The present invention relates to an axial compressor and a control method for stabilizing a fluid in an axial compressor, and more particularly, to an axial compressor capable of suppressing or preventing an occurrence of a stall when a threshold point is exceeded by an unexpected event during driving in a low-flow high-pressure section having a high efficiency on a performance curve of the axial compressor, and a control method for stabilizing a fluid in the axial compressor.
An axial compressor is capable of generating a great output and therefore is widely used for jet engines, gas turbines, oxygen producers, chemical plants, and the like. The axial compressor is applied in various fields since it is capable of achieving a minute vibration, a high efficiency, a high speed rotation, and a small size.
Schematically, the axial compressor is structured in such a manner that rotors and stators fixed to a casing are alternately arranged.
In a conventional axial impeller used as the axial compressor, a stall may occur when a threshold point is exceeded by an unexpected event during driving in a low-flow high-pressure section on a performance curve, in which efficiency is high.
To resolve such a limitation, specific conditions for optimizing the effect have been analyzed in terms of a number of injection nozzles for injecting a fluid, a nozzle shape, a nozzle arrangement, an injection type, a nozzle angle, a nozzle flow volume, and the like. However, such research is still in the early stages with almost no technology currently being commercialized.
Furthermore, due to technological characteristics, the foregoing conditions need to be experimentally verified, which requires a great deal of expenditure and time. Also, since conducting a compressor stability experiment is extremely dangerous, almost no research has been conducted via experiments.
Accordingly, there is an increasing demand for a fluid stabilizing control method capable of suppressing or preventing an occurrence of a stall that may transpire during driving of an axial compressor.
An aspect of the present invention provides an axial compressor that suppresses or prevents an occurrence of a stall when a threshold point is exceeded by an unexpected event during driving in a low-flow high-pressure section having a high efficiency on a performance curve of the axial compressor, and a control method for stabilizing a fluid in the axial compressor.
Another aspect of the present invention provides an axial compressor that reduces an amount of power expended for suppressing a stall by properly controlling an air injection method and, furthermore, minimizes use of a highly-pressurized air, thereby achieving economically feasible stall control, and a control method for stabilizing a fluid in the axial compressor.
According to an aspect of the present invention, there is provided an axial compressor including a casing which configured to include a plurality of stators provided on an inner surface and such that a fluid as a compression object is introduced and discharged, an axial impeller configured to rotate within the casing and to include a plurality of rotors arranged between neighboring stators of the plurality of stators, and a stall controller configured to suppress or prevent a stall that may occur during rotation of the axial impeller by supplying highly-pressurized compressed air into the casing according to a preset time and volume. According to the structure, the occurrence of a stall may be suppressed or prevented, the occurrence of the stall that may transpire when a threshold point is exceeded by an unexpected event during driving in a low-flow high-pressure section on a performance curve, in which efficiency is high. Additionally, by properly controlling air injection method for suppressing the stall, an amount of power expended for the stall control may be reduced. Also, since supply of the highly-pressurized compressed air is minimized, economically feasible stall control may be achieved.
The stall controller may include a pulsator mounted on a transfer line which connects an injection nozzle for injecting compressed air into the casing with a blower for supplying highly-pressurized compressed air, so as to pulsatively inject the highly-pressurized compressed air.
The pulsator may increase a supplied volume of the compressed air in a stepwise manner after injection of the highly-pressurized compressed air begins.
The pulsator may increase a supplied volume of the highly-pressurized compressed in a linear manner air after injection of the compressed air begins.
The stall controller may inject the highly-pressurized compressed air into the casing by a fixed injection method before the axial impeller goes into an unstable region during driving.
The stall controller may inject the highly-pressurized compressed air into the casing by a stepwise injection method before the axial impeller goes into an unstable region during driving.
According to an aspect of the present invention, there is provided a fluid stabilizing control method of an axial compressor including a casing and an axial impeller that compresses a fluid by rotating the axial impeller in the casing, the control method including driving to drive the axial impeller, and stall controlling to suppress or prevent an occurrence of a stall that may transpire during rotation of the axial impeller by supplying highly-pressurized compressed air into the casing through a stall controller according to a predetermined time and volume.
In the stall controlling, the stall controller may include a pulsator configured to inject the highly-pressurized compressed air into the casing by a pulsed injection method before the axial impeller goes into an unstable region during driving.
In the stall controlling, the stall controller may inject the highly-pressurized compressed air into the casing by a linear injection method before the axial impeller goes into an unstable region during driving.
In the stall controlling, the stall controller may inject the highly-pressurized compressed air into the casing by a combination of a linear injection method and a pulsed injection method, before the axial impeller goes into an unstable region during driving.
In the stall controlling, the stall controller may inject the highly-pressurized compressed air into the casing by a fixed injection method before the axial impeller goes into an unstable region during driving.
In the stall controlling, the stall controller may inject the highly-pressurized compressed air into the casing by a stepwise injection method before the axial impeller goes into an unstable region during driving.
According to an example of the present invention, an occurrence of a stall may be suppressed or prevented, the occurrence of a stall that may transpire when a threshold point is exceeded due to an unexpected event during driving in a low-flow high-pressure section on a performance curve, in which efficiency is high.
