BACKGROUND OF THE INVENTION
(FIELD OF THE INVENTION)
[0001] The present invention relates to an oil cooling type screw compressor
[0002] Such a compressor is disclosed in
JP9-303279.
(DESCRIPTION OF THE RELATED ART)
[0003] In an oil cooling type screw compressor, a secondary separation is performed by a
filter in addition to a primary separation performed by a centrifugal force inside
an oil collector in order to separate an oil included in an air discharged from a
compressor body (see
JP 2013-36397 A). When the oil separated by the secondary separation is collected and is returned
to a system, the oil is directly returned to a suction port of a main body or a tooth
groove of each rotor being in the course of compression and having a pressure lower
than the secondarily separated oil in many cases. However, since the returned oil
includes a large amount of hot-temperature air, volume efficiency is degraded when
the oil is directly returned to the suction port, and a power necessary for driving
the compressor increases when the oil is directly returned to the tooth groove being
in the course of compression.
SUMMARY OF THE INVENTION
[0004] The present invention is made in view of the above-described problems, and an object
thereof is to provide a compressor capable of decreasing a power necessary for a driving
operation
[0005] According to an aspect of the present invention, there is provided a compressor according
to claim 1 including: a compressor body that includes a suction port which suctions
a gas, a pair of rotors comprising a female rotor and a male rotor which are rotatably
supported by a bearing and compressing the gas suctioned from the suction port in
cooperation with a rotor chamber, and an discharge port which discharges the compressed
gas; an oil collector that includes a primary separation unit which primarily separates
an oil from the gas compressed by the compressor body and a secondary separation unit
which secondarily separates an oil from the gas from which the oil is primarily separated
by the primary separation unit; a primary separation oil supply line that is connected
to a compression tooth groove space of the female rotor defined by an inner wall of
the rotor chamber and a pair of adjacent teeth of the female rotor in a cross-section
perpendicular to a rotor shaft of the compressor body, and to the oil collector, the
primary separation oil supply line supplying the oil separated by the primary separation
unit to the compression tooth groove space of the female rotor; an oil drain line
that supplies the oil separated by the primary separation unit and used to lubricate
the bearing of the rotor to a low-pressure tooth groove of the rotor without using
the primary separation oil supply line; and a secondary separation oil supply line
that is connected to the primary separation oil supply line, the secondary separation
oil supply line supplying the oil separated by the secondary separation unit to the
compression tooth groove space of the female rotor.
[0006] A fluid mixture of the oil and the gas passes through the secondary separation oil
supply line. Thus, when the secondary separation oil supply line is connected to the
primary separation oil supply line, the fluid mixture of the primarily separated oil
and the pressurized gas is supplied to the compression tooth groove space of the female
rotor. Accordingly, when the fluid mixture is released to the compression tooth groove
space of the female rotor, the dispersion of the oil is promoted, and hence the deflection
of the oil hardly occurs in the tooth groove of the female rotor. Accordingly, oil
shortage is prevented between the inner wall of the rotor chamber and the tooth tip
of the female rotor as the seal portion where particularly partial oil shortage easily
occurs, and hence a back flow in which the gas in the course of compression leaks
therebetween may be prevented. Thus, the power necessary for driving the rotor in
order to compress the leakage gas again decreases, and hence the amount of the air
discharged from the compressor body may be also increased.
[0007] Further, since the fluid mixture is released to the compression tooth groove space
of the female rotor, the atomization of the oil is promoted, and hence the surface
area of the oil with respect to the amount of the oil supplied to the female rotor
increases. Thus, heat is easily exchanged between the oil supplied to the compressor
body and the gas in the course of compression. Accordingly, since the efficiency of
the cooling process using the oil is improved, the gas almost becomes an isothermal
compression state, and hence the power for driving the female rotor decreases. The
tooth tip width of the tooth of the female rotor is generally narrow, and the amount
of the gas leaking between the tooth tip of the female rotor and the compressor body
is easily affected by the existence of the oil therebetween. Further, since the volume
of the tooth groove of the female rotor is larger than that of the male rotor, it
is considered that the merit in which the fluid mixture is supplied to the compression
tooth groove space of the female rotor is larger than that of the case where the fluid
mixture is supplied to the male rotor.
[0008] The primary separation oil supply line may be further connected to a compression
tooth groove space of the male rotor defined by the inner wall of the rotor chamber
and a pair of adjacent teeth of the male rotor in a cross-section perpendicular to
the rotor shaft of the compressor body and may supply the oil which is separated by
the primary separation unit and does not include the oil passing through the secondary
separation oil supply line to the compression tooth groove space of the male rotor.
Alternately, the compressor may further include another primary separation oil supply
line for the male rotor that is connected to a compression tooth groove space of the
male rotor defined by the inner wall of the rotor chamber and a pair of adjacent teeth
of the male rotor in a cross-section perpendicular to the rotor shaft of the compressor
body and the oil collector and supplies the oil separated by the primary separation
unit to the compression tooth groove space of the male rotor.
[0009] With the above-described configuration, the oil may be supplied to compression tooth
groove space of the male rotor in addition to the compression tooth groove space of
the female rotor so as to perform a lubricating operation and a cooling operation.
Further, since the primarily separated oil is supplied to the compression tooth groove
space of the male rotor, it is possible to ensure the amount of the oil enough for
keeping the sealing performance. As a result, it is possible to prevent the back flow
of the gas between the tooth tip of the male rotor and the inner wall of the rotor
chamber. Thus, the power necessary for driving the rotor in order to compress the
leakage gas again may be decreased, and hence the amount of the air discharged from
the compressor body may be also increased.
[0010] The secondary separation oil supply line may be connected to the primary separation
oil supply line connected to the compression tooth groove space of the male rotor
and may also supply the oil separated by the secondary separation unit to the compression
tooth groove space of the male rotor. Alternatively, the oil separated by the secondary
separation unit may be supplied to the compression tooth groove space of the male
rotor through the primary separation oil supply line.
