556KB - Spansion

The following document contains information on Cypress products.
Energy Calculation
For Energy Harvesting
APPLICATION NOTE
Publication Number
CONFIDENTIAL
AN405-00001
Revision 1.0
Issue Date July 18, 2014
A P P L I C A T I O N
N O T E
Target Products
This application note applies to the following products.
(Buck DC/DC converter)
Part number
MB39C811
Description
Ultra Low Power Buck Power Management IC for Solar/Vibrations Energy Harvesting
(Boost DC/DC converter)
Part number
MB39C831
2
CONFIDENTIAL
Description
Ultra Low Voltage Boost Power Management IC for Solar/Thermal Energy Harvesting
AN405-00001-1v0-E, July 18, 2014
A P P L I C A T I O N
N O T E
Table of Contents
1. Introduction .............................................................................................................................................. 5
1.1 Energy harvesting system .............................................................................................................. 5
2. Energy Calculation .................................................................................................................................. 6
2.1 Energy requirement in application block ......................................................................................... 6
2.2 Sizing of Cin and Cout (for MB39C811) ......................................................................................... 7
2.3 Charging time of Cin and Cout (for MB39C811) ............................................................................. 8
2.4 Sizing of Cin and Cout (for MB39C831) ......................................................................................... 9
2.5 Charging time for Cin and Cout (for MB39C831) .......................................................................... 10
3. Appendix ................................................................................................................................................ 11
3.1 Power generation capability ......................................................................................................... 11
3.2 Amorphous silicon solar cell (for MB39C811) ............................................................................... 12
3.3 Amorphous silicon solar cell in series (for MB39C811) ................................................................ 15
3.4 Piezo (for MB39C811) .................................................................................................................. 17
3.5 Single crystal silicon solar cell -1- (for MB39C831) ...................................................................... 19
3.6 Single crystal silicon solar cell -2- (for MB39C831) ...................................................................... 20
3.7 Peltier (for MB39C831) ................................................................................................................. 21
Figures
Figure 1-1
Figure 2-1
Figure 2-2
Figure 2-3
Figure 2-4
Figure 2-5
Figure 2-6
Figure 3-1
Figure 3-2
Figure 3-3
Figure 3-4
Figure 3-5
Figure 3-6
Figure 3-7
Figure 3-8
Figure 3-9
Figure 3-10
Figure 3-11
Figure 3-12
Figure 3-13
Figure 3-14
Figure 3-15
Figure 3-16
Figure 3-17
Figure 3-18
Popular energy harvesting system ......................................................................................... 5
Measurement of energy requirement...................................................................................... 6
Waveform of VOUT and IVOUT ............................................................................................. 6
Stored Image of capacitors (for MB39C811) .......................................................................... 7
Charging time of Cin and Cout (for MB39C811) ..................................................................... 8
Stored Image of capacitors (for MB39C831) .......................................................................... 9
Charging time of Cin and Cout (for MB39C831) ................................................................... 10
Power generation capability .................................................................................................. 11
Block diagram with Amorphous silicon solar cell .................................................................. 12
Charging time for Cin and Cout ............................................................................................ 12
Block diagram with Amorphous silicon solar cell .................................................................. 13
After the Charging time of Cin and Cout ............................................................................... 13
Characteristic of amorphous silicon solar cell ....................................................................... 14
Block diagram with 2 series Amorphous silicon solar cells ................................................... 15
Measured graph using amorphous silicon solar cells in series ............................................. 15
Measured graph using amorphous silicon solar cell in series ............................................... 16
Energy vs input voltage in capacitor ................................................................................... 16
Testing method using Piezo ................................................................................................ 17
Measured graph using Piezo .............................................................................................. 17
Block diagram with Single crystal silicone solar cell -1- ...................................................... 18
Measured graph using Single crystal silicone solar cell -1- ................................................ 19
Block diagram with Single crystal silicone solar cell -1- ...................................................... 19
Measured graph using Single crystal silicone solar cell -2- ................................................ 20
Block diagram with single crystal silicone solar cell -2- ...................................................... 20
Block diagram with Peltier .................................................................................................. 21
Tables
Table 3-1
Table 3-2
Table 3-3
Examples of power generation capability (for MB39C811) ...................................................... 11
Examples of power generation capability (for MB39C831) ..................................................... 11
Characteristics of Amorphous silicon solar cell ...................................................................... 12
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A P P L I C A T I O N
Table 3-4
Table 3-5
Table 3-6
Table 3-7
Table 3-8
4
CONFIDENTIAL
N O T E
Characteristics of 2 series Amorphous silicon solar cells ....................................................... 15
Characteristics of Piezo ......................................................................................................... 17
Characteristics of single crystal silicone solar cell -1- ............................................................ 19
Characteristics of single crystal silicone solar cell -2- ............................................................ 20
Characteristics of Peltier ........................................................................................................ 21
AN405-00001-1v0-E, July 18, 2014
A P P L I C A T I O N
N O T E
1. Introduction
For the energy harvesting, the system design is very important. The system performing low power operation
should be designed since the amount of energy from harvester is very small. In such cases, the energy
budget calculation is necessary.
