Information
-
Patent Grant
-
6484847
-
Patent Number
6,484,847
-
Date Filed
Thursday, November 30, 200024 years ago
-
Date Issued
Tuesday, November 26, 200222 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 184 616
- 184 617
- 184 625
- 418 94
-
International Classifications
-
Abstract
A hermetic compressor assembly includes a compressor housing having a quantity of liquid lubricant therein. A compressor mechanism is provided within the compressor housing and a drive shaft is selectively rotatable and operably connected to the compressor mechanism. A liquid lubricant displacement element is engaged to the drive shaft and a support member is attached to the compressor housing. A pivotable magnetic member is provided between the liquid lubricant displacement element and the support member and includes a suction port provided therein. The liquid lubricant displacement element is in fluid communication with the quantity of liquid lubricant through the suction port in the magnetic member. At least a portion of any ferrous particles contained in the liquid lubricant are attracted to and retained by the magnetic member as the liquid lubricant is passed through the suction port of the magnetic member.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to hermetic compressors having positive displacement liquid lubricant pumps to supply liquid lubricant to bearing surfaces. More specifically, the present invention relates to compressors including liquid lubricant pumps having cavities disposed within the pump and drive shaft to trap debris by magnetic and centrifugal force.
2. Description of the Related Art
Compressor lubrication systems often include a positive displacement lubrication pump to supply liquid lubricant to bearing surfaces within the compressor. Liquid lubricant, or oil, often contains debris in the form of metallic particles circulating throughout the lubrication system. The particles detrimentally affect bearing surfaces by causing premature wear, and consequently, compressor performance is compromised. It is known to provide cartridge type or screen filters to capture debris, however an inherent disadvantage of cartridge and screen filters is that they clog and consequently block circulation of oil to bearing surfaces which significantly shortens the life of the compressor. Responsive to this clogged filter effect, compressor assemblies have been adapted with bypass valving, for example, which routes the oil around the filter when the filter becomes clogged to effectively maintain an adequate oil supply to the bearing surfaces. However, the circulating oil remains debris-laden which may cause an abrasive attack on the bearing surfaces resulting in bearing seizure and imminent failure of the compression mechanism.
Hermetic compressor assemblies are susceptible to oil-entrained debris, the most destructive being the fine powdered debris, which may not be captured by standard cartridge and filtering methods. The fine powders entrained in the oil are often composed of ferrous material which is attracted to a magnet. While previous compressor assemblies have utilized magnets to attract entrained metallic particles, these compressors have proven to do so inefficiently. Typically, magnets are randomly placed within the interior of the compressor housing, producing marginal particle accumulation performance. Therefore, the marginal benefits provided by these types of compressors, in view of the substantial costs associated with installing magnets to attract ferrous particles, have limited their practicality.
Further, with evolving and more demanding environmental standards, the hydrocarbon based oils and refrigerants traditionally used are yielding to environmental friendly substitutes. However, it is not fully understood whether these substitute lubricants are equally effective in providing comparable levels of lubrication and durability to the compressor mechanism. Thus, improving the ability to remove foreign particles from liquid lubricant, without a substantial compressor assembly cost increase, would be highly desirable.
Yet another problem associated with the use of impeller type pumps in compressor assemblies is one of drive shaft misalignment, relative to the pump housing, during the assembly process. Traditionally, misalignment of the drive shaft and pump housing was avoided by providing the pump housing, compressor mechanism assembly and impeller pump assembly with precise tolerances. A significant labor and handling cost is associated with parts having precise tolerances. What is desired is an impeller type pump assembly structure which requires significantly less labor to manufacture and assemble compared to previously employed structures.
An inexpensive oil pump assembly which includes the ability to trap debris suspended in the oil while continuously providing an ample supply of oil to bearing surfaces is highly desired. Further, an oil pump assembly which provides further cost reduction attributable to avoiding precise part tolerances in preventing drive shaft and pump housing misalignment is desired.
