination oil pump and thrust bearing.
- the motor and the compressor are mounted within a casing comprising a lower pan and an upper pan 11. These two pans are substantially bowl-shaped and are sealed at the edges thereof to form a hermetic casing.
- the axial air-gap motor comprises substantially the lower half of the structure shown therein and the compressor comprises substantially the upper half of the structure shown therein.
- the motor is generally designated with the character 13 and the compressor is generally designated with the character 12.
- the motor is generally mounted within and supported by a substantially bowl-shaped stator support frame 14, and the compressor 12 is generally mounted within and supported by a substantially bowl-shaped crankcase 15.
- crankcase 15 and the stator support frame 14 are rigidly connected together by three bolts 16, which project through three holes 17 provided in the periphery of the crankcase 15, and which are threaded into three tapped holes 18 in the periphery of the stator support frame 14.
- the three bolts 16 are triangularly disposed to each other as can be easily seen in Figure 1.
- a spring hook 19 is attached to the top of the crankcase 15 by the bolt 16, as can be seen in Figure 1.
- Two other spring hooks 19 are provided which are mounted to the crankcase 15 by the other two bolts 16. It is intended that the unit be mounted longitudinally in a horizontal plane with the compressor portion 12 disposed above the motor portion 13.
- the internal assembly is resilientlysuspended by three suspension members 20.
- Each of these suspension members 20 comprises a mounting element 21, a coiled spring 22, and a spring hanger 23.
- the mounting element is connected to the underside of the upper pan 11.
- the spring hanger 23 is rigidly con nected.
- the spring hanger 23 is generally cone-shaped, and the portion thereof which is adjacent to the mounting element 21, has a number of threads formed thereon which are complementary to the turns of the coiled spring 22.
- the upper end of the coiled spring 22 is mounted over and threaded onto the spring hanger 23.
- the lower portion of the coiled spring 22 is formed to have a hook thereon. This hook is mounted in cooperation with the spring hook 19 to thereby resiliently suspend the motorcompressor unit within the casing.
- the effective length of the coiled spring 22 may be increased or decreased by threading and unthreading the coiled spring 22 on the spring hanger 23 in increments of
- a quantity of lubricating oil is provided.
- the lubricating oil 24 is disposed within the lower pan 10 as can be easily seen in Figure 2, and the amount used is that amount sufficient to substantially submerge the motor 13.
- the motor 13 will be described in detail first; As previously noted, the motor is generally supported and contained within a bow-shaped stator support frame 14.
- the stator 25 is rigidly connected to the concave side of the stator support frame 14 by means of bolts 26.
- the stator 25 includes the field windings 9 which are connected to a cable 8.
- the cable 8 is in turn connected without the lower pan 10 by the terminal assembly 17.
- a hearing 27 is provided through the center of the stator support frame 14, and within this bearing 27 the crankshaft 28 is rotatively mounted.
- the center portion of the convex side of the stator support frame 14 is generally formed with a depression therein.
- the tip of the crankshaft 28 projects into this depression and a number of holes 29 are formed through the stator support frame 14 from the concave side thereof into the depression.
- the depression is enclosed by the oil pump and thrust bearing means which are shown generally with the character 30.
- the portion 31 of the depression of the stator support frame 14 is formed with an involute'curve.
- the rotor for the motor is shown generally with the character 32.
- the portion of the crankshaft 28 which cooperates with the rotor 32 is shaped to have a hub 34 and a ring 35.
- the hub 34 and the ring 35 are tapped for four bolts 36.
- the rotor 32 is mounted over the hub 34 and against the ring 35 with a light press fit.
- the major proportion of the rotor 32 is fabricated as a continuous strip of steel wound in a roll and integrally cast with two rings of aluminum and with aluminum bars passing through the steel.
- the roll of steel 37 has radial holes about its periphery and upon casting the aluminum completely fills these holes to form an integral part with v the roll of steel.
- the inner aluminum ring is tapered as shown at 38.
- the complete assembly of the rotor also comprises a rotor support disk 39 and a spacer ring 40.
- the rotor support disk 39 has four holes therethrough which are aligned for cooperation with the bolts 36.
- the oil pump and thrust bearing 30 comprises the impeller retainer 44, the impeller'45, the thrust plate facing 46, and the plate 47.
- the crankshaft 28 is formed with a hole 42 extending axially therethrough.
- the crankshaft 28 is further formed to have two notches 43 formed at the one end thereof which is disposed within the depression formed within the convex surface of the stator support frame 14.
- the impeller retainer 44 is formed of a rectan'gularly shaped material with two prongs extending upward therefrom. The two prongs of the impeller retainer 44 are pressed into the two notches 43 on the end of the crankshaft 28 to thereby maintain the impeller retainer 44 thereagainst.
- the impeller retainer 44 also has a hole through the center thereof and this hole cooperates with the bore 42 in the crankshaft 23.
- the impeller 45 is generally circular in shape, and has a plurality of vanes extending from the circular surface thereof, as can easily be seen in Figure 3.
- the impeller 45 is mounted in cooperation with the impeller retainer 44 so that the edges of the impeller retainer 44 are pressed between the vanes of the impeller 45.
- the impeller 45 also has a hole formed through the center thereof which cooperates with the hole through the center of the impeller retainer 44 and the bore 42 of the crankshaft 2.8.
- the impeller 45 when so mounted operatively cooperates with the involute curve formed within portion 31 of the depression on the convex side of the stator support frame 14, so that any liquid fed centrally of the impeller 45, when the crankshaft 28 is rotating, will be forced outwardly from the vanes of the impeller 45 and in the involute curve.
