US20140064921A1

US20140064921A1 - System and method to align variable diffuser vane with direction of flow of working fluid

Info

Publication number: US20140064921A1
Application number: US13/601,822
Authority: US
Inventors: Dale Eugene Husted
Original assignee: Dresser LLC
Current assignee: Howden Roots LLC
Priority date: 2012-08-31
Filing date: 2012-08-31
Publication date: 2014-03-06
Also published as: BR112015004606A2; WO2014035726A1; CN104919184A; EP2890897A1; RU2015107886A

Abstract

Embodiments of systems and methods permit use of variable diffuser vanes in multi-stage compressor devices. These embodiments deploy a flow sensor to identify the direction of flow for a working fluid that transits the stages of the compressor device. In one embodiment, the flow sensor generates a signal, which a controller processes to align a variable diffuser vane with the direction of flow of the working fluid. This configuration pre-empts the operational difficulties of previous designs by providing independent control over the diffuser vanes in the individual stages of the multi-stage compressor device.

Description

BACKGROUND

The subject matter disclosed herein relates to compressor devices (e.g., centrifugal compressors) and, in particular, to diffusers and diffuser vanes for a compressor device.
Compressor devices (e.g., centrifugal compressors) use a diffuser assembly to convert kinetic energy of a working fluid into static pressure by slowing the velocity of the working fluid through an expanding volume region. An example of a diffuser assembly typically utilizes several diffuser vanes in circumferential arrangement about an impeller. The design (e.g., shapes and sizes) of the diffuser vanes, in combination with the preferred orientation of the leading edge and the trailing edge of the diffuser vanes with respect to the flow of the working fluid, often determine how the diffuser vanes are affixed in the diffuser assembly.
To add further improvement and flexibility to the design, some examples of a diffuser assembly incorporate variable diffuser vanes. These types of diffuser vanes move to change the orientation of the leading edge and the trailing edge. This feature helps to tune operation of the compressor device. Known designs for variable diffuser vanes rotate about an axis that resides in the lower half, i.e., closer to the leading edge than the trailing edge of the diffuser vanes.
Some configurations of compressor devices do not comport with use of variable diffuser vanes. Multi-stage compressors, for example, often forego use of variable diffuser vanes because of problems with maintaining desired flow and pressure rates for the working fluid; namely, that use of variable diffuser vanes can reduce the operating range of the multi-stage compressor device.

BRIEF DESCRIPTION OF THE INVENTION

This disclosure describes embodiments of systems and methods that permit use of variable diffuser vanes in multi-stage compressor devices. These embodiments deploy a flow sensor in combination with a variable diffuser vane to align the variable diffuser vane with the direction of flow of the working fluid. This configuration pre-empts the operational difficulties of previous designs by providing independent control over the diffuser vanes in the individual stages of the multi-stage compressor device.

BRIEF DESCRIPTION OF THE DRAWINGS

Reference is now made briefly to the accompanying drawings, in which:

FIG. 1 depicts a schematic view of an exemplary embodiment of a multi-stage compressor device;

FIG. 2 depicts a schematic view of an exemplary embodiment of a system for controller operation of a compressor device; e.g., the multi-stage compressor device of FIG. 1;

FIG. 3 depicts a flow diagram of an exemplary embodiment of a method for operating a compressor device, e.g., the multi-stage compressor device of FIG. 1;

FIG. 4 depicts a perspective view of an example of a diffuser assembly for use in a compressor device, e.g., the multi-stage compressor device of FIG. 1;

FIG. 5 depicts a top view of the diffuser assembly of FIG. 4 with a flow sensor in a first sensor position and a second sensor position;

FIG. 6 depicts a top view of the diffuser assembly of FIG. 4 with the diffuser vane in a first vane position and a second vane position;

FIG. 7 depicts a detail view of the leading edge of the exemplary diffuser vane of FIG. 4;

FIG. 8 depicts a flow diagram of an exemplary embodiment of a method for operating a compressor device, e.g., the multi-stage compressor device of FIG. 1; and

FIG. 9 depicts a high-level wiring schematic of an example of a controller for use in a system, e.g., the system of FIG. 2.