SUMMARY OF THE INVENTION
The present invention overcomes the disadvantages of prior compressor assemblies by providing a hermetic compressor assembly which includes a compressor housing including a quantity of liquid lubricant therein, a compressor mechanism provided within the compressor housing, a drive shaft selectively rotatable and operably connected to the compressor mechanism, a liquid lubricant displacement element engaged to the drive shaft and a support member attached to the compressor housing, a pivotable magnetic member provided between the liquid lubricant displacement element and the support member provided with a suction port therein. The liquid lubricant displacement element is in fluid communication with the quantity of liquid lubricant through the suction port in the magnetic member. At least a portion of any ferrous particles contained in the liquid lubricant are attracted to and retained by the magnetic member as the liquid lubricant is passed through the suction port of the magnetic member.
The present invention further provides a hermetic compressor assembly including a compressor mechanism and a quantity of liquid lubricant provided in a compressor housing, a selectively operable drive shaft driveably connected to the compressor mechanism, a liquid lubricant displacement element supported by a support member and engaged to the drive shaft. The compression mechanism and the liquid lubricant displacement element are in fluid communication through a passage provided in the drive shaft. A centrifugal particle trap cavity is defined by a wall of the passage within the drive shaft and a portion of the liquid lubricant displacement element. A magnetic member is pivotably supported by the support member and a thrust member is superposed with the magnetic member. A magnetic particle trap cavity is provided within a lateral face of the thrust member and is partially enclosed by a lateral surface of the magnetic member. The liquid lubricant is urged from the sump to the compression mechanism through the passage in the drive shaft and any debris in the liquid lubricant is successively retained by the magnetic particle trap cavity and the centrifugal particle trap cavity prior to the lubricants introduction to the compression mechanism.
BRIEF DESCRIPTION OF THE DRAWINGS
The above-mentioned and other features and advantages of this invention, and the manner of attaining them, will become more apparent and the invention itself will be better understood by reference to the following description of embodiments of the invention taken in conjunction with the accompanying drawings, wherein:
FIG. 1
is a sectional view of a hermetic compressor assembly provided with an oil pump assembly in accordance with the present invention;
FIG. 2A
is an exploded view of a first embodiment of an oil pump assembly in accordance with the present invention, viewing the pump from the bottom;
FIG. 2B
is an exploded view of the thrust plate and magnetic disk assembly of a second embodiment of an oil pump assembly in accordance with the present invention, viewing the assembly from the bottom;
FIG. 3A
is an exploded view of the oil pump assembly of
FIG. 2A
, viewing the pump from the top;
FIG. 3B
is an exploded view of the thrust plate and magnetic disk assembly of
FIG. 2B
, viewing the assembly from the top;
FIG. 4
is a sectional view of the oil pump assembly taken along line
4
—
4
of
FIG. 11
, however shown in an operational mode, illustrating a flow of oil therethrough and particles being trapped in respective magnetic and centrifugal traps;
FIG. 5
is a sectional view of the oil pump assembly taken along lines
5
—
5
of
FIG. 11
, however shown in a non-operational mode;
FIG. 6
is a plan view of the bottom of the impeller of the oil pump of
FIG. 2A
, showing the plurality of impeller blades;
FIG. 7
is a plan view of the bottom of the thrust plate of the oil pump of
FIG. 2A
, showing the pair of arcuate slots and the magnetic particle trap cavity;
FIG. 8
is a plan view of the bottom of the magnetic disk of the oil pump of
FIG. 2A
;
FIG. 9
is a plan view of the top of the pump housing of the oil pump of
FIG. 3A
;
FIG. 10A
is a fragmentary sectional view of the oil pump assembly according to the present invention enclosed within the circular portion shown as line
10
A—
10
A of
FIG. 11
, showing the engagement between the frustoconical surfaces of the pump housing and magnetic disk;
FIG. 10B
is a fragmentary sectional view of a third embodiment of the oil pump assembly according to the present invention showing the engagement between the spherical surfaces of the pump housing and magnetic disk; and
FIG. 11
is a bottom view of the oil pump assembly of FIG.
2
A.
