U.S. patent number 3,900,277 [Application Number 05/439,512] was granted by the patent office on 1975-08-19 for rotary compressor.
This patent grant is currently assigned to Borg-Warner Corporation. Invention is credited to Alwin B. Newton.
United States Patent |
3,900,277 |
Newton |
August 19, 1975 |
Rotary compressor
Abstract
A rotary gas compressor of the sliding vane type having a rotor
positioned eccentrically within a working chamber provided by a
cylinder in the stator housing which is closed by end plates
secured to the housing. The rotor carries blades or vanes slidable
within slots formed in the rotor to engage the cylinder and sweep
the working chamber to compress gas introduced therein. The end
plates are formed with arcuate, gas discharge slots connecting the
outlet port of the housing with circumferentially-spaced discharge
slots in the rotor in a manner to provide an alternate, low
resistance path for gas flow at a point located a substantial
distance from the outlet port. This arrangement is effective to
reduce the extremely high pressure which is normally generated in
the discharge zone as the vanes approach the main outlet port and
valve assembly.
Inventors: |
Newton; Alwin B. (York,
PA) |
Assignee: |
Borg-Warner Corporation
(Chicago, IL)
|
Family
ID: |
26948877 |
Appl.
No.: |
05/439,512 |
Filed: |
February 4, 1974 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
|
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261846 |
Jun 12, 1972 |
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Current U.S.
Class: |
418/184;
418/236 |
Current CPC
Class: |
F04C
29/12 (20130101) |
Current International
Class: |
F01c 021/12 () |
Field of
Search: |
;418/159,183,184,236 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Husar; C. J.
Assistant Examiner: Smith; Leonard
Attorney, Agent or Firm: Hunter; Thomas B.
Parent Case Text
CROSS-REFERENCE TO RELATED APPLICATION
This application is a continuation-in-part of my copending
application Ser. No. 261,846, filed June 12, 1972, now abandoned.
Claims
What is claimed is:
1. A rotary gas compressor comprising a housing having a
substantially cylindrical interior surface and opposed end plates
defining a closed chamber;
a rotor having a cylindrical peripheral surface and opposed side
faces, said rotor being mounted in said chamber and rotatable about
an axis which is offset with respect to the axis of said
cylindrical interior surface, said rotor and said housing defining
a generally crescent shaped compression cavity;
a gas inlet port and a gas discharge port communicating with said
compression cavity;
a valve associated with said gas discharge port;
a plurality of vanes slidably supported in said rotor and engaging
said cylindrical interior surface;
means defining an elongated slot in at least one of said end plates
having an exit end located in communication with said discharge
port and an entrance end located at a point circumferentially
spaced in a direction toward said inlet port and inwardly spaced
from said cylindrical peripheral surface, the entire slot being
substantially covered by one of the side faces of said rotor;
and
means defining a passage immediately adjacent each vane in said one
rotor end surface extending away from the cylindrical surface and
providing a first flow path for gas which intermittently connects
that portion of the compression cavity ahead of the vane with the
entrance end of said elongated slot, a second flow path,
communicating with said discharge port, for gas being provided
between the cylindrical surface on said rotor, the cylindrical
interior surface of said housing and said end plates within said
housing.
Description
BACKGROUND AND SUMMARY OF THE INVENTION
This invention relates to gas compressors and more particularly to
gas discharge arrangements for compressors.
One common type of rotary gas compressor comprises a bladed or
vaned rotor eccentrically mounted in a cylindrical stator housing
to provide a crescent-shaped working chamber between the rotor and
housing. The chamber communicates with an inlet or suction port and
an outlet or discharge port. During rotation of the rotor, gas
flows through the suction port and into the chamber and is then
compressed by the vanes between the converging walls of the rotor
and the cylinder. As the blades approach the discharge port, the
distance between the cylinder wall and the rotor surface is very
small; and, as a result, gas is under extremely high pressure in
the zone adjacent to the discharge port. When the compressor is
operating with high discharge pressure, this restriction adjacent
the discharge port becomes even more troublesome, resulting in
extreme overcompression of the gas and concommitant loss of
efficiency.
There are numerous examples in the prior art of discharge
arrangements which provide a continuous flow path for discharge gas
after suction is closed. In U.S. Pat. No. 1,949,723 (Kotelevtseff)
issued Mar. 6, 1934, a rotor sweeps the compression chamber in such
a way that discharge gas is continuously directed through a passage
in one end wall during the final 90.degree. of rotation. Such a
device is mechanically fixed as to discharge and provides only a
single path for discharge gas flow.
In U.S. Pat. No. 2,674,953 (Conde), issued Apr. 13, 1954, the
compression chamber is defined in part by an end wall having an
elongated, arcuate discharge port formed therein. This has the
disadvantage that the gas, which is in the final stage of
compression before the vane passes into the area of the port, will
blow-back (short circuit) into the pocket defined between the
leading and trailing vanes. This could cause a serious loss in
capacity, because it would perform a considerable part of its work
forcing the gas from a leading pocket to a trailing pocket.
