Information
-
Patent Grant
-
6488480
-
Patent Number
6,488,480
-
Date Filed
Friday, May 11, 200123 years ago
-
Date Issued
Tuesday, December 3, 200222 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 418 197
- 418 2011
- 417 310
- 417 371
- 417 4104
-
International Classifications
- F04B3906
- F04B4903
- F04C1816
-
Abstract
A housing for a screw compressor, includes a single-piece casting defining a motor housing section and a rotor housing section and has an inlet for compressor medium, an outlet end and a bridge member disposed between the motor housing section and the rotor housing section and defining an inlet side bearing housing; a discharge housing mounted to the outlet end and defining an outlet and a discharge side bearing housing; and at least one rotor disposed in the rotor housing section and rotatably mounted between the inlet side bearing housing and the discharge side bearing housing.
Description
BACKGROUND OF THE INVENTION
The invention relates to a housing for a screw compressor and, more particularly, to a housing for a hermetic multi-rotor screw compressor.
Screw compressors typically have several different housing members. A housing must be provided for the rotor or rotors, and a separate housing is typically provided for the motor which drives the rotors. Separate housings are typically required due to the length of the rotors, and for other reasons.
These housing designs can be problematic in providing a hermetic compressor. Further, access to the rotor for servicing and the like is difficult in that entire housing members must be repositioned to access same, and these housings are heavy and bulky.
Multi-rotor screw compressors typically have multiple discharge ports, see for example U.S. Pat. No. 5,807,091 to Shaw. These discharge ports typically remove refrigerant or other compressed medium from the rotors in a radially outward direction and then convey this flow to a collection chamber for discharging a single stream. The positioning of these discharge ports and collection chambers impose a change in direction of flow on the refrigerant which can cause reduction in efficiency.
The motor portion of such compressors tends to general heat and requires cooling. Cooling cab be accomplished with oil or other cooling medium, and U.S. Pat. No. 6,045,344 shows a compressor wherein coolant is passed through the motor housing by an end suction which causes the cooling medium to pass through the entire motor assembly.
It is clear that the need remains for an improved housing for screw compressors so as to address the aforesaid disadvantages.
It is therefore the primary object of the present invention to provide such a housing.
It is a further object of the present invention to provide a housing including a discharge port which improves flow efficiency of refrigerant or other compressor medium.
It is a still further object of the present invention to provide such a housing which provides for simplified cooling of the motor.
It is another object of the present invention to provide a housing which has a low manufacturing cost.
Other objects and advantages of the present invention will appear hereinbelow.
SUMMARY OF THE INVENTION
The foregoing objects and advantages of the present invention have been readily attained.
In accordance with the present invention, a housing for a screw compressor is provided, which comprises a single-piece casting defining a motor housing section and a rotor housing section and having an inlet for compressor medium, an outlet end and a bridge member disposed between said motor housing section and said rotor housing section and defining an inlet side bearing housing; a discharge housing mounted to said outlet end and defining an outlet and a discharge side bearing housing; and at least one rotor disposed in said rotor housing section and rotatably mounted between said inlet side bearing housing and said discharge side bearing housing.
In accordance with one aspect of the invention, the inlet is arranged so as to introduce compressor medium into the housing between the motor housing section and the rotor housing section, by suction, which leads to cooling of the motor housing section as the compressor medium is passed to the rotors.
In accordance with a further aspect of the present invention, the bridge member extends inwardly from an inner surface of the housing so as to define an inlet side bearing housing for the rotors and motor, while allowing compressor medium to flow around the bridge through flow channels defined therebetween and to the rotors.
In accordance with yet another aspect of the present invention, the discharge housing defines discharge ports for the rotor which extend away from the rotor both radially and axially so as to provide for more efficient flow of compressor medium from the rotors to the discharge pipe.
