The present invention is directed to an engine exhaust flow meter and method of measuring engine exhaust flow rate and, in particular, to such measuring engine exhaust flow in the presence of significant pressure pulsation.
The use of portable emissions testing systems (PEMS) requires direct exhaust flow measurements. These measurements are complicated by the presence of pressure pulsations which are inherent in piston engines. Small displacement gasoline engines with four (or fewer) cylinders in particular can produce pulsations with very large amplitudes that bias readings high.
Magnitude of the pressure pulses in a four cylinder engine may be up to 600% higher than the mean pressure. Also negative pressure spikes are present, which indicate reverse flowrate. Conventional flow measurement standards specify that these pressure pulses should not exceed 10% of the mean pressure value.
The measurement of pulsating flows has been a long standing challenge. One issue is the Inertia effect. It takes more energy (pressure) to reverse the flow due to its inertia than to produce steady flow. The result is an over-estimate by prior techniques of flow due to the higher differential pressures measured. Another issue with prior techniques is that reverse flow is local transitions from turbulent to laminar flows, which create a non-uniform velocity profile.
Flow measurement techniques according to aspects of the invention apply a compensation algorithm based on measurements of the amplitude of differential pressure pulsations to correct the square root average of the differential pressure and calculated flow rate from the effect of pulsations. The differential pressure signals are measured at high speed, such as 2.5 KHz or greater, and the mean pulse magnitude is determined over a time interval, for example 200 msec, and compared to the mean differential pressure value for that time interval. The pulsation modulation is defined as the ratio of the mean pulse magnitude to the mean differential pressure. In addition, an average of the square root of the differential pressures is calculated over the same time interval. The compensation algorithm adjusts the square root average of the differential pressure and calculated flow rate as a function of the pulsation modulation and pipe Reynolds number.
An engine exhaust flow meter and method of measuring engine exhaust flow rate, according to an aspect of the invention, includes a flow tube and differential pressure meter that is adapted to measure differential pressure in exhaust flow through the flow tube. A computer samples the differential pressure meter at a rate that is greater than the pulsation of exhaust flow to obtain a differential pressure signal. The computer is responsive to the differential pressure signal to compute a mean differential pressure value over a certain time interval. The computer is responsive to the differential pressure signal to compute a mean magnitude of pressure pulses over the same time interval. The computer is responsive to the differential pressure signal to compute an average of the square root of the differential pressures over the same time interval. The computer determines a compensation factor as a function of the mean magnitude of pressure pulses and adjusts the square root average of the differential pressure value as a function of the compensation factor to obtain an engine exhaust flow value that is flow pulsation compensated.
A pulsation dampener may be provided that is adapted to mechanically reduce magnitude of flow pulsation in the flow tube. The pulsation dampener may include a flexible bag such as a bag made of silicone. A shield may surround the bag and may be attached to the flow tube at one end portion of the shield and support the bag at an opposite end portion of the shield.
In an embodiment of the present invention, the differential pressure meter includes a pitot tube in the flow tube and a differential pressure sensor sensing pressure across said pitot tube and producing a differential pressure signal that is responsive to forward and reverse flow in the flow tube. The differential pressure sensor may include a plurality of differential pressure sensors connected in parallel. The computer may calculate the mean differential pressure signal over an interval of time and a square root average of the differential pressure signal over an interval of time. The computer may calculate the mean peak to peak amplitude of the differential pressure pulses over an interval of time. The computer may be adapted to compute a pulsation correction factor and a Reynolds number of the flow tube, the pulsation correction factor being a function of the mean peak to peak amplitude of differential pressure pulses divided by mean differential pressure. The computer may be adapted to adjust the square root average of the differential pressure and calculated flowrate by the compensation factor and re-compute the Reynolds number and the compensation factor in an iterative process.
These and other objects, advantages and features of this invention will become apparent upon review of the following specification in conjunction with the drawings.
Referring now to the drawings and the illustrative embodiments depicted therein, an engine exhaust flow meter 20 includes a flow tube 22 that is adapted to be connected with the exhaust of an internal combustion engine and a differential pressure meter 24 that is adapted to measure differential pressure in exhaust flow through the flow tube (
A sensing assembly 36 is mounted to flow tube 22 and includes a pressure sensor and electronic assembly 37 having a heated manifold housing 38 for sensing assembly 36 and a computer assembly 40 having a computer such as a microprocessor (
As illustrated in the flow chart of
The computer 40 is adapted to calculate a mean magnitude of pressure from a square root average of the differential pressure signal. The computer 40 calculates the mean magnitude of pressure from the square root average of the differential pressure signal over an interval of time, such as 200 ms for example 106. The computer 40 is adapted to compute the compensation factor from a pulsation correction factor and a Reynold number of the flow tube. The Reynolds number is calculated over the same interval used for obtaining mean magnitude of the pressure using conventional calculation techniques. The pulsation correction factor is a function of mean peak to peak amplitude of pressure pulses divided by the mean magnitude of pressure. The computer 40 is adapted to adjust the mean magnitude of pressure by the compensation factor and re-computes the Reynolds number 120 and the compensation factor in an iterative process 122.
