Embodiments of the subject matter disclosed herein generally relate to methods and systems and, more particularly, to mechanisms and techniques for sealing an actuator rod in a variable inlet vanes system.
During the past years, the importance of compressors in various industries has increased. The compressors are used in engines, turbines, power generation, cryogenic applications, oil and gas processing, etc. Therefore, various mechanisms and techniques related to compressors are often subject to research for improving the efficiency of this turbomachine and solving problems related to specific situations.
Actuation systems are used in various equipments, such as, compressors, pumps and expanders, to apply a force in order to modify a current state of the equipment. For example, an actuation system may operate adjustable inlet guide vanes (IVG) used in compressor applications to adjust an angle of incidence of inlet air into a compressor rotor and to control an amount of inlet air such as to ensure proper surge and to maximize efficiency.
An example of an adjustable IGV system 100 is shown in
Given the potentially damaging environment in which the adjustable IGV system 100 may operate (for example, when used in a natural gas installation), the control electronics 140 is isolated from this environment. Conventionally, this separation of the control electronics 140 from the environment is achieved using mechanical seals, for example, a dynamic seal energized by springs closing a space between the body of the actuation device 130 and the actuator rod 120.
It has been observed that the mechanical seals do not operate satisfactory. Moreover, sometimes the gas in the environment (i.e., outside the actuation device) has low (cryogenic) temperature and, therefore, the chilled actuator rod 120, which extends inside the body of the actuator device 130 and is a good heat conductor, may determine ice formation (by condensation of the humidity inside the case). The ice may block the actuators bar's movement.
Further, if the force is generated hydraulically, different pressures inside and outside the actuation device 130 may create further problems (e.g., imbalances and forces) and inefficiencies (e.g., a direction of the force may be altered), when the sealing is not effective.
Accordingly, it would be desirable to provide systems and methods that avoid the afore-described problems and drawbacks.
According to various embodiments, separating a first fluid at one end of an actuator rod and a second fluid at an opposite end of the actuator rod is achieved using at least one fluid flow.
According to one exemplary embodiment, an actuator device useable to change orientation of one or more vanes includes an actuator rod and an actuator device body. The actuator rod is configured to transfer a force along an axis thereof, and having a first end in a first fluid and a second end in a second fluid, the second end being opposite to the first end along the axis. The actuator device body is configured to allow the actuator rod to move along the axis inside the actuator device body, and having has a first inlet flange configured to allow a third fluid to enter a space between the actuator device body and the actuator rod, and a first outlet flange configured to allow the third fluid to exit the actuator device body. The third fluid has a pressure larger than a pressure of the first fluid, and the first outlet flange is closer to the first end of the actuator rod than the first inlet flange.
According to another exemplary embodiment, a compressor has one or more vanes configured to determine at least one of a direction and an amount of a first fluid passing through the compressor, and an actuator device configured to apply a force to the one or more vanes. The actuator device includes an actuator rod and an actuator device body. The actuator rod is configured to transfer a force along an axis thereof, and having a first end in a first fluid and a second end in a second fluid, the second end being opposite to the first end along the axis. The actuator device body is configured to allow the actuator rod to move along the axis inside the actuator device body, and having has a first inlet flange configured to allow a third fluid to enter a space between the actuator device body and the actuator rod, and a first outlet flange configured to allow the third fluid to exit the actuator device body. The third fluid has a pressure larger than a pressure of the first fluid, and the first outlet flange is closer to the first end of the actuator rod than the first inlet flange.
According to another exemplary embodiment, a method of sealing a compressor fluid at a first end of an actuation bar and an environment at a second end of the actuation bar, the second end being opposite to the first end, and the actuation bar being configured to move along an axis, inside an actuator device body is provided. The method includes providing a first flow of compressor fluid routed from an output of the compressor in a space between the actuator device body and the actuator rod, via a first inlet flange of the actuator body and a first outlet flange of the actuator body, (1) the compressor fluid in the first flow having a pressure larger than a pressure of the compressor fluid at a first end of an actuation bar, and (2) the first outlet flange being closer to the first end of the actuator rod than the first inlet flange. The method further includes providing a second flow of neutral fluid in the space between the actuator device body and the actuator rod, via a second inlet flange of the actuator body and a second outlet flange of the actuator body, (3) the first inlet flange and the first outlet flange being closer to the first end than the second inlet flange and the second outlet flange, and (4) the second inlet flange being closer to the second end of the actuation bar than the second outlet flange.
The accompanying drawings, which are incorporated in and constitute a part of the specification, illustrate one or more embodiments and, together with the description, explain these embodiments. In the drawings:
The following description of the exemplary embodiments refers to the accompanying drawings. The same reference numbers in different drawings identify the same or similar elements. The following detailed description does not limit the invention. Instead, the scope of the invention is defined by the appended claims. The following embodiments are discussed, for simplicity, with regard to the terminology and structure of compressors having inlet vanes that are modified by applying a force via an actuator device. However, the embodiments to be discussed next are not limited to these compressors, but may be applied to other systems that require to isolate an environment at one end of an actuator rod thereof from an environment at another end of the actuation rod.
