BACKGROUND OF THE INVENTION
[0001] The present invention relates to a thrust balance device. More specifically, the
present invention relates to a thrust balance device significantly improving thrust
balance in a device such as a canned motor pump.
[0002] Conventional canned motor pumps include an impeller mounted on a rotating shaft.
In the type of canned motor pump, a fluid is sucked through a suction opening i.e.
inlet which opens axially. Centrifugal force from the impeller causes discharge of
the sucked fluid from radial discharging openings i.e. outlet. Since the suction opening
is oriented toward an end of the rotation shaft, a force is applied on the impeller
in the direction of thrust. Thus, in primitive canned motor pumps, the impeller is
pushed toward an inner wall of the chamber holding the impeller. This pushing force
interferes with the rotation of the impeller. As a result, almost all recent canned
motor pumps are equipped with a thrust balance mechanism.
[0003] Suction of the fluid generates a pressure in the direction of thrust. A thrust balance
mechanism prevents obstruction of the rotation of the impeller caused by the pressure
of the sucked fluid. Generally, a thrust balance mechanism includes:
(1) a fixed orifice formed between an outer surface of a ring-shaped cylinder formed
on a rear surface of an impeller having a balance hole and a cylindrical inner perimeter
surface of a cavity disposed on a casing by inserting the ring-shaped cylinder into
the cavity to form a gap between the outer perimeter surface of the cylinder and the
cylindrical inner perimeter surface of the cavity;
(2) a thrust balance chamber which is formed from the following: a bottom surface
of the cylinder; an inner perimeter surface of the cylinder; a surface of a first
projection projected from the casing toward an inner space of the cylinder, the surface
thereof facing and being separated from the bottom surface of the cylinder by a prescribed
gap; and an outer perimeter surface of a ring-shaped second projection, surrounding
the rotating axis and projecting further than the first projection; and
(3) a variable orifice which is formed from the rear surface of the impeller and an
end surface of the second projection facing it.
[0004] In the above thrust balance mechanism, the centrifugal force from the rotation of
the impeller causes fluid to be discharged radially. A portion of the fluid discharged
in the centrifugal direction flows into the thrust balance chamber via the fixed orifice.
The fluid which enters the thrust balance chamber flows out from the thrust balance
chamber through the variable orifice. The fluid exiting the thrust balance chamber
passes through the balance hole and combines with the fluid to be discharged.
[0005] If the pressure of the sucked and discharged fluid increases, a pressure in the direction
of thrust is applied to the impeller. This pressure causes the back surface of the
impeller to approach the casing surface facing it. However, pressure from the fluid
also increases the flow rate, resulting in higher fluid pressure within the thrust
balance chamber. The increase in fluid pressure in the thrust balance chamber causes
a pressure to be applied on the rear surface of the impeller to push the impeller
away from the casing surface facing it. This pressure is sometimes referred to as
independent pressure. Fluid pressure within the thrust chamber causes the impeller
to move against the pressure from the fluid being sucked and discharged.
[0006] The gap in the variable orifice increases when the impeller is displaced away from
the casing surface facing its rear surface, i.e., when the impeller is shifted so
that it moves away from the casing surface facing the rear surface of the impeller.
This movement causes high-pressure fluid to flow rapidly from the variable orifice.
As a result, fluid pressure within the thrust balance chamber drops. The pressure
in the thrust direction applied to the impeller from the fluid being sucked and discharged
becomes greater than the fluid pressure within the thrust balance chamber. The pressure
in the thrust direction causes the impeller to shift toward the casing surface facing
the rear surface of the impeller.
[0007] As described above, in order to balance the pressure within the thrust balance chamber
and the pressure from the fluid being sucked and discharged, the impeller changes
its position according to the gap in the fixed orifice, the gap in the variable orifice,
as well as the volume of the thrust balance chamber. The change of position of the
impeller maintains balance for the rotating axis along the thrust direction.
[0008] However, with a thrust balance chamber in conventional thrust balance devices, the
rear surface of the impeller is a rotating surface, while the casing surface facing
the impeller is a fixed surface. Thus, fluid flowing into the thrust balance chamber
receives an angular momentum energy from the impeller rotation. Additionally, fluid
flowing into the thrust balance chamber rotates together with the impeller. As a result,
the fluid rotating in the thrust balance chamber with the impeller generates a very
high flow-path resistance.
