Determining top-dead-center (tdc) of reciprocating compressor
Abstract
Various embodiments include approaches for determining a top-dead-center (TDC) of a reciprocating compressor. In some cases, an apparatus includes: a pressure transducer configured to measure pressure fluctuations inside a compressor cylinder and convert the pressure fluctuations into an asynchronous waveform; and at least one computing device operably connected with the pressure transducer, the at least one computing device configured to: extract a data set representing piston angles over a single revolution of a piston within the compressor cylinder from the asynchronous waveform; remove data representing invalid piston angles from the data set to form a refined data set; determine an average piston angle for the single revolution from the refined data set; and adjust the refined data set to identify a top-dead-center (TDC) position of the piston within the compressor cylinder.
Claims
exact text as granted — not AI-modifiedI claim:
1 . An apparatus comprising:
a pressure transducer configured to measure pressure fluctuations inside a compressor cylinder and convert the pressure fluctuations into an asynchronous waveform; and at least one computing device operably connected with the pressure transducer, the at least one computing device configured to:
extract a data set representing piston angles over a single revolution of a piston within the compressor cylinder from the asynchronous waveform;
remove data representing invalid piston angles from the data set to form a refined data set;
determine an average piston angle for the single revolution from the refined data set; and
adjust the refined data set to identify a top-dead-center (TDC) position of the piston within the compressor cylinder.
2 . The apparatus of claim 1 , wherein the at least one computing device is configured to remove the data representing invalid piston angles from the data set by identifying and excluding piston angles based upon a compression ratio of the single revolution of the piston within the compressor cylinder.
3 . The apparatus of claim 1 , wherein the at least one computing device is configured to remove the data representing invalid piston angles from the data set by identifying and excluding piston angles based upon a volumetric efficiency of the single revolution of the piston within the compressor cylinder.
4 . The apparatus of claim 1 , wherein the at least one computing device is configured to remove the data representing invalid piston angles from the data set by identifying and excluding piston angles based upon a clearance volume of the single revolution of the piston within the compressor cylinder.
5 . The apparatus of claim 1 , wherein the at least one computing device is configured to adjust the refined data set to position a data value corresponding to the TDC position of the piston within the compressor as a first data value in the refined data set.
6 . The apparatus of claim 1 , wherein the asynchronous waveform includes a series of uniformly spaced time domain data points.
7 . The apparatus of claim 1 , wherein the at least one computing device is configured to extract the data set representing the piston angles over the single revolution using a threshold-hysteresis model.
8 . A system comprising:
at least one computing device configured to identify a top-dead-center (TDC) position of a piston within a compressor cylinder by performing actions including:
obtaining an asynchronous waveform indicating pressure fluctuations inside a compressor cylinder;
extracting a data set representing piston angles over a single revolution of the piston within the compressor cylinder from the asynchronous waveform;
removing data representing invalid piston angles from the data set to form a refined data set;
determining an average piston angle for the single revolution from the refined data set; and
adjusting the refined data set to identify the TDC position of the piston within the compressor cylinder.
9 . The system of claim 8 , wherein the at least one computing device is configured to remove the data representing invalid piston angles from the data set by identifying and excluding piston angles based upon a compression ratio of the single revolution of the piston within the compressor cylinder.
10 . The system of claim 8 , wherein the at least one computing device is configured to remove the data representing invalid piston angles from the data set by identifying and excluding piston angles based upon a volumetric efficiency of the single revolution of the piston within the compressor cylinder.
11 . The system of claim 8 , wherein the at least one computing device is configured to remove the data representing invalid piston angles from the data set by identifying and excluding piston angles based upon a clearance volume of the single revolution of the piston within the compressor cylinder.
12 . The system of claim 8 , wherein the at least one computing device is configured to adjust the refined data set to position a data value corresponding to the TDC position of the piston within the compressor as a first data value in the refined data set.
13 . The system of claim 8 , wherein the asynchronous waveform includes a series of uniformly spaced time domain data points.
14 . The system of claim 8 , wherein the at least one computing device is configured to extract the data set representing the piston angles over the single revolution using a threshold-hysteresis model.
15 . A computer program product comprising program code, which when executed on at least one at least one computing device, causes the at least one computing device to identify a top-dead-center (TDC) position of a piston within a compressor cylinder by performing actions including:
obtaining an asynchronous waveform indicating pressure fluctuations inside the compressor cylinder; extracting a data set representing piston angles over a single revolution of a piston within the compressor cylinder from the asynchronous waveform; removing data representing invalid piston angles from the data set to form a refined data set; determining an average piston angle for the single revolution from the refined data set; and adjusting the refined data set to identify the top-dead-center (TDC) position of the piston within the compressor cylinder.
16 . The computer program product of claim 15 , wherein the removing of the data representing invalid piston angles from the data set includes identifying and excluding piston angles based upon a compression ratio of the single revolution of the piston within the compressor cylinder.
17 . The computer program product of claim 15 , wherein the removing of the data representing invalid piston angles from the data set includes identifying and excluding piston angles based upon a volumetric efficiency of the single revolution of the piston within the compressor cylinder.
18 . The computer program product of claim 15 , wherein the removing of the data representing invalid piston angles from the data set includes identifying and excluding piston angles based upon a clearance volume of the single revolution of the piston within the compressor cylinder.
19 . The computer program product of claim 15 , further comprising:
adjusting the refined data set to position a data value corresponding to the TDC position of the piston within the compressor as a first data value in the refined data set.
20 . The computer program product of claim 15 , wherein the asynchronous waveform includes a series of uniformly spaced data points, and wherein the extracting of the data set representing the piston angles over the single revolution includes using a threshold-hysteresis model.Join the waitlist — get patent alerts
Track US2014205471A1 — get alerts on status changes and closely related new filings.
We store only your email — no account needed. See our privacy policy.