Cirrus Logic AN364 User Manual

AN364
Application Note
Design Guide for a CS1610 and CS1611
Dimmer-Compatible SSL Circuit

1 Overview of the CS1610/11

The CS1610/11 integrates a critical conduction mode (CRM) boost converter that provides power factor correction and dimmer compatibility with a constant output current, quasi-resonant second stage. An adaptive dimmer compatibility algorithm controls the boost stage and dimmer compatibility operation mode to enable flicker-free operation to 2% output current with leading-edge, trailing-edge, and digital dimmers (dimmers with an integrated power supply).

1.1 Features

Best-in-Class Dimmer Compatibility
- Leading-edge (TRIAC) Dimmers
- Trailing-edge Dimmers
- Digital Dimmers (with Integrated Power Supply)
Up to 90% Efficiency
Flicker-free Dimming
0% Minimum Dimming Level
Quasi-resonant Second Stage with Constant-current Output
- Flyback for 1610/ 11
Fast Startup
Tight LED Current Regulation: Better than ±5%
Primary-side Regulation (PSR)
>0.9 Power Factor
IEC-61000-3-2 Compliant
Soft Start
Protections:
- Output Open/Short
- Current-sense Resistor Open /Short
- External Overtemperature Using NTC
Cirrus Logic, Inc.
http://www.cirrus.com
Copyright Cirrus Logic, Inc. 2012
(All Rights Reserved)
AUG’12
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Contacting Cirrus Logic Support
For all product questions and inquiries contact a Cirrus Logic Sales Representative. To find the one nearest to you go to www.cirrus.com
IMPORTANT NOTICE
Cirrus Logic, Inc. and its subsidiaries ("Cirrus") believe that the information contained in this document is accurate and reliable. However, the information is subject to change without notice and is provided "AS IS" without warranty of any kind (express or implied). Customers are advised to obtain the latest version of relevant information to verify, before placing orders, that information being relied on is current and complete. All products are sold subject to the terms and conditions of sale supplied at the time of order acknowledgment, including those pertaining to warranty, indemnification, and limitation of liability. No responsibility is assumed by Cirrus for the use of this information, including use of this information as the basis for manufacture or sale of any items, or for infringement of patents or other rights of third parties. This document is the property of Cirrus and by furnishing this information, Cirrus grants no license, express or implied under any patents, mask work rights, copyrights, trademarks, trade secrets or other intellectual property rights. Cirrus owns the copyrights associated with the information contained herein and gives consent for copies to be made of the information only for use within your organization with respect to Cirrus integrated circuits or other products of Cirrus. This con­sent does not extend to other copying such as copying for general distribution, advertising or promotional purposes, or for creating any work for resale.
CERTAIN APPLICATIONS USING SEMICONDUCTOR PRODUCTS MAY INVOLVE POTENTIAL RISKS OF DEATH, PERSONAL INJURY, OR SEVERE PROP­ERTY OR ENVIRONMENTAL DAMAGE ("CRITICAL APPLICATIONS"). CIRRUS PRODUCTS ARE NOT DESIGNED, AUTHORIZED OR WARRANTED FOR USE IN PRODUCTS SURGICALLY IMPLANTED INTO THE BODY, AUTOMOTIVE SAFETY OR SECURITY DEVICES, LIFE SUPPORT PRODUCTS OR OTHER CRITICAL APPLICATIONS. INCLUSION OF CIRRUS PRODUCTS IN SUCH APPLICATIONS IS UNDERSTOOD TO BE FULLY AT THE CUSTOMER'S RISK AND CIRRUS DISCLAIMS AND MAKES NO WARRANTY, EXPRESS, STATUTORY OR IMPLIED, INCLUDING THE IMPLIED WARRANTIES OF MERCHANT­ABILITY AND FITNESS FOR PARTICULAR PURPOSE, WITH REGARD TO ANY CIRRUS PRODUCT THAT IS USED IN SUCH A MANNER. IF THE CUSTOMER OR CUSTOMER'S CUSTOMER USES OR PERMITS THE USE OF CIRRUS PRODUCTS IN CRITICAL APPLICATIONS, CUSTOMER AGREES, BY SUCH USE, TO FULLY INDEMNIFY CIRRUS, ITS OFFICERS, DIRECTORS, EMPLOYEES, DISTRIBUTORS AND OTHER AGENTS FROM ANY AND ALL LIABILITY, IN­CLUDING ATTORNEYS' FEES AND COSTS, THAT MAY RESULT FROM OR ARISE IN CONNECTION WITH THESE USES.
Cirrus Logic, Cirrus, the Cirrus Logic logo designs, EXL Core, the EXL Core logo design, TruDim, and the TruDim logo design are trademarks of Cirrus Logic, Inc. All other brand and product names in this document may be trademarks or service marks of their respective owners.
IMPORTANT SAFETY INSTRUCTIONS
Read and follow all safety instructions prior to using this demonstration board.
This Engineering Evaluation Unit or Demonstration Board must only be used for assessing IC performance in a laboratory setting. This product is not intended for any other use or incorporation into products for sale.
This product must only be used by qualified technicians or professionals who are trained in the safety procedures associated with the use of demonstration boards.
Risk of Electric Shock
The direct connection to the AC power line and the open and unprotected boards present a serious risk of electric shock and can cause serious injury or death. Extreme caution needs to be exercised while handling this board.
Avoid contact with the exposed conductor or terminals of components on the board. High voltage is present on exposed conductor and it may be present on terminals of any components directly or indirectly connected to the AC line.
Dangerous voltages and/or currents may be internally generated and accessible at various points across the board.
Charged capacitors store high voltage, even after the circuit has been disconnected from the AC line.
Make sure that the power source is off before wiring any connection. Make sure that all connectors are well
connected before the power source is on.
Follow all laboratory safety procedures established by your employer and relevant safety regulations and guidelines, such as the ones listed under, OSHA General Industry Regulations - Subpart S and NFPA 70E.
Suitable eye protection must be worn when working with or around demonstration boards. Always
comply with your employer’s policies regarding the use of personal protective equipment.
All components and metallic parts may be extremely hot to touch when electrically active.
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2 Introduction