1.1
Energy harvesting system
Figure 1-1 shows the popular energy harvesting system.
Figure 1-1
Popular energy harvesting system
Enveronmental Energy
Power Good
VIN
Harvester
Block
Cin
VOUT
PMIC
Block
Cout
Power
Gating
Application Block
MCU
RF
Sensor
Low power consumption devices are needed to design the energy harvesting system. Select low power
PMIC and ICs for the application block because the energy from harvester is limited.
Also, energy from harvester should be stored on the Cin and Cout to operate the application block. If the size
of these capacitors were too big, it would take too much time to charge energy into these capacitors, and the
system cannot be operated frequently. On the other hand, if these capacitors were too small, enough energy
cannot be stored on these capacitors for the application block. The sizing of the Cin and Cout is important,
too.
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A P P L I C A T I O N
N O T E
2. Energy Calculation
2.1
Energy requirement in application block
Once the system is designed, make the prototype. The Figure 2-1 shows the measurement method of the
energy requirement in application block.
Figure 2-1
Measurement of energy requirement
Power Good
VIN
Power
Source
Cin
VOUT
PMIC
Block
Current
Probe
Power
Gating
Cout
V
Application Block
MCU
RF
Sensor
To calculate the necessary energy for the application, measure the voltage and current of VOUT. After the
measurement, apply the following equation to calculate the energy requirement.
EAppli. [J] = VAppli. × IAppli. × t Appli.
The Figure 2-2 shows actual measurement waveform of the energy harvesting system. In this example, the
energy requirement for the application block is roughly calculated at 2,534µJ.
Figure 2-2
Waveform of VOUT and IVOUT
Waveforms
VIN ≧ 5.2V
Preset output voltage = 3.3V
VOUT
2V/DIV
3.3V
Power good off
MCU & Sensor
IVOUT
10mA/DIV
MCU
RF
transmission
3.3V x 16mA x 48ms
=2534µJ
16mA
48ms
Application Operation starts
10ms/DIV
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A P P L I C A T I O N
2.2
N O T E
Sizing of Cin and Cout (for MB39C811)
The Cin and Cout should be sized. The Figure 2-3 shows the image of the capacitors with the buck DC/DC
converter, MB39C811.
Figure 2-3
Stored Image of capacitors (for MB39C811)
Power Good
VIN
Power
Source
VIN≧5.2V
Buck
DC/DC
VOUT=3.3V
Power
Gating
Application
MB39C811
VUVLOH
VUVLOL
Cin
0V
Cout
=47µF
VVOUT
VOPGL
0V
2534µJ
Efficiency=80%
Available Energy
VUVLOH : UVLO release voltage
VUVLOL : UVLO detection voltage
VVOUT
VOPGL
: Preset output voltage
: Output power-good reset voltage
The energy stored on a capacitor is calculated by the following equation.
1
Ecapacitor [J] = CV 2
2
Because the energy in a capacitor is proportional to the square of the voltage, it is energetically
advantageous for the buck DC/DC converter to make the Cin larger. On the other hand, for the boost DC/DC
converter, it is energetically advantageous to make the Cout larger. In the example with MB39C811 of the
Figure 2-3, adjust the Cin, and keep the Cout = 47µF (refer to the MB39C811 datasheet).