Corresponding reference characters indicate corresponding parts throughout the several views. Although the drawings represent embodiments of the present invention, the drawings are not necessarily to scale and certain features may be exaggerated in order to better illustrate and explain the present invention. The exemplifications set out herein illustrate embodiments of the invention, and such exemplifications are not to be construed as limiting the scope of the invention in any manner.
DETAILED DESCRIPTION OF THE INVENTION
Referring to
FIG. 1
, compressor assembly
10
includes hermetically sealed housing
12
, having base
17
provided at a lower end thereof. Motor assembly
14
, enclosed within housing
12
, includes rotor
11
and stator
13
and is directly connected to, and operatively drives, compression mechanism
15
. Compression mechanism
15
may constitute a reciprocating piston-type compression mechanism, as shown, which includes cylinder block
16
having reciprocating piston
18
therein. Alternatively, compression mechanism
15
may be a rotary or scroll type mechanism. Drive shaft or crankshaft
20
is driveably coupled to motor assembly
14
and extends vertically from a lowermost portion of compressor assembly
10
upwardly towards compression mechanism
15
. Upper end of crankshaft
20
is rotatably supported by main bearing
22
and is generally hollow, including inner passage
23
extending axially, and continuously, along the length of crankshaft
20
. Arrows
25
illustrate flow of liquid lubricant (e.g., oil), which is directed through passage
23
of crankshaft
20
, to supply oil to bearing surfaces, such as rod bearing
24
, and to wrist pin
27
, as shown. Oil pump assembly
42
is positioned at lower end
36
of crankshaft
20
to urge oil from oil sump
30
to upper end
38
of crankshaft
20
. Support member
43
, provided within lower portion
28
of housing
12
to support pump
42
, includes a plurality of arms
33
equidistantly spaced and radially extended between pump
42
and inner surface
35
of housing
12
. Oil sump
30
, formed by lower portion
28
of housing
12
, contains surplus oil to supply pump assembly
42
with oil. Oil level
32
within sump
30
is preferably maintained above oil pump assembly
42
, as shown, such that a continuous supply of oil is pumped to bearing surfaces by pump assembly
42
.
Referring to
FIGS. 2A and 3A
, shown is oil pump assembly
42
, engaged with lower end
36
of crankshaft
20
. Lower end
36
of crankshaft
20
includes end face
50
and outer surface
46
. Lower end
36
of crankshaft is attached to oil displacement element or impeller
52
. Alternatively, oil displacement element
52
may include a gerotor or gear type element to transfer oil from sump
30
to compression mechanism
15
(FIG.
1
). It may be seen that counterbore
40
(
FIG. 2A
) is formed in lower end
36
of crankshaft
20
to receive stem
56
of impeller
52
. End face
50
of crankshaft
20
includes angled counterbore or chamfer
44
provided in counterbore
40
of crankshaft
20
(FIG.
2
A). A pair of diametrically opposed slots
48
(
FIG. 2A
) radially extend from counterbore
40
of crankshaft
20
toward outer surface
46
of crankshaft
20
to engageably receive tangs
60
of impeller
52
. Tangs
60
axially extend from disk shaped drive portion
54
and are attached to a periphery of impeller stem
56
(FIG.
3
A).
Impeller stem
56
axially extends from drive portion
54
and includes circumferentially disposed groove
58
(FIGS.
4
and
5
), having a U-shaped cross section and O-ring
62
is received therein. O-ring
62
provides a liquid seal between the outer periphery of impeller stem
56
and counterbore
40
of drive shaft
20
(FIGS.
4
and
5
). Drive portion
54
of impeller
52
includes a plurality of radially arranged impeller blades
66
. Each impeller blade
66
is separated from an adjacent impeller blade
66
by circumferential spaced groove
65
(FIG.
6
). As best seen in
FIGS. 2A and 6
, impeller
52
includes annular groove
68
located substantially centered on lower surface of drive portion
54
of impeller
52
. Impeller
52
includes center portion
69
provided with generally planar surface
71
which is coextensive with surface
73
of each respective impeller blade
66
(FIG.
6
). Hole
64
extends axially through impeller
52
. Surfaces
71
and
73
form thrust face
70
(
FIGS. 4-5
) of impeller
52
.