This application note is a guide to designing a Solid State Lighting (SSL) LED lamp circuit using Cirrus Logic's CS1610/11. The first half of the document presents a step-by-step design procedure for calculating the required components for each stage of the system. The second half of the document supports the design effort by showing an example of a CS1611 design. The CS1611 example will be based on the Cirrus Logic CRD1611-8W reference design. See the CS1610/11/12/13 TRIAC Dimmable LED Driver IC data sheet for more details about the CS1610/11 IC. See the CRD1610-8W 8 Watt Reference Design and CRD1611-8W 8 Watt Reference Design data sheets for more details regarding the reference design.

2.1 Definition of Symbols

Symbol Description
F
sw
TT Switching period
T1 Primary FET ‘ON’ time
T2 Secondary rectifier diode conduction time
T3 Time when the FET and diode are OFF
D Duty ratio (T1/TT)
V
Reflected
V
CLAMP
I
PK(FB)
R
FBGAIN
R
Sense
I
PK(BST)
L
P
L
BST
V
BST
N
V
OUT
P
OUT
Power stage efficiency
Switching frequency
Voltage across secondary winding reflected onto primary
Primary clamping voltage above boost output voltage (V
Peak current in primary-side FET
A resistor used to program the switching period TT
Primary current sense resistor
Maximum boost inductor current
Flyback transformer primary inductance
Boost inductance
Boost output voltage
Flyback transformer turns ratio N
Secondary output voltage DC = the LED string supply voltage
Load power = Power to the LED string
P/NS
BST
)