Calculate the available energy in Cout
The output power-good reset voltage (minimum voltage of the Cout) is 70 % of the preset output voltage
(VOUT voltage), VOPGL is 2.31V (refer to the MB39C811 datasheet).
Available energy in Cout [μJ] =
1
× Cout × (VVOUT 2 − VOPGL2 )
2
Available energy in Cout [μJ] =
1
× 47[μF] × (3.3[V]2 − 2.31[V]2 ) = 131[μJ]
2
In the Figure 2-2, the energy requirement for the application block was calculated at 2,534[µJ]. The available
energy stored on the Cout was found 131µJ, so that the remaining energy requirement is
Remaining energy requirement [μJ] = 2,534[μJ] − 131[μJ] = 2,403[μJ]
1
2
The remaining energy requirement should be stored on the Cin.
Calculate the size of the Cin
For the Cin calculation, it is necessary to take the efficiency of PMIC into account. According to the
datasheet, the efficiency is about 80% in the 16mA load current. (The “η” is the efficiency of PMIC.)
Available energy in Cin [μJ] =
1
× η × Cin × (VUVLOH 2 − VUVLOL2 )
2
Available energy i2403 [μJ] =
1
× 80[%] × Cin[μF] × (5.2[V]2 − 4.0[V]2 )
2
Available energy in Cin [μF] = 544[μJ]
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A P P L I C A T I O N
2.3
N O T E
Charging time of Cin and Cout (for MB39C811)
In order to calculate the charging time, the power generation capability is needed. (Refer to the Appendix,
e.g. a solar cell has 155µW generation capability at the 1000[lx]). The Figure 2-4 shows the example of
energy harvesting system focused on the charging time with a harvester.
Figure 2-4
Charging time of Cin and Cout (for MB39C811)
Light(1000[lx])
Power Good
155µW
Amorphous
Si solar cell
VIN
Cin
=544µF
Buck
DC/DC
MB39C811
VOUT
Power
Gating
Application
2534µJ
Cout
=47µF
Efficiency=80%
Step1 for Initial charging time
Before calculating the initial charging time, calculate the total energy stored on both Cin and Cout.
Total energy of Cin [μJ] =
1
1
× Cin × (VUVLOH 2 ) = × 544[μF] × 5.2[V]2 = 7355[μJ]
2
2
Total energy of Cout [μJ] =
1
1
× Cout × (VVOUT 2 ) = × 47[μF] × 3.3[V]2 = 256[μJ]
2
2
Step2 for Initial charging time
Initial charging time of Cin [s] =
Total energy of Cin [μJ]
7355 [μJ]
=
= 49.5[sJ]
Power of solar cell [μW] 155 [μW]
Initial charging time of Cout [s] =
Total energy of Cout [μJ]
256 [μJ]
=
= 2[sJ]
Power of solar cell [μW] × 80[%] 155 [μW] × 0.8
Initial charging time [s] = Initial charging time of Cin [s] + Initial charging time in Cout [s]
Initial charging time [s] = 49.5 [s] + 2 [s] = 51.5 [s]
1
2
1
2
Repeat charging time
Repeat time for charging time of Cin [s] =
Repeat charging time of Cout [s] =
Available energy in Cin [μJ] 2403 [μJ]
=
= 15.5[sJ]
Power of solar cell [μW]
155 [μW]
Available energy in Cout [μJ]
131 [μJ]
=
= 1[sJ]
Power of solar cell [μW] × 80[%] 155 [μW] × 0.8
Repeat charging time [s] = Repeat charging time of Cin [s] + Repeat charging time of Cout [s]
Repeat charging time [s] = 15.5 [s] + 1 [s] = 16.5 [s]
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2
1
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A P P L I C A T I O N
2.4
N O T E
Sizing of Cin and Cout (for MB39C831)
The Figure 2-5 shows the image of the capacitors with the boost DC/DC converter, MB39C831.
