1. A computer-implemented method, comprising:
accessing historical operating data for a unit of information technology equipment, wherein the historical operating data includes power consumption, fan speed, inlet air temperature, workload, and any processor throttling events, the historical operating data being acquired continuously or periodically during a period of time in which the unit of information technology equipment was operating or in response to an event of the unit of information technology equipment occurring in the period of time;
receiving user input selecting a fan speed ranging from a minimum fan speed to a maximum fan speed;
using the historical operating data to determine a performance impact that is expected from operating the unit at the selected fan speed, where the power consumption is a proxy for performance; and
displaying the estimated performance impact of the selected fan speed and one or more alternative fan speeds.
2. The method of claim 1, further comprising:
determining a correlation between power consumption and performance of the unit using the historical operating data; and
displaying a performance that is correlated with the power consumption.
3. The method of claim 1, further comprising:
determining a correlation between fan speed and sound levels using the historical operating data; and
displaying sound levels that are correlated with the displayed fan speeds.
4. The method of claim 1, further comprising:
determining that first and second units of information technology equipment have similar hardware and workload; and
using historical operating data associated with the first device to estimate a performance impact of implementing a selected fan speed on the second device.
5. The method of claim 1, further comprising:
displaying the performance impact as a graphical bar divided into performance zones, wherein the performances zones are aligned with the associated fan speeds.
6. The method of claim 5, wherein the performance zones include at least a first performance zone illustrating the range of fan speeds that historically do not impact performance, a second performance zone illustrating the range of fan speeds that historically impact performance yet are above the historical average of fan speed, and a third performance zone illustrating a range of fan speeds that have historically prevented one or more jobs from being completed.
7. The method of claim 5, further comprising:
displaying a second graphical bar divided into performance zones that are aligned vertically with the selector states associated with the performance zone, wherein the performance zones in the second graphical bar are determined from the historical data associated with a highest measured inlet air temperature.
8. The method of claim 1, wherein the unit of information technology equipment includes a computer server.
9. The method of claim 1, wherein the unit of information technology equipment is an application specific integrated circuit (ASIC) and the fan is dedicated to the ASIC, wherein an ASIC operating condition is used as a proxy for the speed of the fan, and wherein the ASIC operating condition is selected from the power consumption, temperature and performance of the ASIC.
10. The method of claim 9, further comprising:
determining a correlation between the fan speed and an ASIC operating condition using the historical operating data; and
displaying fan speeds that are correlated with the ASIC operating conditions.
11. The method of claim 1, further comprising:
displaying a historical median of the actual fan speed of the system; and
displaying a warning in response to detecting that the user has selected a selector state that will impose a fan speed that is less than the median fan speed.
12. The method of claim 1, further comprising:
displaying a second graphical bar divided into performance zones that are aligned vertically with the selector states associated with the performance zone, wherein the performance zones in the second graphical bar are determined from the historical data associated with a highest inlet air temperature range that is supported.
13. The method of claim 1, further comprising:
determining one or more measure of variability in the inlet air temperature based upon the historical data; and
displaying the one or more measure of variability in the inlet air temperature.
14. The method of claim 13, wherein the one or more measure of variability in the inlet air temperature includes an inlet air temperature range and a median inlet air temperature.
15. The method of claim 1, wherein the step of receiving user input selecting a fan speed ranging from a minimum fan speed to a maximum fan speed, includes:
receiving user input selecting one of a plurality of fan speed selector states ranging from a minimum fan speed to a maximum fan speed.
16. The method of claim 15, wherein the plurality of fan speed selector states are normalized values representing a plurality of fan speeds ranging from the minimum fan speed to the maximum fan speed.
17. The method of claim 15, further comprising:
receiving user input selecting a number of fan speed selector states; and
establishing the selected number of fan speed selector states distributed across the full range of fan speeds from a minimum fan speed to a maximum fan speed, wherein each of the fan speed selector states is associated with a different fan speed.