[0011] Since the fluid mixture of the primarily separated oil and the secondarily separated
oil including the compressed gas may be supplied to the compression tooth groove space
of the male rotor in addition to the compression tooth groove space of the female
rotor, the atomization of the oil is promoted when the fluid mixture is released to
the compression tooth groove space of the male rotor. Accordingly, since the surface
area of the oil with respect to the amount of the oil supplied to the male rotor increases,
heat is easily exchanged between the oil supplied to the compressor body and the gas
in the course of compression. Since the efficiency of the cooling process using the
oil is improved, the gas almost becomes an isothermal compression state, and hence
the power for driving the rotor decreases. Further, when the fluid mixture is released
to the compression tooth groove space of the male rotor, the dispersion of the oil
is promoted, and hence the deflection of the oil inside the tooth groove of the male
rotor hardly occurs. Accordingly, since the sealing performance inside the compressor
body is improved, the back flow in which the gas in the course of compression leaks
may be prevented. Accordingly, the power necessary for driving the rotor in order
to compress the leakage gas again decreases, and hence the amount of the air discharged
from the compressor body may be also increased.
[0012] The compressor may further include a primary separation oil supply line that supplies
oil to the bearing on the side of the discharge port, wherein the primary separation
oil supply line that supplies oil to the discharge side bearing is provided with a
throttle portion which decreases an oil supply amount.
[0013] Since the throttle portion is provided, the amount of the oil supplied to the bearing
may be suppressed to the minimum amount necessary to lubricate the bearing. Meanwhile,
even in the oil which increases in temperature after the lubrication of the bearing,
there is no need to worry the suction even when the oil is returned to the suction
space if the amount of the oil is extremely small. For that reason, since the throttle
portion is provided, it is possible to select the suction space as a place where the
oil lubricating the bearing while suppressing an increase in power necessary for a
driving operation or degradation in performance may be returned.
[0014] According to the present invention, it is possible to decrease the power necessary
for driving the compressor.
BRIEF DESCRIPTION OF THE DRAWINGS
[0015]
FIG. 1A is a schematic view illustrating a compressor according to a first embodiment
of the present invention, FIG. 1B is an enlarged side view illustrating the inside
of a compressor body, and FIG. 1C is a schematic view illustrating the position of
an oil inflow port provided in a rotor chamber.
FIG. 2 is an enlarged side view illustrating the inside of a compressor body according
to a second embodiment of the present invention.
FIG. 3 is an enlarged side view illustrating the inside of a compressor body according
to a reference example of the present invention.
FIG. 4 is an enlarged side view illustrating the inside of a compressor body according
to a modified example of the present invention.
FIG. 5 is an enlarged side view illustrating the inside of a compressor body according
to another modified example of the present invention.
FIG. 6A is a schematic view illustrating a compressor according to a first comparative
example, and FIG. 6B is an enlarged side view illustrating the inside of a compressor
body.
FIG. 7A is a schematic view illustrating a compressor according to a second comparative
example and
FIG. 7B is an enlarged side view illustrating the inside of a compressor body.
FIG. 8 is a graph illustrating a specific power with respect to a shaft power.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0016] Hereinafter, a first embodiment of the present invention will be described with reference
to the accompanying drawings.
[0017] FIG. 1A illustrates a compressor 1 according to a first embodiment of the present
invention. The compressor of the present invention is a screw type compressor 1, and
is lubricated and cooled by oil flowing therein. The compressor 1 includes a compressor
body 10 and an oil collector 30.
[0018] The compressor body 10 includes a rotor casing 12 which is provided in a rotor chamber
11 therein so as to accommodate a screw rotor 20 to be described later in a rotatable
state. The compressor body 10 includes a suction port 13 which suctions a gas from
the outside and a discharge port 14 which discharges a gas.
[0019] As illustrated in FIG. 1B, the screw rotor 20 includes a pair of rotors, that is,
a female rotor 22 and a male rotor 24. A tooth groove 27a is formed between a pair
of teeth 22a and 22a adjacent to each other in the circumferential direction of the
female rotor 22. When taking a look at a cross-section perpendicular to a rotor shaft
of the compressor body 10, a compression tooth groove space 27 of the female rotor
22 is defined between the inner wall of the rotor chamber 11 as the inner surface
of the rotor casing 12 and the pair of teeth 22a and 22a adjacent to each other in
the circumferential direction of the female rotor 22. When taking a look at a cross-section
perpendicular to the rotor shaft of the compressor body 10, in the same way as the
female rotor 22, a compression tooth groove space 28 of the male rotor 24 is defined
between the inner wall of the rotor chamber 11 as the inner surface of the rotor casing
12 and a pair of teeth 24a and 24a adjacent to each other in the circumferential direction
of the male rotor 24. One of both rotors 22 and 24 is connected to an electric motor
(not illustrated) provided in the rotor casing 12. In each of a rotor shaft 23 which
serves as the rotation center of the female rotor 22 and a rotor shaft 25 which serves
as the rotation center of the male rotor 24, the suction side is supported by a suction
side bearing 15 which is provided in the rotor casing 12. The discharge side of each
of the rotor shafts 23 and 25 is supported by a discharge side bearing 16 which is
provided in the rotor casing 12. Furthermore, FIG. 1A representatively illustrates
only the female rotor 22 as the screw rotor 20.
[0020] A gas which is suctioned from the upside through the suction port 13 in a manner
such that an electric motor rotates the screw rotor 20 is compressed by the rotation
of the female rotor 22 and the male rotor 24, and is discharged as a high-pressure
gas to the downside through the discharge port 14.
