[TECHNICAL FIELD]
[0001] The present invention relates to a centrifugal compressor in which a vane blade is
able to be moved into and out of a diffuser passage.
[BACKGROUND ART]
[0002] There has been disclosed a technique in which a vane blade is formed integrally with
a diaphragm, and fluid pressure inside the diaphragm is adjusted to deform the diaphragm,
so that the deformation of the diaphragm is transmitted to the vane blade, thereby
causing the vane blade to move into and out of the diffuser passage (see, for example,
a first patent document). With this construction, in the first patent document, when
the operation flow rate of a centrifugal compressor is a small flow rate, the vane
blade is caused to project into the diffuser passage, whereas when the operation flow
rate of the centrifugal compressor is a large flow rate, the vane blade is caused
to be buried into the side wall of the diffuser passage.
[PRIOR ART REFERENCES]
[PATENT DOCUMENTS]
[0003]
[First patent Document] Patent Laid-Open Publication No. 2001-329996
[SUMMARY OF THE INVENTION]
[PROBLEMS TO BE SOLVED BY THE INVENTION]
[0004] In the technique of the first patent document, the diaphragm is formed integrally
with the vane blade. Therefore, when the diaphragm is not able to be deformed in an
accurate manner because of variation in the thickness of the diaphragm or difference
in the hardness of a part of the diaphragm from the others thereof, the direction
of protrusion of the vane blade will deviate from a specified direction. When the
direction of protrusion of the vane blade deviates from the specified direction, the
vane blade may bite a peripheral edge portion of a slit through which the vane blade
is caused to protrude into the diffuser passage. In addition, the friction at the
time of the vane blade passing through the slit may become large, thus giving rise
to wear of the vane blade and an increase in a driving force for operating the vane
blade.
[0005] The present invention has been made in view of the above-mentioned circumstances,
and has for its object to provide a technique in a centrifugal compressor in which
the direction of protrusion of a vane blade is avoided from deviating from a specified
direction as a result of a deformation of a deformation member.
[MEANS FOR SOLVING THE PROBLEMS]
[0006] In the present invention, the following construction is adopted. That is, the present
invention resides in a centrifugal compressor which is provided with:
a vane blade that is movable into and out of a diffuser passage;
a space that is formed in a wall of the diffuser passage in which said vane blade
is caused to be buried;
and
a deformation member that divides said space into a diffuser side chamber and an anti-diffuser
side chamber, and deforms to change the volume of said anti-diffuser side chamber,
said deformation member causing said vane blade to move in a specified direction thereby
to protrude into said diffuser passage due to a deformation thereof at the time of
increasing the volume of said anti-diffuser side chamber;
wherein said vane blade and said deformation member are separate bodies from each
other, and only a displacement in the specified direction of a portion of said deformation
member which is made into contact with said vane blade due to the deformation thereof
at the time of increasing the volume of said anti-diffuser side chamber acts on said
vane blade.
[0007] In the deformation of the deformation member at the time of increasing the volume
of the anti-diffuser side chamber, a portion of the deformation member, being in contact
with the vane blade, is not only displaced in the specified direction to cause the
vane blade to protrude into the diffuser passage, but also can be displaced in a direction
other than the specified direction, too. At this time, when the portion of the deformation
member, which is in contact with the vane blade, is formed integrally with the vane
blade, the vane blade may also move not in the specified direction but in the direction
other than the specified direction, in accordance with the deformation of the deformation
member.
[0008] However, in the present invention, the vane blade and the deformation member are
separate bodies from each other. For this reason, the displacement in the direction
other than the specified direction of the portion of the deformation member in contact
with the vane blade only causes the portion of the deformation member in contact with
the vane blade to move with respect to the vane blade, but does not act on the vane
blade, thus making it difficult for the vane blade to move in a direction other than
the specified direction. On the other hand, only a displacement in the specified direction
of the portion of the deformation member in contact with the vane blade acts on the
vane blade, thereby causing the vane blade to move in the specified direction. Accordingly,
it is possible to avoid the direction of protrusion of the vane blade from deviating
from the specified direction as a result of the deformation of the deformation member.
