BACKGROUND OF THE INVENTION:
Field of the Invention:
[0001] The present invention relates to a centrifugal compressor in a gas compressing system
available in the field of the petrochemistry or the like.
Description of the Prior Art:
[0002] Generally, regarding a centrifugal compressor, a capability of raising a pressure
with one stage of impeller has a limit, and in the case where a high pressure ratio
or a high pressure head is required, a multi-stage arrangement is employed. Normally,
the number of stages of impellers that can be accommodated within a single casing
is limited in order to insure rigidity of an axle and to realize safe operations.
Accordingly, in the prior art, in the case where a high pressure head was required,
it was realized by arraying a plurality of casings either in series or in parallel.
[0003] Fig. 3 illustrates one example of the arrangement in the prior art, in which in order
to realize a high pressure head, a gas compressing system was constructed by arraying
three casings of a first compressor 49, a second compressor 50 and a third compressor
51 in series as numbered sequentially from the suction side. The interior of the individual
compressor casing is composed of a multiple stages of centrifugal compressors. Driving
power fed from a driving machine is transmitted via a drive shaft 57, and it is distributed
from the third compressor 51 to the second compressor 50, and from the second compressor
50 to the first compressor 49, respectively by the intermediary of an intermediate
coupling.
[0004] An intake gas is sucked through a gas suction pipe 41, then it is compressed by the
first compressor 49, and it is delivered through a gas delivery pipe 42. The delivered
gas passes through an intermediate gas cooler 43, in which heat-exchange is effected
between the gas and a coolant water introduced from the outside through a coolant
water feed pipe 58, and thereby the gas is cooled. Again the gas is sucked through
a gas suction pipe 44 of the second compressor 50, and it is delivered through a gas
delivery pipe 45. Further again, the gas cooled by an intermediate gas cooler 46 in
a similar manner is sucked through a gas suction pipe 47 and compressed by the third
compressor 51, then it is delivered from a final gas delivery port 48, and it is used
as a high-pressure gas.
[0005] In the respective compressors, bearings are disposed in the proximities of the opposite
axial end surfaces of the casing, and in order to prevent the gas enclosed within
the casing from leaking out, gas seal means are disposed at the locations where the
drive shaft penetrates the end plates of each casing.
[0006] In the case of the illustrated example, use of a film seal or a mechanical seal as
the gas seal means is illustrated, and sealing oil appropriately adjusted so as to
meet the order of the gas pressure within the casing, is fed through sealing oil feed
tubes 52, 53 and 54, respectively. Though these mechanisms for feeding sealing oil
are constructed so as to follow the change of the pressure within the casing, if the
feed of sealing oil should become faulty, the sealing capability would be lost, and
hence, the gas seal means per se as well as the sealing oil feed mechanism are respectively
required to individually have a high reliability, and their manufacturing expense
would become high.
[0007] In addition, lubricant oil is fed to the bearings through a lubricant oil feed tube
55, and drain oil in the bearing boxes is drained through a lubricant oil pipe 56.
[0008] In the case where a compressor is composed of a large number of casings as is the
case with the above-described centrifugal compressor in the prior art, a large number
of seals for preventing the internal gas from leaking out to the atmosphere are necessitated
at the locations where the axle penetrates through the opposite axial end surfaces
of the respective casings. As the method for sealing the axle, various methods such
as an oil film seal method, a mechanical seal method, a gas seal method, etc. can
be employed depending upon the respective uses. However, in any event, the gap space
between the axle rotating at a high speed and a seal ring mounted to a stationary
portion is necessitated to be held narrow, and so, manufacture, assembly and maintenance
are necessitated to be paid with careful caution. Even if it were to be done, a possibility
that one of the large number of seal means may become faulty is large, and so, in
order to insure high reliability, it is necessary to use expensive materials and perform
machining at a high precision for the respective seal means.
[0009] Accordingly, in the case where a compressor is constructed by making use of a large
number of casings and employing a large number of seals as in the above-described
case, it is difficult to economically insure stable operations for a long period
of time.