- the thrust plate facing 46 which is formed of a hard metal, and the thrust plate 47 are mounted together and rigidly connected over the depression in the convex side of the stator support frame 14. The thrust plate facing 46 is mounted between the thrust plate 47 and the stator support frame 14.
- the thrust plate facing 46 and the thrust plate 47 are rigidly mounted over the depression on the convex side of the stator support frame 14 by four bolts 48 which project through four holes in the thrust plate facing 46 and the thrust plate 47, and are threaded into four tapped holes in the stator support frame 14.
- the thrust plate facing 46 is further formed to have four holes 49 formed therethrough, and these holes 49 are positioned beneath the vanes of the impeller 45.
- the thrust plate facing 46 is further formed to have four slots 50 formed therethrough'. The four slots 50 intersect each other at an opening in the center of the thrust plate facing 46, as can easily be seen in Figure 3. These slots 50 are positioned beneath the circular flat portion of the impeller 45.
- the thrust plate 47 has four channels 51 formed therein.
- These channels 51 which are substantially wider than the slots 50, and which may easily be seen in Figure 3, are so positioned as to intersect at an opening in the center thereof.
- Each of the slots 51 are formed of a length equal to the length of each of the slots 50 plus the distance from the end of each of the slots 50 to the outermost side of the holes 49.
- the slots 50 of the thrust plate facing 46 are not centered directly above the channels 51 in the thrust plate 47, but are positioned off-center thereof in a direction dependent upon the direction of rotation of the impeller 45.
- each of the slots 50 would be the, leading edge of these slots and the side 53 of each of these slots would be the trailing edge of these slots.
- the slots 50 are then positioned in relation to the channels 51 so that the leading edge of each of the slots 50 is positioned upon the center line of each of the channels 51.
- the leading edges of each of the slots 50 overhang the channels 51 a substantially greater amount than do the trailing edges of each of the slots 50.
- the rotating impeller 45 will move the oil radially thereof into the vanes thereof. From the vanes of the impeller 45, the oil will flow downward through each of the openings 49 in the thrust plate facing From the opening 49, the oil will flow into and through the channels 51 of the thrust plate 47. From the channels 51 of the thrust plate 47, a portion of the oil will flow upward through the center thereof, through the center of the thrust plate facing 46, through the hole in the center of the impeller 45, through the hole in the center of the impeller retainer 44 and into and through the bore 42 of the crankshaft 28. Another portion of the oil flowing through the channels 51 will flow upward through the slots 50 to lubricate the thrust bearing previously described.
- crankcase 15 comprises a substantially bow-shaped casting, which as previously described is mounted to the peripheral edge of the stator support frame 14 by the bolts 16. To further aid in the alignment of the crankcase 15 with the stator support frame 14, three dowels 55 are provided.
- a bearing 56 is formed through the center of the crankcase 15 as can easily be seen in Figures 1 and 2.
- the bearing 56 supports the upper end of the crankshaft 23.
- the bore 42 extends upwardly through the crankshaft 28 and near the upper end thereof is formed to slant away from the axis of rotation of said crankshaft 28 as can be seen in Figure 1.
- crankshaft 28 When the crankshaft 28 is rotated by the motor 13, the oil which flows from the oil pump 30 upward through the crankshaft 28 and out of the top thereof is given a lateral component of motion. Thus as the crankshaft 28 rotates, the oil is sprayed. about the inner surface of the upper pan 11 and will then flow downward along the inner walls of the casing to the lower pan 11. As the oil flows along the inner surfaces of the casing, heat from the oil will be conducted to the casing, thereby cooling the oil.
- the crankshaft 28 is further provided with an eccentric 57 formed as a part thereof. A channel 53 is formed through the eccentric 57 to the bore 42 of the crankshaft 28 to provide lubrication for the eccentric 5'7.
- a further channel 59 is formed radially from the bore 42 to the outer surface of the crankshaft 28 which is disposed within the bearing 56.
- the oil flowing through the channel 59 serves to lubricate the bearing 56 and the cylinder 60.
- the specific structure cooperating with the channel 59 to provide lubrication for the cylinder 60 includes a depression 61 formed in the upper surface of the crankcase 15, and two holes 62 and 63.
- the hole 62 is formed in the crankcase 15 from an upper portion of the depression 61 into the bearing 56 and in vertical alignment with the channel 59.
- the hole 63 is formed through the crankcase 15 from the lowest portion of the depression 61 downward into the cylinder 60.
- crankshaft 28 Whenever the crankshaft 28 is rotated to the position wherein the channel 59 is in horizontal alignment with the hole 62, oil flowing upward through the bore 42 will flow through the channel 59, through the hole 62 into and filling the depression 61. From the depression 61 the oil will flow downward through the hole 63 into the cylinder 60.
- the cylinder 60 is cast as an integral portion of the crankcase 15 on the concave side thereof as can be easily seen in Figure 2.
- the cylinder 60 is further formed so that the longitudinal axis thereof is at a right angle to the axis of rotation of the crankshaft 28.
- a piston 64 is slidably mounted within the cylinder 60.
- a connecting rod 65 is rotatively mounted about the eccentric 57 and is pivotally connected to the piston 64 by a wrist-pin 66, as can be easily seen in Figure 2. It can thus be seen that as themotor 13 is operated to rotate the shaft 28, the
- a cylinder head 67 is mounted over the cylinder. 64) in cooperation with the piston 64.