[0021] The oil collector 30 includes a hollow cylinder 31, a separation unit 34 which serves
as a primary separation unit including the inner wall (the inner wall surface) of
the oil collector 30, a filter 32 which serves as a secondary separation unit, and
an oil reservoir 33. The discharged compression gas is introduced into the separation
unit 34 of the oil collector 30 through a discharge line 35 including the discharge
port 14 and the discharge passageway. At this time, a compression air is introduced
in a substantially tangential direction to an annular passageway formed between the
hollow cylinder 31 and the inner wall of the oil collector 30, and the oil and the
gas are centrifugally separated from each other by a swirl flow generated at that
time. In this way, the oil is primarily separated from the compression gas which includes
an oil element flowing into the oil collector 30 through the discharge line 35. The
compression gas from which the oil is primarily separated is guided to the filter
32 through the hollow cylinder 31. The filter 32 is formed as, for example, a demister,
and the oil is secondarily separated from the gas when the compression gas passes
through the filter. The oil reservoir 33 collects the oil which is primarily separated
and falls along the inner wall surface of the oil collector 30 by the own weight.
Furthermore, the compression gas from which the oil is separated twice is supplied
to a compression gas supply target through a supply pipe 36 communicating with the
filter 32. For example, the compression gas is supplied to a gas supply target such
as a factory. The oil which is primarily separated from the gas inside the oil collector
30 is guided into the rotor casing 12 through a supply side line of an oil circulation
line 40 causing the oil collector 30 and the compressor body 10 to communicate with
each other.
[0022] The oil circulation line 40 includes a supply side line including a primary separation
oil supply line 41, a secondary separation oil supply line 52, and a discharge side
bearing oil drain line 54 and a collection side line including the discharge line
35. One end of the primary separation oil supply line 41 communicates with the oil
reservoir 33, and the other end thereof is divided into three sub-oil supply lines
42, 46, and 48.
[0023] The end of the rotor chamber oil supply line 42 as the sub-oil supply line 42 is
divided into a female rotor side oil supply line 43 and a male rotor side oil supply
line 44 (see FIG. 1B). The female rotor side oil supply line 43 communicates with
the female rotor side compression tooth groove space 27 through an oil inflow port
17 which is provided in the rotor chamber 11 on the side of the female rotor 22. Specifically,
the female rotor side oil supply line 43 is connected to the female rotor side compression
tooth groove space 27 which is defined between the inner wall of the rotor chamber
11 and the pair of teeth 22a and 22a adjacent to each other in the female rotor 22
in the cross-section perpendicular to the rotor shaft of the compressor body 10 (see
FIG. 1C). The oil inflow port 17 is provided at a position facing the female rotor
22 in the rotor chamber 11. The male rotor side oil supply line 44 communicates with
the male rotor side compression tooth groove space 28 through an oil inflow port 18
provided in the rotor chamber 11 on the side of the male rotor 24. Specifically, the
male rotor side oil supply line 44 is connected to the male rotor side compression
tooth groove space 28 which is defined between the inner wall of the rotor chamber
11 and the pair of teeth 24a and 24a adjacent to each other in the male rotor 24 in
the cross-section perpendicular to the rotor shaft of the compressor body 10 (see
FIG. 1C). The oil inflow port 18 is provided at a position facing the male rotor 24
in the rotor chamber 11. The end of the discharge side bearing oil supply line 46
as the sub-oil supply line 46 communicates with the discharge side bearing 16. The
end of the suction side bearing oil supply line 48 as the sub-oil supply line 48 communicates
with the suction side bearing 15.
[0024] A throttle portion 50 which reduces the oil supply amount to the discharge side bearing
16 is provided in the middle of the discharge side bearing oil supply line 46. The
throttle portion 50 is, for example, an orifice formed in an oil hole. Since the throttle
portion 50 is provided, it is possible to suppress the amount of the oil necessary
for lubricating the discharge side bearing 16 as minimal as possible. Similarly, the
throttle portion 50 is provided in the middle of the suction side bearing oil supply
line 48. Furthermore, in the first embodiment, the discharge side bearing oil supply
line 46 and the suction side bearing oil supply line 48 are provided with the throttle
portion 50, but the present invention is not limited thereto. For example, a configuration
may be employed in which the throttle portion 50 is provided only in the discharge
side bearing oil supply line 46 in which the temperature of the oil used to lubricate
the bearing easily increases.
[0025] One end of the secondary separation oil supply line 52 communicates with the filter
32 of the oil collector 30, and the other end thereof communicates with the female
rotor side oil supply line 43 of the primary separation oil supply line 41 in a connection
state. Furthermore, a fluid mixture obtained by mixing at least a part of the oil
secondarily separated by the filter 32 and a part of the gas is guided into the secondary
separation oil supply line 52.
[0026] One end of the discharge side bearing oil drain line 54 communicates with the discharge
side bearing 16, and the other end thereof communicates with the inside of the rotor
chamber 11 through a communication port 19 which is provided at a position just after
the confinement of both rotors 22 and 24.
[0027] Hereinafter, the circulation line of the oil used to lubricate the compressor 1 will
be described.
[0028] The oil which is primarily separated from the compression gas discharged from the
compressor body 10 and is accumulated in the oil reservoir 33 is supplied to the compressor
body 10 through the primary separation oil supply line 41. The oil which is guided
to the rotor chamber oil supply line 42 of the primary separation oil supply line
41 is supplied to the compression tooth groove space 27 of the female rotor 22 through
the female rotor side oil supply line 43, and is supplied to the compression tooth
groove space 28 of the male rotor 24 through the male rotor side oil supply line 44.
The oil which is supplied from the oil inflow ports 17 and 18 into the rotor chamber
11 is used to cool the compression gas, to lubricate the rotors 22 and 24, and to
seal a gap between the rotors 22 and 24.