[0010] In addition, in the case where a compressor is constructed of a large number of casings,
it is necessary to maintain the axes between the casings invariant during an operation,
hence the structures of the mounting tables of the respective casings would become
complex, moreover contrivance is made for the method of supporting the suction and
delivery pipings of gases to and from the respective casings, and a complex method
for mounting the pipings so that forces generated by deformation of the pipings may
not unnecessarily applied to the casings, is employed. In addition, since cooling
of gas for the purpose of efficiently compressing the gas is effected between delivery
from one casing and suction into the next casing, a gas cooler disposed separately
outside of the casings is employed, and hence, high-pressure gas pipings between the
respective implements would become long and complex.
[0011] As these disadvantages in the prior art would overlap on one another, a compressing
system for realizing compression of high pressure head is complicated in structure
and apt to have its reliability lowered, but nevertheless it was difficult to provide
the compressing system at a low cost.
[0012] Furthermore, since the volume of gas sucked into the first compressor is large, in
order to compress the gas efficiently, suction through an axial end surface is desirable,
but in the prior art, as oil-lubricated bearings are used, a complicated seal for
preventing oil from mixing into the gas is necessitated, and therefore, an extension
length of the axle to the outside of the bearing becomes too large, and there was
difficulty in a stable operation.
SUMMARY OF THE INVENTION:
[0013] It is therefore one object of the present invention to provide an improved centrifugal
compressor, that is free from the above-mentioned shortcomings in the prior art.
[0014] A more specific object of the present invention is to provide a centrifugal compressor,
in which stable operations over a long period time can be insured in an economical
manner.
[0015] Another object of the present invention is to provide a centrifugal compressor which
does not necessitate a large number of seal means.
[0016] Yet another object of the present invention is to provide a centrifugal compressor
which can be constructed in a less expensive matter without necessitating expensive
materials nor machining at a high precision.
[0017] Still another object of the present invention is to provide a centrifugal compressor
which does not necessitate a complicated mounting structure for maintaining axial
alignment of a plurality of axles having impellers thereon.
[0018] According to one feature of the present invention, there is provided a centrifugal
compressor comprising a plurality of axles each having centrifugal impellers that
can compress gas by making use of a centrifugal force exerted upon the gas, electromagnetic
bearings for supporting the axles at their opposite ends without being held in contact
with the axles, coupling means for coupling the axles with one another as arrayed
in series sequentially in such order that said gas can be compressed towards one side,
in such manner that misalignment of their axes with one another may be allowed, a
casing for supporting the plurality of coupled axles integrally with the electromagnetic
bearings therefor and having a suction port of gas at one end in the axial direction
and a delivery port thereof at the other end, and seal means around the axle provided
on the side having the delivery port of the casing.
[0019] According to another feature of the present invention, there is provided the above-featured
centrifugal compressor, wherein a gas cooling section for cooling the gas compressed
by the centrifugal impellers on the axles, is mounted to the casing.
[0020] According to still another feature of the present invention, there is provided the
first-featured centrifugal compressor, wherein a suction magnetic bearing for sucking
the axle on the gas suction side towards the gas delivery side is provided, and the
electromagnetic bearing on the gas delivery side is a thrust bearing for holding the
axle on the gas delivery side at a predetermined position in its axial direction.
[0021] According to yet another feature of the present invention, there is provided the
first-featured centrifugal compressor, wherein the coupling means is composed of restraining
shafts mounted to the adjacent axial ends of the axles so as to oppose to each other,
two flexible discs disposed around the restraining shafts and respectively mounted
to the respective axles, and a torque transmission tube connected to the flexible
discs.
[0022] According to the present invention, owing to the above-described construction that
a plurality of axles are disposed in series within a single casing and the respective
axles are supported by magnetic bearings at their opposite ends, bearing oil is not
necessitated. And, by disposing the bearings in the gas, the location where the axle
penetrates through the end surface on the high pressure side of the casing becomes
only one location on the side for transmitting driving power, and so, the number of
places where counter-measure for leakage of gas must be taken is greatly reduced,
and high reliability can be realized.