2.2 Definition of Acronyms

Acronym Description
PFC Power Factor Correction
OVP Overvoltage Protection
eOTP External Overtemperature Protection
OCP Overcurrent Protection
iOTP Internal Overtemperature Protection
OLP Open Loop Protection
LED Light Emitting Diode
TXF Transformer
TRIAC
SSL
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TRIode for Alternating Current, which is an electronic component that can conduct current in either direction when it is triggered. It is formally called a bidirectional triode thyristor.
Solid State Lighting. Refers to a type of lighting that uses semiconductor LEDs as a source of illumination rather than electrical filaments, plasma, or gas.
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T1
D3
LED +
LED -
Z2
L1
L3
R8
R11
R3
R7
R1
R2
Q3
L2
Z1
C2
D7
D6
Q1
R17R13
Q2
D5
R18
NTC
R14
R15
R22
R23
Q4
R21
R19
R9
BR1
F1
R12
D8
R4
CS1610 /11
FBGAIN
IAC
FBAUX
BSTOUT
GNDSGNDIPK
CLAMP
GD
FBSEN SE
eOTP
VDD
SOURCE
CY
D2
L
N
AC Main s
D4
R10
R16
R6
R20
R5
D1
BSTAUX
R24
Boost
Gate Bias
Steady State
Supply
Active Clamp
FlybackEMI
C11
C8 C10
C9
C7
C6
C5
C4
C3
C1
C12
Figure 1. Block Diagram of CS1610/11 Design

3 Design Process

The design process for a two-stage power converter system can be partitioned into six circuit blocks (see Figure 1). The AC line voltage is passed through an electromagnetic interference (EMI) filter to suppress conducted interfer­ence found on the power line. The output of the EMI filter is then converted to the desired DC output by a boost­flyback converter. The power converter system includes the Gate Bias, Steady State Supply, and Active Clamp sup­port circuitry.

3.1 Operating Parameters

To initiate the design procedure, a set of operating parameters are required. Operating parameters required for the analytical process are outlined in the table below. Parameters critical to the overall design, but not specifically addressed in this document, include: EMI compliance, efficiency, form factor, layout, and operating temperature.
Output Power
AC line Input Voltage
Output Voltage
Load Current
Parameters Symbol
Maximum Switching Frequency*
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* Increasing Fsw may reduce the size of the magnetics but increase switching losses in the FET.
P
OUT
V
IN
V
OUT
I
OUT
F
sw(max)

3.2 Overview of Design Steps

The CS1610/11 LED driver IC controls a power converter system that has two distinct power conversion stages. The IC requires supporting circuitry to provide a steady state power supply with gate bias, a clamp circuit, and EMI filtering. The recommended design process is outlined below:
1. Start with the flyback stage.
2. Design for full power at minimum V operating parameters.
3. Optimize the flyback stage through validation and design iteration.
4. Base the boost stage design on the power requirement of the flyback stage.
5. Start the boost stage design in No-dimmer Mode.
6. Determine the peak current in the boost inductor, I
7. Determine a boost inductance, L Consider the impact on the EMI.
8. Pick the boost FET based on peak current ratings.
9. Choose the power supply components.
10.Complete the non-power-converting circuitry: ZCD, OVP, eOTP, Clamp Circuit, Charge Pumps, and Bias Circuits.
11. Design the EMI filter.
12.Lay out the PCB.
. Note that any design may require design trade-offs for different
BST
PK(BST)
, that adjusts the switching frequency within the defined range.
BST
.
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The flyback stage design is carried out at the full brightness (full load) point. To achieve an optimal solution, several iterations of the design process may be required. The EMI filter is particularly critical because there is a small degree of freedom in selecting the EMI component values that meet the requirements below:
Comply with EMI regulations
Achieve compatibility with the largest variety of dimmers
Smooth dimming, no flicker with a variable number of identical lamps controlled by one dimmer
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3.3 Flyback Stage Design