Figure 2-5
Stored Image of capacitors (for MB39C831)
DET[1:0]
VDD
Power
Source
Boost
DC/DC
VOUT=3.3V
MB39C831
VDD≧0.35V
VDD
0.3V
0V
Cin
=10µF
Efficiency=70%
Power
Gating
Application
2534µJ
VOUT
2.9V
Cout
=470µF
0V
Available Energy
VDD : VDD input voltage
0.3V : Min VDD input voltage
VOUT
2.9V
:
:
Preset
:
output voltage
Output
:
power-good reset voltage
Because the energy in a capacitor is proportional to the square of the voltage, it is energetically
advantageous for the boost DC/DC converter to make the Cout larger. In the example with MB39C831 of the
Figure 2-5, only adjust the Cout. Although the Cin = 10µF is used as the input capacitor, the Cin is excluded
from the energy calculation because the stored energy on the Cin is very small.
In the Figure 2-2, the energy requirement for the application block was calculated at 2,534[µJ]. The energy
requirement should be stored on the Cout.
Calculate the size of the Cout
The output power-good reset voltage (minimum voltage of the Cout) is set by 2.9V in MB39C831. (Refer to
the MB39C831 datasheet).
Available energy in Cout [μJ] =
1
× Cout × (VOUT 2 − 2.9[V]2 )
2
Available energy i 2534 [μJ] =
1
× Cout[μF] × (3.3[V]2 − 2.9[V]2 )
2
Available energy in Cout [μF] = 2044[μF]
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A P P L I C A T I O N
2.5
N O T E
Charging time for Cin and Cout (for MB39C831)
In order to calculate the charging time, the power generation capability is needed. (Refer to the Appendix,
e.g. the single crystal silicon solar cell (Vmax=0.5V) has 233µW generation capability including the
MB39831’s consumption at the 50000[lx]). The Figure 2-6 shows the example of energy harvesting system
focused on the charging time with a harvester.
Figure 2-6
Charging time of Cin and Cout (for MB39C831)
Light(50000[lx])
Power Good
Single
crystal Si
solar cell
VIN
Cin
=10µF
(Vmax=0.5V)
Boost
DC/DC
MB39C831
233µW
VOUT
Power
Gating
Cout
=2044µF
Application
2534µJ
Step1 for Initial charging time
Before calculating the initial charging time, calculate the total energy stored on the Cout.(excluding the Cin
because the stored energy on the Cin is very small.)
Total energy of Cout [μJ] =
1
1
× Cout × (VOUT 2 ) = × 2044[μF] × 3.3[V]2 = 11127[μJ]
2
2
Step2 for Initial charging time
Initial charging time of Cout [s] =
Total energy of Cout [μJ]
11127 [μJ]
=
= 44.8[s]
generation capability including IC[μW]
233 [μW]
Repeat charging time
Repeat charging time of Cout [s] =
10
CONFIDENTIAL
Available energy in Cout [μJ]
2534 [μJ]
=
= 11[s]
generation capability including IC[μW] 233 [μW]
AN405-00001-1v0-E, July 18, 2014
A P P L I C A T I O N
N O T E
3. Appendix
3.1
Power generation capability
Figure 3-1
Power generation capability
INPUT
Harvester
Cin
OUTPUT
DC/DC
Cout
To make it simple to calculate charging time at the section 2.3 and the section 2.5, the power generation
capability is calculated based on the measured charging time of capacitors.
Table 3-1
Generator
Solar
Solar
Piezo
Type
Amorphous
Si
Examples of power generation capability (for MB39C811)
Size
Vmax
Imax
[mm]
[V]
[mA]
46×30
6.68
(6.4 + 0.28)
Amorphous
46×30
13.08
Si
(2 series)
(12.8 + 0.28)
Polymer
80×30
80(Vpp)
condition
Power generation
capability [µW]
---
1000[lx]
155 [µW]
---
1000[lx]
193 [µW]
---
3Hz
578 [µW]
hand push
The MB39C831 is designed for harvesters that have a high power generation capability, such as an outdoor
solar cell. It is not possible to start up with a small indoor solar cell.