BRIEF DESCRIPTION OF THE DRAWING
A detailed description of preferred embodiments of the present invention follows, with reference to the attached drawings, wherein:
FIG. 1
illustrates a side sectional view of a compressor including a housing in accordance with the present invention;
FIG. 2
illustrates a further sectional view of the housing of
FIG. 1
, sectioned at a 90° angle to the view of
FIG. 1
;
FIG. 3
is a cross section taken through the housing of
FIG. 1
to illustrate the structure of the bridge member;
FIG. 4
is a cross section taken through an end cap of the housing of
FIG. 1
to show the discharge ports in accordance with the present invention;
FIG. 5
is a discharge side view of a discharge housing in accordance with the present invention;
FIG. 6
is a rotor-side view of a discharge housing in accordance with the present invention; and
FIG. 7
is an end view of a housing showing the surface for connection with the discharge housing in accordance with the present invention.
DETAILED DESCRIPTION
The invention relates to a screw compressor and, more particularly, to a housing design for a multi-rotor screw compressor, preferably a tri-rotor screw compressor, wherein the housing is advantageously a single casting and various other advantages are provided.
Multi-screw compressor may for example have a male rotor and at least two female rotors, and helical type compressors are well known in the art. In such a configuration, the male rotor is typically the drive rotor, and is driven by a motor of the compressor, and such compressors find use in numerous environments, for example in the heating, ventilation, refrigeration and air conditioning (HVRAC) industry.
Referring to the figures, a compressor including a housing in accordance with the present invention is illustrated.
FIG. 1
shows a compressor
10
having a housing
12
defining a motor housing section
14
and a rotor housing section
16
. Housing
12
in accordance with the present invention is preferably a single-piece casting so as to facilitate use of the housing in providing a hermetic screw compressor assembly.
A motor
18
is disposed in motor housing section
14
, and one or more rotors
20
are disposed in rotor housing section
16
. Motor
18
drives rotors
20
so as to draw refrigerant or other compressor medium into an inlet
22
of housing
12
for feed to rotors
20
as desired. Rotors
20
compress the refrigerant drawn therein, and discharge such compressor medium through a discharge housing
24
to a collection chamber
26
and on to the intended use of the discharged medium.
An end cover
15
may advantageously be provided closing the end of motor housing section
14
.
Referring to
FIGS. 1 and 2
together, housing
12
has an inner surface
28
which serves to define the various housing sections, and from which a bridge member
30
extends so as to define an inlet side bearing housing. Referring also to
FIG. 3
, which is a cross sectional view taken through bridge member
30
, it is readily apparent that bridge member defines three bearings
32
,
34
,
36
, and further defines two flow channels
38
,
40
between bridge member
30
and inner surface
28
.
Bearing
32
serves to receive a central or sun rotor as will be discussed below, and bearings
34
,
36
are positioned to receive two corresponding planet rotors so as to define a trirotor assembly. Further, motor
18
is typically operatively associated with or directly connected to the sun rotor through bridge member
30
as illustrated in
FIGS. 1 and 2
.
Also as shown in
FIGS. 1 and 2
, housing
12
may advantageously have an increased diameter section
42
positioned at the location of bridge member
30
so as to further define an inlet area for receiving compressor medium through inlet
22
, by suction, as desired. As shown by arrows in
FIG. 1
, compressor medium flows through inlet
22
and around bridge member
30
, through flow channels
38
,
40
so as to feed rotors
20
from both sides of bridge member
30
. This is advantageous in providing efficient flow of refrigerant to the rotors.
Still referring to
FIGS. 1-3
and particularly to
FIG. 1
, positioning of inlet
22
between motor housing section
14
and rotor housing section
16
advantageously provides for flow of compressor medium past a portion of motor
18
so as to provide a cooling of same. This is accomplished without flowing compressor medium through motor housing section
14
as is done in the prior art.
Referring to
FIG. 2
, sun rotor
44
is schematically illustrated and connected to motor
18
through a shaft
46
which passes through bridge member
30
and sun rotor bearing
32
.
FIG. 2
also illustrates planet rotors
48
,
50
rotatably disposed in planet rotor bearings
34
,
36
and engaged with sun rotor
44
for being driven by same.