Referring again to
FIGS. 2A and 3A
, shown is thrust member or thrust plate
72
having thrust face
74
which rotatably supports thrust face
70
of impeller
52
(FIGS.
4
-
5
). It may be seen that a clearance “c” exists between main bearing
22
and shoulder portion
75
of crankshaft
20
such that the weight of crankshaft
20
and displacement element
52
urges displacement element
52
into engagement with face
74
of thrust plate
72
(FIG.
1
). Those having ordinary skill will understand that the combined weight of crankshaft
20
, and displacement element
52
, bearing down on face
74
of thrust plate
72
prevents a significant and detrimental loss of lubricant through an interface provided by displacement element
52
and face
74
of thrust plate
72
.
Thrust plate
72
includes outer radial surface
76
and lateral surface
77
(FIG.
7
). Lateral surface
77
is provided with lower faces
78
a
,
78
b
and
78
c
which collectively form a planar support surface which abuts upper face
86
of magnetic member or disk
84
(FIGS.
2
A and
7
). Thrust plate
72
is provided with central hole
80
which is aligned with central hole
64
of impeller
52
(FIGS.
4
and
5
). As best seen in
FIGS. 2A and 4
, thrust plate
72
includes extended annular nose portion
81
, split into two arcuate halves, each of which axially extend from lower face
78
b
. The two halves of nose portion
81
are engaged with recess
94
in magnetic disk
84
to center thrust plate
72
relative to magnetic disk
84
(FIG.
3
A).
Magnetic disk
84
includes upper face
86
, lower face
88
and peripheral surface
90
, and as best seen in
FIGS. 3A and 8
, is provided with semi-circular notch
92
which receives semi-circular protrusion
82
(
FIG. 7
) axially extended from thrust plate
72
. Protrusion
82
, extended into notch
92
, prevents rotation between magnetic disk
84
relative to thrust plate
72
. Lower face
88
of magnetic disk
84
includes three projections
96
intersected at centerline axis
85
and radially extended towards peripheral surface
90
of magnetic disk
84
(FIGS.
2
A and
11
). Referring to
FIG. 11
, radial projections
96
are engaged with three circumferentially spaced slots
116
(
FIG. 9
) located in pump housing
104
to prevent rotation between magnetic disk
84
and pump housing
104
. Housing
104
is fixed to support member
43
by, for example, a press fit engagement between outer surface
106
of housing
104
and counterbore
105
located in support member
43
(FIG.
1
). Alternatively housing
104
may be eliminated and in its place support member
43
may be provided with identically internal characteristics as that of housing
104
.
Magnetic disk
84
may be manufactured from a magnetized metallic material through, for example, a sinterized powder metal process. The magnetic properties of magnetic disk
84
attract ferrous particles
87
(
FIG. 4
) entrained or suspended in the oil as described below. Impeller
52
and thrust plate
72
may be made of an abrasion resistant moldable plastic, such as a phenolic material for example, through an injection molding process. Crankshaft
20
may be preferably made from a carbon steel and formed through a forging process to produce high durability and abrasion resistant properties.
An alternate thrust plate and magnetic disk engagement is shown in
FIGS. 2B and 3B
. As best seen in
FIG. 2B
, magnetic disk
84
′ includes a pair of through holes
98
aligned with a pair of holes
99
in thrust plate
72
′. Holes
99
are engaged by a pair of fasteners
100
, which may include, for example, brads, to secure magnetic disk
84
′ to thrust plate
72
′.
Referring to
FIGS. 2-5
, pump housing
104
is provided with cylindrical outer surface
106
and cylindrical inner surface
108
(FIGS.