Where applicable like reference characters designate identical or corresponding components and units throughout the several views, which are not to scale unless otherwise indicated.

DETAILED DESCRIPTION OF THE INVENTION

FIG. 1 illustrates a schematic view of an exemplary embodiment of a compressor device 100. The compressor device 100 includes an inlet 102, an outlet 104, and one or more stages (e.g., a first stage 106 and a second stage 108) disposed in flow connection with the inlet 102 and the outlet 104. The stages 106, 108 include an impeller (e.g., a first impeller 110 and a second impeller 112) and a diffuser assembly (e.g., a first diffuser assembly 114 and a second diffuser assembly 116). The diffuser assemblies 114, 116 include one or more diffuser vanes (e.g., a first diffuser vane 118 and a second diffuser vane 120) and a flow sensor (e.g., a first flow sensor 122 and a second flow sensor 124). The compressor device 100 also includes a drive unit 126 and a drive shaft 128, which couples with the drive unit 126 and with one or more of the impellers 110, 112.
Embodiments of the compressor device 100 find use in a variety of settings and industries including automotive industries, electronics industries, aerospace industries, oil and gas industries, power generation industries, petrochemical industries, and the like. During one implementation, the shaft 128 transfers power from the drive unit 126 to rotate the first impeller 110 and the second impeller 112. Rotation of the first impeller 110 draws a working fluid (e.g., air) through the inlet 102. In the first stage 106, the first impeller 110 compresses the working fluid. The compressed working fluid flows into the first diffuser assembly 114, which allows the working fluid to expand before the working fluid enters the second stage 108. In the second stage 108, the working fluid undergoes compression and expansion by, respectively, the second impeller 112 and the second diffuser assembly 116. In one embodiment, the compressor device 100 can couple at the outlet 104 with industrial piping to expel the working fluid under pressure and/or with certain designated flow parameters as desired.
Examples of the diffuser vanes 118, 120 can move (e.g., rotate) from one position (e.g., a first position) to another position (e.g., a second position), and vice versa. Movement between the first position and the second position allows the diffuser vanes 118, 120 to align with the direction of flow of the working fluid. This feature avoids flow separation of the working fluid from the surfaces of the diffuser vane 118, 120.
The flow sensors 122, 124 monitor the direction of flow of the working fluid upstream of the diffuser vanes 118, 120. As the direction of the flow changes, e.g., due to changes in operation of the compressor device 100, the flow sensor 122 will generate a signal. Examples of the signal convey information to indicate the extent, direction, and other characteristics relevant to the direction of the flow. The controller 132 can process this signal and, in response, generate an output to impart changes to the position of the diffuser vanes 118, 120. In one example, the output encodes instructions to move the actuators 134, 136 which in turn causes the diffuser vanes 118, 120 to change position, e.g., from the first position to the second position.
As shown in FIG. 2, the compressor device 100 can form part of a system 130 (also “control system 130”), which can change operating settings for the first diffuser assembly 114 and the second diffuser assembly 116 independent of one another during operation of the compressor device 100. The system 130 includes a controller 132, which couples with the flow sensors 122, 124 and with actuators (e.g., a first actuator 134 and a second actuator 136). Examples of the actuators 134, 136 change the position of, respectively, the first diffuser vane 118 and the second diffuser vane 120. In one embodiment, the controller 132 (and/or one or more other devices in the system 130) can communicate via a network 138 with a peripheral device 140 (e.g., a display, a computer, a smartphone, a laptop, a tablet, etc.) and/or an external server 142.
The controller 132 can comprise computers and computing devices with processors and memory that can store and execute certain executable instructions, software programs, and the like. The controller 132 can be a separate unit, e.g., part of a control unit that operates the compressor device 100 and other equipment. In other examples, the controller 132 integrates with the compressor device 100, e.g., as part of the hardware and/or software configured on such hardware. In still other examples, the controller 132 can be located remote from the compressor device 100, e.g., in a separate location where the controller 132 can issue commands and instructions using wireless and wired communication, e.g., via the network 124.