18. The method of claim 15, further comprising:
displaying the performance impact as a graphical bar divided into performance zones, wherein the performances zones are aligned with the fan speed selector states associated with the performance zone.
19. The method of claim 18, where in the performance zones include at least a first performance zone illustrating the range of fan speed selector states that historically do not impact performance, a second performance zone illustrating the range of fan speed selector states that historically impact performance yet are above the historical average of fan speed, and a third performance zone illustrating a range of fan speed selector states that have historically prevented one or more jobs from being completed.
20. The method of claim 15, further comprising:
determining a relationship between inlet air temperature and cooling capacity of the fans;
estimating a loss in performance that is likely to occur at the selected fan speed selector state if the inlet air temperature reaches the highest inlet air temperature in the historical operating data or the highest inlet air temperature supported by the unit.
21. The method of claim 20, further comprising:
displaying the cooling capacity as a function of inlet air temperature for each of the fan speed selector states.
22. The method of claim 21, wherein the cooling capacity as a function of inlet air temperature for each of the fan speed selector states is displayed as a table.
23. A computer program product including computer usable program code embodied on a non-transitory computer readable storage medium, the computer program product comprising:
computer usable program code for accessing historical operating data for a unit of information technology equipment, wherein the historical operating data includes power consumption, fan speed, inlet air temperature, workload, and any processor throttling events, the historical operating data being acquired continuously or periodically during a period of time in which the unit of information technology equipment was operating or in response to an event of the unit of information technology equipment occurring in the period of time;
computer usable program code for receiving user input selecting a fan speed ranging from a minimum fan speed to a maximum fan speed;
computer usable program code for using the historical operating data to determine a performance impact that is expected from operating the unit at the selected fan speed, where the power consumption is a proxy for performance; and
computer usable program code for displaying the estimated performance impact of the selected fan speed and one or more alternative fan speeds.
24. The computer program product of claim 23, further comprising:
computer usable program code for displaying the performance impact as a graphical bar divided into performance zones, wherein the performances zones are aligned with the associated fan speeds.
25. The computer program product of claim 24, where in the performance zones include at least a first performance zone illustrating the range of fan speeds that historically do not impact performance, a second performance zone illustrating the range of fan speeds that historically impact performance yet are above the historical average of fan speed, and a third performance zone illustrating a range of fan speeds that have historically prevented one or more jobs from being completed.
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 lithographic mask, comprising:
a first energy emitting layer, including:
a first active region configured to emit a first energy flux at a first selected intensity in response to an energy input; and
a second energy emitting layer, including:
a second active region configured to emit a second energy flux at a second selected intensity in response to the first energy flux; and
a first inactive region configured not to emit an energy flux at the second selected intensity in response to the first energy flux.
2. The mask of claim 1, wherein the first energy flux is electromagnetic radiation.
3. The mask of claim 2, wherein the first energy flux has a first selected frequency, and the second energy flux is electromagnetic radiation having a second selected frequency.
4. (canceled)
5. The mask of claim 1, wherein the first energy flux is charged particles.
6. (canceled)
7. The mask of claim 1, wherein the second energy flux is charged particles.
8. (canceled)
9. The mask of claim 1, wherein the first energy flux is an evanescent wave.
10. The mask of claim 1, wherein the first energy flux is an electromagnetic field.
11.-14. (canceled)
15. The mask of claim 1, wherein the second energy flux is an electromagnetic field.
16.-19. (canceled)
