Airflow sensing systems and methods

Patent metadata

Field	Value
Publication number	US-10191076-B1
Application number	US-201514950243-A
Country	US
Kind code	B1
Filing date	Nov 24, 2015
Priority date	Nov 24, 2015
Publication date	Jan 29, 2019
Grant date	Jan 29, 2019

Abstract

A flow of air induces vibration of a tip of an airflow sensor. A cantilever coupled to the tip vibrates as the tip is displaced, and a piezoelectric element associated with the cantilever generates an electrical signal in response to mechanical stress or strain induced by vibration of the cantilever. A control element that is in communication with the piezoelectric element of the cantilever receives the electrical signal and derives at least one parameter indicative of the flow of air sensed by the sensor. The control element communicates or otherwise transmits an output signal that is indicative of the parameter to an output device to display sensor data to a user as desired.

First claim

Now, therefore, the following is claimed:

1. An airflow sensing system, comprising:
a first cantilever having a first beam, wherein a bluff body is formed at an end of the first beam for generating aerodynamic forces in response to an airflow;
a second cantilever having a second beam, wherein a second bluff body is formed at an end of the second beam for generating aerodynamic forces in response to the airflow;
a first piezoelectric element positioned on the first cantilever and configured to provide a first electrical signal indicative of a vibration of the first cantilever;
a second piezoelectric element positioned on the second cantilever and configured to provide a second electrical signal indicative of a vibration of the second cantilever;
a control element coupled to the first and second piezoelectric elements and configured to receive the first and second electrical signals, the control element further configured to determine, based on the first and second electrical signals, a velocity of an airflow causing each of the first and second cantilevers to vibrate;
an output device configured to provide an output based on the velocity; and
a shield positioned adjacent to the first cantilever for shielding the first beam from the airflow.

2. The system of claim 1 , wherein the control element comprises a processor and memory, the processor programmed to determine the velocity based on each of the first and second electrical signals and to store a value indicative of the velocity in the memory.

3. The system of claim 1 , wherein the control element is configured to determine the velocity based on a first frequency of the first electrical signal and a second frequency of the second electrical signal.

4. The system of claim 1 , wherein the first cantilever is oriented in a first direction, wherein the second cantilever is oriented in a second direction, and wherein the first direction differs from the second direction.

5. The system of claim 4 , wherein the first direction is orthogonal to the second direction.

6. The system of claim 5 , wherein the first cantilever extends from a curved substrate.

7. The system of claim 1 , further comprising:
a wind vane coupled to the first cantilever for rotating based on a direction of the airflow; and
a sensor for sensing a position of the wind vane,
wherein the control element is configured to determine a direction of the airflow based on the sensor.

8. The system of claim 1 , wherein the first bluff body has a surface on a side of the first bluff body exposed to the airflow opposite of the first beam, and wherein the surface is curved thereby affecting the aerodynamic forces generated by the first bluff body.

9. The system of claim 1 , wherein the first bluff body is shaped such that the first cantilever begins to gallop in response to the aerodynamic forces generated by the first bluff body when the airflow exceeds a threshold speed.

10. An airflow sensing system, comprising:
a first cantilever having a first beam, wherein a first bluff body is formed at an end of the first beam for generating aerodynamic forces in response to an airflow;
a second cantilever having a second beam, wherein a second bluff body is formed at an end of the second beam for generating aerodynamic forces in response to the airflow;
a first piezoelectric element associated with the first cantilever;
a second piezoelectric element associated with the second cantilever;
a control element coupled to each of the first and second piezoelectric elements, the control element configured to receive a first electrical signal generated by the first piezoelectric element and a second electrical signal generated by the second piezoelectric element, wherein the first electrical signal is indicative of vibration of the first cantilever induced by aerodynamic forces generated by the first bluff body, wherein the second electrical signal is indicative of vibration of the second cantilever induced by the aerodynamic forces generated by the second bluff body, and wherein the control element is configured to determine a velocity of the airflow based on the first and second electrical signals;
an output device in communication with the control element, wherein the control element is configured to provide an output via the output device based on the velocity;
a substrate from which the first cantilever extends; and
a shield coupled to the substrate and disposed around a longitudinal axis of the first cantilever.

11. The system of claim 10 , wherein the control element is configured to determine the velocity of the airflow based on a first frequency of the first electrical signal and a second frequency of the second electrical signal.

12. The system of claim 10 , wherein the control element further comprises logic configured to receive at least the first electrical signal, store the at least the first electrical signal in memory, generate an output signal, and communicate the output signal to the output device.

13. The system of claim 10 , wherein the output device comprises a display for displaying the output.

14. The system of claim 10 , wherein the output device is configured to transmit a message indicative of the velocity.

15. The system of claim 10 , wherein the first cantilever is mounted on substrate, and wherein the first bluff body has a face on a side of the first bluff body opposite of the substrate.

16. The system of claim 15 , wherein the face comprises a flat surface profile shape.

17. The system of claim 15 , wherein the face comprises a curved surface profile shape.

18. An airflow sensing system, comprising:
a cantilever comprising a beam having an end, wherein a bluff body is formed at the end of the beam for generating aerodynamic forces in response to an airflow, and wherein the bluff body is shaped such that the cantilever begins to gallop in response to the aerodynamic forces when a speed of the airflow exceeds a threshold;
a piezoelectric element positioned on the cantilever and configured to provide an electrical signal indicative of a vibration of the cantilever;
a control element coupled to the piezoelectric element and configured to receive the electrical signal, the control element further configured determine, based on the electrical signal, the speed of the airflow;
an output device configured to provide an output based on the speed; and
a shield disposed around the cantilever for blocking the airflow.

19. The system of claim 18 , wherein the bluff body has a surface on a side of the bluff body exposed to the airflow opposite of the beam, and wherein the surface is curved thereby affecting the aerodynamic forces generated by the bluff body.

20. The system of claim 18 , wherein the control element is configured to determine the speed of the airflow based on a frequency of the electrical signal.

21. An airflow sensing method, comprising:
providing an airflow sensor having a cantilever, the cantilever comprising a beam having an end, wherein a bluff body is formed at the end of the beam;
positioning the airflow sensor within an airflow;
generating aerodynamic forces from the airflow with the bluff body, wherein the bluff body is shaped such that the aerodynamic forces cause the cantilever to begin galloping when a speed of the airflow exceeds a threshold;
sensing, with a piezoelectric element, vibration of the cantilever;
determining, with a control element, a speed of the airflow based on the sensing;
providing an output based on the speed; and

Assignees

• Wang Gang
• Ewere Felix
• Board Of Trustees Of The Univ Of Alabama For And On Behalf Of The Univ Of Alabama In Huntsville

Inventors

• Wang Gang
• Ewere Felix

Classifications

• G01P5/086

  by using special arrangements and constructions for measuring the dynamo-electric effect · CPC title

• G01P5/08

  by measuring variation of an electric variable directly affected by the flow, e.g. by using dynamo-electric effect · CPC title

• G01H11/08 Primary

  using piezoelectric devices · CPC title

• G01P5/07

  with electrical coupling to the indicating device · CPC title

• G01P5/06

  using rotation of vanes (measuring speed of rotating shafts G01P3/00) · CPC title