Examples of the system 130 orient one or both of the diffuser vanes 118, 120 to modify flow and expansion that occurs as the working fluid transits the corresponding diffuser assemblies 114, 116. By utilizing separate flow sensors 122, 124 to measure the direction of flow upstream of the respective diffuser vanes 118, 120, the system 130 can account for variations in flow that occur from stage to stage, e.g., from stage 106 to stage 108. The system 130 can use the information about the direction of flow to instruct the actuators 134, 136 to place the diffuser vanes 118, 120 in different positions relative to one another. This feature effectively decouples operation of the compressor device 100 in the first stage 106 from the second stage 108, which allows the diffuser vanes 118, 120 to operate independent of one another and, in one example, independent of additional stages without having an adverse effect on overall performance of the compressor device 100.
FIG. 3 depicts a flow diagram of an exemplary method 200 to improve performance of a compressor device (e.g., compressor device 100 of FIG. 1). The method 200 includes, at step 202, receiving a first signal from a first flow sensor and, at step 204, receiving a second signal from a second flow sensor. In one embodiment, the first signal and the second signal encode information that identifies a first direction and a second direction of flow for a working fluid upstream of, respectively, a first diffuser vane and a second diffuser vane. The method 200 also includes, at step 206, identifying a first position for the first diffuser vane and the second diffuser vane. In one example, the first position aligns the first diffuser vane and the second diffuser vane with the first direction of flow of the working fluid. The method 200 further includes, at step 208, generating an output encoding instructions to move the first diffuser vane and the second diffuser vane to the first position.
In one embodiment, the first signal (e.g., at step 202) and the second signal (e.g., at step 204) indicate the position of the first flow sensor and the second flow sensor. To illustrate, FIG. 4 depicts a perspective view of an example of a diffuser assembly 300 for use in a compressor device (e.g., compressor device 100 (FIG. 1)). The diffuser assembly 300 includes a diffuser vane 302 and a flow sensor 304 upstream of the diffuser vane 302. In one example, the flow sensor 304 has a base element 306 and a directional element 308 disposed in the path of a flow F of a working fluid. The diffuser vane forms a vane body 310 with a leading edge 312 and a trailing edge 314. A chord length L defines the straight-line distance between the leading edge 312 and the trailing edge 314. The vane body 310 forms an aerodynamic shape (e.g., an airfoil) with a suction side surface 316 and a pressure side surface 318 identified relative to the orientation and angle of attack of the leading edge 312 relative to the flow F. At the leading edge 312, the vane body 310 converges to a tip 320.
The flow sensor 304 can move and, in one example, the directional element 308 rotates relative to the base element 306 to indicate the direction of flow F. Examples of the base element 306 can secure to components of the diffuser assembly 300. These components can include wall members, frame member, and other structure (e.g., volute) that can position the flow sensor 304 in the flow of the working fluid. For example, the flow base element 306 can reside a bore and/or counter bore in such structure to position the directional element 308 in the flow path. Examples of the base element 306 can include a pin and/or other bearing element, which receives the directional element 308. The pin acts as a pivot about which the directional element 308 can freely rotate. When placed in the path of flow F, the directional element 308 will align with the direction of the flow F. In one example, the base element 306 can comprise a rotary potentiometer and/or other like devices that can measure angular displacement. The rotary potentiometer can couple with the directional element 308 to register changes in the position of the directional element 308 in response to the direction of flow F.
With reference to FIG. 5, during one implementation, a compressor device may operate in a manner that causes the flow F to flow in a number of different directions (e.g., a first flow direction F1 and a second flow direction F2). The directional element 308 assumes one of a first sensor position 322 and a second sensor position 324, which correspond to, respectively, the first flow direction F1 and the second flow direction F2. In one example, the flow sensor 304 can register the change in the position of the directional element 308, e.g., between the first sensor position 322 and the second sensor position 324.
