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8 Some Perspectives on MEMS-Based Active Control

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NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

8 Some Perspectives on MEMS-Based Active Control

NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

Micromachines 2000 In cooperation

with EPFL

Packaging and Integration Mechanical Modeling

and Optimization Parallel

Manipulators Programmable

Vector Fields CMOS Integrated Micromanipulators

Microactuator Arrays

Active acoustical Impedance

Active Microsuspensions Flapping Wing Propulsion Systems Autonomous Micro Air Vehicles MEMS-based

Smart Structures

On-chip Characterization of Silicon-based Materials

Tests Microlabs

Mechanical Characterization of Biological Cells 2001

2002

2003

2004

MEMS Technology

(in cooperation with EPFL)

NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

High Density Hard Drives

M a ch in in g (n m )

De n si ty ( cm

-2

)

Year IC Transistor Density Bit Density

(Magnetic Recording)

From web site: www.storage.ibm.com

NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

MEMS-Based Active Control of Read / Write Magnetic Head

Specifications:

- Disk Rotation Speed: 7800 rpm - Angular Partitioning: 52 sectors - Radial Partitioning: 0.4µm/step - Magnetic Head Altitude: 15 nanometers - Positioning Precision: 50 nanometers - Lifetime: 10 years Market Perspectives:

- 2 B US S

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NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

Tiny Hard Drives

From web site: www.storage.ibm.com

NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

Toward MEMS-Based Control of Acoustical Impedance

Objective: Kill the Source of Noise due to Mechanical Vibrations by Using Distributed Acoustic Transducers

NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

Experimental Setup

Doc. LMARC

NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

106 dB (distance : 1m)

Cross Section of an Elementary Acoustic Transducer

Acoustic Radiation of the Uncontrolled Wafer Acting as a Membrane

δ

(3)

NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

MEMS-Based Acoustic Transducer Array

Doc. LMARC / web site: www.micromachines.univ-fcomte.fr

NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

Design of an Elementary Acoustic Transducer

Localisation des électrodes Raidisseurs : 4µm

l1/2 l2

l3

l4

l7

l5

l6

l8

l9

X

Y

Geometrical Parameters

l

1

= 20µm ; l

2

= 470µm ; l

3

= 460µm ; l

4

= 460µm ; l

5

= 5µm ; l

6

= 10µm ; l

7

= 160µm ; l

8

= 30µm ; l

9

= 10µm.

Acoustic Transducer Thickness : ep

1

= 2µm Mechanical Stiffener : ep

2

= 4µm

Transducer/Substrate Gap: g

1

= 7µm Driving Electrode: S = l

7

× l

7

Doc. LMARC

NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

Acoustic Transducers using Electrostatic Actuation: Out-of-Plane Motion Analysis

Doc. LMARC / web site: www.micromachines.univ-fcomte.fr

nitrure

nitrure nitrure in air

pull

g ep

ε ε δ ε

3 +

1

=

( )

[ ]

S l

ep El ep

V g

nitrure air

air nitrure nitrure

2 32

13 1 2 1

2

16 ε

ε

δ ε ε

δ +

= +

V V

µm pull in

in

pull = 2 . 36 ; = 22

δ

Quasi-Static Control of Out-of-Plane Motion (Up to 9800 Hz)

NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

Toward MEMS-Based Active Control of Turbulence

From web site: www.ensimag.fr

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NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

Toward MEMS-Based Active Control of Turbulence

Doc. LMARC

NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

MEMS-Based Micro Air Vehicles

Centimeter Scale

“Mesicopter”

(After UC Berkeley)

Flapping Wing Micro Air Vehicle (After UC Berkeley)

Insect-Scale Aerodynamics 3D Micromanufacturing Power/Control/Sensors Battery Technology

NATO Advanced Study Institute RESPONSIVE SYSTEMS … / MEMS Course Brussels, September 10-19, 2001

Laboratoire de Mécanique Appliquée – UMR CNRS 6604 – Université de Franche Comté Institut des Microtechniques de Franche Comté

Micromechanical Flying Insects (After UC Berkeley)

Stainless Steel Thorax Driven with PZT Actuator

From web site: robotics.eecs.berkeley.edu

6 µm Polyester Wing with Calliphora Wing

< 20mg/mm

2

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