[0009] The flow-path resistance of the fluid interposed between the rotating surface and
the fixed surface is proportional to the square of the peripheral speed of the fluid
rotating with the rotating surface. Thus, in a high-speed pump in which its impeller
rotates at a very high speed, the flow-path resistance of the fluid in the thrust
balance chamber thereof is high. Further, in a large pump wherein a large amount of
fluid exist at the gap between the fixed and rotating surfaces thereof, even if it
is not a high speed pump, and consequently, the peripheral speed of the rotating fluid
is high, the flow-path resistance of the fluid in the thrust balance chamber thereof
is also high. Such a high flow-path resistance prevents the thrust balance of the
pump from being maintained appropriately.
[0010] In order to overcome this problem, bypass structures known as pressure-equalizing
holes or pressure-decreasing holes have been conventionally formed in the fixed surface
of the thrust balance chamber. However, these pressure-equalizing holes have been
unable to lower the flow-path resistance and maintain thrust balance. While forming
this kind of bypass may be able to increase the independent pressure, this kind of
bypass cannot significantly reduce the angular momentum of the fluid inside the thrust
chamber.
OBJECTS AND SUMMARY OF THE INVENTION
[0011] It is an object of the present invention to provide a thrust balance device which
overcomes the foregoing problems.
[0012] It is another object of the present invention to provide a thrust balance device
which has superior thrust balance properties.
[0013] It is a further object of the present invention to provide a thrust balance device
which has good thrust balance properties regardless of pump discharge rate.
[0014] It is still a further object of the present invention to provide a thrust balance
device which has good thrust balance properties regardless of impeller rotation speed.
[0015] Briefly stated, the present invention provides a flow channel and pressure equalizing
sections introducing a fluid having substantially no angular momentum into a thrust
balance chamber of a thrust balance device. The introduction of this fluid reduces
the angular momentum of the fluid in the thrust balance chamber, facilitating the
discharge of fluid out of the thrust balance chamber through the variable orifice.
The thrust balance chamber exerts a variable pressure onto a rear surface of an impeller
of a centrifugal pump. This pressure prevents significant displacement of the impeller
during pump operation. Therefore, the present invention provides a centrifugal pump
with a good thrust balance property regardless of flow rate and impeller speed of
the centrifugal pump.
[0016] According to an embodiment of the present invention, there is provided a thrust balance
device in a centrifugal pump comprising a fixed orifice permitting flow of a portion
of a fluid passing through the centrifugal pump into a thrust balance chamber of the
thrust balance device, the thrust balance chamber facing the rear surface of the impeller
in the centrifugal pump, a variable orifice permitting a variable flow of the portion
from the thrust balance chamber depending on a balance between a fluid pressure in
the thrust balance chamber and the pressure from the fluid being pumped, and means
for introducing a fluid having substantially no angular momentum into the thrust balance
chamber, whereby the introduced fluid facilitates the flow of the portion to flow
out through the variable orifice.
[0017] According to another embodiment of the present invention, there is provided a thrust
control device for controlling an axial position of an impeller of a centrifugal pump,
comprising an impeller having a first surface exposed to a pressure of a fluid being
pumped, a thrust balance chamber adjacent a second surface of the impeller, at least
one balance hole communicating between the first surface and the second surface, a
projection facing the second surface of the impeller, a fixed orifice permitting a
controlled leakage of the fluid from an outlet of the centrifugal pump into the thrust
balance chamber, a variable orifice adjusting flow rate of fluid flowing out from
the thrust balance chamber when the impeller is displaced axially at a predetermined
distance in the direction toward said projection, whereby the controlled leakage is
enabled to increase a fluid pressure in the thrust balance chamber, and thereby to
resist axial displacement of the impeller in said direction, and at least one stationary
flow channel conveying a portion of the fluid with substantially reduced angular momentum
to the thrust balance chamber.
[0018] According to still another embodiment of the present invention, there is provided
a device for feeding fluid having substantially no angular velocity to a thrust balance
chamber of a centrifugal pump comprising a radially arranged opening and a ring-shaped
groove opening at the thrust balance chamber. The ring-shaped groove connects the
inner end of the opening with the thrust balance chamber. The fluid is accepted at
the outer end of the opening and conducted to its inner end, then fed into the thrust
balance chamber through the ring-shaped groove.
[0019] In the above embodiment, the device for feeding fluid having substantially no angular
velocity to the thrust balance chamber can have a plurality of the radially arranged
openings.