Examples of the first signal and/or the second signal can encode information to identify the position and/or the relative change in position of the directional element 308. In one example, the first signal and the second signal may encode an angular position to each of the first sensor position 322 and the second sensor position 324. Examples of the angular position can utilize a radial scale that covers 360°, wherein the first position 322 and the second position 324 assume different values on the radial scale, e.g., 0° for the first position 322 and 300° for the second position 324. In other examples, the first signal and the second signal my encode an angular offset to each of the first sensor position 322 and the second sensor position 324. The angular offset can define a value, e.g., a radial value, on the radial scale by which the first sensor position 322 and the second sensor position 324 deviate relative to a fixed or home position. For purposes of the present example of FIG. 5, the radial value for the first sensor position 322 is 0 and or 0° and the radial value for the second sensor position 324 is −30 and/or −30°.
The steps for identifying a first position (e.g., at step 206) for the diffuser vane 302 can use the information in the first signal and the second signal to align the diffuser vane 302 with the direction of flow F. In this connection, FIG. 6 illustrates an example of the diffuser vane 302 in a first vane position 326 and a second vane position, identified by phantom lines and the numeral 328. In one example, the vane body 302 can rotate about a rotation axis 330, which permits the position of the trailing edge 314 to change relative to, in one example, the leading edge 314. This disclosure also contemplates configurations of the diffuser vane 302 in which the rotation axis 330 is located at various positions, e.g., in positions spaced apart from the leading edge 312 and the trailing edge 314 along the chord length L (FIGS. 4 and 5). In these other configurations, both the leading edge 312 and the trailing edge 314 can rotate, e.g., about the rotation axis 330.
Implementations in which the trailing edge 314 rotates the leading edge 312 are advantageous to accommodate the first flow direction F1 and the second flow direction F2. As shown in the example of FIG. 6, despite the relatively large angular displacement of the trailing edge 314 that occurs, the leading edge 312 is secured on the rotation axis 330 to limit changes to the position of the leading edge 312, e.g., as the trailing edge 314 moves between the first vane position 326 and the second vane position 328. This feature maintains the orientation of the leading edge 312 with the second flow direction F2 to reduce the likelihood of flow separation, while providing adequate adjustment of the trailing edge 314 to dictate changes in the performance (e.g., of compressor device 100 of FIGS. 1 and 2).
FIG. 7 illustrates a detail view of the diffuser vane 302. The example of FIG. 7 shows that the tip 320 is round and/or has a curvilinear outer surface 332 defined by a radius R_TIPthat extends from a center axis 334. Other examples the tip 320 exhibit a shape (e.g., a point) that maintains the aerodynamics of the vane body 310. This disclosure also contemplates configurations of the tip 320 having less than optimal aerodynamic shapes (e.g., blunt shapes) as desired.
In the example of FIG. 7 (and FIG. 6), the rotation axis 330 resides proximate the leading edge 312 and, for example, within 5% or less of the chord length L (FIG. 4) (as measured from the leading edge 312). Depending on the size and shape of the tip 320, the rotation axis 330 can also be found within an area that the radius R_TIPdefines about the center axis 330. In one example, the rotation axis 330 is coaxial with the center axis 334 of the tip 320.
Examples of the diffuser vane 302 can comprise various materials and combinations, compositions, and derivations thereof. These materials include metals (e.g., steel, stainless steel, aluminum), metal alloys, high-strength plastics, composites, and the like. Material selection may depend on the type and composition of the working fluid. For example, working fluids with caustic properties may require that the diffuser vanes comprise relatively inert materials and/or materials that are chemically inactive with respect to the working fluid, and/or have one or more coatings and/or surface treatments that provide prevent corrosion, erosion, or other degradation of the surface of the diffuser vanes.
Geometry for the diffuser vane 302 is determined as part of the design, build, and fitting of the compressor device for the application. The geometry can include airfoil shapes, e.g., the shape shown in FIG. 4 for the vane body 310, examples of which take the form of wings and blades and/or other forms that can generate lift. In one embodiment, the diffuser vane 302 can mount, e.g., to one of the wall members, using fasteners and fastening techniques that permit rotation of the diffuser vanes about the leading edge. Screws, bolts, pins, bearings, and like components can be used to maintain the position of the leading edge, while further allowing the trailing edge to change position as contemplated herein. These fasteners can secure to the wall members of the diffuser assembly, which can comprise pieces separate from the components of the compressor device or can integrate with existing hardware found in the compressor device.