3
-
5
). Housing
104
and support member
43
may be made from an aluminum alloy through a die cast molding process or a powder metal process, for example. As best seen in
FIG. 10A
, lower end
109
of housing
104
includes annular platform
110
which provides support for magnetic disk
84
. Platform
110
includes inwardly angled frustoconical surface
112
providing support for outwardly angled frustoconical surface
102
(
FIG. 8
) provided on lower face
88
of magnetic disk
84
(
FIGS. 4
,
5
and
10
). Lower end
109
of housing
104
includes through hole
114
extended axially through housing
104
to provide an inlet for oil to be drawn into pump
42
by the oil displacement element, i.e. impeller
52
. Frustoconical surface
112
, provided on annular platform
110
, forms a frustoconical engagement with frustoconical surface
102
of magnetic disk
84
. The frustoconical engagement provides a degree of self alignment of the abutting faces of impeller
52
and thrust plate
72
, despite angular variations in the housing centerline relative to the shaft centerline. As a result, reliance on close manufacturing and assembling tolerances of impeller
52
, crankshaft
20
and thrust plate
72
, traditionally employed, are not required with oil pump
42
.
Referring to
FIG. 10B
, a third embodiment of a lubricant pump is shown and includes mating hemispherically shaped surfaces
102
′,
112
′ of magnetic member and housing
104
′,
84
′ respectively. As an alternative to frustoconical surfaces
102
,
112
shown, in
FIG. 10A
, hemispherical surfaces
102
′,
112
′ shown in
FIG. 10B
provide increased pivoting mobility between magnetic member
84
′ relative to housing
104
′ to remedy the angular variations in the housing centerline relative to the shaft centerline.
The flow of oil through oil pump assembly
42
will now be described. Referring to
FIG. 4
, oil is drawn through suction port or hole
114
of housing
104
from sump
30
and into a pair of arcuate suction ports
120
formed in magnetic disk
84
(
FIGS. 4
,
8
and
11
). Arcuate suction ports
120
extend completely through the magnetic disk from lower face
88
to upper face
86
(FIG.
8
). Similarly, arcuate suction port
122
extends completely through thrust plate
72
between thrust face
74
and lower face
78
a
thereof (FIG.
7
). Arcuate suction port
122
, provided in thrust plate
72
, is radially aligned with the, pair of arcuate suction ports
120
in magnetic disk
84
. It may be seen that thrust plate
72
includes a pair of U-shaped discharge slots
126
provided in outer periphery
76
of thrust plate
72
(FIG.
3
A). Slots
126
are oppositely located relative to one another and axially extend into a pair of arcuate channels
130
formed in thrust plate
72
(
FIGS. 2A
,
7
). Channels
130
are provided in lateral surface
77
of thrust plate
72
as described below.
As best seen in
FIG. 7
, each channel
130
includes transverse wall
132
, first sidewall
136
, and second sidewall
138
. Transverse wall
132
is substantially planar and is formed within lateral surface
77
of thrust plate
72
. First sidewall
136
is arcuate and extends from its respective discharge slot
126
to hole
80
in thrust plate
72
. Each second side wall
138
of channel
130
includes U-shaped slot
140
. A portion of oil received by slots
126
from impeller
52
flows into channels
130
and into central hole
80
in thrust plate
72
. The other portion of oil flows into magnetic particle trap cavity
142
as described below.
Lateral surface
77
of thrust plate
72
is provided with crescent-shaped magnetic particle trap cavity
142
. First sidewall
144
of magnetic particle trap cavity
142
includes a plurality of circumferentially spaced semi-circular inclusions
146
(FIG.
7
). Second sidewall
148
of magnetic particle trap cavity
142
is generally smooth and continuous. Magnetic particle trap cavity
142
includes transverse wall
150
provided in lateral surface
77
of thrust plate
72
. Magnetic particle trap cavity
142
is enclosed by upper face
86
of magnetic disk
84
(FIGS.
4
and
5
).