[0029] The oil which is secondarily separated by the filter 32 from the compression gas
from which the oil is primarily separated is guided to the female rotor side oil supply
line 43 through the secondary separation oil supply line 52. Accordingly, a fluid
mixture of the primary separation oil and the pressurized gas including the secondary
separation oil is injected toward the compression tooth groove space 27 of the female
rotor 22 corresponding to the position in the course of the compression of the gas
of the female rotor. Furthermore, when the pressure of the compression tooth groove
space 27 of the female rotor 22 is too high, the oil supply amount decreases. For
this reason, it is desirable to supply the fluid mixture to the compression tooth
groove space 27 having a pressure less than an intermediate pressure between a suction
pressure and a discharge pressure.
[0030] As described above, when the secondary separation oil supply line 52 is connected
to the female rotor side oil supply line 43 (the primary separation oil supply line
41), the fluid mixture of the oil and the gas is injected when the oil is supplied
from the oil reservoir 33 to the compression tooth groove space 27 of the female rotor
22. For this reason, the dispersion of the oil released to the compression tooth groove
space 27 is promoted and the deflection of the oil inside the tooth groove hardly
occurs. Accordingly, oil shortage is prevented between the rotor chamber 11 and the
tooth tip of the female rotor 22 as a portion in which partial oil shortage particularly
easily occurs, and hence a back flow in which the gas in the course of compression
leaks therebetween may be prevented. Thus, the power necessary for driving the rotors
22 and 24 in order to compress the leakage gas again decreases, and hence the amount
of air discharged from the compressor body 10 may be also increased.
[0031] Further, since the fluid mixture of the oil and the pressurized gas is released to
the compression tooth groove space 27 of the female rotor 22, the atomization of the
oil is promoted, and hence the surface area of the oil with respect to the amount
of the oil supplied to the female rotor 22 increases. Thus, heat is easily exchanged
between the fluid mixture supplied to the rotor chamber 11 and the gas in the course
of compression. Accordingly, since the efficiency of the cooling process using the
oil is improved, the gas almost becomes an isothermal compression state, and hence
the power for driving the female rotor 22 decreases. The tooth in the female rotor
22 generally has a narrow tooth tip width, and the amount of the gas leaking between
the tooth tip of the female rotor 22 and the rotor chamber 11 easily affects the existence
oil therebetween. Further, since the volume of the tooth groove in the female rotor
22 is larger than that of the male rotor 24, the merit in which the fluid mixture
is supplied to the compression tooth groove space 27 of the female rotor 22 is larger
than that of the case where the fluid mixture is supplied to the male rotor 24.
[0032] The oil which is supplied to the discharge side bearing 16 so as to lubricate and
cool the discharge side bearing 16 and is guided to the discharge side bearing oil
drain line 54, and is returned to the rotor chamber 11 having a low pressure just
after the confinement through the communication port 19.
[0033] The present invention is not limited to the first embodiment, and may be modified
into various forms. In the first embodiment, the other end of the secondary separation
oil supply line 52 is connected to only the female rotor side oil supply line 43,
and communicates with the compression tooth groove space 27 of the female rotor 22
through the primary separation oil supply line 41. However, the present invention
is not limited thereto. For example, as an example illustrated in FIG. 2, the other
end of the secondary separation oil supply line 52 may be connected to the female
rotor side oil supply line 43 and the male rotor side oil supply line 44, and may
communicate with the compression tooth groove space 27 of the female rotor 22 and
the compression tooth groove space 28 of the male rotor 24 through the rotor chamber
oil supply line 42 as the primary separation oil supply line 41 (a second embodiment).
[0034] With the above-described configuration, the fluid mixture of the primary separation
oil and the gas including the secondary separation oil may be supplied to not only
the female rotor 22, but also the compression tooth groove space 28 of the male rotor
24. Accordingly, since the fluid mixture is released to the compression tooth groove
space 28 of the male rotor 24, the atomization of the oil is promoted, and hence the
surface area of the oil with respect to the amount of the oil supplied to the male
rotor 24 increases. Thus, heat is easily exchanged between the oil supplied to the
compressor body 10 and the gas in the course of compression. Accordingly, since the
efficiency of the cooling process using the oil is improved, the gas almost becomes
an isothermal compression state, and hence the power for driving the rotors 22 and
24 may be decreased. Further, the dispersion of the oil when the fluid mixture is
released to the compression tooth groove space 28 of the male rotor 24 is promoted,
and hence the deflection of the oil inside a tooth groove 28a of the male rotor 24
hardly occurs. Accordingly, it is possible to improve the sealing performance inside
the rotor chamber 11. Thus, the power necessary for driving the rotors 22 and 24 may
be decreased, and the amount of air discharged from the compressor body 10 may be
increased.
[0035] However, since the fluid mixture supplied to the compression tooth groove space 27
of the female rotor 22 decreases as much as the fluid mixture supplied to the compression
tooth groove space 28 of the male rotor 24, a power reduction effect due to the improvement
in sealing performance becomes smaller than that of the first embodiment. The power
reduction effect decrease amount is larger than the power reduction effect increase
amount obtained by the improvement in cooling efficiency of the second embodiment.
In a balance state, the power increases and the sealing performance decreases, and
hence the performance of the compressor 1 is slightly degraded compared to the first
embodiment as a whole. This is because the width of the tool tip of the female rotor
22 is narrower than that of the male rotor 24 and the tooth groove space is also large
as described above. Accordingly, it is considered that the oil distribution becomes
more sensitive compared to the male rotor 24.
[0036] Furthermore, in the second embodiment, the other end of the secondary separation
oil supply line 52 is connected to the female rotor side oil supply line 43 and the
male rotor side oil supply line 44 through the rotor chamber oil supply line 42. However,
the present invention is not limited thereto, and the secondary separation oil supply
line 52 may be divided into the secondary separation oil supply line 52 connected
to the female rotor side oil supply line 43 and the secondary separation oil supply
line 52 connected to the male rotor side oil supply line 44. In that case, the secondary
separation oil supply line 52 may be a secondary separation oil supply line in which
the line from one end to the other end thereof is separated or a secondary separation
oil supply line in which one line is divided from the other end (see FIG. 4).