Turning now to
FIGS. 4
,
5
and
6
, discharge housing
24
is further illustrated. In accordance with the present invention, discharge housing
24
advantageously defines a discharge bearing housing for receiving the discharge ends of sun rotor
44
and planet rotors
48
,
50
. Discharge housing
24
advantageously has a rotor side surface
52
which is illustrated in
FIG. 6 and a
discharge side surface
54
which is illustrated in
FIGS. 4 and 5
. As shown in these figures, discharge housing
24
defines a sun rotor bearing
56
and two planet rotor bearings
58
,
60
. Discharge housing
24
, by being connectable and removable from housing
12
, advantageously allows access to rotors disposed in housing
12
without requiring separation of the entire rotor housing from the entire motor housing as is required in conventional devices.
Discharge housing
24
and/or housing
12
further define discharge ports
62
which are communicated with rotors
20
, and discharge ports
62
are advantageously positioned so as to extend away from rotors
20
both radially and axially. Discharge ports
62
may be defined by discharge housing
24
alone, or may be partially defined by housing
12
, specifically a portion of rotor housing section
16
.
FIGS. 5-7
illustrate portions of each of these members which define the desired discharge ports.
Discharge ports
62
allow for rotor tips and end clearances to be checked, through the discharge ports, after the compressor is assembled.
FIG. 7
shows an end face
64
of rotor housing section
16
, including inner surfaces
66
which define at least partially cylindrical areas for housing rotors
20
as desired. A portion of discharge port
62
is shown at
68
, and extends away from rotors
20
in a radial direction so as to allow radial discharge from rotors
20
as desired.
Turning to
FIG. 6
, another portion
70
of discharge ports
62
is illustrated, as defined on rotor side surface
52
of discharge housing
24
.
FIG. 6
shows the extent of rotors
20
in dashed lines so as to illustrate that portion
70
overlaps or intersects with an end surface of the area defined for rotors such that compressor medium can be discharged axially, as well as radially, from rotors
20
into discharge ports
62
as desired.
As shown, discharge port portion
70
as defined through discharge housing
24
preferably extends helically from rotor side surface
52
to discharge side surface
54
so as to accommodate the imparted swirling motion of discharged compressor medium as the medium flows to collection chamber
26
for discharge through an outlet pipe as desired. Thus, discharge housing
24
has an inlet
72
to portion
70
of discharge port
62
and an outlet
74
from portion
70
of discharge port
62
which are both illustrated in FIG.
6
.
Discharge ports
62
as illustrated in
FIGS. 4-7
are preferably contoured as shown so as to encourage efficient flow through same. It should of course be appreciated that these ports could be provided having a different shape, and with different contours, as desired. It is particularly advantageous, however, that discharge ports
62
intersect the substantially cylindrically-shaped housings for rotors
20
both radially and axially, at the end surface of the chamber, so as to allow for both radially and axially discharge of compressor medium from rotors
20
as desired.
Referring back to
FIG. 5
, it may also be desirable to provide internal relief valves
76
,
78
so as to allow for relief of over-pressure behind discharge housing
24
. In accordance with the present invention, discharge housing
24
has a thickness defined between rotor side surface
52
and discharge side surface
54
, and reduced thickness sections
80
, with relief valves
76
,
78
advantageously positioned at reduced thickness sections
80
. This advantageously simplifies the installation and structure of relief valves. In further accordance with this aspect of the present invention, reduced thickness sections
80
are preferably provided by forming contoured walls, or depressions in discharge side surface
54
so as to define the reduced thickness sections in which valves
76
,
78
are mounted. The contoured walls advantageously serve to reduce disruption of flow in collection chamber
26
, which is defined in part by discharge side surface
54
, while nevertheless allowing for installation of relief valves
76
,
78
at positions of reduced thickness as desired.
Collection chamber
26
is illustrated in FIG.