Table 3-2
Generator
Solar
Solar
Peltier
Type
Single
crystal Si
Single
crystal Si
---
Examples of power generation capability (for MB39C831)
Size
Vmax
Imax
[mm]
[V]
[mA]
50×50
0.5
500
50000[lx]
233 [µW] (*1)
82×68
1.5
500
50000[lx]
1706 [µW] (*1)
0.704
117
ΔT=30℃
Larger than 44000 [µW] (*2)
10×10
(2 series)
condition
Power generation
capability [µW]
*1: the value including the MB39C831’s consumption.
*2: the value from a peltier’s datasheet
July 18, 2014, AN405-00001-1v0-E
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A P P L I C A T I O N
3.2
N O T E
Amorphous silicon solar cell (for MB39C811)
Table 3-3
Generator
Solar
Size
Vmax
Imax
[mm]
[V]
[mA]
46×30
6.68
---
Type
Amorphous
Si
Characteristics of Amorphous silicon solar cell
Figure 3-2
Power generation
condition
capability [µW]
1000[lx]
155 [µW]
Block diagram with Amorphous silicon solar cell
Light(1000[lx])
155µW VIN
Solar Cell
46mm×30mm
9 cells
Vf=0.28V
MB39C811
VUVLOH
VVOUT
Cin
=470µF
0V
Cout
=47µF
0V
VUVLOH : UVLO release voltage
Figure 3-3
VOUT=3.3V
Buck
DC/DC
VVOUT : Preset output voltage
Charging time for Cin and Cout
Amorphous Si solar cell
8
9 cells, Size: 46x30mm
Voltage [V]
Preset output voltage = 3.3V
7 Illuminance = 1000lx
transfer of energy
Cin = 470µF
from Cin to Cout
6 Cout = 47µF
5
4
42s
VIN
3.3V
3
2
1
41s
VOUT
0
0
5
10
15
20 25 30
Time [s]
35
40
45
50
①Charging energy in Cin
Charging energy[μJ] =
1
1
× Cin × (VUVLOH 2 ) = × 470[μF] × 5.2[V]2 = 6354[μJ]
2
2
②Charging time in Cin (measured value)
Charging time[s] = 41 [s]
1
2
③Power generation capability
Power generation capability[μW] = Charging energy[μJ] ÷ Charging time[s] =
Power generation capability[μW] = 6354 [μJ] ÷ 41 [s] = 155 [μW] =
1
2
1
2
After the voltage of the Cout becomes the preset output voltage, more energy is charged into the Cin until
the open circuit voltage of the solar cell. The power generation capability during the period is calculated.
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A P P L I C A T I O N
Figure 3-4
N O T E
Block diagram with Amorphous silicon solar cell
Light(1000[lx])
35µW VIN
Solar Cell
46mm×30mm
9 cells
Vf=0.28V
Vopen
VUVLOH
MB39C811
VVOUT
Cin
=470µF
0V
VVOUT : Preset output voltage
After the Charging time of Cin and Cout
Amorphous Si solar cell
20
Amorphous Si solar cell
9 cells, Size: 46x30mm
8
12
41s
8
VIN
9 cells, Size: 46x30mm
Preset output voltage = 3.3V
Illuminance = 1000lx
Cin = 470µF
7 Cout = 47µF
open circuit voltage
6.4V
Voltage [V]
Voltage [V]
Preset output voltage = 3.3V
18 Illuminance = 1000lx
16 Cin = 470µF
Cout = 47µF
14
10
Cout
=47µF
0V
VUVLOH : UVLO release voltage
Vopen
: Combined open voltage
Figure 3-5
VOUT=3.3V
Buck
DC/DC
open circuit voltage
6.4V
VIN
6
6
5.1V
5
4
VOUT
2
0
0
50
100
150
200
Time [s]
42s
250
300
4
40
142 s
60
80
100
120
Time [s]
140
160
④Charging more energy in Cin
Charging energy[μJ] =
1
× 80[%] × 470[μF] × (6.4[V]2 − 5.1[V]2 ) = 3513[μJ]
2
⑤Charging time in Cin (measured value)
Charging time [s] = 100 [s]
1
2
⑥Power generation capability
Power generation capability[μW] = Charging energy[μJ] ÷ Charging time [s] =
Power generation capability[μW] = 3513[μJ] ÷ 100 [s] = 35[μW] =
1
2
1
2
The power generation capability is much smaller than that until the Cin become the preset output voltage.