[0037] FIG. 3 illustrates a reference example in which the other end of the secondary separation
oil supply line 52 is connected to only the male rotor side oil supply line 44 instead
of the female rotor side oil supply line 43 (a reference example).
[0038] Referring to FIG. 8, it is understood that the specific power of the second embodiment
is higher than that of the first embodiment. Thus, it is proved that energy may be
saved in that the compressor of the first embodiment may compress a large amount of
air by a power smaller than the compressor of the second embodiment. In the reference
example, it is understood that the specific power is larger than those of the first
embodiment and the second embodiment. Thus, in the compressors of the first embodiment
and the second embodiment of the present invention including the primary separation
oil supply line 41 which is connected to the oil collector 30 and the compression
tooth groove space 27 of the female rotor 22 and supplies the oil separated by the
separation unit 34 as the primary separation unit of the oil collector 30 to the compression
tooth groove space 27 of the female rotor 22 and the secondary separation oil supply
line 52 which supplies the oil separated by the filter 32 as the secondary separation
unit to the compression tooth groove space 27 of the female rotor 22 and is connected
to the primary separation oil supply line 41, it is proved that energy may be saved
in that a large amount of air may be compressed by a power smaller than the compressor
of the reference example.
[0039] Further, in the first embodiment, the discharge side bearing oil supply line 46 and
the suction side bearing oil supply line 48 are formed by dividing the primary separation
oil supply line 41. However, the present invention is not limited thereto, and the
ends of the discharge side bearing oil supply line 46 and the suction side bearing
oil supply line 48 may directly communicate with the oil reservoir 33. However, in
any case, there is a need to supply the oil used to lubricate the bearing to the tooth
groove 27a and 28a of the rotors 22 and 24 just before the compression start (just
before the confinement) or the low-pressure tooth grooves of the rotors 22 and 24
as the tooth grooves 27a and 28a of the rotors 22 and 24 just after the compression
start (just after the confinement) without using the primary separation oil supply
line 41.
[0040] Furthermore, a method of connecting the secondary separation oil supply line 52 to
the primary separation oil supply line 41 is not limited to the above-described embodiment,
and may be modified into various forms.
[0041] Further, in the above-described embodiment, the end of the rotor chamber oil supply
line 42 as the sub-oil supply line 42 is divided into the female rotor side oil supply
line 43 and the male rotor side oil supply line 44. However, as illustrated in FIG.
5, the female rotor side oil supply line 43 and the male rotor side oil supply line
44 may be formed respectively as the separate primary separation oil supply lines.
Here, in a case where the secondary separation oil supply line is connected to the
female rotor side oil supply line 43 and the male rotor side oil supply line 44 as
the primary separation oil supply line, the secondary separation oil supply line may
be connected only to the female rotor side oil supply line 43. As a modified example,
the secondary separation oil supply line may be connected to the male rotor side oil
supply line 44 in addition to the female rotor side oil supply line 43.
[0042] FIG. 6A illustrates the compressor 2 of a first comparative example in which the
end of the secondary separation oil supply line 52 directly communicates with the
rotor chamber 11. In this drawing, the same reference numerals will be given to the
same components as the compressor 1 of FIGS. 1A to 1C, and the repetitive description
will not be presented.
[0043] In the first comparative example, as illustrated in FIG. 6B, the end of the rotor
chamber oil supply line 42 communicates with the rotor chamber 11 through a primary
separation oil inflow port 81 provided between the female rotor 22 and the male rotor
24 of the rotor chamber 11. That is, in the first comparative example, the end of
the rotor chamber oil supply line 42 is connected to the compression tooth groove
space as the connection portion of the compression tooth groove spaces 27 and 28 of
the female and male rotors 22 and 24 defined by the inner wall of the rotor chamber
11 and the tooth 24a of the male rotor 24 and the tooth 22a of the female rotor 22
in the cross-section perpendicular to the rotor shaft of the compressor body 10. The
end of the secondary separation oil supply line 52 is located on the side of the suction
side bearing 15 of the rotor chamber 11 in relation to the primary separation oil
inflow port 81, and directly communicates with the rotor chamber 11 through a secondary
separation oil inflow port 82 provided between the female rotor 22 and the male rotor
24. The discharge side bearing oil drain line 54 communicates with the rotor chamber
11 through a communication port 83 provided between the female rotor 22 and the male
rotor 24. The communication port 83 is disposed between the primary separation oil
inflow port 81 and the secondary separation oil inflow port 82 in the axial direction
of the screw rotor 20.
[0044] With the above-described configuration, in the compressor 2 of the first comparative
example, the secondarily separated oil is directly returned to the low-pressure tooth
grooves of the female rotor 22 and the male rotor 24 just after the compression start
through the secondary separation oil inflow port 82 provided on the side of the suction
side bearing 15 of the rotor chamber 11. The temperature of a large amount of gas
including the oil flowing through the secondary separation oil supply line 52 becomes
higher than that of the gas in the low-pressure tooth groove. Thus, when the high-temperature
gas including the oil is supplied to the low-pressure tooth groove having a uniform
volume, a force in which the gas in the course of compression expands serves as a
pressure. Further, since a difference in pressure between the low-pressure tooth groove
receiving the high-temperature gas and the upstream pressure increases, the back flow
of the gas in the course of compression easily occurs. Accordingly, the power necessary
for driving the compressor 2 increases and the amount of the discharge air decreases.
Referring to FIG. 8, it is proved that the performance is improved by 3.6% at the
specific power in the first embodiment compared to the first comparative example when
the shaft power is around A (kW).