[0020] Additionally, both of the opening area of the ring-shaped groove and the sum total
of the cross-sectional area of the radially arranged opening(s) are preferably larger
than the opening area of the balance hole of the impeller.
[0021] The present invention achieves these objects by providing a thrust balance device
that includes the following elements:
(1) A fixed orifice forming a gap between an outer perimeter surface of a cylinder
formed on a rear surface of an impeller in a centrifugal pump and a cylindrical inner
perimeter surface of a cavity disposed in a casing thereof, wherein the impeller has
at least one balance hole and the cylinder is inserted into the cavity;
(2) A thrust balance chamber which is formed from the following: a base surface of
the cylinder; an inner perimeter surface of the cylinder; a surface of a first projection
projected from the casing toward an inner space of the cylinder, the surface being
separated from the rear surface by a prescribed gap; and an outer perimeter surface
of a ring-shaped second projection, surrounding the rotating axis, projecting further
than the first projection;
(3) A variable orifice which is formed between the rear surface of the impeller and
an end surface of the second projection facing it;
(4) A ring-shaped groove, surrounding the rotating axis, which is formed on the first
projection; and
(5) A pressure-equalizing section which leads to the ring-shaped groove and the cavity.
[0022] The above, and other objects, features and advantages of the present invention will
become apparent from the following description read in conjunction with the accompanying
drawings, in which like reference numerals designate the same elements.
BRIEF DESCRIPTION OF THE DRAWINGS
[0023]
Fig. 1 is a longitudinal section of a thrust balance device of one embodiment of the
present invention.
Fig. 2 is a longitudinal section of another embodiment of a thrust balance device
of the present invention.
Fig. 3 is a longitudinal section of a thrust balance device of yet another embodiment
of the present invention.
Fig.4 is a longitudinal section of still another embodiment of a thrust balance device
of the present invention.
Fig.5 is a graph indicating the variation of the remaining thrust value to various
discharge amount for canned motor pump having the thrust balance device shown in Fig.1
and for canned motor pump that is the same as the above canned motor pump except for
not having the above thrust balance device.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0024] Referring to Fig.1, a centrifugal pump 1 equipped with a thrust balance device according
to the present invention includes an impeller 6 mounted on a rotating axis 5. Impeller
6 is positioned in a pump chamber 4 formed by a casing 2 and a liner disk 3.
[0025] A suction opening of centrifugal pump 1 (not shown) is formed at an axial orientation
relative to impeller 6. A cylindrical guide path 7, co-axial with rotating axis 5,
extends from the suction opening to pump chamber 4.
[0026] Impeller 6 includes a base 8 which has a circular shape when seen from an axial direction.
Impeller 6 rotates together with rotating axis 5, discharging fluid introduced through
guide path 7 in a centrifugal direction. Thus, in centrifugal pump 1, a discharging
opening (not shown) is formed centrifugally in the relationship to impeller 6.
[0027] A cylinder 9 projects from a rear surface, i.e. the surface facing liner disk 3,
of base 8, which is a section of impeller 6. Cylinder 9 projects toward liner disk
3. Furthermore, a balance hole 10 extends from the rear surface of base 8 to the front
surface thereof toward guide path 7.
[0028] A cavity 11 is formed on a surface of liner disk 3 facing base 8. Cavity 11 has a
cylindrical inner perimeter surface which has an inner diameter slightly larger than
a diameter of cylinder 9. When cylinder 9 is inserted into cavity 11, a slight gap
is formed between an outer perimeter surface of cylinder 9 and an inner perimeter
surface of cavity 11. This gap serves as a fixed orifice 12.
[0029] A disc-shaped first projection 13, on cavity 11 inward from cylinder 9, projects
toward a rear surface of impeller 6. A second projection 14, having a ring-shaped
end surface, is located on cavity 11 at a position inward from first projection 13,
toward rotating axis 5. Second projection 14 projects closer to the rear surface of
impeller 6 than first projection 13. An end surface of first projection 13 facing
a bottom surface of cylinder 9 has a ring shape. When cylinder 9 is inserted into
cavity 11, a prescribed gap is formed between an outer perimeter surface of first
projection 13 and an inner perimeter surface of cylinder 9. This gap is much larger
than the gap formed by fixed orifice 12. The ring-shaped end surface of second projection
14 has a ring-like shape when seen from an axial direction.