- the cylinder head 67 is mounted to the crankcase by means of the bolts 68.
- intake and exhaust valves 69 are mounted within the cylinder head 67. These valves may be of any type well known in the art, and therefore the construction thereof will not be described in detail.
- the crankcase 15 is further provided with two muumbler chambers 70 and 71.
- muffler chambers 7b and 71 are cast as integral parts of the crankcase 15, the muffler chamber 79 serving as an intake muffler and the mufller chamber 71 serving as an exhaust mufiler.
- a hole 72 in the top of the mufiler chamber 70 is provided when the crankcase 15 is cast to aid in the casting thereof. This hole 72 is sealed by a plug '73.
- a hole 7d is formed through an end wall of the muftler chambers 71 to aid in the casting thereof and to serve as an outlet from the muffler chamber 71.
- An opening 75 is formed through one wall of the mulfier chamber 76.
- This hole 75 is formed on the concave side of the crankcase 15, so that refrigerant gases are drawn into the murller chamber 70 through the hole 75, from the concave side of the crankcase 15, from the open spaces about the periphery of and between the crankcase 15 and the stator support frame 14, and from a tube 76 connected through the upper pan ill of the casing.
- Any refrigerant gases which enter the muffler chamber 78 are delivered to the cylinder head 67 and the cylinder 65 through a channel 7'7 formed through the crankcase 15 from the muffler chamber 76 to the cylinder head 67.
- the exhaust mutller chamber 71 is connected to the cylinder head 67 and the cylinder so by means of a channel '78 extending from the exhaust muffler chamber 71 to the cylinder head 67.
- An exhaust mufiier chamber cover '79 is provided over the opening '74 of the exhaust muffler chamber 71.
- a length of tubing 8i) is connected to the exhaust muffler chamber cover 79. This length of tubing 8d extends from the exhaust mulller chamber cover '79 about the inside of the upper pan ll in one complete turn, and is then connected without the upper pan if by means of the tube b2.
- a bolt 53 extends through the exhaust mufiler chamber cover 7% to maintain the exhaust mui'ller chamber cover '79 against the opening '74.
- This bolt 83 is threaded into a tapped hole in the crankcase 15.
- a specific counterweight 84 is provided.
- a plan view of the counterweight 84 can be seen in Figure 5, and a cross-sectional view thereof, taken along the line 2l2 of Figure 1, can be seen in Figure 2.
- the counterweight 34 is formed in the general shape of a semi-circular ring.
- the lower portion of the inner periphery of the counterweight 84 is formed with a bevel 85 as can be seen in Figure 2.
- the crankshaft 928 is further shaped to have a circular beveled portion 33.
- the bevel 85 of the counterweight 84 matches the beveled portion 3h of the crankshaft 28.
- the outer periphery of the counterweight 84- is formed with two slots 3d therein.
- slots 86 are spaced apart a distance equal to the spacing between two of the bolts 36 which maintain the rotor 32 mounted to the crankshaft 28.
- the counterweight 84' is further pro vided with 'a counterbored hole 87. Further, a portion of the hub 34, between the aforementioned two bolts 36, is tapped so that a .bolt 88 may be projected through the hole 87 and threaded thereinto.
- a bearing element a bored shaft rotatively mounted within said bearing element, a thrust plate, a thrust plate facing, said thrust plate facing and said thrust plate mounted over one end of said bearing element with said thrust plate facing positioned between said thrust plate and said one end of said bearing element, whereby an enclosed space is defined by'one end of said shaft, said bearing element and said thrust plate facing, an impeller having a hole in the center thereof, said impeller connected to the end of said shaft within said enclosed space and projecting against said thrust plate facing, said hole in said impeller cooperating with said bore, means for supplying oil to said enclosed space so that said oil is caused to move radially of said impeller when said shaft is rotated, said thrust plate facing having a plurality of openings therethrough positioned radially of said impeller and a plurailty' of intersecting slots therethrough, said plurality of slots intersecting in the center of said thrust plate facing so that said intersection of said slots cooperates with said hole in said impeller, said thrust plate being formed to have
- a bearing element a bored shaft rotatively mounted within said bearing element, a thrust plate, a thrust plate facing, said thrust plate facing and said thrust plate mounted over one end of said bearing element with said thrust plate facing positioned between said thrust plate and said one end of said bearing element, whereby an enclosed space is defined by one end of said shaft, said bearing element and said thrust plate facing, a casing, a quantity of oil disposed within said casing, said bearing element submerged within said oil, an impeller having a hole in the center thereof, said impeller connected to the end of said shaft within said enclosed space and abutting against said thrust plate facing, said hole in, said impeller.
- said bearing element further formed to have at least one hole formed therethrough into said enclosed space so that said oil enters said enclosed space through said hole in said bearing element, and so that said oil is caused to move radially of said impeller when said shaft is rotated
- said thrust plate facing having openings therethrough positioned radially of said impeller and a center opening therethrough cooperating with said hole in said impeller
- said thrust plate having radial channels positioned therein, each of said channels further positioned so that one end thereof cooperates with one of said openings in said thrust plate facing and so that the other end thereof cooperates with said center opening in said thrust plate facing, so that said oil which is moved radially of said impeller will flow into said openings in said thrust plate facing, through said channels, through said center opening in said thrust plate facing, and through said hole in said impeller and said bore.