[0009] As a result, it is possible to avoid the direction of protrusion of the vane blade
from deviating from the specified direction, thus avoiding the vane blade from biting
a peripheral edge portion of a slit through which the vane blade is caused to protrude
into the diffuser passage. In addition, it is also possible to avoid friction at the
time of the vane blade passing through the slit from becoming large, thereby avoiding
the occurrence of wear of the vane blade and an increase in a driving force for operating
the vane blade.
[0010] Provision may further be made for:
an urging member that urges said vane blade in a manner such that said vane blade
is caused to be buried into said diffuser passage wall; and
a stopper that positions said vane blade against the urging of said urging member
when an amount of protrusion into said diffuser passage of said vane blade is equal
to or less than a predetermined amount;
wherein said deformation member is able to be moved away from said vane blade that
is positioned by said stopper, by decreasing the volume of said anti-diffuser side
chamber.
[0011] Here, the predetermined amount is an amount which, when the amount of protrusion
is equal to or less than that amount, can deal with a case where the operation flow
rate of the centrifugal compressor is a large flow rate.
[0012] According to this, in cases where the amount of protrusion of the vane blade into
the diffuser passage is equal to or less than the predetermined amount, the deformation
member can be caused to separate from the vane blade positioned by the stopper. As
a result of this, it is possible to avoid heat transfer from the vane blade to the
deformation member. Accordingly, it is possible to suppress the deformation member
from being thermally deteriorated resulting from the heat transfer from the vane blade.
[0013] In cases where the centrifugal compressor operates so as to make air to be supplied
at a high flow rate and at a high supercharging pressure, the volume of said anti-diffuser
side chamber may be made small until said deformation member and said vane blade positioned
by said stopper are separated from each other.
[0014] In cases where the centrifugal compressor operates to make air to be supplied at
a high flow rate and at a high supercharging pressure, the air flowing through the
diffuser passages becomes a high temperature, and the vane blade, which has been caused
to be buried into the diffuser passage wall, is similarly at a high temperature. In
this case, the volume of the anti-diffuser side chamber is made small until the deformation
member and the vane blade positioned by the stopper are separated from each other,
so the deformation member and the vane blade are separated or away from each other,
thus making it possible to avoid the heat transfer from the vane blade of the high
temperature to the deformation member. Accordingly, in cases where the centrifugal
compressor operates to make air to be supplied at a high flow rate and at a high supercharging
pressure, it is possible to suppress the deformation member from being thermally deteriorated
resulting from the heat transfer from the vane blade of the high temperature.
[EFFECT OF THE INVENTION]
[0015] According to the present invention, in a centrifugal compressor, it is possible to
avoid the direction of protrusion of a vane blade from deviating from a specified
direction as a result of a deformation of a deformation member.
[BRIEF DESCRIPTION OF THE DRAWINGS]
[0016]
[Fig. 1] is a view showing the schematic construction of a centrifugal compressor
according to a first embodiment of the present invention.
[Fig. 2] is views showing a protruded state and a buried state of a vane blade according
to the first embodiment.
[Fig. 3] is a view showing a problem of a conventional vane blade.
[Fig. 4] is a view showing a feature of the vane blade according to the first embodiment.
[BEST MODE FOR CARRYING OUT THE INVENTION]
[0017] Hereinafter, a specific embodiment of the present invention will be described.
<First Embodiment>
(Construction of a Centrifugal Compressor)
[0018] Fig. 1 is a view showing the schematic construction of a centrifugal compressor according
to a first embodiment of the present invention. The centrifugal compressor 1 shown
in Fig. 1 is provided with a scroll casing 2, and it has an impeller 3 arranged in
an axial center inside the scroll casing 2. Air as a gas, which has flowed into the
centrifugal compressor 1, is guided to flow into a diffuser passage 5 formed on an
outer peripheral side of the impeller 3 by means of vanes 4 which are arranged in
a circumferential direction of the impeller 3 at equal intervals.