[0030] A thrust balance chamber 15 is formed as a space created between the ring-shaped
end surface of first projection 13 (this surface is also a fixed surface) and a bottom
surface of cylinder 9 (this surface is the rear surface of impeller 6 and is also
a rotating surface).
[0031] A variable orifice 16 is formed of a space between the ring-shaped end surface of
second projection 14 and a bottom surface of cylinder 9, i.e. the rear surface of
base 8.
[0032] A ring-shaped groove 17, centered on rotating axis 5, is positioned between first
projection 13 and second projection 14. Ring-shaped groove 17 has a space surrounded
by an opening facing a ring-shaped end surface of first projection 13, an inward inner
perimeter surface which is an outer perimeter surface of a cylinder, and an outward
inner perimeter surface which is an inner perimeter surface of a cylinder. The resulting
space is a ring-shaped space centered on rotating axis 5. In Fig. 1, which is a longitudinal
section of the centrifugal pump 1, a line representing a longitudinal section of an
inward inner perimeter surface of ring-shaped groove 17 is parallel with a line representing
a longitudinal section of an outward inner perimeter surface of ring-shaped groove
17.
[0033] Pressure-equalizing sections 18 are openings extending from an outer perimeter surface
of first projection 13 to ring-shaped groove 17. Pressure-equalizing sections 18 are
connected with ring-shaped groove 17 and cavity 11, Preferably, twelve pressure-equalizing
sections 18 are formed at first projection 13. Each of pressure-equalizing sections
18 has a circular cross-sections cut along a plane perpendicular to the axis thereof.
In other words, pressure-equalizing sections 18 have cylindrical inner spaces.
[0034] The following is a description of how centrifugal pump 1 operates together with the
thrust balance device of the present invention.
[0035] Rotating axis 5 rotates together with impeller 6. Fluid introduced from the suction
opening flows through guide path 7 into pump chamber 4. Since impeller 6 is rotating
inside pump chamber 4, the fluid is discharged through a discharging opening by centrifugal
force. This is the standard operation of centrifugal pump 1.
[0036] A portion of the fluid in pump chamber 4 flows through fixed orifice 12, into thrust
balance chamber 15. The fluid passes through variable orifice 16 and balance hole
10 to return to a front side of impeller 6.
[0037] If the discharge pressure on impeller 6 increases, impeller 6 is displaced toward
liner disk 3 by this increase in the discharge pressure. This pressure change causes
the width of the opening of variable orifice 16 to be decreased, lowering the flow
through variable orifice 16. While the width of the gap at variable orifice 16 decreases,
the width of the gap at fixed orifice 12 remains unchanged. Thus, fluid continues
to flow into thrust balance chamber 15, increasing the fluid pressure inside thrust
balance chamber 15 until the fluid pressure in thrust balance chamber 15 exceeds the
discharge pressure.
[0038] When the fluid pressure of thrust balance chamber 15 exceeds the discharge pressure,
impeller 6 is displaced in the direction where cylinder 9 is pushed out from cavity
11, This displacement of impeller 6 increases the width of the opening in variable
orifice 16. As the width of the opening in variable orifice 16 increases, the amount
of fluid coming out through variable orifice 16 from balance chamber 15 exceeds the
amount of fluid going into balance chamber 15 through fixed orifice 12. Thus, the
fluid and the fluid pressure in thrust balance chamber 15 are reduced, displacing
impeller 6 toward liner disk 3. When the fluid pressure in thrust balance chamber
15 is in equilibrium with the discharge pressure toward impeller 6, displacement of
impeller 6 stops.
[0039] Fluid inside thrust balance chamber 15 rotates together with the rotation of impeller
6. Fluid rotating inside thrust balance chamber 15 has an angular momentum and generates
flow-path resistance. If this flow-path resistance is high, the flow of fluid in thrust
balance chamber 15 through variable orifice 16 is hindered, even when the opening
in variable orifice 16 enlarges.
[0040] The object of the present invention is to reduce the flow-path resistance caused
by the angular momentum of the fluid in thrust balance chamber 15. Ring-shaped groove
17 and pressure-equalizing sections 18 help achieve this goal. Fluid having no angular
momentum flows from pressure-equalizing sections 18 into thrust balance chamber 15
via ring-shaped groove 17, mixing with fluid having angular momentum. The addition
of a fluid having no angular momentum into thrust balance chamber 15 dramatically
reduces the angular momentum of fluid in thrust balance chamber 15. Thus, by reducing
the flow-path resistance caused by angular momentum of fluid in thrust balance chamber
15, fluid in thrust balance chamber quickly and smoothly flows out through variable
orifice 16.