- a bearing element a bored shaft rotatively mounted within said hearing element, a thrust plate, a thrust plate facing, said thrust plate facing and said thrust plate mounted over one end of said bearing element with said thrust plate facing positioned between said thrust plate and said one end of said bearing element, whereby an enclosed space is defined by one end of said shaft, said bearing element and said thrust plate facing, said bearing element further formed to have an involute on the portion thereof disposed within said enclosed space and radially about said shaft, a circular impeller having a hole in the center thereof, said impeller formed to having a plurality of said bearing element and with said circular portion of said impeller abutting against said thrust plate facing, said hole in said impeller cooperating with said bore, means for supplying oil to said' enclosed space so that said oil is caused to move radially of said impeller when said shaft is rotated, said thrust plate facing having openings formed therethrough and positioned radially of said impeller and a center opening formed therethrough cooperating with said hole in said imp
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Description
LUBRICATING BEARING OF REFRIGERATOR COMPRESSOR Original Filed July 16, 1953 2 Sheets-Sheet 1 Z7 Z%72f071' flilfan K Warner Oct. 15, 1957 Y. WARNER 2,809,372 LUBRIC ATING BEARING OF REFRIGERATOR COMPRESSOR Original Filed July 16, 1953 2 Sheets-Sheet 2 I Z7 2?/72i0r.' 6%2'25072 Y Warner v United States Patent LUBRICATING BEARlN GS 0F REFRIGERATOR COMPRESSOR Milton Y. Warner, Evansville, Ind., assignor, by mesne assignments, to Whirlpool-Seeger Corporation, a corporation of Delaware Original application July 16, 1953, Serial No. 368,293. Divided and this application December 1, 1954, Serial No. 479,803
3 Claims. (Cl. 308--172) This invention relates generally to lubricating bearings of motor-compressor units, and more specifically to an improved hermetic motor-compressor unit for use in a refrigeration system wherein the motor is of the axial air-gap type. This application is a division of an original application by the same inventor, filed July 16, 1953, Serial No. 368,293, and entitled Refrigerator Compressor.
One of the objects of the invention is the provision of improved structure for the lubrication of the bearings of motor compressor unit.
It is another feature of this invention that a novel arrangement is provided for lubricating the cylinder of the compressor portion of the unit.
Other objects and features of the present invention will be apparent upon a perusal of the following specification and drawings of which:
Fig. 1 is a cross sectional view taken through the motor compressor on a plane passing through the axis of its shaft.
Fig. 2 is an exploded view of the parts of a combination oil pump and thrust bearing.
The present embodiment is the preferred embodiment, but it is to be understood that changes can be made in the present embodiment by one skilled in the art without departing from the spirit and scope of this invention.
Generally, the motor and the compressor are mounted within a casing comprising a lower pan and an upper pan 11. These two pans are substantially bowl-shaped and are sealed at the edges thereof to form a hermetic casing. Referring to Figure 1, the axial air-gap motor comprises substantially the lower half of the structure shown therein and the compressor comprises substantially the upper half of the structure shown therein. The motor is generally designated with the character 13 and the compressor is generally designated with the character 12. The motor is generally mounted within and supported by a substantially bowl-shaped stator support frame 14, and the compressor 12 is generally mounted within and supported by a substantially bowl-shaped crankcase 15. The crankcase 15 and the stator support frame 14 are rigidly connected together by three bolts 16, which project through three holes 17 provided in the periphery of the crankcase 15, and which are threaded into three tapped holes 18 in the periphery of the stator support frame 14. The three bolts 16 are triangularly disposed to each other as can be easily seen in Figure 1. A spring hook 19 is attached to the top of the crankcase 15 by the bolt 16, as can be seen in Figure 1. Two other spring hooks 19 are provided which are mounted to the crankcase 15 by the other two bolts 16. It is intended that the unit be mounted longitudinally in a horizontal plane with the compressor portion 12 disposed above the motor portion 13. The internal assembly is resilientlysuspended by three suspension members 20. Each of these suspension members 20 comprises a mounting element 21, a coiled spring 22, and a spring hanger 23. The mounting element is connected to the underside of the upper pan 11. To the mounting element 21, the spring hanger 23 is rigidly con nected. The spring hanger 23 is generally cone-shaped, and the portion thereof which is adjacent to the mounting element 21, has a number of threads formed thereon which are complementary to the turns of the coiled spring 22. Thus the upper end of the coiled spring 22 is mounted over and threaded onto the spring hanger 23. The lower portion of the coiled spring 22 is formed to have a hook thereon. This hook is mounted in cooperation with the spring hook 19 to thereby resiliently suspend the motorcompressor unit within the casing. Since the coiled spring 22 is threaded onto the spring hanger 23, it may easily be seen that the effective length of the coiled spring 22 may be increased or decreased by threading and unthreading the coiled spring 22 on the spring hanger 23 in increments of For lubrication and cooling of the unit a quantity of lubricating oil is provided. The lubricating oil 24 is disposed within the lower pan 10 as can be easily seen in Figure 2, and the amount used is that amount sufficient to substantially submerge the motor 13.
The motor 13 will be described in detail first; As previously noted, the motor is generally supported and contained within a bow-shaped stator support frame 14. The stator 25 is rigidly connected to the concave side of the stator support frame 14 by means of bolts 26. The stator 25 includes the field windings 9 which are connected to a cable 8. The cable 8 is in turn connected without the lower pan 10 by the terminal assembly 17. A hearing 27 is provided through the center of the stator support frame 14, and within this bearing 27 the crankshaft 28 is rotatively mounted. The center portion of the convex side of the stator support frame 14 is generally formed with a depression therein. The tip of the crankshaft 28 projects into this depression and a number of holes 29 are formed through the stator support frame 14 from the concave side thereof into the depression. The depression is enclosed by the oil pump and thrust bearing means which are shown generally with the character 30. The portion 31 of the depression of the stator support frame 14 is formed with an involute'curve.