20. The mask of claim 1, wherein the first energy emitting layer is photoemissive.
21. The mask of claim 1, wherein the second energy emitting layer is photoemissive.
22. The mask of claim 1, wherein the first energy emitting layer is luminescent.
23. The mask of claim 1, wherein the second energy emitting layer is luminescent.
24. The mask of claim 1, wherein the first energy emitting layer includes an active gain material.
25. The mask of claim 1, wherein the second energy emitting layer includes an active gain material.
26. The mask of claim 25, wherein the second energy emitting layer is configured to function as an optical cavity.
27. The mask of claim 1, wherein the second energy emitting layer includes a nonlinear optical material.
28.-29. (canceled)
30. The mask of claim 1, wherein the first energy emitting layer includes a quantum dot.
31. The mask of claim 1, wherein the second energy emitting layer includes a quantum dot.
32. The mask of claim 1, wherein the first energy emitting layer includes a fluorescent material.
33. The mask of claim 1, wherein the second energy emitting layer includes a fluorescent material.
34. The mask of claim 1, wherein the second energy emitting layer includes a scintillation material.
35. The mask of claim 1, wherein the second energy emitting layer includes a photocathode.
36. The mask of claim 1, wherein the second energy emitting layer includes a field emission material.
37. The mask of claim 1, wherein the first energy emitting layer includes a waveguide.
38. The mask of claim 1, wherein the second energy emitting layer includes a waveguide.
39. The mask of claim 1, wherein the first energy emitting layer includes a region supporting plasmon propagation.
40. The mask of claim 1, wherein the second energy emitting layer includes a region supporting plasmon propagation.
41. The mask of claim 1, wherein the energy input is an electrical input.
42. The mask of claim 1, wherein the energy input is an optical input.
43. The mask of claim 1, wherein the first energy emitting layer includes a second inactive region configured not to emit an energy flux at the first selected intensity in response to the energy input.
44.-90. (canceled)
91. A lithographic apparatus, comprising:
a patterned energy emitting mask, the mask including at least one active region that emits an energy flux and at least one inactive region that does not emit an energy flux; and
a substrate support arranged to hold a substrate in a position to receive the energy flux,
wherein the patterned energy emitting mask includes at least two layers, at least one of the at least two layers being an energy emitting layer.
92. The apparatus of claim 91, wherein the at least two layers include two energy emitting layers.
93. The apparatus of claim 92, wherein the at least two layers include a patterned energy emitting layer and a homogeneous energy emitting layer.
94. The apparatus of claim 92, wherein the at least two layers include two patterned energy emitting layers.
95. The apparatus of claim 91, wherein the at least two layers include an energy emitting layer and a patterned transmissivity layer.
96.-116. (canceled)
117. A lithographic method, comprising:
generating an energy flux by activating a patterned energy emitting mask, wherein the mask includes at least one active region that emits an energy flux and at least one inactive region that does not emit an energy flux and wherein the mask includes at least two layers, at least one of the at least two layers being an energy emitting layer; and
exposing a flux sensitive material to the generated energy flux at a level selected to modify the flux sensitive material.
118. The lithographic method of claim 117, wherein the at least two layers include two energy emitting layers.
119. The lithographic method of claim 118, wherein the at least two layers include a patterned energy emitting layer and a homogeneous energy emitting layer.
120. The lithographic method of claim 118, wherein the at least two layers include two patterned energy emitting layers.
121. The lithographic method of claim 117, wherein the at least two layers include an energy emitting layer and a patterned transmissivity layer.
122.-144. (canceled)
145. A lithographic mask, comprising:
a patterned energy emitting layer, the layer including:
at least one active region configured to emit an energy flux at a selected level in response to an energy input; and
at least one inactive region configured not to emit an energy flux at the selected level in response to the energy input,
wherein the active region includes a structure selected from the group consisting of an active gain material, a nonlinear optical material, a waveguide, a quantum dot, and a plasmon-supporting region.
146.-150. (canceled)
151. A lithographic mask, comprising:
a patterned energy emitting layer, the layer including:
a first active region configured to emit a first energy flux at a first selected level in response to an energy input; and
a second active region configured to emit a second energy flux at a second selected level in response to the energy input,
wherein the first and second energy fluxes differ in frequency or intensity.
152. The lithographic mask of claim 151, wherein the first and second energy fluxes differ in frequency.
153. The lithographic mask of claim 151, wherein the first and second energy fluxes differ in intensity.