In operation, pump
42
is activated by motor driven shaft
20
urging rotation of impeller
52
and oil in sump
30
(
FIG. 1
) is drawn, illustrated by arrows
149
in
FIG. 4
, into suction port
120
of magnetic disk
84
. Thereafter, oil enters suction port
122
provided in thrust plate
72
. It is well understood that over time a compressor assembly generates debris which becomes entrained in the oil and frequently a portion of the debris is in the form of ferrous particles. Ferrous particles, which may be included in the present invention lubricant pump
42
, are attracted to and retained by magnetic disk
84
before the oil enters suction port
122
of thrust plate
72
. Oil then enters annular groove
68
within impeller
52
and is centrifugally flung radially outward through radially positioned grooves
65
between impeller blades
66
. The oil is then urged downwardly into U-shaped discharge slots
126
in thrust plate
72
, and thereafter, a portion of the oil is urged into the pair of arcuate channels
130
which extend toward central hole
80
of the thrust plate
72
. Oil entering central hole
80
of thrust plate
72
via channels
130
is urged upwardly through hole
64
in impeller
52
, into passage
23
of crankshaft
20
, and is ultimately received by the bearing surfaces within the compressor mechanism.
The portion of oil which does not travel through arcuate slots
130
enters magnetic particle trap cavity
142
and is slow moving due to the debris entrained therein. The oil entering magnetic particle trap cavity
142
is flung radially outward into the plurality of inclusions
146
in first sidewall
144
. Oil circulates through magnetic particle trap cavity
142
, entering one of the U-shaped slots
140
and exiting the other U-shaped slot
140
. Since thrust plate
72
is symmetrical, pump
42
may operate in either rotational direction with similar particle trapping results, i.e., pump
42
is reversible.
Referring to
FIGS. 4 and 5
, it may be seen that upper face
86
of magnetic disk
84
overlays arcuate channels
130
and magnetic particle trap cavity
142
of thrust plate
72
. Ferrous particles
87
entering magnetic particle trap cavity
142
are carried with the oil and are attracted to and trapped by upper face
86
of magnetic disk
84
under the influence of magnetic force established by magnetic disk
84
(FIG.
4
). Additionally, oil flowing through channels
130
includes ferrous particles which pass over magnetic disk
84
and become attracted and attached to face
86
of magnetic disk. Additional particles and debris, which may include ferrous or non-ferrous particles, are caught within inclusions
146
of magnetic particle trap cavity
142
as oil flows through cavity
142
. Therefore, magnetic particle trap cavity
142
and face
86
of magnetic disk
84
provide a two-stage debris retaining structure, the first stage provided by inclusions
146
within thrust plate
72
, trapping a portion of the debris therein, and a second stage, provided by face
86
of magnetic disk
84
, trapping additional debris, in the form of ferrous particles
87
.
As best seen in
FIG. 4
, drive shaft
20
is provided with centrifugal particle trap cavity
155
radially located within a wall defining passage
23
. Specifically, centrifugal particle trap cavity
155
is bound by counterbore
40
and frustoconical surface
156
of impeller stem
56
, on one axial end, and frustoconical surface
160
of the other axial end. Thus, it may be seen that annular, frustoconical surfaces
156
,
160
, and a portion of counterbore
40
in crankshaft
20
, form centrifugal particle trap cavity
155
to capture debris
162
, as it is transported by the oil flowing through passage
23
, shown by flow arrow
149
(FIG.
4
). Particles
162
, under the influence of centrifugal force as crankshaft
20
is rotated by motor assembly
14
, are flung into centrifugal particle trap cavity
155
as oil moves through passage
23
. Particles
162
are thereby centrifugally trapped in centrifugal particle trap cavity
155
during compressor operation, and are prevented from thereafter continuing with the oil upwards through passage
23
.
Referring to
FIG. 5
, it may be seen that once shaft
20
ceases rotation, at least a portion of particles
162
travel downwardly and rest upon conical surface
156
formed by impeller stem
56
. The remaining particles continue downwardly from second chamber
155
and accumulate at center portion
164
of magnetic disk
84
and some particles may eventually flush back through oil pump
42
and into oil sump
30
or magnetic particle trap cavity
142
. Those having ordinary skill in the art will understand that an abundance of debris entrained in the oil will not plug inventive pump
42
. Rather, magnetic and centrifugal particle trap cavities
142
,
155
are so positioned within the oil circuit such that oil is allowed to pass through pump
42
regardless of whether the magnetic and centrifugal particle trap cavities are replete with debris. Since hermetically sealed compressor assembly
10
of the present invention is manufactured to be non-maintainable, i.e., not to be disassembled for maintenance purposes, it is particularly important that oil pump
42
continues to perform even if a significant amount of debris is accumulated within magnetic and centrifugal particle trap cavities
142
,
155
.