[0023] The above-mentioned and other objects, features and advantages of the present invention
will become more apparent by reference to the following description of one preferred
embodiment of the invention taken in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS:
[0024] In the accompanying drawings:
Fig. 1 is a longitudinal cross-section view of a centrifugal compressor according
to one preferred embodiment of the present invention;
Fig. 2 is a detailed longitudinal cross-section view of an intermediate coupling employed
in the same embodiment; and
Fig. 3 is a plan view of one example of a centrifugal compressor in the prior art.
DESCRIPTION OF THE PREFERRED EMBODIMENT:
[0025] Now, one preferred embodiment of the present invention will be described with reference
to Figs. 1 and 2.
[0026] In Fig. 1, gas sucked through a gas suction port 2 provided at one end of a casing
1 for sucking gas in the axial direction, is compressed by an impeller 26 mounted
to the tip end of a first axle 3. This gas passes along the outer circumference of
a bearing body supporting the axle 3, and while it is being compressed by a multiple
stages of centrifugal impellers, it is delivered from the last stage centrifugal impeller
mounted to the axle 3, and it flows out through a first delivery port 38. Thereafter,
the gas flows into a gas cooling section 4 mounted on the outer circumference of the
casing 1, where it passes through the interstices in a cooling tube group 6 which
is cooled by an externally supplied coolant water 5, and after it has been cooled
down to a predetermined temperature, it is led to a gas suction port 8 of a multi-stage
compressor assembly mounted to a second axle 7. The gas compressed again and delivered
through a delivery port 9 is again introduced into the gas cooling section 4 on the
outer circumference of the casing 1, and it is cooled there. The gas side chamber
in the gas cooling section 4 is partitioned into two chambers for use with the axle
3 and for use with the axle 7. The cooled gas is again introduced to a gas suction
port 10 of a multi-stage compressor assembly constructed by a third axle 12, and it
is again compressed there by a compressing action consisting of the action of the
impeller and the already known diffuser effect, in combination. The gas compressed
up to the final stage is delivered through a final delivery port 11 at a predetermined
pressure.
[0027] As described above, within a single casing 1 is disposed a compressor assembly composed
of a plurality of axles 3, 7 and 12 each having impellers mounted thereon, and a stationary
member for forming gas passageways to properly compress gas.
[0028] The axle 3 is supported by radial bearings 13 and 14, the axle 7 is supported by
radial bearings 15 and 16, the axle 12 is supported by radial bearings 17 and 18,
and all these axles are supported independently in a non- contact manner by an electromagnetic
effect making use of magnets. Since these bearings do not necessitate lubricant oil
as is the case with the bearings in the prior art, they could be disposed even in
gas without being accompanied by any problem. The respective axles 3, 7 and 12 are
connected with each other via an intermediate coupling 19 as will be described later,
and a necessary torque is transmitted through the intermediate coupling 19. This intermediate
coupling 19 has the function that it allows relative displacement in the radial direction
freely among the axles 3, 7 and 12, but among the relative displacement in the axial
direction, it restrains the relative displacement in the direction of the respective
axles approaching to each other.
[0029] The necessary input torque to this compressor is applied externally via a drive coupling
20 by means of a drive machine such as an electric motor or a turbine. In this way,
the above-mentioned respective axles 3, 7 and 12 would rotate at the same speed.
[0030] Owing to the above-described construction, the compressor can tightly seal the gas
by disposing a gas seal device 23 for preventing gas within the casing from leaking
out to the outside, only at the location where the third axle 12 for transmitting
a torque transmitted from the drive coupling 20 to the respective axles 3, 7 and 12
within the casing 1, penetrates the casing end plate 22 forming a part of the casing
1. In other words, as compared to the centrifugal compressor in the prior art, the
number of locations of gas seal devices is remarkably reduced.
[0031] Behind the final stage impeller on the axle 12 is disposed a pressure balancing disc
25 mounted to the axle 12, and a high-pressure gas is reduced in pressure toward a
pressure balancing chamber 24 via labyrinth fins to make the gaseous forces in the
axial directions applied to the axle 12 appropriately balance with each other. The
pressure balancing chamber 24 is connected through a pressure balancing tube 21 additionally
provided on a casing end plate 22 to a low-pressure environment at the gas suction
port 2.