Referring back to the method 200 of FIG. 3, the steps for generating an output (e.g., at step 206) can cause the diffuser vane 302 to move, e.g., as between the first position 326 and the second position 328. The output can comprise any signal (e.g., analog and/or digital) that can encode instructs to operate a device. In the examples herein, the output can cause an actuator to move, which can facilitate movement either directly and/or indirectly of the diffuser vane 302 among and between one or more of the first position 326 and the second position 328.
FIG. 8 illustrates another exemplary embodiment of a method 400 to operate a compressor device. The method 400 includes, at step 402, receiving a first signal from the first flow sensor encoding information that identifies a first direction of flow for a working fluid upstream of the first diffuser vane. The method also includes, at step 404, receiving a second signal from the second flow sensor encoding information that identifies a second direction of flow for the working fluid upstream of the second diffuser vane. The method further includes, at step 406, comparing the first direction and the second direction to, respectively, a first reference direction and a second reference direction. In one example, the first reference direction and the second reference direction relate to a value for the first direction and the second direction. As shown in FIG. 8, the method 400 also includes, at step 408, identifying a first position for the first diffuser vane and the second diffuser vane aligning the first diffuser vane and the second diffuser vane with, respectively, the first direction and the second direction of the working fluid. In one embodiment, this step can include, at step 410, determining whether the first position and the second position are different from the first reference position and the second reference position. If the first position and/or the second position are different, then the method 400 can include, at step 412, selecting a first increment by which to move the first diffuser vane and/or a second increment by which to move the second diffuser vane. In one example, the first increment defines the relative position of the first direction with respect to the first reference direction and the second increment defining the relative position of the second direction with respect to the second reference direction. The method 400 can also include, at step 414, generating an output encoding instructions to move the first diffuser vane and the second diffuser vane to the first position. In one example, the instructions cause the first diffuser vane and the second diffuser vane to move from the first position to a second position, wherein the second position is defined relative to the first position for the first diffuser vane by the first increment and for the second diffuser vane by the second increment.
In view of the foregoing discussion, one or more of the steps of the methods 200 and 400 can be coded as one or more executable instructions (e.g., hardware, firmware, software, software programs, etc.). These executable instructions can be part of a computer-implemented method and/or program, which can be executed by a processor and/or processing device. Examples of the controller 132 (FIG. 2) can execute these executable instruction to generate certain outputs, e.g., a signal that encodes instructions to change the position of the diffuser vanes as suggested herein.
FIG. 9 depicts a schematic diagram that presents, at a high level, a wiring schematic for a controller 500 that can processing data (e.g., signals) to generate an output that instructs operation of a compressor device (e.g., compressor device 100 of FIGS. 1 and 2). The controller 500 can be incorporated as part of compressor device to provide an integrated, effectively stand alone system. In other alternatives, the controller 500 can remain separate and/or as part of a control system, which can also monitor various operations of the compressor device as well as the systems coupled thereto.
In one embodiment, the controller 500 includes a processor 502, memory 504, and control circuitry 506. Busses 508 couple the components of the controller 500 together to permit the exchange of signals, data, and information from one component of the controller 500 to another. In one example, the control circuitry 506 includes sensor driver circuitry 510 which couples with one or more sensors (e.g., first flow sensor 512 and second flow sensor 514) and motor drive circuitry 516 that couples with a drive unit 518. The control circuitry 506 also includes an actuator drive circuitry 520, which couples with one or more actuators (e.g., first actuator 522 and second actuator 524), and a radio circuitry 526 that couples to a radio 528, e.g., a device that operates in accordance with one or more of the wireless and/or wired protocols for sending and/or receiving electronic messages to and from a peripheral device 530 (e.g., a smartphone). As also shown in FIG. 9, memory 504 can include one or more software programs 532 in the form of software and/or firmware, each of which can comprise one or more executable instructions configured to be executed by the processor 502.