Reference throughout the specification to “one embodiment” or “an embodiment” means that a particular feature, structure, or characteristic described in connection with an embodiment is included in at least one embodiment of the subject matter disclosed. Thus, the appearance of the phrases “in one embodiment” or “in an embodiment” in various places throughout the specification is not necessarily referring to the same embodiment. Further, the particular features, structures or characteristics may be combined in any suitable manner in one or more embodiments.
In actuator devices according to various embodiments, the mechanical seals with springs are replaced by dynamical sealing using one or more flows of fluid circulating between an actuator rod and an actuator body. At least one of the flows of fluid may heat the actuator rod preventing the formation of ice.
The actuator rod 310 is mounted to move through an actuator device body 320. In other words, the actuator device body 320 is configured to allow the actuator rod 310 to move along the axis 305 inside the actuator device body 320. A second end 314 of the actuator rod 310 (which second end is opposite to the first end 312 along the axis 305) may be exposed to a second fluid that may be confined inside a cavity 316 of the actuator device body 320. Control electronics 318 may be mounted on the actuator device body 320 to be exposed with the second fluid. The term control electronics may stand for an actuator and/or an actuator motor. The invention is not limited by the device(s) collectively named control electronics exposed to the second fluid kept isolated from the corrosive first fluid.
The second fluid may be air or other fluid that does not have a negative effect on the electronics 318. However, the natural gas that may be compressed in a compressor is usually corrosive and typically leads to rapid degradation of the electronics. Therefore, the actuator device body 320 and the actuator rod 310 are configured and operated to prevent the first fluid (e.g., natural gas) from mixing with the second fluid (e.g., air).
The actuator body 320 is therefore configured to allow a third fluid to flow inside the actuator body, in a space between the actuator rod 310 and the actuator body 320. In order to allow the third fluid to enter this space, the actuator device body 320 has a first inlet flange 322. In order to allow the third fluid to exit the actuator device body, the actuator device body 320 has a first outlet flange 324. Thus, the third fluid flows from the first inlet flange 322 to the first outlet flange 324 parallel to the axis 305 and between the actuator rod 310 and the device body 320. The outlet flange 324 may be closer to the first end 312 of the actuator rod 310 than the first inlet flange 322. The third fluid may have a pressure larger than a pressure of the first fluid and/or substantially the same composition as the first fluid. For example, the third fluid may be compressed first fluid (i.e., gas) re-circulated from an outlet of the compressor.
The third fluid may have a temperature different from a temperature of the first fluid. To control the temperature of the third fluid, a heat exchanger or similar known devices may be used. Thereby, the actuator rod 310, which is made of a good heat conductor (e.g., metal or metallic alloy), may be heated due to the third fluid so that condensation and ice do not occur.
A number of mechanical seals 330 may be present at various locations but the present inventive concept is not limited by the presence of other seals. Between the actuator 310 rod and the one or more vanes moved due to a force generated along the axis 305 in the actuator device 300, it may be a connecting rod 340, but the present inventive concept is not limited by the presence of such a connecting rod.
The third fluid flow may also be used to develop a force along the axis. For example, as illustrated in
In another exemplary embodiment illustrated in
When a pressure of the neutral fluid entering the space is larger than a pressure of the fluid entering the first inlet flange 322, it may further prevent the fluid from 322 to advance toward the closed cavity 316 where the electronics 318 is installed. Thus, the sealing around the actuator rod 310 is further enhanced. Of course, traditional seals 330 may also be provided closer to the end 314 of the rod 310 for further sealing.
Further, the actuator device body may include a vent 550 located between the first inlet flange 322 and the second outlet flange 534 along the axis 305, and configured to allow the neutral fluid and/or the third fluid to exit the actuator device body 520.
In an overall view illustrated in
Some of the embodiments described about may execute a method 800 of sealing a compressor fluid at a first end of an actuator rod and an environment at a second end of the actuator rod, the second end being opposite to the first end, and the actuator bar being configured to move along an axis, inside an actuator device body. The method 800 illustrated in
The method 800, further includes providing a second flow of neutral fluid in the space between the actuator device body and the actuator rod, via a second inlet flange of the actuator body and a second outlet flange of the actuator body, (3) the first inlet flange and the first outlet flange being closer to the first end than the second inlet flange and the second outlet flange, and (4) the second inlet flange being closer to the second end of the actuation bar than the second outlet flange, at S820.
The disclosed exemplary embodiments provide devices and methods for sealing, preventing icing and balancing an actuator of an IGV of a turbo-machine. It should be understood that this description is not intended to limit the invention. On the contrary, the exemplary embodiments are intended to cover alternatives, modifications and equivalents, which are included in the spirit and scope of the invention as defined by the appended claims. Further, in the detailed description of the exemplary embodiments, numerous specific details are set forth in order to provide a comprehensive understanding of the claimed invention. However, one skilled in the art would understand that various embodiments may be practiced without such specific details.
Although the features and elements of the present exemplary embodiments are described in the embodiments in particular combinations, each feature or element can be used alone without the other features and elements of the embodiments or in various combinations with or without other features and elements disclosed herein.
This written description uses examples of the subject matter disclosed to enable any person skilled in the art to practice the same, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the subject matter is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims.
Number | Date | Country | Kind |
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CO2011A000037 | Sep 2011 | IT | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2012/067447 | 9/6/2012 | WO | 00 | 3/6/2014 |