FIELD OF THE INVENTION
[0002] The present application relates to refrigerant equipment, and more specifically relates
to a volute structure, a centrifugal compressor and a refrigerant equipment.
BACKGROUND OF THE INVENTION
[0003] In double-stage and multi-stage centrifugal compressor structures, in order to reduce
the length of a cantilever end of a main shaft, enhance a threshold rotating speed,
and enhance stability, a pneumatic part of multi-stage compression is always made
very compact. However, the pneumatic part of a centrifugal compressor includes many
components, such that it is very difficult to arrange the components of the pneumatic
part of the centrifugal compressor. Particularly in a volute front tilting-type multi-stage
compression, the volute is very close to a curve passage behind a first-stage diffuser
outlet, such that the structure is not satisfied.
[0004] Fig. 1 is a schematic diagram of a layout of a pneumatic part of a volute front tilting-type
double-stage centrifugal compressor, in which an internal arc cavity of the volute
faces downstream of air flow. The centrifugal type compressor pneumatic part mainly
comprises a deflector, a first-stage impeller, a first-stage diffuser, a curve passage,
a backflow device, a second-stage impeller, a second-stage diffuser, and a volute
21. The centrifugal compressor comprises a main shaft 20 and the volute 21. In the
prior art, in order to improve the structure, the curve passage is arranged as far
as possible from the volute 21 by narrowing the length of the first-stage diffuser,
while increasing the cantilever end length of the main shaft 20.
[0005] The inventors find that the prior art at least has the following drawbacks: narrowing
the length of the first-stage diffuser section will result in that the gas entering
the centrifugal compressor cannot be sufficiently diffused, which will deteriorate
the performance of the centrifugal compressor. Further, increasing the length of the
main shaft 20 results in reduction of the threshold rotating speed, deterioration
of the operation stability, and degradation of performance of the compressor.
SUMMARY OF THE INVENTION
[0006] One of objectives of the present application is to provide a volute structure, a
centrifugal compressor, and a refrigerant device, for optimizing a pneumatic structure
of the existing centrifugal compressor, and enhancing unit performance and stability
of the compressor.
[0007] In order to achieve the objective above, the present application provides the following
technical solutions:
[0008] The present application provides a volute structure, comprising: a cabinet, a volute
housing, and a backflow device; the volute housing comprising an inner volute and
an outer volute which are separately provided, a fluid passage being formed between
the inner volute and the outer volute; and the inner volute being arranged with the
backflow device.
[0009] In the above volute structure, optionally, the inner volute and the backflow device
are casted integrally.
[0010] In the above volute structure, optionally, outer volute and the cabinet are casted
integrally.
[0011] In the above volute structure, optionally, a connection portion between the inner
volute and the outer volute is rounded.
[0012] In the above volute structure, optionally, the volute structure further comprises
a curve passage that is fixed on backflow device.
[0013] In the above volute structure, optionally, the curve passage and the backflow device
are casted integrally.
[0014] The present application further provides a centrifugal compressor, comprising a volute
structure according to the present application
[0015] In the above centrifugal compressor, optionally, the centrifugal compressor also
comprises a housing, and the volute structure further comprises a one-stage diffuser;
and the housing, the cabinet, the one-stage diffuser, and the backflow device enclose
a one-stage gas supply cavity.
[0016] In the above centrifugal compressor, optionally, the centrifugal compressor is a
double-stage or multi-stage centrifugal compressor.
[0017] The present application further provides a refrigerant device, comprising a centrifugal
compressor according to the present application.
[0018] Based on the technical solution above, embodiments of the present application could
at least achieve the following technical effect:
[0019] In the technical solutions above, the volute housing is divided into two separate
parts: an inner volute and an outer volute. Moreover, the inner volute and the backflow
device are arranged together, which saves the space occupied by the inner volute and
the backflow device, downsizes the structure of connecting the volute, backflow device,
and curve linkage, such that the volute housing and the curve are arranged close enough
in the structure. Meanwhile, it guarantees enough length of the first-stage diffuser
and improves the diffusion effect of the gas entering into the first-stage diffuser,
thereby enhancing unit performance and the operation stability of the centrifugal
compressor. In addition, the technical solution also shortens the length of a main
shaft, thereby raising the threshold rotating speed of the rotary part of the compressor,
enhancing the operation stability and compressor performance of the centrifugal compressor.