1
and is any suitable end-cap structure suitable for securing to discharge housing
24
. Collection chamber
26
and the end wall of discharge housing
24
define a collection zone for compressed medium, and collection chamber
26
is preferably provided having an outlet
82
for discharge of compressed medium from compressor
10
.
It should readily be appreciated that the foregoing disclosure provides a housing for a compressor which is a substantial improvement over existing compressor housings and which allows for efficient cooling of the motor and flow of compressor medium while also allowing simplified access to rotors disposed in the housing for routine maintenance and the like.
The compressor housing finds particular use in connection with screw compressors for the HVRAC industry, and is particularly useful for this motor-rotor configuration. The housing is equally useful in connection with other helical type compressors, for example compressors with different working fluids such as helium, air, ammonia and the like, and this housing finds equal application in compressors which have different configurations of driven rotors, as well.
It is to be understood that the invention is not limited to the illustrations described and shown herein, which are deemed to be merely illustrative of the best modes of carrying out the invention, and which are susceptible of modification of form, size, arrangement of parts and details of operation. The invention rather is intended to encompass all such modifications which are within its spirit and scope as defined by the claims.
Claims
- 1. A housing for a screw compressor, comprising:a single-piece casting defining a motor housing section and a rotor housing section and having an inlet for compressor medium, an outlet end and a bridge member disposed between said motor housing section and said rotor housing section and defining an inlet side bearing housing; a discharge housing mounted to said outlet end and defining a discharge outlet and a discharge side bearing housing; and at least one rotor disposed in said rotor housing section and rotatably mounted between said inlet side bearing housing and said discharge side bearing housing, wherein said rotor comprises a sun rotor and at least two planet rotors, and wherein said inlet side bearing housing and said discharge side bearing housing define bearings for said sun rotor and said at least two planet rotors, and wherein at least one of said rotor housing section and said discharge housing define at least one discharge port for discharging medium from said sun rotor, said discharge port extending away from said sun rotor both radially and axially.
- 2. The housing of claim 1, wherein said inlet is positioned between and communicated with said motor housing section and said rotor housing section, whereby compressor medium flow into said inlet cools said motor housing section.
- 3. The housing of claim 1, further comprising a collection chamber communicated with said at least one discharge port and having an outlet whereby medium from said at least one discharge port is conveyed to said outlet.
- 4. The housing of claim 1, wherein said rotor housing section and said discharge housing define in combination an at least partially cylindrical surface within which said rotor is positioned and a discharge end surface, and wherein said discharge port intersects both said at least partially cylindrical surface and said end surface whereby discharged medium is discharged from said rotor to said discharge port both radially and axially.
- 5. The housing of claim 1, wherein said casting has an inner surface and said bridge member extends inwardly from said casting to define said inlet side bearing housing with at least two flow channels defined between said bridge member and said inner surface whereby said rotor is fed with said compressor medium through said at least two flow channels.
- 6. The housing of claim 5, wherein said bridge member defines bearings for said at least one rotor, said bearings comprising a substantially continuous circular surface.
- 7. The housing of claim 1, further comprising a motor disposed in said motor housing section and operatively associated with said rotor through said bridge member.
- 8. The housing of claim 7, wherein said motor has an axial length, and wherein said motor housing section extends at least as far as said axial length of said motor.
- 9. The housing of claim 1, wherein said discharge housing has a rotor side surface and a discharge side surface, and a thickness defined between said rotor side surface and said discharge side surface and further comprising at least one reduced thickness section in said discharge housing and at least one relief valve positioned through said discharge housing at said reduced thickness section.
- 10. The housing of claim 9, wherein said reduced thickness section is defined by a contoured wall set into said discharge housing from said discharge side surface.
US Referenced Citations (6)
Foreign Referenced Citations (4)
Number |
Date |
Country |
235303 |
Apr 1986 |
DE |
54-34111 |
Mar 1979 |
JP |
54-115409 |
Sep 1979 |
JP |
6-173871 |
Jun 1994 |
JP |