That is because of the characteristics of the solar cell. This solar cell acts as a current source until around
5V (see Figure 3-6). However, the current supply suddenly decrease after the voltage goes over 5V.
July 18, 2014, AN405-00001-1v0-E
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A P P L I C A T I O N
Figure 3-6
N O T E
Characteristic of amorphous silicon solar cell
Amorphous Si characteristics
100
9 cells, Size: 46x30mm
Illuminance = 1000lx
Current [µA]
80
60
40
20
0
0
14
CONFIDENTIAL
Vf of diode
0.28V
1
2
3
4
5
Voltage [V]
6
7
6.4V
8
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A P P L I C A T I O N
3.3
N O T E
Amorphous silicon solar cell in series (for MB39C811)
Table 3-4
Generator
Characteristics of 2 series Amorphous silicon solar cells
Type
Solar
Size
Vmax
Imax
[mm]
[V]
[mA]
13.8
---
Amorphous
46×30
Si
(2 series)
Figure 3-7
Light(1000[lx])
capability [µW]
1000[lx]
193 [µW]
Block diagram with 2 series Amorphous silicon solar cells
Light(1000[lx])
193µW VIN
Solar Cell
Solar Cell
46mm×30mm
9 cells
46mm×30mm
9 cells
VOUT=3.3V
Buck
DC/DC
Vf=0.28V
MB39C811
VUVLOH
VVOUT
Cin
=470µF
0V
0V
Cout
=47µF
VVOUT : Preset output voltage
VUVLOH : UVLO release voltage
Figure 3-8
Power generation
condition
Measured graph using amorphous silicon solar cells in series
Amorphous Si solar cell
8
[2 series] 9 cells, Size: 46x30mm
Voltage [V]
Preset output voltage = 3.3V
7 Illuminance = 1000lx
transfer of energy
Cin = 470µF
from Cin to Cout
6 Cout = 47µF
5
4
34s
VIN
3.3V
3
2
1
33s
VOUT
0
0
5
10
15
20 25 30
Time [s]
35
40
45
50
①Charging energy in Cin
Chargeing energy[μJ] =
1
1
× Cin × (VUVLOH 2 ) = × 470[μF] × 5.2[V]2 = 6354[μJ]
2
2
②Charging time in Cin (measured value)
Charging time [s] = 33 [s]
1
2
③Power generation capability
Power generation capability[μW] = Charging energy[μJ] ÷ Charging time[s] =
Power generation capability[μW] = 6354 [μJ] ÷ 33 [s] = 193 [μW] =
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2
1
2
15
A P P L I C A T I O N
Figure 3-9
N O T E
Measured graph using amorphous silicon solar cell in series
Amorphous Si solar cell
20
[2 series] 9 cells, Size: 46x30mm
Voltage [V]
Preset output voltage = 3.3V
18 Illuminance = 1000lx
16 Cin = 470µF
Cout = 47µF
14
12.8V
12
10
VIN
33s
8
6
VOUT
4
2
0
0
50
100
150
200
Time [s]
250
300
The more energy from a harvester can be stored on a capacitor because the energy in a capacitor is
proportional to the square of the voltage.