[0045] FIGS. 7A and 7B illustrates the compressor 3 of a second comparative example in which
the end of the discharge side bearing oil drain line 54 communicates with the rotor
chamber oil supply line 42 in a connection state in addition to the end of the secondary
separation oil supply line 52. In this drawing, the same reference numerals will be
given to the same components as the compressor 1 of FIGS. 1A to 1C, and the repetitive
description will not be presented. In the compressor 3 of the second comparative example,
the rotor chamber oil supply line 42 communicates with the rotor chamber 11 through
an oil inflow port 88 provided between the female rotor 22 and the male rotor 24 of
the rotor chamber 11. That is, even in the second comparative example, the end of
the rotor chamber oil supply line 42 is connected to the compression tooth groove
space as the connection portion of the compression tooth groove spaces 27 and 28 of
the female and male rotors 22 and 24 defined by the inner wall of the rotor chamber
11 and the tooth 24a of the male rotor 24 and the tooth 22a of the female rotor 22
in the cross-section perpendicular to the rotor shaft of the compressor body 10.
[0046] In the second comparative example, since the rotor chamber oil supply line 42 becomes
a high pressure state, the oil is not easily returned from the discharge side bearing
oil drain line 54 to the rotor chamber oil supply line 42, and the flow of the oil
used to lubricate the discharge side bearing 16 is blocked. Accordingly, there is
a concern that the lifetime of the discharge side bearing 16 may be degraded. Further,
the mixing loss in the discharge side bearing 16 is large. In the second comparative
example, the oil may not be forcedly caused to flow to the discharge side bearing
16 by using the existing oil line. For this operation, there is a need to provide
an orifice and the like between the joint point of the secondary separation oil supply
line 52 and the joint point of the discharge side bearing oil drain line 54 in the
rotor chamber oil supply line 42. However, in this method, the oil supply amount of
the rotor chamber oil supply line 42 essentially decreases. At this time, the oil
supply amount to the rotor chamber 11 decreases, the compression gas temperature increases,
and the leakage amount increases. Accordingly, there is a high possibility that the
power necessary for driving the compressor increases and the amount of the discharge
air decreases. In this way, the second comparative example is not practical in that
the power necessary for the driving operation may not be decreased, and is different
from the first and second embodiments although there is similarity. The first and
second embodiments are practical in that the power necessary for driving the rotors
22 and 24 may be decreased and the amount of the air discharged from the compressor
body 10 may be increased.
[0047] The present invention is not limited to the above-described embodiments, and may
be modified into various forms.
1. A compressor (1) comprising:
a compressor body (10) that includes a suction port (13) which suctions a gas, a pair
of rotors comprising a female rotor (22) and a male rotor (24) which are rotatably
supported by a suction side bearing (15) and a discharge side bearing (16) and compressing
the gas suctioned from the suction port (13) in cooperation with a rotor chamber (11),
and a discharge port (14) which discharges the compressed gas;
an oil collector (30) that includes a primary separation unit (34) which primarily
separates an oil from the gas compressed by the compressor body (10) and a secondary
separation unit (32) which secondarily separates an oil from the gas from which the
oil is primarily separated by the primary separation unit (34);
a primary separation oil supply line (41) that is connected to the oil collector (30),
and a secondary separation oil supply line (52) that is connected to the primary separation
oil supply line (41), wherein
one end of the primary separation oil supply line (41) communicates with the oil collector
(30), and the other end thereof is divided into a rotor chamber oil supply line (42),
a discharge side bearing oil supply line (46) and a suction side bearing oil supply
line (48),
the primary separation oil supply line (41) is connected to a compression tooth groove
space (27) of the female rotor (22) defined by an inner wall of the rotor chamber
(11) and a pair of adjacent teeth of the female rotor (22) in a cross-section perpendicular
to a rotor shaft of the compressor body (10), the primary separation oil supply line
(41) supplying the oil separated by the primary separation unit (34) to the bearings
(15, 16) of the rotor and the compression tooth groove space (27) of the female rotor
(22);
the secondary separation oil supply line (52) supplying the oil separated by the secondary
separation unit (32) to the compression tooth groove space (27) of the female rotor
(22), and
one end of the secondary separation oil supply line (52) communicates with the secondary
separation unit (32), and the other end of the secondary separation oil supply line
(52) is connected to the rotor chamber oil supply line (42) of the primary separation
oil supply line (41), the compressor further comprising
an oil drain line (54) connected to the compressor body (10) that supplies the oil
separated by the primary separation unit (34) and used to lubricate the discharge
side bearing (16) of the rotor (22, 24) to a low-pressure tooth groove of the rotor
(22, 24) without using the primary separation oil supply line (41).
2. The compressor (1) according to claim 1,
wherein the rotor chamber oil supply line (42) is further connected to a compression
tooth groove space (28) of the male rotor (24) defined by the inner wall of the rotor
chamber (11) and a pair of adjacent teeth of the male rotor (24) in a cross-section
perpendicular to the rotor shaft of the compressor body (10) and supplies the oil
which is separated by the primary separation unit (34) and does not include the oil
passing through the secondary separation oil supply line (52) to the compression tooth
groove space (28) of the male rotor (24).
3. The compressor (1) according to claim 1, further comprising:
another primary separation oil supply line for the male rotor (24) that is connected
to a compression tooth groove space (28) of the male rotor (24) defined by the inner
wall of the rotor chamber (11) and a pair of adjacent teeth of the male rotor (24)
in a cross-section perpendicular to the rotor shaft of the compressor body (10) and
the oil collector (30) and supplies the oil separated by the primary separation unit
(34) to the compression tooth groove space (28) of the male rotor (24).
4. The compressor (1) according to claim 3,
wherein the secondary separation oil supply line (52) is connected to the rotor chamber
oil supply line (42) connected to the compression tooth groove space (28) of the male
rotor (24) and also supplies the oil separated by the secondary separation unit (32)
to the compression tooth groove space (28) of the male rotor (24).
5. The compressor (1) according to claim 3,
wherein the oil separated by the secondary separation unit (32) is supplied to the
compression tooth groove space (28) of the male rotor (24) through the primary separation
oil supply line (41).