The rotor for the motor is shown generally with the character 32. The portion of the crankshaft 28 which cooperates with the rotor 32 is shaped to have a hub 34 and a ring 35. The hub 34 and the ring 35 are tapped for four bolts 36. The rotor 32 is mounted over the hub 34 and against the ring 35 with a light press fit. The major proportion of the rotor 32 is fabricated as a continuous strip of steel wound in a roll and integrally cast with two rings of aluminum and with aluminum bars passing through the steel. The roll of steel 37 has radial holes about its periphery and upon casting the aluminum completely fills these holes to form an integral part with v the roll of steel. The inner aluminum ring is tapered as shown at 38. The complete assembly of the rotor also comprises a rotor support disk 39 and a spacer ring 40. The rotor support disk 39 has four holes therethrough which are aligned for cooperation with the bolts 36. When the rotor 32 is mounted to the crankshaft 28, the bolts 36 are tightened to cause the rotor support disk 39 to be bent against therotor spacer ring 40 and the bevel 38 of the inner aluminum ring of the rotor 32.
For a description of the oil pump and thrust bearing reference is made to Figures 2 and 3.. The oil pump and thrust bearing 30 comprises the impeller retainer 44, the impeller'45, the thrust plate facing 46, and the plate 47. The crankshaft 28 is formed with a hole 42 extending axially therethrough. The crankshaft 28 is further formed to have two notches 43 formed at the one end thereof which is disposed within the depression formed within the convex surface of the stator support frame 14. The impeller retainer 44 is formed of a rectan'gularly shaped material with two prongs extending upward therefrom. The two prongs of the impeller retainer 44 are pressed into the two notches 43 on the end of the crankshaft 28 to thereby maintain the impeller retainer 44 thereagainst. The impeller retainer 44 also has a hole through the center thereof and this hole cooperates with the bore 42 in the crankshaft 23. The impeller 45 is generally circular in shape, and has a plurality of vanes extending from the circular surface thereof, as can easily be seen in Figure 3. The impeller 45 is mounted in cooperation with the impeller retainer 44 so that the edges of the impeller retainer 44 are pressed between the vanes of the impeller 45. The impeller 45 also has a hole formed through the center thereof which cooperates with the hole through the center of the impeller retainer 44 and the bore 42 of the crankshaft 2.8. The impeller 45 when so mounted operatively cooperates with the involute curve formed within portion 31 of the depression on the convex side of the stator support frame 14, so that any liquid fed centrally of the impeller 45, when the crankshaft 28 is rotating, will be forced outwardly from the vanes of the impeller 45 and in the involute curve. The thrust plate facing 46 which is formed of a hard metal, and the thrust plate 47 are mounted together and rigidly connected over the depression in the convex side of the stator support frame 14. The thrust plate facing 46 is mounted between the thrust plate 47 and the stator support frame 14. The thrust plate facing 46 and the thrust plate 47 are rigidly mounted over the depression on the convex side of the stator support frame 14 by four bolts 48 which project through four holes in the thrust plate facing 46 and the thrust plate 47, and are threaded into four tapped holes in the stator support frame 14. The thrust plate facing 46 is further formed to have four holes 49 formed therethrough, and these holes 49 are positioned beneath the vanes of the impeller 45. The thrust plate facing 46 is further formed to have four slots 50 formed therethrough'. The four slots 50 intersect each other at an opening in the center of the thrust plate facing 46, as can easily be seen in Figure 3. These slots 50 are positioned beneath the circular flat portion of the impeller 45. The thrust plate 47 has four channels 51 formed therein. These channels 51, which are substantially wider than the slots 50, and which may easily be seen in Figure 3, are so positioned as to intersect at an opening in the center thereof. Each of the slots 51 are formed of a length equal to the length of each of the slots 50 plus the distance from the end of each of the slots 50 to the outermost side of the holes 49. The slots 50 of the thrust plate facing 46 are not centered directly above the channels 51 in the thrust plate 47, but are positioned off-center thereof in a direction dependent upon the direction of rotation of the impeller 45. Assuming for purposes of explanation that the impeller 45 is rotating in a counterclockwise direction as viewed in Figure 3, then the side 54 of each of the slots 50 would be the, leading edge of these slots and the side 53 of each of these slots would be the trailing edge of these slots. The slots 50 are then positioned in relation to the channels 51 so that the leading edge of each of the slots 50 is positioned upon the center line of each of the channels 51. Thus the leading edges of each of the slots 50 overhang the channels 51 a substantially greater amount than do the trailing edges of each of the slots 50. Thus when the motor 13 is operating, the thrust exerted by the crankshaft 28, due to the magnetic attraction between the rotor 37 and the stator 25, will be distributed throughout the area between the impeller 45 and the thrust plate facing 46, and the thrust plate facing 46 will act as thrust shoe. Now if oil is supplied to the channels 51, a wedgeshaped film of oil will be formed between the trailing and leading edges of the slots 50 as the crankshaft 28 is rotating. This will result in a lubrication of the thrust bearing similar to that supplied by the well known Kingsbury thrust bearing. To discuss the operation of the oil pump, when the crankshaft 23 is rotating, the oil 24 disposed within the lower pan 1% will flow into and through the holes 29 in the stator support frame 14. This oil will flow into the space centrally of the impeller 45. The rotating impeller 45 will move the oil radially thereof into the vanes thereof. From the vanes of the impeller 45, the oil will flow downward through each of the openings 49 in the thrust plate facing From the opening 49, the oil will flow into and through the channels 51 of the thrust plate 47. From the channels 51 of the thrust plate 47, a portion of the oil will flow upward through the center thereof, through the center of the thrust plate facing 46, through the hole in the center of the impeller 45, through the hole in the center of the impeller retainer 44 and into and through the bore 42 of the crankshaft 28. Another portion of the oil flowing through the channels 51 will flow upward through the slots 50 to lubricate the thrust bearing previously described.