[0019] The diffuser passage 5 is sandwiched or enclosed by diffuser passage walls, which
are part of the scroll casing 2. One of the diffuser passage walls on a left-hand
side of Fig. 1 is composed of a plate-shaped diffuser plate 6, and is formed separately
from a casing main body. Space 7, which can be covered with the diffuser plate 6,
is formed in the one diffuser passage wall (hereinafter referred to as the diffuser
passage wall) on which the diffuser plate 6 is arranged. The space 7 is of a hollow
cylindrical shape, and can receive a vane blade 8 which is movable into and out of
the interior of the diffuser passage 5.
[0020] The vane blade 8 is provided with an annular disk 9, and a plurality of blade portions
10 which have their one ends fixed to the disk 9 and are arranged in a circumferential
direction at intervals. The diffuser plate 6 is formed with slits 11 into which the
blade portions 10 of the vane blade 8 are inserted, respectively. With this construction,
when the disk 9 of the vane blade 8 is brought close to the diffuser plate 6, the
blade portions 10 of the vane blade 8 protrude from the slits 11, respectively, into
the diffuser passage 5. On the other hand, when the disk 9 of the vane blade 8 is
moved away from the diffuser plate 6 (the diffuser passage 5), the blade portions
10 are received in the space 7 while being guided by the slits 11, respectively, so
that the vane blade 8 is buried or drawn in the diffuser passage wall.
[0021] In the space 7 where the vane blade 8 is received, there is arranged a diaphragm
12, as a deformation member, which serves to divide the space 7 into a diffuser side
chamber 7a and an anti-diffuser side chamber 7b, and to deform to change the volume
of the anti-diffuser side chamber 7b. The diaphragm 12 is of an annular shape which
can swell or expand in the direction of the diffuser side chamber 7a, and is composed
of a rubber-like elastic body so as to be elastically deformable, and has an outer
edge and an inner edge both fixedly secured to the wall of the space 7 in an airtight
manner. The diaphragm 12 can push the disk 9 of the vane blade 8 toward the side of
the diffuser passage 5 by being swelled or expanded in a manner such that the anti-diffuser
side chamber 7b is made larger. The diaphragm 12 and the disk 9 are different bodies
from each other. If the diaphragm 12 has not been deformed to swell, the diaphragm
12 and the disk 9 are separated or away from each other. In other words, the diaphragm
12 is able to be moved away from the disk 9 of the vane blade 8 that is positioned
by stoppers 13, by decreasing the volume of the anti-diffuser side chamber 7b.
[0022] In the diffuser side chamber 7a in the space 7, there is arranged a compression
spring 14, as an urging member, which serves to urge the disk 9 of the vane blade
8 so as to cause the vane blade 8 to be buried in the diffuser passage wall. The compression
spring 14 is compressed inside the diffuser side chamber 7a, and urges the disk 9
in a direction opposite to the direction of the diffuser passage 5.
[0023] In a position in which the compression spring 14 in the diffuser side chamber 7a
urges the disk 9 of the vane blade 8 thereby to cause the vane blade 8 to be buried
in the diffuser passage wall, there is arranged a stopper 13 which serves to position
the disk 9 of the vane blade 8 against the urging of the compression spring 14. If
the disk 9 abuts against the stoppers 13 in a state urged by the compression springs
14, respectively, so that there will be no action due to the swelling or expanding
deformation of the diaphragms 12, the vane blade 8 can be maintained in a state in
which it is caused to be buried in the diffuser passage 5.
[0024] The centrifugal compressor 1 of this embodiment is provided with a fluid pressure
adjusting mechanism 15 which serves to apply fluid pressure to the anti-diffuser side
chamber 7b. Between the fluid pressure adjusting mechanism 15 and the anti-diffuser
side chamber 7b, there is arranged a fluid passage 16 which circulates or supply fluid
from the fluid pressure adjusting mechanism 15 to the anti-diffuser side chamber 7b.
(Operation of the Centrifugal Compressor)
[0025] Fig. 2 is views showing a protruded state and a buried state of the vane blade according
to this embodiment, wherein Fig. 2A shows the protruded state in which the vane blade
has been protruded into the diffuser passage, and Fig. 2B shows the buried state in
which the vane blade has been buried in the diffuser passage wall.
