1. A system for visualizing multi-color industrial displays, comprising:
a memory comprising computer-executable components; and
a processor, coupled to the memory, that facilitates execution of the computer-executable components, the computer-executable components comprising:
a display generation component configured to initiate generation of a first heat map display representing first information relating to a device associated with an industrial automation system and a second heat map display representing second information relating to a component of the device, wherein at least one of the first heat map display or the second heat map display is configured to render prognostic information identifying a potential failure occurrence of the device; and
a visualization component configured to modify the first heat map display in response to a first determination that a first subset of data received from the industrial automation system indicates a first change in a first operational state of the device, and modify the second heat map display in response to a second determination that a second subset of the data indicates a second change in a second operational state of the component.
2. The system of claim 1, wherein the prognostic information further identifies a recommended operator action for addressing the potential failure occurrence.
3. The system of claim 1, wherein the display generation component is further configured to at least partially overlay a graphical representation of the device over the second heat map display.
4. The system of claim 1, wherein the display generation component is further configured to initiate a transition between a first presentation of the second heat map display that renders overview information relating to an operational state of the component and a second presentation of the second heat map that renders additional information relating to the operational state of the component.
5. The system of claim 4, wherein the display generation component is further configured to initiate the transition in response to a determination that a second subset of the data indicates the potential failure occurrence of the device.
6. The system of claim 1, wherein the display generation component is further configured to generate at least one of the first heat map display or the second heat map display based on at least one of source address information, filter information, classifier information, preference information, profile information, design layout information, or rule information.
7. The system of claim 1, wherein the display generation component is further configured to generate at least one of the first heat map display or the second heat map display based at least in part on historical data collected from the industrial automation system.
8. The system of claim 1, wherein the visualization component is further configured to animate at least one of the first heat map display or the second heat map display based on real-time or near real-time data collected from the industrial automation system.
9. The system of claim 1, wherein at least one of the first heat map display or the second heat map display is further configured to render maintenance information identifying a recommended maintenance activity to be performed on the device.
10. An operator interface product, comprising:
a display component; and
a processor, coupled to a memory, that facilitates execution of computer-executable components stored on the memory to perform operations, comprising:
displaying, on a first heat map display, first data relating to a device of an industrial process;
displaying, on a second heat map display, second data relating to a component of the device;
displaying, on at least one of the first heat map display or the second heat map display, prognostic data indicating a potential failure of the device;
altering the first heat map display based on a first determination that the first data indicates a first change in a first operational state of the device; and
altering the second heat map display based on a second determination that the second data indicates a second change in a second operational state of the component.
11. The operator interface product of claim 10, the wherein the operations further comprise displaying at least a portion of a graphical representation of the device as an overlay over the second heat map display.
12. The operator interface product of claim 10, wherein the operations further comprise transitioning between a first presentation of the second heat map display that renders overview information relating to the operational state of the component and a second presentation of the second heat map that renders other information relating to the operational state of the component.
13. The operator interface product of claim 12, wherein the transitioning comprises transitioning between the first presentation and the second presentation in response to determining that at least one of the first data or the second data indicates the potential failure of the device.
14. The operator interface product of claim 10, wherein the operations further comprise configuring a presentation of at least one of the first heat map display or the second heat map display based on at least one of source address information, filter information, classifier information, preference information, profile information, design layout information, rule information, or historical data.
15. The operator interface product of claim 10, wherein the operations further comprise configuring a presentation of at least one of the first heat map display or the second heat map display based at least in part on historical data collected for the industrial process.
16. The operator interface product of claim 15, wherein the operations further comprise displaying real-time or near real-time data collected from the industrial process simultaneously with at least a subset of the historical data on the at least one of the first heat map display or the second heat map display.
17. The operator interface product of claim 15, further comprising modifying the second heat map display based at least in part on a deviation of real-time or near real-time data collected from the industrial process from a corresponding subset of the historical data.
18. A method, comprising:
generating, by a system comprising a processor, a first graphical heat map configured to render first data relating to a device associated with an industrial automation system;
generating a second graphical heat map configured to render second data relating to a component of the device;
rendering, on at least one of the first graphical heat map or the second graphical heat map, prognostic information indicating a potential failure of the device;
in response to determining that the first data is indicative of a first change in a first operational state of the device, modifying the first graphical heat map; and
in response to determining that the second data is indicative of a second change to a second operational state of the component, modifying the second graphical heat map.