This configuration of components can dictate operation of the controller 500 to analyze data, e.g., information encoded by the signals from sensors 512, 514 and/or drive unit 518, to identify appropriate changes to the diffuser vanes and/or other changes to other operating properties (e.g., motor speed) of the compressor device. For example, the controller 500 can provide signals (or inputs or outputs) to align diffuser vanes in various stages of the compressor device with the direction of flow, independent of the other stages and without disrupting operation (e.g., output pressure) of the compressor device.
The controller 500 and its constructive components can communicate amongst themselves and/or with other circuits (and/or devices), which execute high-level logic functions, algorithms, as well as executable instructions (e.g., firmware instructions, software instructions, software programs, etc.). Exemplary circuits of this type include discrete elements such as resistors, transistors, diodes, switches, and capacitors. Examples of the processor 502 include microprocessors and other logic devices such as field programmable gate arrays (“FPGAs”) and application specific integrated circuits (“ASICs”). Although all of the discrete elements, circuits, and devices function individually in a manner that is generally understood by those artisans that have ordinary skill in the electrical arts, it is their combination and integration into functional electrical groups and circuits that generally provide for the concepts that are disclosed and described herein.
The structure of the components in the controller 500 can permit certain determinations as to selected configuration and desired operating characteristics that an end user convey via the graphical user interface or that are retrieved or need to be retrieved by the device. For example, the electrical circuits of the controller 500 can physically manifest theoretical analysis and logical operations and/or can replicate in physical form an algorithm, a comparative analysis, and/or a decisional logic tree, each of which operates to assign the output and/or a value to the output that correctly reflects one or more of the nature, content, and origin of the changes that occur and that are reflected by the inputs to the controller 500 as provided by the corresponding control circuitry, e.g., in the control circuitry 506.
In one embodiment, the processor 502 is a central processing unit (CPU) such as an ASIC and/or an FPGA that is configured to instruct and/or control operation one or more devices. This processor can also include state machine circuitry or other suitable components capable of controlling operation of the components as described herein. The memory 504 includes volatile and non-volatile memory and can store executable instructions in the form of and/or including software (or firmware) instructions and configuration settings. Each of the control circuitry 506 can embody stand-alone devices such as solid-state devices. Examples of these devices can mount to substrates such as printed-circuit boards and semiconductors, which can accommodate various components including the processor 502, the memory 504, and other related circuitry to facilitate operation of the controller 500.
However, although FIG. 9 shows the processor 502, the memory 504, and the components of the control circuitry 506 as discrete circuitry and combinations of discrete components, this need not be the case. For example, one or more of these components can comprise a single integrated circuit (IC) or other component. As another example, the processor 502 can include internal program memory such as RAM and/or ROM. Similarly, any one or more of functions of these components can be distributed across additional components (e.g., multiple processors or other components).
Moreover, as will be appreciated by one skilled in the art, aspects of the present invention may be embodied as a system, method or computer program product. Accordingly, aspects of the present invention may take the form of an entirely hardware embodiment, an entirely software embodiment (including firmware, resident software, micro-code, etc.) or an embodiment combining software and hardware aspects that may all generally be referred to herein as a “circuit,” “module” or “system.” Furthermore, aspects of the present invention may take the form of a computer program product embodied in one or more computer readable medium(s) having computer readable program code embodied thereon.