Flyback Specification
Determine N, Fsw,
V
Refle cted
, and V
CLAMP
Estimate T3
Calculate TT
fb
Calculate R
Sense
,
R
FBG AIN
, and Primary
Inductance
R
Sense,RFBG AIN
Fit?
Yes
No
Calculate T1,
T2, and I
PK(FB)
Calculate RMS Current
and Output Capacitor
Transformer Core
Steps for the Flyback Design
1. Set boost output voltage V
BST
.
2. Select a MOSFET that aligns with the quality standards of the designer’s company.
3. Determine the transformer turns ratio from the
V
BST
, FET
voltage, and reflected voltage V
Reflected
.
4. Use the nominal switching frequency and an initial estimate for time T3 to determine the value of time TT at full brightness.
5. Use V
BST
, TT, and V
Reflected
to determine time T1 and T2.
6. Use time T2 and TT, turns ratio N and load current to determine the value of peak primary current I
PK(FB)
.
7. Use I
PK(FB)
to determine R
Sense
.
8. Calculate the primary side inductance using time T1.
9. Calculate flyback gain resistor R
FBGAIN
using full load conditions. Ensure linearity of the load versus the dim curve.
10. Calculate primary and secondary RMS currents using I
PK(FB)
and duty cycle.
11. Select an output capacitor.
12. Determine the flyback transformer specifications.
13. Determine if the flyback transformer fits into specified form factor after designing and constructing flyback transformer. Repeat steps 3 to 12 until form factor criteria is met.
14. Refine the circuit using the final flyback transformer design.
15. Validate that the system meets the operating criteria.
Figure 2 illustrates the steps for designing the flyback stage.
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Figure 2. Flyback Stage Design
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V
Drain maxVBST maxVCLAMP max
+=
[Eq. 1]
V
OvershootVCLAMPVReflecteed
=
[Eq. 2]
Overshoot is a brief condition above V
Reflected
, required to quickly dissipate the energy stored in the transformer leakage inductance.
During this time, the primary current is kept from transferring to the secondary, siphoning energy from the load to the clamp zener (snubber).
Figure 3. FET Breakdown Voltage
V
Margin
V
CLAMP
V
BST
V
Overshoot
V
Reflected
ET Breakdown Voltage Rating
Clamp
Voltage
Boost Output
Voltage
Margin
Reflected Voltage
Overshoot Voltage
Step 1) Select a Value for Boost Output Voltage
The value of the boost output voltage, V The maximum V
voltage, V
BST
BST(max)
requirement within economical constraints.
V
is determined by an internal parameter and changes slightly depending on the type of dimmer detected.
BST
With sense resistors R7, R8, R14, and R15 set to 1.5M, the resulting V system. For a 120V system, sense resistors R7, R8, R14, and R15 are set to 750k each, and the resulting V
is approximately 200V. V
BST
each half line-cycle. V
droops to its lowest value towards the end of each half line-cycle until the boosting
BST
is regulated by charging the boost output capacitor to its nominal value
BST
process starts again in the next half line-cycle.
Step 2) Select an Appropriate FET
Determine the FET breakdown voltage, V voltage, V
Drain(max)
, is calculated using Equation 1.
The ringing associated with the transformer leakage inductance usually does not have enough energy to cause a destructive avalanche breakdown. Voltages closely approaching the FET breakdown voltage are acceptable.
Ideally, V
Reflected
should have nearly the same value as V duty cycle optimizes the transformer efficiency. Alternatively, V to rapidly discharge the energy stored in the transformer leakage inductance.
The FET breakdown voltage is constrained by cost and performance. A compromise must be reached in partitioning voltage between V divide V
CLAMP
into V
Reflected
, V
BST
CLAMP
and a reasonable overshoot voltage portion, V
The losses caused by the leakage inductance are inversely proportional to V Equation 2.
, must be greater than the maximum input AC line voltage peak.
BST
, should be kept as low as possible to help maintain the FET breakdown
is approximately 405V for a 230V
BST
Breakdown
, and V
, and reflected voltage, V
because operating the transformer near 50%
BST
CLAMP
. A second compromise will then determine how to
Margin
Reflected
should be much greater than V
Overshoot
. The FET maximum drain
.
Overshoot
, which is determined by
Reflected
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F
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V
Breakdown
V
BSTVReflected
V+
CLAMP
V
Reflected
V
Minarg
++=
[Eq. 3]
N
V
Reflected
V
OUT max
----------------------------=
[Eq. 4]
T1 T2+
1
F
sw
---------