[0026] In cases where the centrifugal compressor 1 operates so as to cause air to be supplied
at a low flow rate and at a low supercharging pressure, the fluid pressure adjusting
mechanism 15 causes fluid to flow into the anti-diffuser side chamber 7b thereby to
pressurize the anti-diffuser side chamber 7b, so that the diaphragm 12 is caused to
perform swelling deformation, thus increasing the volume of the anti-diffuser side
chamber 7b. As a result of this, the diaphragm 12 is displaced to push the disk 9
of the vane blade 8, so the disk 9 is moved in the specified direction of an illustrated
arrow A to cause the blade portions 10 of the vane blade 8 to protrude into the diffuser
passage 5, whereby the blade portions 10 of the vane blade 8 are protruded from the
slits 11, respectively, into the diffuser passage 5, as shown in Fig. 2(a).
[0027] Fig. 3 is a view showing a problem of a conventional vane blade. Here, in the swelling
deformation of a diaphragm at the time of increasing the volume of an anti-diffuser
side chamber, a portion of the diaphragm, being in contact with a disk of the vane
blade, is not only displaced in a specified direction to cause the disk of the vane
blade to protrude into a diffuser passage, but also can be displaced in a direction
other than the specified direction, too. At this time, if the portion of the diaphragm
in contact with the disk of the vane blade as shown in a region C of Fig. 3 is formed
integrally with the vane blade, the vane blade may not move in the specified direction
shown by a broken line arrow, in accordance with the swelling deformation of the diaphragm
as shown by an arrow B, but may move in a direction other than the specified direction,
as shown in the arrow B. If so, the direction of protrusion of the blade portions
of the vane blade may deviate from the specified direction, and the blade portions
of the vane blade may bite peripheral edge portions of slits to stop moving. In addition,
even if the blade portions of the vane blade do not bite, they may be rubbed against
the peripheral edge portions of the slits, and friction at that time may become large,
thus giving rise to an increase in wear of the blade portions of the vane blade or
an increase in the driving forces of a fluid pressure adjusting mechanism.
[0028] Fig. 4 is a view showing a feature of the vane blade according to this first embodiment.
In this embodiment, the vane blade 8 and a diaphragm 12 are different or separate
bodies from each other, and in a portion shown in a region D of Fig. 4, the diaphragm
12 is only in contact with the disk 9 of the vane blade 8. For this reason, even in
cases where the diaphragm 12 is deformed in a direction of the arrow B other than
the specified direction, such a displacement in a direction other than the specified
direction of the portion of the diaphragm 12 in contact with the vane blade 8 only
causes the portion of the diaphragm 12 in contact with the disk 9 of the vane blade
8 to move in position (shift in position) with respect to the vane blade 8, but does
not act on the vane blade 8, thus making it difficult for the vane blade 8 to move
in a direction other than the specified direction. On the other hand, only a displacement
in the specified direction of the portion of the diaphragm 12 in contact with the
disk 9 of the vane blade 8 acts on the vane blade 8, so that the vane blade 8 is caused
to move in the specified direction of the illustrated arrow A. Accordingly, in the
present embodiment, it is possible to avoid the direction of protrusion of a blade
portion 10 of the vane blade 8 from deviating from the specified direction as a result
of the deformation of the diaphragm 12.
[0029] As a result, it is possible to avoid the direction of protrusion of the blade portions
10 of the vane blade 8 from deviating from the specified direction, thus avoiding
the blade portions 10 of the vane blade 8 from biting the peripheral edge portions
of the slits 11 to stop moving. In addition, it is also possible to avoid the blade
portions 10 of the vane blade 8 from being rubbed against the peripheral edge portions
of the slits 11 at the time of the blade portions 10 passing through the slits 11,
respectively, and hence, friction at that time from becoming large, thereby avoiding
the occurrence of wear of the blade portions 10 of the vane blade 8 and an increase
in the driving forces of the fluid pressure adjusting mechanism 15.