[0032] At one end of the axle 12 is additionally provided a thrust collar 28, an electromagnetic
thrust bearing 29 sandwiching this thrust collar 28 from the opposite sides in the
axial direction is fixedly secured to the stationary side, and this electromagnetic
thrust bearing 29 operates to detect the position in the axial direction of the axle
12 via a control device disposed externally and to return the axle 12 to a predetermined
position. At one end of the first axle 3, a suction magnetic bearing 27 is provided
on the back surface of an impeller 26 which achieves initial gas suction effects.
The suction force of this suction magnetic bearing 27 acts upon the first axle 3 and
the second axle 7. By making this suction magnetic bearing 27 have a capability of
generating a suction force exceeding the sum of the unbalanced forces caused by gas
pressure directed towards the gas suction port, the first and second axles 3 and 7
are always applied with a force tending to move them towards the gas delivery side.
Since the intermediate coupling 19 has a structure adapted to prevent the axles from
approaching to each other as described above, this force is transmitted to the third
axle 12, but as the position in the axial direction of the axle 12 is controlled
by the action of the electromagnetic thrust bearing 29, the axles 3, 7 and 12 are
all fixed in position in the axial direction, and so, their relative positions with
respect to the stationary structure are maintained at predetermined positions. While
provision was made so as to suck the impeller 26 on the axle 3 in the above-described
case, the object to be sucked need not be the impeller 26, but so long as it is a
disc-shaped one rotatable integrally with the axle, anything could be employed, and
in essence, if the object is adapted to generate a force based on a magnetic effect
which sucks the first axle 3 towards the delivery port side, the desired purpose can
be achieved.
[0033] Next, details of the above-described intermediate coupling 19 will be explained
with reference to Fig. 2. For example, to the axial ends of the first axle 3 and the
second axle 7, respectively, are mounted coupling hubs 31 through a conventional method,
and a torque transmission tube 33 is coupled to flanges formed on these hubs via thin
flexible discs 32, by means of bolts and nuts 35. Reference numeral 34 designates
a protective plate for the flexible disc 32.
[0034] To the axial ends of the axles 3 and 7 are mounted restraining shafts 36 and 37,
respectively, directed in the axial direction. The restraining shaft 36 has a projection
39 at the center of its axial end surface, so that in the case where the respective
restraining shafts 36 and 37 come into contact with each other, the contact is made
at the center of their end surfaces and the respective axles cannot approach further
to each other.
[0035] Owing to the above-described structure, the axles 3 and 7 would not move in the direction
of approaching to each other during the operation, and even if their rotary axes
should become misaligned, no reaction force is generated in the radial direction thanks
to the flexibility of the flexible discs 32 and the torque transmission tube 33,
so that smooth torque transmission can be achieved.
[0036] While the casing 1 is illustrated in Fig. 1 so as to be divided into parts forming
gas passageways and an outside box-like part for integrally holding these parts (applied
with differently directed hatchings), as a matter of course, there is no need to divide
into these parts, but so long as it is possible in view of the manufacturing technique,
for instance, the casing could be formed integrally as by casting. Moreover, the intermediate
coupling also need not be limited to the illustrated structure, but so long as relative
misalignment between the axes of the respective axles is permissible, any other structure
could be employed.
[0037] Since the present invention is characterized by the structural features as described
in detail above, the invention provides the following advantages:
(1) Since a compressing system realizing a high pressure head can be constructed with
a single casing, a large number of seal devices as necessitated in the prior art become
unnecessary, a seal device at only one location can suffice, hence dangerous locations
where leakage of gas is apt to occur are reduced in number, and reliability is greatly
improved.
(2) As a single casing is employed, there is no fear that misalignment of axes between
the respective compressor units may arise. Even if such misalignment should occur,
the novel coupling between the axles can compensate for the disadvantages.
(3) Since electromagnetic bearings not being held in contact with the axle are employed,
a lubricant oil device is not necessitated, and the inconvenience that lubricant oil
may be mixed in the gas, can be eliminated.
[0038] While a principle of the present invention has been described above in connection
to one preferred embodiment of the invention, it is intended that all matter contained
in the above description and shown in the accompanying drawings shall be interpreted
to be illustrative and not in a limiting sense.