As an example, pulsation correction factor=f (pulsation modulation, Reynolds number) where:
In one embodiment, as illustrated in
While the foregoing description describes several embodiments of the present invention, it will be understood by those skilled in the art that variations and modifications to these embodiments may be made without departing from the spirit and scope of the invention, as defined in the claims below. The present invention encompasses all combinations of various embodiments or aspects of the invention described herein. It is understood that any and all embodiments of the present invention may be taken in conjunction with any other embodiment to describe additional embodiments of the present invention. Furthermore, any elements of an embodiment may be combined with any and all other elements of any of the embodiments to describe additional embodiments.
The present application claims the filing benefits of U.S. provisional application, Ser. No. 62/640,760, filed Mar. 9, 2018, which is hereby incorporated herein by reference in its entirety.
Number | Name | Date | Kind |
---|---|---|---|
4183338 | Lindberg | Jan 1980 | A |
4527953 | Baker | Jul 1985 | A |
6148656 | Breton | Nov 2000 | A |
6725731 | Wiklund et al. | Apr 2004 | B2 |
6865472 | Nakamura | Jun 2005 | B2 |
7110878 | Nakamura et al. | Sep 2006 | B2 |
8280645 | Nakamura | Oct 2012 | B2 |
9617933 | Liu | Apr 2017 | B2 |
20020059797 | Kreso | May 2002 | A1 |
20030136196 | Wiklund et al. | Jul 2003 | A1 |
20070000218 | Wirth | Jan 2007 | A1 |
20070251214 | Nishino | Nov 2007 | A1 |
20090114168 | Lee | May 2009 | A1 |
20110283705 | Oliver | Nov 2011 | A1 |
20150020504 | Nicole | Jan 2015 | A1 |
Number | Date | Country |
---|---|---|
0154531 | Nov 1988 | EP |
Entry |
---|
Brochure disclosing SEMTECH-EFM3, Published by Sensor Inc. Published prior to Jan. 1, 2016. |
Brochure disclosing SEMTECH EFM2, Published by Sensor Inc. Published prior to Jan. 1, 2016. |
Brochure disclosing SEMTECH hs-EFM High Speed Exhaust Flow Meter, Published by Sensor Inc. Published prior to Jan. 1, 2016. |
Brochure disclosing SEMTECH EFM3 High Speed Exhaust Flow Meter, Published by Sensor Inc. Published prior to Jan. 1, 2016. |
Brochure disclosing SEMTECH EFM-HS High Speed Exhaust Flow Meter, Published by Sensor Inc. Published prior to Jan. 1, 2016. |
Brochure disclosing SEMTECH-FEM Fuel Economy Meter, Published by Sensor Inc. Published prior to Jan. 1, 2016. |
Brochure disclosing SEMTECH-EFM3 Vehicle Exhaust Flow Meter, Published by Sensor Inc. Published prior to Jan. 1, 2016. |
Sensors Inc. Users Manual, Entitled “Vehicle Exhaust Flow Meter SEMTECH EFM”, Last Updated May 20, 2005 by Vahan D. Shahinian. |
Sensors Inc. Users Manual, Entitled “Vehicle Exhaust Flow Meter SEMTECH EFM”, Last Updated May 18, 2007 by Vahan D. Shahinian. |
Sensors Inc. Users Manual, Entitled “High Speed Exhaust Flow Meter”, Last Updated Jan. 17, 2012 by Laura J. Dillmann. |
Aerospace Sciences & Aviation Technology, M. Metwally, “Review of Compressible Pulsating Flow Effects on System Performance”, May 26, 2009, 13th International Conference on Aerospace Sciences & Aviation Technology, ASAT-13. |
American School of Gas Measurement Technology, Robert J. McKee, “Pulsation effects on orifice metering considering primary and secondary elements”, Jan. 12, 2004, ASGMT.com/paper/2004, Southwest Research Institute, 6220 Culebra Road, San Antonio, TX 78238. |
Number | Date | Country | |
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20190277674 A1 | Sep 2019 | US |
Number | Date | Country | |
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62640760 | Mar 2018 | US |