Any combination of one or more computer readable medium(s) may be utilized. The computer readable medium may be a computer readable signal medium or a computer readable storage medium. Examples of a computer readable storage medium include an electronic, magnetic, electromagnetic, and/or semiconductor system, apparatus, or device, or any suitable combination of the foregoing. More specific examples (a non-exhaustive list) of the computer readable storage medium would include the following: an electrical connection having one or more wires, a portable computer diskette, a hard disk, a random access memory (RAM), a read-only memory (ROM), an erasable programmable read-only memory (EPROM or Flash memory), an optical fiber, a portable compact disc read-only memory (CD-ROM), an optical storage device, a magnetic storage device, or any suitable combination of the foregoing. In the context of this document, a computer readable storage medium may be any tangible medium that can contain, or store a program for use by or in connection with an instruction execution system, apparatus, or device.
A computer readable signal medium may include a propagated data signal with computer readable program code embodied therein, for example, in baseband or as part of a carrier wave. Such a propagated signal may take any of a variety of forms and any suitable combination thereof. A computer readable signal medium may be any computer readable medium that is not a computer readable storage medium and that can communicate, propagate, or transport a program for use by or in connection with an instruction execution system, apparatus, or device.
Program code embodied on a computer readable medium may be transmitted using any appropriate medium, including but not limited to wireless, wireline, optical fiber cable, RF, etc., or any suitable combination of the foregoing.
Computer program code for carrying out operations for aspects of the present invention may be written in any combination of one or more programming languages, including an object oriented programming language and conventional procedural programming languages. The program code may execute entirely on the user's computer, partly on the user's computer, as a stand-alone software package, partly on the user's computer and partly on a remote computer or entirely on the remote computer or server. In the latter scenario, the remote computer may be connected to the user's computer through any type of network, including a local area network (LAN) or a wide area network (WAN), or the connection may be made to an external computer (for example, through the Internet using an Internet Service Provider).
Aspects of the present invention are described herein with reference to flowchart illustrations and/or block diagrams of methods, apparatus (systems) and computer program products according to embodiments of the invention. It will be understood that each block of the flowchart illustrations and/or block diagrams, and combinations of blocks in the flowchart illustrations and/or block diagrams, can be implemented by computer program instructions. These computer program instructions may be provided to a processor of a general purpose computer, special purpose computer, or other programmable data processing apparatus to produce a machine, such that the instructions, which execute via the processor of the computer or other programmable data processing apparatus, create means for implementing the functions/acts specified in the flowchart and/or block diagram block or blocks.
These computer program instructions may also be stored in a computer readable medium that can direct a computer, other programmable data processing apparatus, or other devices to function in a particular manner, such that the instructions stored in the computer readable medium produce an article of manufacture including instructions which implement the function/act specified in the flowchart and/or block diagram block or blocks.
The computer program instructions may also be loaded onto a computer, other programmable data processing apparatus, or other devices to cause a series of operational steps to be performed on the computer, other programmable apparatus or other devices to produce a computer implemented process such that the instructions which execute on the computer or other programmable apparatus provide processes for implementing the functions/acts specified in the flowchart and/or block diagram block or blocks.
Accordingly, a technical effect of embodiments of the systems and methods disclosed herein is to change the position of one or more diffuser vanes to align with the direction of flow of the working fluid.
As used herein, an element or function recited in the singular and proceeded with the word “a” or “an” should be understood as not excluding plural said elements or functions, unless such exclusion is explicitly recited. Furthermore, references to “one embodiment” of the claimed invention should not be interpreted as excluding the existence of additional embodiments that also incorporate the recited features.
This written description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention 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 if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal language of the claims.

