# US 5,347,873 A · Double wing vortex flowmeter with strouhal number corrector

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- Number: US 5,347,873 A
- Document ID: US5347873A
- Status: Granted
- Kind: A
- Application number: 08/119,312
- Filed: 1993-09-09
- Granted: 1994-09-20
- Earliest claimed: 1993-04-09
- Assignees: Badger Meter, Inc.
- Inventors: William H. Vander Heyden
- Web page: https://patentgrep.com/patent/US5347873A

## CPC

- G01F 1/3266: {by sensing mechanical vibrations}
- G01F 1/325: Means for detecting quantities used as proxy variables for swirl
- G01F 1/3287: {circuits therefor}
- G01F: MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME

## Abstract

A vortex flowmeter includes a body having a flow passage, a vortex generator that generates a standing transverse wave in the flow passage, and first wing and second wings in the passage downstream of the generator. A circuit that utilizes sensors in the two wings is provided for first determining an operational phase difference, .DELTA..phi..sub.m between the signals representing movement of the first and second wings. A microprocessor then determines a corrected vortex frequency, .sup.f corr, in response to a ratio of a predetermined calibration phase difference .DELTA..phi..sub.c to the measured phase difference .DELTA..phi..sub.m.

## Claims

### Claim 1

A vortex flowmeter comprising:
a body having a passage for flow of a fluid therethrough in a longitudinal direction;
a vortex generator positioned in the passage for transmitting vortices downstream;
a first vortex sensor located at a first sensor position downstream of the vortex generator, the first vortex sensor producing a first signal of the vortex frequency, f.sub.m, in response to passage of vortices through the first sensor position;
a second vortex sensor located at a second sensor position downstream of the vortex generator, the second vortex sensor producing a second signal of the vortex frequency, f.sub.m, in response to passage of vortices through the second sensor position, said second signal being phase delayed from said first signal;
means for determining a measured phase difference .DELTA..phi..sub.m between the first signal and the second signal; and
means for comparing the measured phase difference .DELTA..phi..sub.m to a calibration phase difference .DELTA..phi..sub.c representing the phase difference between the first sensor position and the second sensor position wing under pre-operational, calibration conditions;
means for determining a corrected vortex frequency, f.sub.corr, of said flow meter during operation in response to a ratio of the predetermined calibration phase difference .DELTA..phi..sub.c to the measured phase difference .DELTA..phi..sub.m.

### Claim 2 (depends on 1)

The vortex flow meter of claim 1, wherein
the first vortex sensor is located in the passage in a first wing downstream of the vortex generator; and
wherein the second vortex sensor is located in the passage in a second wing downstream of the vortex generator.

### Claim 3 (depends on 2)

The vortex flowmeter of claim 2, wherein the sensors are piezoelectric transducers.

### Claim 4 (depends on 2)

The vortex flowmeter of claim 2, wherein the means for determining the measured phase difference, .DELTA..phi..sub.m, comprises a circuit for comparing the signals from the first and second vortex sensors located in the first and second wings, respectively.

### Claim 5 (depends on 1)

The vortex flowmeter of claim 1, further comprising means for determining a fluid velocity V.sub.m in accordance with the following relation: ##EQU13## where .DELTA..phi..sub.m is the determined phase difference, .DELTA..phi..sub.c is a calibrated phase difference between the first and second wings as determined before operating the flowmeter, f.sub.m is the vortex frequency, D is a characteristic length associated with the vortex generator as determined before operating the flowmeter, and N.sub.si is the initial Strouhal Number as determined before operating the flowmeter.

### Claim 6 (depends on 1)

The flowmeter of claim 1 wherein the calibration phase difference .DELTA..phi..sub.c is predetermined to be 180.degree..

### Claim 7

A method of determining a fluid velocity V.sub.m of fluid flowing through a flow passage comprising:
using a vortex generator with a characteristic dimension D to generate rows of vortices in the flow passage to form a standing transverse wave flow pattern;
detecting the vortices at one position in the flow passage;
detecting the vortices at a second position in the flow passage located downstream from the first position;
producing a first signal of a vortex frequency, f.sub.m, in response to detecting the vortices at the first detection position;
producing a second signal of a vortex frequency, f.sub.m, in response to detecting the vortices at the second detection position;
determining a phase difference .DELTA..phi..sub.m between the first and second signals;
determining measured fluid velocity V.sub.m by obtaining a corrected vortex frequency, f.sub.corr, by multiplying the vortex frequency, f.sub.m, by the ratio of the predetermined calibration phase difference .DELTA..phi..sub.c to the measured phase difference .DELTA..phi..sub.m.

### Claim 8 (depends on 7)

The method of claim 7, wherein the fluid velocity V.sub.m is further obtained by multiplying the correction frequency, f.sub.corr, by the ratio of ##EQU14## where D is the characteristic diameter of the vortex generator as determined before operation, and N.sub.si is the initial Strouhal Number as determined before operation.

### Claim 9 (depends on 7)

The method of claim 7, wherein the second position is located downstream from the first position a distance that is an odd multiple of half of a wavelength of the standing transverse wave.

### Claim 10 (depends on 7)

A method as recited in claim 7 wherein the phase difference .DELTA..phi..sub.m is determined by:
continuously transmitting the generated signals to a circuit; and
analyzing the continuously transmitted signals in the circuit.