[0041] A computer was used to simulate the thrust balance in rotating axis 5 for a pump
having pressure-equalizing sections 18 and ring-shaped groove 17 versus a pump having
only pressure-equalizing sections 18. According to the results of the simulation,
the outgoing flow from variable orifice 16 was 290 liters/min. for the pump having
only pressure-equalizing sections 18. The flow pressure at the backside of impeller
6 (the pressure inside thrust balance chamber 15) was 2363 N (241 kgf). With the pump
having pressure-equalizing sections 18 and ring-shaped groove 17, the outgoing flow
from variable orifice 16 was 301 liters/min. and the flow pressure at the back side
of impeller 6 was 2157 N (220kgf), thus showing a dramatic reduction in flow path
resistance caused by angular momentum of fluid in thrust balance chamber 15. In these
calculations the pump specifications were as follows: SUC 125 A, DIS 100 A, 200m
3/h × 32m × 2900 rpm, impeller diameter, 190mm.
[0042] The groove space of ring-shaped groove 17 formed on first projection 13 can be of
any shape, as long as it surrounds rotating axis 5.
[0043] Referring to Fig. 2, an alternate embodiment of the present invention is shown. Ring-shaped
groove 17 has a groove space surrounded by an opening facing the ring-shaped end surface
of first projection 13, an inward inner perimeter surface corresponding to an outer
perimeter surface of a cylinder co-axial with rotating axis 5, and an outward inner
perimeter surface corresponding to an inner perimeter surface of a cone that is co-axial
with rotating axis 5. The longitudinal section of the groove space of ring-shaped
groove 17 of this embodiment of the present invention forms a wedge shape as shown
in Fig. 2.
[0044] Referring to Fig. 3, an alternate embodiment of the present invention is shown. Ring-shaped
groove 17 has a groove space surrounded by an opening facing a ring-shaped end surface
of first projection 13, an inward inner perimeter surface corresponding to on outer
perimeter surface of a cone that is co-axial with rotating axis 5, and an outward
inner perimeter surface corresponding to an inner perimeter surface of a cone that
is co-axial with rotating axis 5. The longitudinal section of the groove space of
ring-shaped groove 17 of this embodiment forms a wedge shape having a configuration
opposite of the wedge shape of the embodiment shown in Fig. 2.
[0045] Referring to Fig. 4, in yet another embodiment of the present invention, ring-shaped
groove 17 has a groove space surrounded by an opening facing a ring-shaped end surface
of first projection 13, an inward inner perimeter surface corresponding to an outer
perimeter surface of a cone that is co-axial with rotating axis 5, and an outward
inner perimeter surface of a cone that is co-axial with rotating axis 5. The longitudinal
section of the groove space of ring-shaped groove 17 of this embodiment of the present
Invention forms a v-shape.
[0046] Regardless of the shape of the groove space formed by ring-shaped groove 17, it is
desirable that A, the sum total of the cross-sectional area of each of pressure-equalizing
sections 18 cut along the plane perpendicular to the axis thereof or the circular
cross-section area of pressure-equalizing sections 18 (A is calculated as

, where n is the number of pressure-equalizing sections 18 and d
1 is the diameter of the circular cross-section) is equal to or smaller than B, an
area of the opening of ring-shaped groove 17 (B is calculated as

, where D
2 and D
3 are the outer and inner diameters of the opening of ring-shaped groove 17, respectively),
i.e. A≦B.
[0047] There are no specific restrictions placed on the number of pressure-equalizing sections
18.
[0048] The present invention provides a thrust balance device having superior thrust balance
properties, Furthermore, the present invention provides a thrust balance device having
good thrust balance properties, regardless of the discharge from the pump. The present
invention also provides a thrust balance device having good thrust balance properties,
regardless of the speed of rotation of the impeller.
[0049] Having described preferred embodiments of the invention with reference to the accompanying
drawings, it is to be understood that the invention is not limited to those precise
embodiments, and that various changes and modifications may be effected therein by
one skilled in the art without departing from the scope or spirit of the invention
as defined in the appended claims.
EXAMPLE
1. Example 1
[0050] For a canned motor pump (type: HN25E) having a thrust balance device with the structure
shown in Fig.1, a difference between the fluid pressure in thrust balance chamber
15 and the discharge pressure at impeller 6, i.e., remaining thrust was measured with
varying discharge of the canned motor pump from 10 to 140 m
3/hr.