To discuss the detailed structure of the compressor 12 reference is made to Figures 1 and 2. The crankcase 15 comprises a substantially bow-shaped casting, which as previously described is mounted to the peripheral edge of the stator support frame 14 by the bolts 16. To further aid in the alignment of the crankcase 15 with the stator support frame 14, three dowels 55 are provided. A bearing 56 is formed through the center of the crankcase 15 as can easily be seen in Figures 1 and 2. The bearing 56 supports the upper end of the crankshaft 23. The bore 42 extends upwardly through the crankshaft 28 and near the upper end thereof is formed to slant away from the axis of rotation of said crankshaft 28 as can be seen in Figure 1. Thus when the crankshaft 28 is rotated by the motor 13, the oil which flows from the oil pump 30 upward through the crankshaft 28 and out of the top thereof is given a lateral component of motion. Thus as the crankshaft 28 rotates, the oil is sprayed. about the inner surface of the upper pan 11 and will then flow downward along the inner walls of the casing to the lower pan 11. As the oil flows along the inner surfaces of the casing, heat from the oil will be conducted to the casing, thereby cooling the oil. The crankshaft 28 is further provided with an eccentric 57 formed as a part thereof. A channel 53 is formed through the eccentric 57 to the bore 42 of the crankshaft 28 to provide lubrication for the eccentric 5'7. A further channel 59 is formed radially from the bore 42 to the outer surface of the crankshaft 28 which is disposed within the bearing 56. The oil flowing through the channel 59 serves to lubricate the bearing 56 and the cylinder 60. The specific structure cooperating with the channel 59 to provide lubrication for the cylinder 60 includes a depression 61 formed in the upper surface of the crankcase 15, and two holes 62 and 63. The hole 62 is formed in the crankcase 15 from an upper portion of the depression 61 into the bearing 56 and in vertical alignment with the channel 59. The hole 63 is formed through the crankcase 15 from the lowest portion of the depression 61 downward into the cylinder 60. Whenever the crankshaft 28 is rotated to the position wherein the channel 59 is in horizontal alignment with the hole 62, oil flowing upward through the bore 42 will flow through the channel 59, through the hole 62 into and filling the depression 61. From the depression 61 the oil will flow downward through the hole 63 into the cylinder 60. The cylinder 60 is cast as an integral portion of the crankcase 15 on the concave side thereof as can be easily seen in Figure 2. The cylinder 60 is further formed so that the longitudinal axis thereof is at a right angle to the axis of rotation of the crankshaft 28. A piston 64 is slidably mounted within the cylinder 60. A connecting rod 65 is rotatively mounted about the eccentric 57 and is pivotally connected to the piston 64 by a wrist-pin 66, as can be easily seen in Figure 2. It can thus be seen that as themotor 13 is operated to rotate the shaft 28, the
piston'64 will operate within thecylinder 60, and oil will flow from the hole 63 to'lubricate the piston 64 and the cylinder 60. A cylinder head 67 is mounted over the cylinder. 64) in cooperation with the piston 64. The cylinder head 67 is mounted to the crankcase by means of the bolts 68. Within the cylinder head 67 intake and exhaust valves 69 are mounted. These valves may be of any type well known in the art, and therefore the construction thereof will not be described in detail. The crankcase 15 is further provided with two muiiler chambers 70 and 71. These muffler chambers 7b and 71 are cast as integral parts of the crankcase 15, the muffler chamber 79 serving as an intake muffler and the mufller chamber 71 serving as an exhaust mufiler. A hole 72 in the top of the mufiler chamber 70 is provided when the crankcase 15 is cast to aid in the casting thereof. This hole 72 is sealed by a plug '73. A hole 7d is formed through an end wall of the muftler chambers 71 to aid in the casting thereof and to serve as an outlet from the muffler chamber 71. An opening 75 is formed through one wall of the mulfier chamber 76. This hole 75 is formed on the concave side of the crankcase 15, so that refrigerant gases are drawn into the murller chamber 70 through the hole 75, from the concave side of the crankcase 15, from the open spaces about the periphery of and between the crankcase 15 and the stator support frame 14, and from a tube 76 connected through the upper pan ill of the casing. Any refrigerant gases which enter the muffler chamber 78 are delivered to the cylinder head 67 and the cylinder 65 through a channel 7'7 formed through the crankcase 15 from the muffler chamber 76 to the cylinder head 67. The exhaust mutller chamber 71 is connected to the cylinder head 67 and the cylinder so by means of a channel '78 extending from the exhaust muffler chamber 71 to the cylinder head 67. An exhaust mufiier chamber cover '79 is provided over the opening '74 of the exhaust muffler chamber 71. To the exhaust muffler chamber cover 79, a length of tubing 8i) is connected. This length of tubing 8d extends from the exhaust mulller chamber cover '79 about the inside of the upper pan ll in one complete turn, and is then connected without the upper pan if by means of the tube b2. A bolt 53 extends through the exhaust mufiler chamber cover 7% to maintain the exhaust mui'ller chamber cover '79 against the opening '74. This bolt 83 is threaded into a tapped hole in the crankcase 15.