Energy[μJ] =
1
× 470[μF] × Voltage2
2
Figure 3-10
Energy vs input voltage in capacitor
Energy vs Voltage in Cin
50
Cin = 470µF (maximum rating ≧ 12.8V)
38.5mJ
Energy [mJ]
40
30
12.8V
6.4V
5.2V
20
9.6mJ
10
6.4mJ
0
0
16
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2
4
8
6
Voltage [V]
10
12
14
AN405-00001-1v0-E, July 18, 2014
A P P L I C A T I O N
3.4
N O T E
Piezo (for MB39C811)
Table 3-5
Generator
Piezo
Type
Polymer
Characteristics of Piezo
Size
Vmax
Imax
[mm]
[V]
[mA]
80(Vpp)
80×30
Figure 3-11
Power generation
condition
capability [µW]
3Hz,
---
578 [µW]
hand push
Testing method using Piezo
Hand push
Piezo(8cm x 3cm)
based plates that
are flexible
about 5 cm
Figure 3-12
Measured graph using Piezo
Piezo
20
Based plate that is flexible
Voltage [V]
Preset output voltage = 3.3V
18 About 3Hz by hand push
16 Cin = 470µF
Cout = 47µF
14
12
10
VIN
8
11s
6
14s
4
VOUT
3.3V
2
0
0
10
20
30
Time [s]
40
50
60
①Charging energy in Cin
Energy for charging[μJ] =
1
1
1
× Cin × (VUVLOH 2 ) = × 470[μF] × 5.2[V]2 = 6354[μJ]
2
2
2
②Charging time in Cin (measured value)
Charging time[s] = 11 [s]
1
2
③Power generation capability
Power generation capability[μW] = Charging energy[μJ] ÷ Charging time[s] =
Power generation capability[μW] = 6354[μJ] ÷ 11 [s] = 578 [μW] =
July 18, 2014, AN405-00001-1v0-E
CONFIDENTIAL
1
2
1
2
17
A P P L I C A T I O N
Figure 3-13
N O T E
Block diagram with Single crystal silicone solar cell -1-
Hand push (3[Hz])
Piezo
80mm×30mm
578µW VIN
Polymer
VUVLOH
0V
VUVLOH : UVLO release voltage
18
CONFIDENTIAL
Buck
DC/DC
VOUT=3.3V
MB39C811
Cin
=470µF
VVOUT
0V
Cout
=47µF
VVOUT : Preset output voltage
AN405-00001-1v0-E, July 18, 2014
A P P L I C A T I O N
3.5
N O T E
Single crystal silicon solar cell -1- (for MB39C831)
Table 3-6
Generator
Characteristics of single crystal silicone solar cell -1Size
Vmax
Imax
[mm]
[V]
[mA]
50×50
0.5
500
Type
Single
Solar
crystal Si
Power generation
condition
capability [µW]
50000[lx]
233 [µW] (*1)
*1: the value including the MB39C831’s consumption
Figure 3-14
Measured graph using Single crystal silicone solar cell -1Single crystal Si solar cell
5
Vopen = 0.5V, Ishort = 500mA
Voltage [V]
Preset output voltage = 3.3V
Illuminance = 50000lx
4 Cin = 10µF
Cout = 470µF
11s
3.3V
3
VOUT
2
1
0
0
2
4
6
10
8
Time [s]
14
12
16
The Cin is excluded from the energy calculation because the input voltage (VDD) is not stable in the start-up
and the stored energy is very small.
①Charging energy in Cout
Chargeing energy[μJ] =
1
1
× Cout × (VOUT 2 ) = × 470[μF] × 3.3[V]2 = 2559[μJ]
2
2
②Charging time in Cout (measured value)
Time for charging[s] = 11 [s]
1
2
③Power generation capability
Power generation capability[μW] = Charging energy[μJ] ÷ Charging time [s] =
Power generation capability[μW] = 2559 [μJ] ÷ 11 [s] = 233 [μW] =
Figure 3-15
1
2
1
2
Block diagram with Single crystal silicone solar cell -1-
Light(50000[lx])
VDD
Single Crystal Si
Solar Cell
50mm×50mm
Vmax = 0.5V
Imax = 500 mA
VDD : VDD input voltage
July 18, 2014, AN405-00001-1v0-E
CONFIDENTIAL
Boost
DC/DC
MB39C831
VDD
0V
Cin
=10µF
VOUT
:
VOUT=3.3V 233µW
VOUT
0V
Cout
=470µF
Preset output voltage
19
A P P L I C A T I O N
3.6
N O T E
Single crystal silicon solar cell -2- (for MB39C831)
Table 3-7
Generator
Solar
Characteristics of single crystal silicone solar cell -2Size
Vmax
Imax
[mm]
[V]
[mA]
80×70
1.5
500
Type
Single
crystal Si
Power generation
condition
capability [µW]
50000[lx]
1706 [µW] (*1)
*1: the value including the MB39C831’s consumption
Figure 3-16
Measured graph using Single crystal silicone solar cell -2Single crystal Si solar cell
5
Vopen = 1.5V, Ishort = 500mA
Voltage [V]
Preset output voltage = 3.3V
Illuminance = 50000lx
4 Cin = 10µF
Cout = 470µF
VOUT
3
3.3V
1.5s
2
1
0
0
2
4
6
10
8
Time [s]
12
14
16
The Cin is excluded from the energy calculation because the input voltage (VDD) is not stable in the start-up
and the stored energy is very small.
