1. Field of the Invention
The present invention relates generally to flow measurement techniques. More particularly, the present invention provides a MEMS chip for wind speed measurements.
2. Description of the Related Art
Wind speed is a fundamental atmospheric rate and affects weather forecasting, aircraft and maritime operations, construction projects, growth and metabolism rate of many plant species, and countless other implications. Wind speed is measured using anemometer, which measures wind's speed or pressure. The wind pressure is calculated as:
And Bernoulli's equation states:
pt=ps+pw
Solving that for speed we get:
where:
V is the wind speed;
Pw is the wind pressure;
Pt is the stagnation pressure;
Ps is the static pressure;
ρ is the air density.
To date, microfabricated MEMS pressure sensor is widely used. However, to the best of my knowledge, MEMS pressure sensor has limited application in measuring the wind pressure.
Microelectromechanical systems (MEMS) (also written as micro-electro-mechanical, MicroElectroMechanical or microelectronic and microelectromechanical systems) is the technology of very small devices. MEMS pressure sensor usually consists of several components that interact with the pressure to be measured and some electrical components that process data. MEMS pressure sensor usually outperforms a pressure sensor made using the most precise macroscale level machining techniques. The benefits include high output sensibility, reliable batch production, good repeatability, low costs, low power, miniaturization, high performance, and integration etc. Anemometer based on MEMS chip is expected to carry on these benefits into the field and is highly desired.
The present invention comprises a MEMS chip for wind speed measurements and a method of measuring the wind speed by the MEMS chip. The invention includes one or multiple embedded channels inside a conventional MEMS pressure sensor chip. The pressure sensor consists of a membrane with a cavity beneath it. Each channel has one end connect to the cavity and the other end open on the edge of the chip. The channel connects the cavity to the static pressure when measuring the wind speed. The invention is configured to have the membrane facing the wind during the measurement and the moving air is brought to rest (stagnates) onto it. Then one side of the membrane is under the stagnation pressure while the other side is under the static pressure. And the membrane deforms according to the wind pressure.
1. channel
2. cavity
3. membrane
4. substrate
5. electrode
As
The membrane 3 faces the wind and the air is stagnated onto it during the measurement. Bernoulli's equation also tells that the edge of the chip is under the static pressure. So the cavity 2 is connected to the static pressure through the channel 1. And the membrane 3 deforms according to the pressure difference between the stagnation pressure and the static pressure, i.e. the wind pressure. This deformation is then transformed into measurable capacitance changes by the electrodes 5.
The whole chip size is 4 mm×4 mm and the cross section of the channel 1 is 200 μm×5 μm. The size of the cavity 2 is 900 μm×900 μm. The size of the electrodes 5 is 810 μm×810 μm. Without deformation, the distance between two electrodes 5 is 1 μm and the capacitance between them is calculated as:
Where:
C is the capacitance between two parallel electrodes 5;
ϵ is the permittivity of the space between two electrodes 5;
A is the surface area of the electrodes 5;
d is the distance between two electrodes 5 without deformation;
When a uniform wind pressure Pw deforms the membrane 3, the maximum deformation w0 is at the center of the cavity 2. And the relationship between Pw and w0 is,
Where:
h is the thickness of the membrane 3;
E is the Young's modulus of the membrane 3;
ν is the Poisson ratio of the membrane 3;
a is the half length of the edge of the cavity 2;
In a two dimensional coordinate system (x, y) on the surface of the membrane 3, the origin of the coordinate system is at the center of the cavity 2. The axis x and the axis y are parallel to the edges of the surface of the cavity 2. The deformation w of the other locations of the membrane 3 is a function of x and y,
Then the capacitance between two electrodes 5 after the deformation is calculated as,
The wind pressure changes the separation distance between two electrodes 5, and the capacitance changes accordingly.
It is also understood that the examples and embodiments described herein are for illustrative purposes only and that various modifications or changes in light thereof will be suggested to persons skilled in the art and are to be included within the spirit and purview of this application and scope of the appended claims.
Filing Document | Filing Date | Country | Kind |
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PCT/US2013/022590 | 1/22/2013 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
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WO2014/116205 | 7/31/2014 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
3418546 | Beavers | Dec 1968 | A |
5515735 | Sarihan | May 1996 | A |
7788981 | Schmid | Sep 2010 | B2 |
8479580 | Shike | Jul 2013 | B2 |
8650963 | Barr | Feb 2014 | B2 |
20150377662 | Ray | Dec 2015 | A1 |
Entry |
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Wang, YH., Chen, CP., Chang, CM. et al. MEMS-based gas flow sensors, (2009), Springer Link, Microfluid Nanofluid 6:333-346. |
Berberig et al. The Prandtl micro flow sensor (PMFS): a novel silicon diaphragm capaciti9ve sensor for flow-velocity measurement, (1998), Elsevier, Sensors and actuators, pp. 93-98. |
Number | Date | Country | |
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20170199216 A1 | Jul 2017 | US |