T3=
[Eq. 5]
T1 T2
-------
V
Reflected
V
BST
--------------------------=
[Eq. 6]
For optimum efficiency, the increase in transformer losses (created by an uneven duty cycle) must balance the reduction of the losses caused by discharging the leakage inductance (obtained by increasing the overshoot voltage). Equation 3 is used to balance all voltages contributing to the FET voltage drain and source.
where
V
Overshoot
Step 3) Determine the Flyback Transformer Turns Ratio
Select a turns ratio based on the output voltage, V
where
V
OUT(max)
Step 4) Select the Full Brightness Switching Frequency
The CS1611 maximum switching frequency is 200kHz. Test results indicate that optimal performance is obtained in the range of 75kHz to 120kHz. Higher frequencies allow the use of smaller magnetics, but switching losses increase. Transformer size versus switching frequency is limited by designs that require isolation. Selecting too low a full brightness switching frequency risks impairing dimmer compatibility while also allowing the minimum frequency to drop into the audible range.
From the full brightness frequency, determine the value of (T1 +T2) using Equation 5.
= V
CLAMP
- V
Reflected
OUT
, and V
= the maximum LED string forward voltage V
Reflected
at full current plus the rectifying diode voltage VF.
OUT
using Equation 4.
where
T3 is 1/2 the transformer resonant period
The transformer primary inductance resonates with the total parasitic capacitance of the drain node. For initial calculations, T3 is estimated as 1s and must be measured for final accuracy.
Step 5) Determine the Flyback Nominal Timing T1 and T2
From the reflected voltage and the turns ratio, determine T1 and T2. Equation 6 ensures zero DC voltage across the transformer T1 magnetizing inductance.
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Figure 4 illustrates the switching frequency used in the system design.
t
i(t)
T1 T2
TT
No Curr ent
T3
Peak Primary Current, I
PK(FB)
Primar y Current
Secondary
Current
Figure 4. Timing Diagram of T1, T2, T3, and TT
T1
1
F
sw
--------- T 3
V
Reflected
V
ReflectedVBST
+
----------------------------------------------------
=
[Eq. 7]
T2
1
F
sw
--------- T 3
V
BST
V
ReflectedVBST
+
----------------------------------------------------
=
[Eq. 8]
I
PK FB
2P
OUT max
TT
fb
V
BST
T1fb
----------------------------------------------
=
[Eq. 9]
R
Sense
1.4V
I
PK FB
------------------=
[Eq. 10]
L
P
V
BST
T1
I
PK FB
---------------------------
=
[Eq. 11]
Solve for T1 and T2 using Equation 7 and Equation 8:
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Period T1 is limited to a maximum duration of 8.8s by the IC algorithm. Verify that period T1 at full power is less that 7.8s, leaving sufficient time for a probe cycle, which requires a slightly longer T1 period.
Step 6) Calculate Peak Current on the Flyback Primary-side
Calculate I
using Equation 9:
PK(FB)
where
TT
= switching period at full brightness (full load condition)
fb
T1
= period T1 at full brightness (full load condition)
fb
Step 7) Calculate R
Calculate sense resistor R
Sense
Sense
(R23)
(R23) for flyback using Equation 10:
where
R23 = R
Sense
in
Step 8) Calculate the Flyback Primary-side Inductance
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