[0051] Both of A, the sum total of the areas of the circular cross section of pressure-equalizing
sections 18 and B, the area of the opening of ring-shaped groove 17 were larger than
the sum total of the area of the openings of balancing holes 10 on base 8. Further,
A is less than B. Applying an alternating current of 50 Hz drove the canned motor
pump. Results are shown in Fig.5.
[0052] As shown in Fig. 5, at a discharge of 10 to 140 m
3/hr, the canned motor pump of Example 1 showed almost no remaining thrust, in other
word, the fluid pressure in thrust balance chamber 15 balanced well to the discharge
pressure on impeller 6.
2. Comparative Example 1
[0053] Remaining thrust is measured for a canned motor pump (type: HN25E-F4) having the
same structure as that of the canned motor pump of Example 1 except for having neither
ring-shaped groove 17 nor pressure-equalizing sections 18. Results are shown in Fig
5.
[0054] As shown in Fig. 5, the above canned motor pump showed a maximum remaining thrust
of about 70 kgf.
1. A thrust balance device in a centrifugal pump comprising:
a fixed orifice permitting flow of a portion of a fluid passing through said centrifugal
pump into a thrust balance chamber of said thrust balance device;
said thrust balance chamber facing the rear surface of the impeller of said centrifugal
pump; and
a variable orifice permitting a variable flow of a fluid from said thrust balance
chamber depending on a balance between a fluid pressure in said thrust balance chamber
and a fluid being pumped;
characterized in having means for introducing a fluid having substantially no angular
momentum into said thrust balance chamber, whereby the flow-path resistance of the
fluid in the thrust barance chamber thereof is reduced.
2. A thrust balance device according to claim 1, wherein:
said means includes one or more pressure-equalizing sections connected to at least
one stationary flow channel;
said at least one stationary flow channel having an opening to permit flow of the
fluid in the pressure-equalizing sections into said thrust balance chamber.
3. A thrust balance device according to claim 2, wherein said stationary flow channel
is a ring shaped groove.
4. A thrust balance device according to claim 3, wherein the outer perimeter surface
of said ring shaped groove and inner perimeter surface thereof are parallel.
5. A thrust balance device according to claim 3, wherein said ring shaped groove has
a wedge shape in cross-section.
6. A thrust balance device according to claim 3, wherein each of said pressure-equalizing
sections has a circular cross section:
each of said circular cross sections having a cross-sectional area wherein a sum total
of said cross-sectional area of said pressure-equalizing section is smaller than an
area of said opening of said ring-shaped groove.
7. A thrust balance device including:
(1) A fixed orifice forming a gap between an outer perimeter surface of a cylinder
formed on a rear surface of an impeller in a centrifugal pump and a cylindrical inner
perimeter surface of a cavity disposed in a casing thereof, wherein sad impeller have
at least one balance hole and the cylinder is inserted into the cavity;
(2) a thrust balance chamber which is formed from the following: a base surface of
the cylinder; an inner perimeter surface of the cylinder; a surface of a first projection
projected from the casing toward an inner space of the cylinder, the surface being
separated from the rear surface by a prescribed gap; and an outer perimeter surface
of a ring-shaped second projection, surrounding the rotating axis and projecting further
than the first projection; and
(3) a variable orifice which is formed between the rear surface of the impeller and
an end surface of the second projection facing it;
characterized in having:
a ring-shaped groove formed on the first projection and surrounding the rotating axis
of the impeller, and
a pressure-equalizing section which leads to the ring-shaped groove and the cavity.
8. A thrust balance device according to claim 7, wherein the outer perimeter surface
of said ring shaped surface and inner perimeter surface thereof are parallel.
9. A thrust balance device according to claim 7, wherein said ring shaped groove has
a wedge shape in cross-section.
10. A thrust balance device according to one of claims 7 to 9 having a plurality of said
pressure-equalizing sections.
11. A thrust balance device according to claim 10, wherein each of said pressure-equalizing
sections has a circular cross section, and a sum total of the area of the circular
cross sections of said pressure-equalizing sections is smaller than the area of said
opening of said ring-shaped groove.
12. A thrust balance device according to claim 10 or 11, wherein both of the opening area
of said ring-shaped groove and the sum total of the cross-sectional area of said pressure-equalizing
sections are larger than the opening area of the balance hole of the impeller.