To next describe the operation of the compressor f2, when connected in a refrigeration system, (not shown) refrigerant gases are drawn into the tube 76 between the peripheral edges of the crankcase 15 and the stator support frame 14, within the concave side of the crankcase 15, into and through the hole 75, into the intake muffler chamber 78, through the tube 77, into the cylinder head 67 and the cylinder as, through the cylinder head 67 into and through the tube '78, into the muffler chamber 71, through the hole 74 into the exhaust muifier chamber cover 79, through the tubing 3t? and out of the unit through the length of tubing 82.
To balance the crankshaft 28, a specific counterweight 84 is provided. A plan view of the counterweight 84 can be seen in Figure 5, and a cross-sectional view thereof, taken along the line 2l2 of Figure 1, can be seen in Figure 2. The counterweight 34 is formed in the general shape of a semi-circular ring. The lower portion of the inner periphery of the counterweight 84 is formed with a bevel 85 as can be seen in Figure 2. The crankshaft 928 is further shaped to have a circular beveled portion 33. The bevel 85 of the counterweight 84 matches the beveled portion 3h of the crankshaft 28. The outer periphery of the counterweight 84- is formed with two slots 3d therein. These slots 86 are spaced apart a distance equal to the spacing between two of the bolts 36 which maintain the rotor 32 mounted to the crankshaft 28. The counterweight 84'is further pro vided with 'a counterbored hole 87. Further, a portion of the hub 34, between the aforementioned two bolts 36, is tapped so that a .bolt 88 may be projected through the hole 87 and threaded thereinto. When the counterweight 84 is mounted to the crankshaft 28, the two bolts 36 are positioned within the two slots 36 and the bevel cooperates with the beveled portion 33, and as the bolt 88 is tightened, the counterweight 84 is forced downward and outward until the two bolts 36 are tightly wedged against the twoslots 86.
Having described the invention what is considered new and desired to be protected by Letters Patent is:
1. In a device of the class described, a bearing element, a bored shaft rotatively mounted within said bearing element, a thrust plate, a thrust plate facing, said thrust plate facing and said thrust plate mounted over one end of said bearing element with said thrust plate facing positioned between said thrust plate and said one end of said bearing element, whereby an enclosed space is defined by'one end of said shaft, said bearing element and said thrust plate facing, an impeller having a hole in the center thereof, said impeller connected to the end of said shaft within said enclosed space and projecting against said thrust plate facing, said hole in said impeller cooperating with said bore, means for supplying oil to said enclosed space so that said oil is caused to move radially of said impeller when said shaft is rotated, said thrust plate facing having a plurality of openings therethrough positioned radially of said impeller and a plurailty' of intersecting slots therethrough, said plurality of slots intersecting in the center of said thrust plate facing so that said intersection of said slots cooperates with said hole in said impeller, said thrust plate being formed to have a plurality of intersecting channels formed therein, said channels formed to intersect substantially at the center thereof so that said intersection of said channels cooperates with said intersection of said slots, said channels having a substantially greater width than said slots, each of said channels further positioned adjacent to one of said slots and having one edge of said slot in alignment with the center line of said channel, so that said oil when moved radially of said impeller will flow into said openings in said thrust plate facing, through said channels, into said slots, and between said impeller and said thrust plate facing to lubricate the area between said impeller and said thrust plate facing, and so that said oil will further flow through said intersection in said thrust plate, through said intersection in said thrust plate facing, through said hole in said impeller and through said bore.
2. In a device of the class described, a bearing element, a bored shaft rotatively mounted within said bearing element, a thrust plate, a thrust plate facing, said thrust plate facing and said thrust plate mounted over one end of said bearing element with said thrust plate facing positioned between said thrust plate and said one end of said bearing element, whereby an enclosed space is defined by one end of said shaft, said bearing element and said thrust plate facing, a casing, a quantity of oil disposed within said casing, said bearing element submerged within said oil, an impeller having a hole in the center thereof, said impeller connected to the end of said shaft within said enclosed space and abutting against said thrust plate facing, said hole in, said impeller. cooperating with said bore, said bearing element further formed to have at least one hole formed therethrough into said enclosed space so that said oil enters said enclosed space through said hole in said bearing element, and so that said oil is caused to move radially of said impeller when said shaft is rotated, said thrust plate facing having openings therethrough positioned radially of said impeller and a center opening therethrough cooperating with said hole in said impeller, said thrust plate having radial channels positioned therein, each of said channels further positioned so that one end thereof cooperates with one of said openings in said thrust plate facing and so that the other end thereof cooperates with said center opening in said thrust plate facing, so that said oil which is moved radially of said impeller will flow into said openings in said thrust plate facing, through said channels, through said center opening in said thrust plate facing, and through said hole in said impeller and said bore.