Referring to
FIGS. 2-5
, gas vent
166
extends from chamfer
44
of crankshaft
20
to outer surface
46
of crankshaft
20
to provide an escape path for refrigerant gases flashed from the oil in pump
42
. Gases or vapor which are not vented may be detrimental to proper lubricant flow, inasmuch as it may cause an insufficient amount of oil being delivered to the bearing surfaces. Vent
166
provides an escape for these gases to avoid bearing damage.
While this invention has been described as having exemplary designs, the present invention may be further modified within the spirit and scope of this disclosure. Therefore, this application is intended to cover any variations, uses, or adaptations of the invention using its general principles. For example, aspects of the present invention may be applied to compressors other than reciprocating piston compressors such as rotary and scroll compressor assemblies, for example. Further, this application is intended to cover such departures from the present disclosure as come within known or customary practice in the art to which this invention pertains.
Claims
- 1. A hermetic compressor assembly comprising:a compressor housing including a quantity of liquid lubricant therein; a compressor mechanism disposed in said compressor housing; a drive shaft selectively rotatable and operably connected to said compressor mechanism; and a liquid lubricant displacement element engaged to said drive shaft; a support member attached to said compressor housing; a pivoting magnetic member disposed between said liquid lubricant displacement element and said support member; a suction port defined within said magnetic member, said liquid lubricant displacement element is in fluid communication with said quantity of liquid lubricant through said suction port in said magnetic member, wherein at least a portion of any ferrous particles contained in said liquid lubricant are attracted to and retained by said magnetic member as said liquid lubricant is passed through said suction port of said magnetic member.
- 2. The compressor assembly according to claim 1, further comprising a thrust member, said liquid lubricant displacement element being supported by said thrust member.
- 3. A hermetic compressor assembly comprising:a compressor housing including a quantity of liquid lubricant therein; a compressor mechanism disposed in said compressor housing; a drive shaft selectively rotatable and operably connected to said compressor mechanism; and a liquid lubricant displacement element engaged to said drive shaft; a support member attached to said compressor housing; a pivotable magnetic member disposed between said liquid lubricant displacement element and said support member; a suction port defined within said magnetic member, said liquid lubricant displacement element is in fluid communication with said quantity of liquid lubricant through said suction port in said magnetic member; and a thrust member, said liquid lubricant displacement element being supported by said thrust member; wherein at least a portion of any ferrous particles contained in said liquid lubricant are attracted to and retained by said magnetic member as said liquid lubricant is passed through said suction port of said magnetic member and said thrust member defines a magnetic particle trap cavity, said magnetic particle trap cavity being superposed by said magnetic member, whereby an additional portion of said any ferrous particles contained in said liquid lubricant is retained within said magnetic particle trap cavity under the influence of magnetic force.
- 4. The compressor assembly according to claim 3, wherein said magnetic particle trap cavity includes a plurality of circumferentially disposed inclusions, whereby any debris contained by said liquid lubricant is captured within said inclusions as said liquid lubricant is passed through said magnetic particle trap cavity.
- 5. The compressor assembly according to claim 1, wherein said drive shaft includes a passage, said passage partially defining a centrifugal particle trap cavity, wherein at least a portion of any debris contained in said liquid lubricant is retained within said centrifugal particle trap cavity under the influence of centrifugal force provided by rotation of said drive shaft.
- 6. The compressor assembly according to claim 5, wherein said liquid lubricant displacement element is in fluid communication with an exterior portion of said drive shaft through a gas vent disposed in said drive shaft and any gas intermixed with said liquid lubricant is transported to an interior of said compressor housing through said gas vent.
- 7. The compressor assembly according to claim 5, wherein said centrifugal particle trap cavity is located downstream of said magnetic particle trap cavity.
- 8. The compressor assembly according to claim 3, wherein said thrust member includes a lateral face having a pair of radially extended channels disposed therein, said magnetic particle trap cavity being disposed in said lateral face of said thrust member, wherein said liquid lubricant being urged toward said lateral face of said thrust member is diverted between said channels and said magnetic particle trap cavity.