In addition, according to an embodiment of the present invention, since an air injection method for suppressing the occurrence of a stall is properly applied, an amount of power expended for the stall control may be reduced. Also, since supply of the highly-pressurized compressed air is minimized, the stall control may be performed economically.
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the like elements throughout. The following description illustrates one of various aspects of the present invention and constitutes part of a detailed description about the present invention.
However, in explaining the embodiments of the present invention, generally known functions and structures will not be explained in detail for conciseness.
Referring to
Among the foregoing structures, the casing 110 will be described first. As shown in
Here, the driver 113 may include a direct current (DC) motor. The driving force transmitter 114 may include a gear structure.
A plurality of stators 116 may be provided to an inner surface of the casing 110 in which the axial impeller 120 rotates. The plurality of stators 116 may correspond to a plurality of rotors 112 of the axial impeller 120 that will be described hereinafter. Referring to
The axial impeller 120 is a part actually compressing the fluid through being rotated. The axial impeller 120 may include a rotational shaft 123 axially rotating in connection with the driving force transmitter 114, and the plurality of rotors 121 extended outward from an outer surface of the rotational shaft 123 and arranged between respective neighboring stators 116.
According to the aforementioned structure, a fluid introduced through the inlet 111 may be compressed while passing through a space between the plurality of rotors 121 of the axial impeller 120 and the plurality of stators 116 being in a static position, and then discharged through the outlet 112.
However, as aforementioned, when a threshold point is exceeded by an unexpected event during driving in a low-flow high-pressure section having a high efficiency on a performance curve of the axial compressor, an occurrence of a stall may transpire. The occurrence of a stall may generate a surge, thereby causing a backflow of the introduced fluid. Furthermore, the occurrence of a stall may cause an unstable operation of a system in which the axial impeller 120 is used.
To suppress or prevent the occurrence of a stall, the axial compressor 100 according to an embodiment of the present invention may further include a stall controller 150 to control a stall by controlling an air injection method.
As shown in
Before the axial impeller 120 goes into an unstable region during driving, the pulsator-type stall controller 150 may supply highly-pressurized compressed air by a pulsed injection method into the casing 110 in which the axial impeller 120 rotates, accordingly suppressing or preventing the occurrence of a stall.
For suppression of the stall, a volume of the fluid introduced into the axial impeller 120 is inversely proportional to a volume of the compressed air being injected through the injection nozzle 151. Therefore, when the first occurrence of a stall transpires, the volume of the highly-pressurized compressed air may be reduced. Once the volume of the fluid starts reducing, the volume of the highly-pressurized compressed air may be increased. Such a method is referred to as the stepwise injection method which will be described hereinafter.
Hereinafter, a fluid stabilizing control method of the above-structured axial compressor 100 will be described.
The fluid stabilizing control method of the axial compressor 100 may include driving that drives the axial impeller 120, and stall controlling that suppresses or prevents an occurrence of a stall that may transpire during rotation of the axial impeller 120 by supplying highly-pressurized compressed air into the casing 110 through the stall controller 10 according to a preset time and volume.
The driving may be performed by driving the driver 113 to rotate the axial impeller 120, and introducing a fluid through the inlet 111.
The stall controlling may supply the highly-pressurized compressed air into the casing 110 by the pulsed injection method using the pulsator-type stall controller 150 before the axial impeller 120 goes into an unstable region during driving.
As a result of an actual experiment applying the pulsator as the stall controller 150 as shown in
In addition, as shown in
Thus, according to the embodiment of the present invention, the occurrence of a stall may be suppressed or prevented, the occurrence of a stall which may transpire when the threshold point is exceeded by an unexpected event during driving in a low-flow high-pressure section having a high efficiency on a performance curve of the axial compressor 100.
Moreover, since the pulsed injection method is properly used as the air injection method for suppressing the stall, an amount of power expended for the stall control may be reduced. Also, since supply of the highly-pressurized compressed air is minimized, the stall control may be performed economically.
Hereinafter, a stall control method of an axial compressor according to another embodiment of the present invention will be described.
With the foregoing method as well, the stall may be suppressed up to the low fluid volume. In addition, use of the highly-pressurized compressed air which is expensive may be reduced, thereby achieving economically feasible stall control.
As described above, when the pulsed injection method, the linear injection method, the fixed injection method, the stepwise injection method, or a combination of the foregoing methods, for example a linear-pulsed injection method, are applied as the stall control method, occurrence of the stall may be prevented up to the low fluid volume. Additionally, since use of expensive highly-pressurized compressed air is reduced, economical stall control may be achieved.
Although a few embodiments of the present invention have been shown and described, the present invention is not limited to the described embodiments. Instead, it would be appreciated by those skilled in the art that changes may be made to these embodiments without departing from the principles and spirit of the invention, the scope of which is defined by the claims and their equivalents.
Industrial applicability is included in the specification.
Number | Date | Country | Kind |
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10-2010-0139262 | Dec 2010 | KR | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/KR2011/001401 | 2/28/2011 | WO | 00 | 6/28/2013 |
Publishing Document | Publishing Date | Country | Kind |
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WO2012/091216 | 7/5/2012 | WO | A |
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20130272845 A1 | Oct 2013 | US |