19. The method of claim 18, further comprising overlaying at least a portion of a representation of the device over the second graphical heat map.
20. The method of claim 18, further comprising overlaying at least a portion of a graphical representation of the device on the second heat map display.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. A rotor disk assembly for a gas turbine engine comprising:
a rotor disk defined about an axis of rotation, said rotor disk having a circumferentially intermittent slot structure that extends radially outward relative to said axis of rotation;
a component defined about said axis of rotation, said component having a multiple of radial tabs which extend radially inward relative to said axis of rotation, said multiple of radial tabs engageable with said circumferentially intermittent slot structure; and
a lock assembly engaged with at least one opening formed by said circumferentially intermittent slot structure to provide an anti-rotation interface for said component, said lock assembly comprising a retaining wire that defines a polygon shape.
2. The rotor disk assembly as recited in claim 1, wherein said component is a heat shield.
3. The rotor disk assembly as recited in claim 2, wherein said heat shield separates a relatively hotter outer diameter cavity from a relatively cooler inner diameter cavity.
4. The rotor disk assembly as recited in claim 3, wherein said heat shield spans an interface.
5. The rotor disk assembly as recited in claim 4, wherein said interface is a splined interface between a high pressure turbine and a high pressure compressor.
6. The rotor disk assembly as recited in claim 1, wherein said circumferentially intermittent slot structure extends radially outward from a cylindrical extension from said rotor disk.
7. The rotor disk assembly as recited in claim 1, wherein the rotor disk is a turbine rotor disk.
8. The rotor disk assembly as recited in claim 1, wherein said polygon shape is a substantially hexagonal shape.
9. The rotor disk assembly as recited in claim 1, wherein said retaining wire includes a plurality of linear segments, one of which includes a gap.
10. The rotor disk assembly as recited in claim 9, wherein said retaining wire includes rounded portions between said linear segments.
11. The rotor disk assembly as recited in claim 10, wherein at least one of said rounded portions is captured between said circumferentially intermittent slot structure.
12. The rotor disk assembly as recited in claim 1, wherein said lock assembly comprises a lock body that has an undercut slot, said retaining wire is received within said undercut slot.
13. The rotor disk assembly as recited in claim 1, wherein said lock assembly includes a lock tab, said lock tab protrudes substantially perpendicularly from a lock body of said lock assembly and abuts at least one of said radial tabs.
14. A method to assemble a rotor disk assembly comprising:
locating a cover plate adjacent to a rotor disk along an axis of rotation;
axially locating a heat shield having a multiple of radial tabs which extend radially inward relative to the axis of rotation, the multiple of radial tabs axially aligned with openings defined by a circumferentially intermittent slot structure on the rotor disk;
rotating the heat shield to radially align the multiple of radial tabs with the circumferentially intermittent slot structure to axially retain the cover plate to the rotor disk; and
engaging a lock assembly that has a retaining wire that defines a polygon shape with the circumferentially intermittent slot structure to provide an anti-rotation interface for the heat shield.
15. A method as recited in claim 14, further comprising:
resiliently compressing the retaining wire of the lock assembly and inserting the compressed retaining wire into the circumferentially intermittent slot structure.
16. A method as recited in claim 14, further comprising:
spanning an interface with the heat shield.
17. A method as recited in claim 14, further comprising:
spanning a splined interface between a high pressure turbine and a high pressure compressor.
18. A rotor disk assembly for a gas turbine engine comprising:
a rotor disk defined about an axis of rotation, said rotor disk having a circumferentially intermittent slot structure that extends radially outward relative to said axis of rotation;
a component defined about said axis of rotation, said component having a multiple of radial tabs which extend radially inward relative to said axis of rotation, said multiple of radial tabs engageable with said circumferentially intermittent slot structure; and
a lock assembly comprising a resilient retaining wire that can be compressed such that said compressed resilient retaining wire can engage with at least one opening formed by said circumferentially intermittent slot structure to provide an anti-rotation interface for said component, said resilient retaining wire defining a polygon shape.