6. The compressor (1) according to any one of claims 1 to 5, wherein:
the discharge side bearing oil supply line (46) supplies an oil to the bearing (16)
on the side of the discharge port (14),
wherein the discharge side bearing oil supply line (46) that supplies an oil to the
discharge side bearing (16) is provided with a throttle portion (50) which decreases
an oil supply amount.
1. Verdichter (1), mit:
einem Verdichterkörper (10), der einen Ansauganschluss (13), welcher ein Gas ansaugt,
ein Paar von Rotoren, das einen Nebenrotor (22) und einen Hauptrotor (24) umfasst,
welche durch ein ansaugseitiges Lager (15) und ein abgabeseitiges Lager (16) drehbar
aufgenommen sind und das von dem Ansauganschluss (13) angesaugte Gas in Zusammenwirken
mit einer Rotorkammer (11) verdichtet, und einen Abgabeanschluss (14) umfasst, welcher
das verdichtete Gas abgibt;
einem Ölsammler (30), der eine Primärabscheideeinheit (34), welche ein Öl von dem
durch den Verdichterkörper (10) verdichteten Gas primär abscheidet, und eine Sekundärabscheideeinheit
(32) umfasst, welche ein Öl von dem Gas sekundär abscheidet, von welchem das Öl durch
die Primärabscheideeinheit (34) primär abgeschieden ist;
einer Primärabscheideölversorgungsleitung (41), die an den Ölsammler (30) angeschlossen
ist, und einer Sekundärabscheideölversorgungsleitung (52), die an die Primärabscheideölversorgungsleitung
(41) angeschlossen ist, wobei
ein Ende der Primärabscheideölversorgungsleitung (41) mit dem Ölsammler (30) in Verbindung
steht und das andere Ende davon in eine Rotorkammerölversorgungsleitung (42), eine
abgabeseitige Lagerölversorgungsleitung (46) und eine ansaugseitige Lagerölversorgungsleitung
(48) unterteilt ist,
die Primärabscheideölversorgungsleitung (41) mit einem Verdichtungszahnnutbereich
(27) des Nebenrotors (22) verbunden ist, der durch eine Innenwand der Rotorkammer
(11) und ein Paar in einem Querschnitt, der zu einer Rotorwelle des Verdichterkörpers
(10) senkrecht ist, benachbarter Zähne des Nebenrotors (22) begrenzt ist, wobei die
Primärabscheideölversorgungsleitung (41) das durch die Primärabscheideeinheit (34)
abgeschiedene Öl den Lagern (15, 16) des Rotors und dem Verdichtungszahnnutbereich
(27) des Nebenrotors (22) zuführt;
die Sekundärabscheideölversorgungsleitung (52) das durch die Sekundärabscheideeinheit
(32) abgeschiedene Öl dem Verdichtungszahnnutbereich (27) des Nebenrotors (22) zuführt
und
ein Ende der Sekundärabscheideölversorgungsleitung (52) mit der Sekundärabscheideeinheit
(32) in Verbindung steht und das andere Ende der Sekundärabscheideölversorgungsleitung
(52) mit der Rotorkammerölversorgungsleitung (42) der Primärabscheideölversorgungsleitung
(41) verbunden ist, wobei der Verdichter ferner
eine Ölablaufleitung (54) hat, die mit dem Verdichterkörper (10) verbunden ist, die
das Öl einer Niederdruckzahnnut des Rotors (22, 24) zuführt, das durch die Primärabscheideeinheit
(34) abgeschieden ist und benutzt wird, um das abgabeseitige Lager (16) des Rotors
(22, 24) zu schmieren, ohne die Primärabscheideölversorgungsleitung (41) zu benutzen.
2. Verdichter (1) nach Anspruch 1,
wobei die Rotorkammerölversorgungsleitung (42) ferner mit einem Verdichtungszahnnutbereich
(28) des Hauptrotors (24) verbunden ist, der durch die Innenwand der Rotorkammer (11)
und ein Paar in einem Querschnitt, der zu einer Rotorwelle des Verdichterkörpers (10)
senkrecht ist, benachbarter Zähne des Hauptrotors (24) begrenzt ist und das Öl dem
Verdichtungszahnnutbereich (28) des Hauptrotors (24) zuführt, welches durch die Primärabscheideeinheit
(34) abgeschieden ist und nicht das Öl enthält, das durch die Sekundärabscheideölversorgungsleitung
(52) fließt.
3. Verdichter (1) nach Anspruch 1, ferner mit:
einer anderen Primärabscheideölversorgungsleitung für den Hauptrotor (24), die mit
einem Verdichtungszahnnutbereich (28) des Hauptrotors (24), der durch die Innenwand
der Rotorkammer (11) und ein Paar in einem Querschnitt, der zu einer Rotorwelle des
Verdichterkörpers (10) senkrecht ist, benachbarter Zähne des Hauptrotors (24) begrenzt
ist und dem Ölsammler (30) verbunden ist und das durch die Primärabscheideeinheit
(34) abgeschiedene Öl dem Verdichtungszahnnutbereich (28) des Hauptrotors (24) zuführt.
4. Verdichter (1) nach Anspruch 3,
wobei die Sekundärabscheideölversorgungsleitung (52) mit der Rotorkammerölversorgungsleitung
(42) verbunden ist, die mit dem Verdichtungszahnnutbereich (28) des Hauptrotors (24)
verbunden ist, und das durch die Sekundärabscheideeinheit (32) abgeschiedene Öl zudem
dem Verdichtungszahnnutbereich (28) des Hauptrotors (24) zuführt.
5. Verdichter (1) nach Anspruch 3,
wobei das durch die Sekundärabscheideeinheit (32) abgeschiedene Öl durch die Primärabscheideölversorgungsleitung
(41) dem Verdichtungszahnnutbereich (28) des Hauptrotors (24) zugeführt ist.