[0030] On the other hand, in cases where the centrifugal compressor 1 operates so as to
make air to be supplied at a high flow rate and at a high supercharging pressure,
the fluid pressure adjusting mechanism 15 suck fluid from the anti-diffuser side chamber
7b thereby to reduce the pressure in the anti-diffuser side chamber 7b, so that the
diaphragm 12 is caused to perform deflating or retracting deformation, thus decreasing
the volume of the anti-diffuser side chamber 7b. As a result of this, a force from
the diaphragm 12 to cause the vane blade 8 to move in the specified direction to protrude
into the diffuser passage 5 stop acting thereon. Then, the disk 9 is urged by means
of the compression springs 14 to abut against the stoppers 13 to be positioned thereby,
so that the blade portions 10 of the vane blade 8 are respectively buried in the diffuser
passage wall, as shown in Fig. 2B.
[0031] At this time, the fluid pressure adjusting mechanism 15 operates to make small the
volume of the anti-diffuser side chamber 7b until it separates the diaphragm 12 from
the disk 9 of the vane blade 8 positioned by the stoppers 13, so that the diaphragm
12 takes a steady shape which is not deformed. For this reason, as shown in Fig. 2B,
the diaphragm 12 and the disk 9 of the vane blade 8 positioned by the stoppers 13
are separated or away from each other. Here, in cases where the centrifugal compressor
1 is operated to make air to be supplied at a high flow rate and at a high supercharging
pressure, the air flowing through the diffuser passage 5 becomes a high temperature
of about 180 degrees C, and the vane blade 8, which has been buried in the diffuser
passage wall, is similarly at a high temperature through the action of the air which
flows in from the slits 11. In this case, because the volume of the anti-diffuser
side chamber 7b is made small by means of the fluid pressure adjusting mechanism 15
until the diaphragm 12 is separated or away from the disk 9 of the vane blade 8 positioned
by the stoppers 13, the diaphragm 12 and the disk 9 of the vane blade 8 are separated
or away from each other, thus making it possible to avoid heat transfer from the vane
blade 8 of the high temperature to the diaphragm 12. Accordingly, in cases where the
centrifugal compressor 1 operates so as to make air to be supplied at a high flow
rate and at a high supercharging pressure, it is possible to suppress the diaphragm
12, which is rubber-like elastic body, from being thermally deteriorated resulting
from the heat transfer from the vane blade 8 of the high temperature, thereby making
it possible to improve the endurance reliability of the diaphragm 12.
[0032] The centrifugal compressor according to the present invention is not limited to the
above-mentioned embodiment, but can be subjected to various changes and modifications
within the scope not departing from the gist of the present invention. For example,
as the deformation members, there may be used bellows, besides the diaphragms, and
as a material therefor, there may also be used resin, metal or the like, besides a
rubber-like elastic material. In addition, at the time when the diaphragm is separated
or away from the disk of the vane blade positioned by the stoppers, the volume of
the anti-diffuser side chamber can be made small by continuously reducing fluid pressure
by means of the fluid pressure adjusting mechanism. The driving force to cause the
diaphragm to deform may not be adjusted by fluid pressure supplied by means of the
fluid pressure adjusting mechanism. As the urging members, besides the compression
springs, there may be used rubber-like elastic bodies, elastic bodies using resin,
or the like, in addition to tension springs. As the case where the stoppers position
the vane blade against the urging of the compression springs, there may not only be
a case where the vane blade is in a position in which it is buried in the diffuser
passage wall, but also a case where the amount of protrusion of the vane blade into
the diffuser passage is equal to or less than a predetermined amount. Here, the predetermined
amount is an amount which, when the amount of protrusion is equal to or less than
that amount, can deal with a case where the operation flow rate of the centrifugal
compressor is a large flow rate.
[EXPLANATION OF REFERENCE NUMERALS AND CHARACTERS]
[0033]
1: centrifugal compressor
2: scroll casing
3: impeller
4: vanes
5: diffuser passage
6: diffuser plate
7: space
7a: diffuser side chamber
7b: anti-diffuser side chamber
8: vane blade
9: disk
10: blade portions
11: slits
12: diaphragm
13: stoppers
14: compression springs
15: fluid pressure adjusting mechanism
16: flow passage