Claims

What is claimed is:

1. A system, comprising:

a compressor device comprising a first diffuser vane, a second diffuser vane downstream of the first diffuser vane, and a flow sensor assembly comprising a first flow sensor upstream of the first diffuser vane and a second flow sensor upstream of the second diffuser vane; and

a controller coupled with the first flow sensor and the second flow sensor, the controller comprising a processor, memory, and one or more executable instructions stored on the memory and configured to be executed by the processor, the executable instructions comprising instructions for:

receiving a first signal from the first flow sensor encoding information that identifies a first direction of flow for a working fluid upstream of the first diffuser vane;

receiving a second signal from the second flow sensor encoding information that identifies a second direction of flow for the working fluid upstream of the second diffuser vane;

identifying a first position for the first diffuser vane and the second diffuser vane, the first position aligning the first diffuser vane and the second diffuser vane with, respectively, the first direction and the second direction of the working fluid; and

generating an output encoding instructions to move the first diffuser vane and the second diffuser vane to the first position.

2. The system of claim 1, wherein the compressor device comprises a first actuator coupled with the first diffuser vane and a second actuator coupled with the second diffuser vane, and wherein the first actuator and the second actuator operate in response to the output.

3. The system of claim 1, wherein the first flow sensor and the second flow sensor comprise a directional element and a base element coupled to the directional element, and wherein the information of the first signal and the second signal reflects an angular position of the directional element.

4. The system of claim 3, wherein the base element comprises a rotary potentiometer that measures the angular position of the directional element.

5. The system of claim 1, wherein the compressor device comprises a first impeller upstream of the first diffuser vane and a second impeller downstream of the first diffuser vane and upstream of the second diffuser vane.

6. The system of claim 1, wherein the first diffuser vane and the second diffuser vane rotate in response to the output.

7. The system of claim 1, wherein the first diffuser vane and the second diffuser vane have an airfoil shape that converges at the leading edge to a tip with a center axis, wherein the tip has a curvilinear outer surface defined by a radius from the center axis, and wherein the first diffuser vane and the second diffuser vane rotate about a rotation axis that is found within an area defined by the radius.

8. The system of claim 7, wherein the rotation axis is coaxial with the center axis of the tip.

9. The system of claim 1, wherein the executable instructions comprise instructions for:

comparing the first direction and the second direction to, respectively, a first reference direction and a second reference direction; and

selecting a first increment by which to move the first diffuser vane and a second increment by which to move the second diffuser vane, the first increment defining the relative position of the first direction with respect to the first reference direction and the second increment defining the relative position of the second direction with respect to the second reference direction,

wherein the instructions cause the first diffuser vane and the second diffuser vane to move from the first position to a second position, and wherein the second position is defined relative to the first position for the first diffuser vane by the first increment and for the second diffuser vane by the second increment.

10. A compressor device, comprising:

a first diffuser vane;

a second diffuser vane downstream of the first diffuser vane;

a flow sensor assembly comprising a first flow sensor upstream of the first diffuser vane and a second flow sensor downstream of the first diffuser vane and upstream of the second diffuser vane, the first flow sensor and the second flow sensor comprising a base element and a directional element coupled with the base element, wherein the directional element can move between a first position and a second position to align with a flow of a working fluid.

11. The compressor device of claim 10, wherein the base element provides a pivot about which the directional element can rotate between the first position and the second position.

12. The compressor device of claim 10, wherein the base element comprises a rotary potentiometer.

13. The compressor device of claim 10, wherein the first diffuser vane and the second diffuser vane comprise a vane body with a leading edge and a trailing edge and a rotation axis spaced apart from the leading edge and the trailing edge along a chord length that defines the straight-line distance between the leading edge and the trailing edge

14. The compressor device of claim 10, wherein the first diffuser vane and the second diffuser vane rotate about the leading edge.

15. The compressor device of claim 10, wherein the vane body has an airfoil shape that converges at the leading edge to a tip with a center axis, wherein the tip has a curvilinear outer surface defined by a radius from the center axis, and wherein the first diffuser vane and the second diffuser vane rotate about a rotation axis that is found within an area defined by the radius.

16. The compressor device of claim 16, wherein the rotation axis is coaxial with the center axis of the tip.

17. The compressor device of claim 10, further comprising a controller coupled with the first flow sensor and the second flow sensor, the controller comprising a processor, memory, and one or more executable instructions stored on the memory and configured to be executed by the processor, the executable instructions comprising instructions for:

18. The compressor device of claim 17, wherein the executable instructions comprise instructions for:

19. A controller for operating a compressor device, said controller comprising:

a processor;

memory; and

executable instructions stored on the memory and configured to be executed by the processor, the executable instructions comprising instructions for:

20. The controller of claim 19, further comprising instructions for:

comparing the first direction and the second direction to, respectively, a first reference direction and a second reference direction, wherein the first reference direction and the second reference direction comprise a value for the first direction and the second direction at a time t, and wherein the first position; and