BRIEF DESCRIPTION OF THE ACCOMPANYING DRAWINGS
[0020] The drawings illustrated here are for providing further understanding of the present
application and thus constitute part of the present application. The exemplary embodiments
of the present application and depictions thereof are for interpreting the present
application, not constituting improper limitations of the present application. In
the drawings:
Fig. 1 is a layout diagram of a pneumatic part of a volute front tilting type double-stage
centrifugal compressor in the prior art;
Fig. 2 is a partial section view of a volute structure applied to a centrifugal compressor
according to embodiments of the present application;
Reference Numerals:
[0021] 1. Casing; 2. First-stage impeller; 3. First-stage diffuser; 4. Curve Passage; 5.
Backflow device; 6. Second-stage impeller; 7. Volute housing; 8. Cabinet; 9. First-stage
air supply cavity; 10. Second-stage diffuser; 20. Main shaft; 21. Volute.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0022] Hereinafter, the technical solution of the present application will be described
in more detail with reference to Fig. 2. Any technical solution resulting from replacement
of any technical means of the present application or combination of any two or more
technical means or technical features provided by the present application should be
included in the protection scope of the present application.
[0023] Front and rear in the present disclosure reference the air flow direction of the
volute structure, i.e., upstream of the air flow is front, namely the left side of
Fig. 2; while downstream of the air flow is rear, i.e., right side of Fig. 2.
[0024] The embodiment of the present application provides a volute structure, which is preferably
applied to a centrifugal compressor and the like. The volute structure is configured
to be a front tilting type volute structural (as shown in fig.2, internal curve cavity
of the volute housing 7 faces the upstream of the air flow, i.e. left side of fig.2),
or a rear tilting type volute structural. The volute structural is preferably applied
to double-stage centrifugal compressor or a last stage of the multi-stage centrifugal
compressor in which the volute housing is located, such that the centrifugal compressor
structure is more compact, and the stability and unit performance of the centrifugal
compressor are enhanced.
[0025] The volute structure comprises a cabinet 8, a volute housing 7, and a backflow device
5. The volute housing 7 includes an inner volute and an outer volute, which are separately
provided. A fluid passage is formed between the inner volute and the outer volute,
for fluids to pass through. The inner volute and the backflow device 5 are arranged
together.
[0026] Besides, the volute housing 7 is circumferentially split into two parts: inner volute
and outer volute. The inner volute and the backflow device 5 are arranged together
in at least the following manners: the inner volute and the backflow device 5 are
fixedly connected, or the two are of an integral structure.
[0027] In the technical solution above, the volute housing is divided into two separate
parts: an inner volute and an outer volute. Moreover, the inner volute and the backflow
device are arranged together, which saves the space occupied by the inner volute and
the backflow device, downsize the structure of fixing the volute, backflow device,
and curve linkage, such that the volute housing and the curve may arranged close enough
in the structure. Meanwhile, it guarantees enough length of the first-stage diffuse
and improves the diffusion effect of the gas entering into the first-stage diffuser,
thereby enhancing unit performance of the centrifugal compressor and the operation
stability of the centrifugal compressor. In addition, the technical solution above
also shortens the length of main shaft, thereby raising the threshold rotating speed
of the rotary part of the compressor, enhancing the operation stability and compressor
performance of the centrifugal compressor.