The rotary gas compressor of the present invention is characterized
by the provision of an improved gas discharge arrangement featuring
a housing having a discharge port, which is covered by a discharge
valve, and arcuate slots in its end faces communicating with said
outlet port and cooperating with fluid passages in the rotor
adjacent each vane to provide a secondary, low pressure drop path
for gas flow at a point located at a substantial distance from the
outlet port in the housing. In this arrangement, the gas may begin
to flow to the outlet port as soon as the rotor ports are in
communication with the distal ends of the slots in the housing,
provided there is sufficient pressure to overcome the opening force
on the discharge valve. This alternate, low resistance path is
effective in reducing the extremely high pressures otherwise
normally generated in the discharge zone of a conventional gas
compressor as the vanes approach the discharge port.
Another aspect of the invention relates to the location of the
arcuate slots in the end faces. Except for the outlet end of the
slots, they are completely covered by the side faces of the rotor.
This prevents gas from blowing back through the slot to the
trailing, lower pressure pocket. Thus the only blow-back that can
occur is over the tip of the vane in the outlet zone (inherent in
all sliding vane compressors) and some small carryover of high
pressure gas from the pockets in the rotor side faces.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a cross-sectional view of a rotary gas compressor having
an improved gas discharge arrangement;
FIG. 2 is a cross-sectional view taken along the plane of line 2--2
of FIG. 1;
FIG. 3 is a cross-sectional view taken along the plane of line 3--3
of FIG. 1; and
FIG. 4 is a cross-sectional view taken along the plane of line 4--4
of FIG. 1, but with the valve stop removed.
BRIEF DESCRIPTION OF THE INVENTION
Referring to FIGS. 1 and 2, the gas compressor 10 comprises a rotor
assembly 11 rotatable within a stator assembly 12 and which serves
as a housing for the rotor assembly. More particularly, the stator
assembly 12 comprises a cylinder housing 13 and end plates 14 and
15 held in engagement with housing 13 by bolts 16. The plates 14
and 15 are bored as at 17 and 18 to provide bearings for rotatably
mounting the rotor assembly 11 within the stator assembly 12.
The rotor assembly 11 comprises a cylindrical rotor 19 having a
plurality of equidistantly-spaced slots 20 receiving vanes 21
slidably reciprocable therein. Rotor 19 is keyed at 22 to a drive
shaft 23 journalled in the bearings 17 and 18 and is adapted to be
driven by a pulley 24 connected to a motor (not shown) or other
suitable drive means. In the case of an automotive application, the
compressor is usually driven from the engine through an accessory
drive system.
As shown in FIG. 1, the substantially cylindrical inner surface 25
of the cylinder housing 13 has a contact area 26 engaging the outer
cylindrical surface 19b of the rotor. Since the rotor is rotatably
mounted on an axis 27 offset from the center line of the cylinder
wall, the rotor is substantially in sliding contact with the
contact area 26, leaving a generally crescent-shaped working
chamber 28 extending over a substantial portion of the inner
periphery of the cylinder housing 13.
As best shown in FIGS. 1 and 4, a suction port 29 and a discharge
passage 30 are provided in the cylinder housing 13, both of which
communicate with the working chamber 28. A discharge gas plenum 40
is located between discharge passage 30 and a series of ports 41
which communicate directly with the discharge gas zone 42 adjacent
the contact area 26. Ports 41 are drilled through a valve plate 43
to which is secured a valve 44 and valve stop 45 in a conventional
manner. For clarity, the valve stop is not shown in FIG. 4. Valve
44 is biased to a closed position and requires a predetermined
opening force to build up in the discharge zone 42 before gas may
flow into plenum 40 and discharge passage 30.
The improved gas discharge system comprises a plurality of
substantially arcuate gas discharge slots 31 and 32 in the end
faces of the housing plates 14 and 15, respectively, the slots
communicating with discharge passage 30 in the cylinder housing
through the valve 44. The end faces 19a and 19b of rotor 19 are
provided with circumferentially-spaced fluid passages 33, 34
located on opposite faces 19a and 19b of the rotor immediately
ahead of each vane 21, in terms of the direction of rotation 25
shown by the arrow, FIG. 1. The passages 33 and 34 cooperate with
the slots 31 and 32 in a manner that the respective sets of the
passages 33 and 34 are successively placed in communication with
the slots 31 and 32 in the end plates 14 and 15 during rotation of
the rotor in the direction indicated by the arrow in FIG. 1.
In the operation of the compressor, the discharge slots 31 and 32
in the housing plates 14 and 15 are effective to provide an
alternate, low resistance path for gas flow at a point located a
substantial distance from the outlet port 30 of the stator housing.
As shown in FIG. 1, the passage 33, which would be located directly
across from passage 34, as illustrated, is just beginning
communication with the entrance end 31b of slot 31. It will be
noted that the passage is defined by the slot 31 and the side face
19a of rotor 19 as the vane sweeps along. Accordingly, the gas may
not flow back to the trailing pocket, as would be case if the slot
31 were located radially outwardly of the peripheral surface 19b of
rotor 19.
At the same time, gas may also be discharged through the primary
passage defined between the cylindrical surface 19b of rotor 19,
end plates 14 and 15, and surface 25 of the cylinder, as in a
conventional rotary sliding vane compressor. It will be apparent
from the foregoing description that there is provided an improved
arrangement for discharging high pressure gas from a compressor
which effectively reduces the extremely high pressures normally
generated in the outlet area as the vanes approach the same. The
system also provides minimum flow resistance by avoidance of flow
restriction to thereby insure proper compression at the outlet of
the compressor.
* * * * *