3. In a device of the class described, a bearing element, a bored shaft rotatively mounted within said hearing element, a thrust plate, a thrust plate facing, said thrust plate facing and said thrust plate mounted over one end of said bearing element with said thrust plate facing positioned between said thrust plate and said one end of said bearing element, whereby an enclosed space is defined by one end of said shaft, said bearing element and said thrust plate facing, said bearing element further formed to have an involute on the portion thereof disposed within said enclosed space and radially about said shaft, a circular impeller having a hole in the center thereof, said impeller formed to having a plurality of said bearing element and with said circular portion of said impeller abutting against said thrust plate facing, said hole in said impeller cooperating with said bore, means for supplying oil to said' enclosed space so that said oil is caused to move radially of said impeller when said shaft is rotated, said thrust plate facing having openings formed therethrough and positioned radially of said impeller and a center opening formed therethrough cooperating with said hole in said impeller, said thrust plate having radial channels positioned therein, each of said channels further positioned so that one end thereof cooperates with one of said openings in said thrust plate facing and so that the other end thereof cooperates with said center opening, so that said oil which is moved radially of said impeller will flow into said openings in said thrust plate facing, through said channels, through said center opening, and through said hole in said impeller and said bore.
References Cited in the file of this patent UNITED STATES PATENTS 2,500,751 Halfvarson Mar. 14, 1950
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US479803A US2809872A (en) | 1953-07-16 | 1954-12-01 | Lubricating bearings of refrigerator compressor |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US368293A US2797857A (en) | 1953-07-16 | 1953-07-16 | Refrigerator compressor |
| US479803A US2809872A (en) | 1953-07-16 | 1954-12-01 | Lubricating bearings of refrigerator compressor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2809872A true US2809872A (en) | 1957-10-15 |
Family
ID=27004125
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US479803A Expired - Lifetime US2809872A (en) | 1953-07-16 | 1954-12-01 | Lubricating bearings of refrigerator compressor |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2809872A (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1093387B (en) * | 1957-12-14 | 1960-11-24 | Linde S Eismaschinen Ag Zweign | Lubricating device for motor compressors of refrigeration machines of small and medium power using oil conveyor discs |
| US3154244A (en) * | 1955-06-24 | 1964-10-27 | Tecumseh Products Co | Lubrication of refrigeration compressors |
| US3211365A (en) * | 1961-10-16 | 1965-10-12 | Copeland Refrigeration Corp | Compressor structure |
| US3451615A (en) * | 1967-07-12 | 1969-06-24 | Tecumseh Products Co | Compressor lubricating system |
| US3491939A (en) * | 1968-05-07 | 1970-01-27 | Danfoss As | Vertical crankshaft for a motor compressor |
| US3664461A (en) * | 1971-03-31 | 1972-05-23 | Danfoss As | Oil pump for a motor compressor |
| US3922114A (en) * | 1974-07-19 | 1975-11-25 | Dunham Bush Inc | Hermetic rotary helical screw compressor with improved oil management |
| US4019342A (en) * | 1975-03-13 | 1977-04-26 | Cegedur Societe De Transformation De L'aluminium Pechiney | Compressor for a refrigerant gas |
| FR2549907A1 (en) * | 1983-07-25 | 1985-02-01 | Copeland Corp | HERMETIC REFRIGERATION COMPRESSOR |
| US20060013706A1 (en) * | 2003-03-14 | 2006-01-19 | Yoshinori Ishida | Compressor |
| US20120114504A1 (en) * | 2010-11-10 | 2012-05-10 | Hamilton Sundstrand Corporation | Vertical shaft pumping system |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2500751A (en) * | 1947-05-19 | 1950-03-14 | Westinghouse Electric Corp | Refrigeration apparatus |
-
1954
- 1954-12-01 US US479803A patent/US2809872A/en not_active Expired - Lifetime
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2500751A (en) * | 1947-05-19 | 1950-03-14 | Westinghouse Electric Corp | Refrigeration apparatus |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3154244A (en) * | 1955-06-24 | 1964-10-27 | Tecumseh Products Co | Lubrication of refrigeration compressors |
| DE1093387B (en) * | 1957-12-14 | 1960-11-24 | Linde S Eismaschinen Ag Zweign | Lubricating device for motor compressors of refrigeration machines of small and medium power using oil conveyor discs |
| US3211365A (en) * | 1961-10-16 | 1965-10-12 | Copeland Refrigeration Corp | Compressor structure |
| US3451615A (en) * | 1967-07-12 | 1969-06-24 | Tecumseh Products Co | Compressor lubricating system |
| DE1775061B1 (en) * | 1967-07-12 | 1971-10-14 | Tecumseh Products Co | CRANKSHAFT IN PARTICULAR FOR A COMPRESSOG ENGINE UNIT |
| US3491939A (en) * | 1968-05-07 | 1970-01-27 | Danfoss As | Vertical crankshaft for a motor compressor |
| US3664461A (en) * | 1971-03-31 | 1972-05-23 | Danfoss As | Oil pump for a motor compressor |
| US3922114A (en) * | 1974-07-19 | 1975-11-25 | Dunham Bush Inc | Hermetic rotary helical screw compressor with improved oil management |
| US4019342A (en) * | 1975-03-13 | 1977-04-26 | Cegedur Societe De Transformation De L'aluminium Pechiney | Compressor for a refrigerant gas |
| FR2549907A1 (en) * | 1983-07-25 | 1985-02-01 | Copeland Corp | HERMETIC REFRIGERATION COMPRESSOR |
| US20060013706A1 (en) * | 2003-03-14 | 2006-01-19 | Yoshinori Ishida | Compressor |
| US20120114504A1 (en) * | 2010-11-10 | 2012-05-10 | Hamilton Sundstrand Corporation | Vertical shaft pumping system |
| US8435016B2 (en) * | 2010-11-10 | 2013-05-07 | Hamilton Sundstrand Corporation | Vertical shaft pumping system with lubricant impeller arrangement |
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