- 9. The compressor assembly according to claim 2, wherein said thrust member is supported by a lateral surface of said magnetic member, said magnetic member comprising a magnetized substance to attract and retain any ferrous particles contained in said liquid lubricant.
- 10. The compressor assembly according to claim 1, wherein said liquid lubricant displacement element is an impeller.
- 11. A hermetic compressor assembly comprising:compressor housing including a quantity of liquid lubricant therein; a compressor mechanism disposed in said compressor housing; a selectively operable drive shaft driveably connected to said compressor mechanism; a support member; a liquid lubricant displacement element supported by said support member, said liquid lubricant displacement element engaged to said drive shaft, said compressor mechanism and said liquid lubricant displacement element being in fluid communication through a passage disposed in said drive shaft; a centrifugal particle trap cavity defined by a wall of said passage within said drive shaft and a portion of said liquid lubricant displacement element; a magnetic member pivotably supported by said support member; a thrust member superposed with said magnetic member; and a magnetic particle trap cavity disposed within a lateral face of said thrust member and being partially enclosed by a lateral surface of said magnetic member, wherein said liquid lubricant is urged from said sump to said compression mechanism through said passage in said drive shaft and any debris in said liquid lubricant being successively retained by said magnetic particle trap cavity and said centrifugal particle trap cavity.
- 12. The compressor assembly according to claim 11, wherein said magnetic particle trap cavity is partially defined by a plurality of radially disposed inclusions, wherein any debris contained in said liquid lubricant is retained by said centrifugal particle trap cavity under the influence of centrifugal force and any debris comprising ferrous particles is retained by said magnetic particle trap cavity under the influence of magnetic force.
- 13. The compressor assembly according to claim 11, wherein said magnetic particle trap cavity is positioned upstream relative to said centrifugal particle trap cavity.
- 14. The compressor assembly according to claim 11, wherein said magnetic member is pivotally supported within said housing;
- 15. The compressor assembly according to claim 11, wherein said magnetic member includes a surface moveably engaged with a surface defined by said pump housing.
- 16. The compressor assembly according to claim 15, wherein said surface of said magnetic member and said surface of said support member are superposed spherical surfaces.
- 17. The compressor assembly according to claim 15, wherein said surface of said magnetic member and said surface of said support member are superposed frustoconical surfaces.
- 18. The compressor assembly according to claim 11, wherein said liquid lubricant displacement element is in fluid communication with an interior of said compressor housing through a gas vent disposed in said drive shaft.
- 19. The compressor assembly according to claim 11, further comprising a pump housing disposed between said support member and said magnetic member.
- 20. The compressor assembly according to claim 11, wherein said liquid lubricant displacement element constitutes an impeller.
- 21. The compressor assembly according to claim 20, wherein said compressor housing defines a liquid lubricant sump containing said liquid lubricant, said impeller includes an annular groove disposed therein, said annular groove being in fluid communication with said sump through a suction port extended axially through said thrust member and said magnetic member.
- 22. The compressor assembly according to claim 21, wherein said suction port extended through said thrust member and said magnetic member is offset relative to a centerline extended axially through said drive shaft.
- 23. The compressor assembly according to claim 22, wherein said compressor mechanism includes bearing surfaces in fluid communication with said liquid lubricant displacement element though said passage within said drive shaft, said liquid lubricant displacement element and said thrust member include a centrally located discharge port axially extended therethrough, said suction port within said magnetic member and said thrust member in fluid communication with said discharge port within said liquid lubricant displacement element and said thrust member through a pair of slots disposed in said thrust member.
- 24. The compressor assembly according to claim 11, wherein said magnetic member comprises a disk having a pair of lateral surfaces, one of said pair of lateral surfaces includes a plurality of radially extending projections attached thereto, said projections being received within a plurality of circumferentially spaced and radially extended slots provided in said support member, whereby said magnetic member is substantially rotationally restrained relative to said pump housing.
US Referenced Citations (17)