[0028] In addition, the inner volute and the backflow device are arranged together, which
reduces the number of components, such that while the pneumatic part of the centrifugal
compressor maintains a compact structure, parameters of the components of the pneumatic
part will be coordinated more reasonably with a better pneumatic performance. With
an example of applying the volute structure to a centrifugal compressor, the threshold
rotating speed of the centrifugal compressor is related to the main shaft length of
the centrifugal compressor. By dividing the volute housing into an outer volute and
an inner volute, positions of the outer volute and the inner volute may be arranged
more reasonably without changing the main shaft length of the centrifugal compressor,
i.e., arrangement of the volute housing may be made without affecting the threshold
rotating speed and the unit performance of the centrifugal compressor. In addition,
by dividing the volute housing into an outer volute and an inner volute, the main
shaft length may be shortened based on the existing mechanism, with an enhanced compressor
threshold rotating speed. Enhance of the threshold rotating speed results in enhancement
of the compressor stability, meanwhile the length of the main shaft is shortened,
the bearing length or diameter is be shortened, the power consumption is reduced and
the compressor performance is enhanced.
[0029] Furthermore, the shape of the volute will not change by dividing the volute housing
into separate inner volute and outer volute, thereby not affecting the pneumatic performance
of the volute. In addition, by dividing the volute housing into an outer volute and
an inner volute, the volute casting process would be simplified. Meanwhile, an existing
digital control processing center may be employed for secondary processing of the
inner volute based on casting, which enhances unit performance and cabinet universality,
thereby facilitating universality between different machine models, further reducing
the molding times and expenses of new boxes.
[0030] Further, the volute structure further comprises a curve passage 4 provided on the
backflow device 5.
[0031] In the present embodiment, the inner volute and the curve 4 are simultaneously fixed
to the backflow device 5, which saves an air supply pipeline disposed between the
curve passage and the backflow device in the existing centrifugal compressor, such
that the curve passage and the inner volute would be arranged more compact in structure,
thereby further compacting the structure of a double-stage or multi-stage centrifugal
compressor. However, a integral type volute structure is usually employed in the prior
art, such that in order to mount a backflow device and avoid too small distance between
the curve passage and the volute (i.e., the distance of the apex of the curve passage
from the nearest point of volute housing along a main shaft direction), the axial
length of the main shaft has to be lengthened, which would reduce the threshold rotary
speed of the compressor, thereby reducing stability of the compressor.
[0032] Here, the inner volute and the backflow device 5 are formed into an integral structure
through casting, i.e., the arc shape of the inner volute is formed at an external
side of the backflow device 5. The inner volute is arranged on the backflow device
5. By casting, a profile of the inner volute would be processed by a current processing
center, which expands the structure of the volute, such that the volute would be better
matched with other pneumatic elements (impeller, diffuser) with a better performance,
without changing the volute structure at the ease of arranging the structure, which
might affect the pneumatic performance.
[0033] In order to enhance the strength of the overall structure and reduce the mounting
difficulty, the curve 4 and the backflow device 5 could also be casted into an integral
structure.
[0034] Furthermore, the outer volute and the cabinet 8 are casted into an integral structure,
i.e., the arc shape of the outer volute is formed at an inner side of the box 8. With
this structure, a improved volute profile may be adopted in the overall arrange, without
changing the volute structure at the ease of arranging the structure, which might
affect the pneumatic performance.
[0035] Besides, the inner volute and the backflow device 5 are of an integral structure,
and the inner volute and the cabinet 8 are of an integral structure, which may also
be understood as such that the backflow device 5 and the cabinet 8 together form a
volute housing 7. In the embodiment, the outer volute is disposed on the cabinet 8,
and the inner volute is disposed on the backflow device 5. By means of precise casting
and high-precision processing of the processing center, good connection between the
inner and outer volutes is guaranteed.
[0036] In the present embodiment, further, a connection part between the inner volute and
the outer volute is rounded so as to avoid connection displacement therebetween.
[0037] Embodiments of the present application further provide a centrifugal compressor,
comprising a volute structure according to any technical solution of the present application.
[0038] With reference to Fig. 2, the entire centrifugal compressor mainly comprises a casing
1, a first-stage impellor 2, a first-stage diffuser 3, a curve passage 4, a backflow
device 5, a second-stage impellor 6, a second-stage diffuser 10, a volute housing
7, and a cabinet 8. Particularly, volute front tilting means that volute tilts to
the air inlet side (left side of Fig. 2). The air flow sequentially enters into the
first-stage impellor 2, the first-stage diffuser 3, curve passage 4, second-stage
impellor 6, second-stage diffuser 10, and volute housing 7, finally implementing air
pressure boost.