①Charging energy in Cout
Chargeing energy[μJ] =
1
1
× Cout × (VOUT 2 ) = × 470[μF] × 3.3[V]2 = 2559[μJ]
2
2
②Charging time in Cout (measured value)
Time for charging[s] = 1.5 [s]
1
2
③Power generation capability
Power generation capability[μW] = Charging energy[μJ] ÷ Charging time [s] =
Power generation capability[μW] = 2559 [μJ] ÷ 1.5 [s] = 1706 [μW] =
Figure 3-17
1
2
1
2
Block diagram with single crystal silicone solar cell -2-
Light(50000[lx])
VDD
Single Crystal Si
Solar Cell
80mm×70mm
Vmax = 1.5V
Imax = 500 mA
VDD : VDD input voltage
20
CONFIDENTIAL
VOUT=3.3V 1706µW
Boost
DC/DC
MB39C831
VDD
0V
Cin
=10µF
VOUT
:
VOUT
0V
Cout
=470µF
Preset output voltage
AN405-00001-1v0-E, July 18, 2014
A P P L I C A T I O N
3.7
N O T E
Peltier (for MB39C831)
Peltier elements provide relatively large amount energy upon being given temperature difference. However,
they do not supply high voltage. The peltier element shown in Table 3-8 supplies up to 0.352V. To meet the
minimum start-up input voltage of MB39C831, use the peltier elements connected in series.
Table 3-8
Generator
Type
Peltier
---
Peltier
---
Characteristics of Peltier
Size
Vmax
Imax
[mm]
[V]
[mA]
0.234 -
0.077 -
0.352
0.117
10×10
0.468 -
0.077 -
(2 series)
0.704
0.117
10×10
Power generation
condition
capability [µW]
ΔT=30℃
Larger than 22000 [µW] (*1)
ΔT=30℃
Larger than 44000 [µW] (*1)
*1: the value from a peltier’s datasheet
Figure 3-18
Heat (ΔT=30℃)
Block diagram with Peltier
Heat (ΔT=30℃)
44000µW
Peltier
10mm×10mm
0.234V
to
0.352V
Peltier
10mm×10mm
VDD
Boost
DC/DC
0.468V
to
0.704V
MB39C831
VDD
0V
VOUT=3.3V
VOUT
Cin
=10µF
0V
Cout
=470µF
Efficiency=70%
VDD : VDD input voltage
July 18, 2014, AN405-00001-1v0-E
CONFIDENTIAL
VOUT
:
Preset output voltage
21
A P P L I C A T I O N
N O T E
AN405-00001-1v0-E
Spansion  Application Note
Energy Calculation For Energy Harvesting
APPLICATION NOTE
July 2014 Rev. 1.0
Published
Edited
22
CONFIDENTIAL
Spansion Inc.
Communications
AN405-00001-1v0-E, July 18, 2014
A P P L I C A T I O N
N O T E
Colophon
The products described in this document are designed, developed and manufactured as contemplated for general use,
including without limitation, ordinary industrial use, general office use, personal use, and household use, but are not
designed, developed and manufactured as contemplated (1) for any use that includes fatal risks or dangers that, unless
extremely high safety is secured, could have a serious effect to the public, and could lead directly to death, personal injury,
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chance of failure is intolerable (i.e., submersible repeater and artificial satellite). Please note that Spansion will not be liable
to you and/or any third party for any claims or damages arising in connection with above-mentioned uses of the products.
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July 18, 2014, AN405-00001-1v0-E
CONFIDENTIAL
23