6. Verdichter (1) nach einem der Ansprüche 1 bis 5, wobei:
die abgabeseitige Lagerölversorgungsleitung (46) dem Lager (16) auf der Seite des
Abgabeanschlusses (14) ein Öl zuführt,
wobei die abgabeseitige Lagerölversorgungsleitung (46), die dem abgabeseitigen Lager
(16) ein Öl zuführt, mit einem Drosselabschnitt (50) versehen ist, welcher eine Ölversorgungsmenge
verringert.
1. Compresseur (1) comprenant :
un corps de compresseur (10) qui comprend un orifice d'aspiration (13) qui aspire
un gaz, une paire de rotors comprenant un rotor femelle (22) et un rotor mâle (24)
qui sont supportés de manière rotative par un palier côté aspiration (15) et un palier
côté décharge (16) et comprimant le gaz aspiré par l'orifice d'aspiration (13) en
coopération avec une chambre de rotor (11), et un orifice de décharge (14) qui décharge
le gaz comprimé ;
un collecteur d'huile (30) qui comprend une unité de séparation principale (34) qui
sépare principalement une huile du gaz comprimé par le corps de compresseur (10) et
une unité de séparation secondaire (32) qui sépare secondairement une huile du gaz
duquel l'huile est principalement séparée par l'unité de séparation principale (34)
;
une conduite d'alimentation en huile de séparation principale (41) qui est raccordée
au collecteur d'huile (30), et une conduite d'alimentation en huile de séparation
secondaire (52) qui est raccordée à la conduite d'alimentation en huile de séparation
principale (41), dans lequel
une extrémité de la conduite d'alimentation en huile de séparation principale (41)
communique avec le collecteur d'huile (30), et son autre extrémité est divisée en
une conduite d'alimentation en huile de chambre de rotor (42), une conduite d'alimentation
en huile de palier côté décharge (46) et une conduite d'alimentation en huile de palier
côté aspiration (48),
la conduite d'alimentation en huile de séparation principale (41) est raccordée à
un espace de rainure de dent de compression (27) du rotor femelle (22) défini par
une paroi interne de la chambre de rotor (11) et une paire de dents adjacentes du
rotor femelle (22) dans une section transversale perpendiculaire à un arbre de rotor
du corps de compresseur (10), la conduite d'alimentation en huile de séparation principale
(41) fournissant l'huile séparée par l'unité de séparation principale (34) aux paliers
(15, 16) du rotor et à l'espace de rainure de dent de compression (27) du rotor femelle
(22) ;
la conduite d'alimentation en huile de séparation secondaire (52) fournissant l'huile
séparée par l'unité de séparation secondaire (32) à l'espace de rainure de dent de
compression (27) du rotor femelle (22), et
une extrémité de la conduite d'alimentation en huile de séparation secondaire (52)
communique avec l'unité de séparation secondaire (32), et l'autre extrémité de la
conduite d'alimentation en huile de séparation secondaire (52) est raccordée à la
conduite d'alimentation en huile de chambre de rotor (42) de la conduite d'alimentation
en huile de séparation principale (41), le compresseur comprenant en outre
une conduite de drain d'huile (54) raccordée au corps de compresseur (10) qui fournit
l'huile séparée par l'unité de séparation principale (34) et utilisée pour lubrifier
le palier côté décharge (16) du rotor (22, 24) à une rainure de dent à basse pression
du rotor (22, 24) sans utiliser la conduite d'alimentation en huile de séparation
principale (41) .
2. Compresseur (1) selon la revendication 1,
dans lequel la conduite d'alimentation en huile de chambre de rotor (42) est en outre
raccordée à un espace de rainure de dent de compression (28) du rotor mâle (24) défini
par la paroi interne de la chambre de rotor (11) et une paire de dents adjacentes
du rotor mâle (24) dans une section transversale perpendiculaire à l'arbre de rotor
du corps de compresseur (10) et fournit l'huile qui est séparée par l'unité de séparation
principale (34) et ne comprend pas l'huile passant par la conduite d'alimentation
en huile de séparation secondaire (52) jusqu'à l'espace de rainure de dent de compression
(28) du rotor mâle (24).
3. Compresseur (1) selon la revendication 1, comprenant en outre :
une autre conduite d'alimentation en huile de séparation principale pour le rotor
mâle (24) qui est raccordée à un espace de rainure de dent de compression (28) du
rotor mâle (24) défini par la paroi interne de la chambre de rotor (11) et une paire
de dents adjacentes du rotor mâle (24) dans une section transversale perpendiculaire
à l'arbre de rotor du corps de compresseur (10) et le collecteur d'huile (30) et fournit
l'huile séparée par l'unité de séparation principale (34) à l'espace de rainure de
dent de compression (28) du rotor mâle (24).
4. Compresseur (1) selon la revendication 3,
dans lequel la conduite d'alimentation en huile de séparation secondaire (52) est
raccordée à la conduite d'alimentation en huile de chambre de rotor (42) raccordée
à l'espace de rainure de dent de compression (28) du rotor mâle (24) et fournit également
l'huile séparée par l'unité de séparation secondaire (32) à l'espace de rainure de
dent de compression (28) du rotor mâle (24).
5. Compresseur (1) selon la revendication 3,
dans lequel l'huile séparée par l'unité de séparation secondaire (32) est amenée à
l'espace de rainure de dent de compression (28) du rotor mâle (24) par la conduite
d'alimentation en huile de séparation principale (41).
6. Compresseur (1) selon l'une quelconque des revendications 1 à 5, dans lequel :
la conduite d'alimentation en huile de palier côté décharge (46) fournit une huile
au palier (16) du côté de l'orifice de décharge (14),
dans lequel la conduite d'alimentation en huile de palier côté décharge (46) qui fournit
une huile au palier côté décharge (16) est prévue avec une partie d'étranglement (50)
qui diminue une quantité d'alimentation en huile.