[0039] The volute structure is one of important components of pneumatic parts of the centrifugal
compressor. Besides the volute structure, the centrifugal compressor pneumatic parts
further comprises an impellor and a pneumatic motor.
[0040] Further, the centrifugal compressor further comprises a casing 1. The volute structure
further comprises a first-stage diffuser 3. The casing 1, the cabinet 8, the first-stage
diffuser 3 and the backflow device 5 enclose a first-stage air supply cavity 9. Namely,
the cabinet 8 not only forms the volute housing 7 but also forms a first-stage air
supply cavity 9.
[0041] The centrifugal compressor changes a position of setting the first-stage air supply
cavity 9. The casing 1, the cabinet 8, the first-stage diffuser 3 and the backflow
device 5 enclose the first-stage air supply cavity 9, such that an air supply function
may be implemented without adding an air supply part.
[0042] As mentioned above, the centrifugal compressor is a double-stage or multi-stage centrifugal
compressor.
[0043] Embodiments of the present application further provide a refrigerant equipment, comprising
a centrifugal compressor provided according to any technical solution of the present
application. A refrigerant equipment having the centrifugal compressor has a more
compact centrifugal compressor pneumatic structure with a better operation stability
of the compressor and a better pneumatic performance. The refrigerant equipment comprises
air condition units.
[0044] In depictions of the present application, it should be understood that orientations
or positional relationships indicated by terms like "center", "longitudinal", "transversal",
"front", "rear", "left", "right", "vertical", "horizontal", "top" "bottom", "inner",
"outer" and others are based on the orientations or positional relationships illustrated
in the accompanying drawings, which are only for facilitating depiction of the present
application and simplifying the depiction, rather than indicating or suggesting that
the specified means or elements must have specific orientations or have to be constructed
and operated with the specific orientations; Therefore, they should not be understood
as limitation to the protection scope of the present application.
[0045] If words like "first" and "second" used here are for limiting components, those skilled
in the art should know that use of "first" and "second" is only for at the ease of
distinguishing the spare parts; unless otherwise indicated, the words have no special
meanings.
[0046] Finally, it should be stated that the embodiments above are only for illustrating
the technical solution of the present application, not for limiting it; although the
present application have been described in detail with reference to the preferred
embodiments, those skilled in the art should understand that the preferred embodiments
of the present application may be modified or part of technical features may be replaced
in equivalence; without departing from the spirit of the technical solution of the
present application, such modifications and equivalent replacements should be covered
within the scope of the technical solution as recited in the present application.
1. A volute structure, comprising: a cabinet, a volute housing, and a backflow device;
the volute housing comprising an inner volute and an outer volute which are separately
provided, a fluid passage being formed between the inner volute and the outer volute;
and
the inner volute being arranged with the backflow device.
2. The volute structure according to claim 1, wherein the inner volute and the backflow
device are casted integrally.
3. The volute structure according to claim 1, wherein the outer volute and the cabinet
are casted integrally.
4. The volute structure according to any one of claims 1-3, wherein a connection portion
between the inner volute and the outer volute is rounded.
5. The volute structure according to any one of claims 1-3, wherein the volute structure
further comprises a curve passage that is fixed on backflow device.
6. The volute structure according to claim 5, wherein the curve passage and the backflow
device are casted integrally.
7. A centrifugal compressor, comprising a volute structure according to any one of claims
1-6.
8. The volute structure according to claim 7, wherein the centrifugal compressor also
comprises a housing, and the volute structure further comprises a one-stage diffuser;
and
wherein the housing, the cabinet, the one-stage diffuser, and the backflow device
enclose a one-stage gas supply cavity.
9. The volute structure according to claim 7, wherein the centrifugal compressor is a
double-stage or multi-stage centrifugal compressor.
10. A refrigerant device, comprising a centrifugal compressor according to any one of
claims 7-9.