Micronote 1815 - DRF Series Design Guide (2.56 MB)

Application Note 1815
May 2013
DRF Series Design Guide
George J. Krausse
Microsemi Corp RF Power Products Group
405 SW Columbia St.
Bend, OR 97702 USA
[email protected]
Dick Frey
Microsemi Corp RF Power Products Group
405 SW Columbia St.
Bend, OR 97702 USA
[email protected]
Introduction
In this Design Guide we will detail the design process involved when using the DRF Series of devices and their
performance. As we move through this document it will be necessary to clearly define and explain multiple
technical points so that we have a mutual understanding of the key issues and how to address them. The DRF Series
is based on a Flangeless Mechanical design illustrated in Figure 1. All of these devices incorporate at least one
driver die, the DRF100; all others have one or two driver die and one or two MOSFET devices.
17
1uF
1uF
1uF
DRF100
Microsemi
1uF
1uF
1uF
5600
Microsemi
DRF1201
5600
5600
5600
5600
5600
5600
5600
15
16
Microsemi
DRF1300
Microsemi
DRF1400
1
2
3
4
5
6
7
8
9
10 11 12 13
14
DRF100
DRF1200
DRF1300
DRF1400
Driver Test Device
and Die Qualification
package
Single Ended
Push-Pull
Half-Bridge
Driver and 1 HV
MOSFET
2 Driver and 2 HV
MOSFETs
2 Driver and 2 HV
MOSFETs
Figure 1. DRF Series Devices
The DRF100 was the platform used to develop and qualify the RF Driver IC. Understanding the design, layout and
function of the DRF100 is necessary to appropriately understand the DRF family of devices. The DRF devices are
capable of multiple Kilowatts at RF Frequencies of < 2MHz to > 30MHz; the DRF1200 Series 1KW; the DRF1300
Series 1-2KW; and the DRF1400 Series 2-3KW.
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Application Note 1815
May 2013
DRF100
C1
U1
Figure 2. Simplified DRF100 Circuit Diagram
FN Invert
Non-Invert
IN
Output
FUNCTION
High
High
High
Non-Inverting
High
Low
Low
Non-Inverting
Low
High
Low
Inverting
Low
Low
High
Table 1
Inverting
The simplified DRF100 Circuit Diagram is
illustrated in Figure 2 above. By including the high speed by-pass capacitor, the contribution to the internal parasitic
loop inductance of the driver output is greatly reduced. This low parasitic approach, coupled with the Schmitt
Trigger input (pin 4), Kelvin Signal Ground (pin 5) and the Anti-Ring Function, provide improved stability and
control. The IN pin (4) is applied to a Schmitt Trigger. The signal is then applied to the intermediate drivers and
level shifters; this section contains proprietary circuitry designed specifically for ring abatement. The P channel and
N channel power drivers provide the high current to the Output (pin 9). Table 1 is the truth table for the DRF100.
Electrical
MOSFET Model and Parasitics
The DRF100 is a High-Speed Power RF MOSFET driver. It is intended to drive the gate of a power RF MOSFET
with ≥ 3nF gate capacitance to 15V at frequencies up to 30MHz. It can produce output currents ≥ 8A RMS, while
dissipating 60W. The Driver output can be configured as Inverting or Non-Inverting.
To understand the driver and its integration into a power RF package with a power MOSFET, it will be useful to
review the important design considerations in that process. The Driver circuit model is illustrated in Figure 3.
V1
R1
.15
1
L1
.15n
2
V3
3
C1
2.5n
V1
4
R2
.35
R1 represents the on resistance of the internal MOSFETs in the output
section of the Driver. This parameter is driven by driver performance
requirements. L1 accounts for Loop Inductance in the driver output. C1
models the effective output capacitance of the driver and R2 is the ESR of
C1. V1 provides the control signal.
(Node 0)
Figure 3. Driver Circuit Model
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Application Note 1815
May 2013
CNET = CISS + CRSS (
∆VDS − ∆VGS
)
∆VGS
Miller Capacitance
Negative Feedback
LD is a Small value
and Most Often has
Little Effect on Device
Performance
Source Inductance
Negative Feedback
LG and RG Limit Bandwidth
VLS = LS ×
di
dt
MOSFET MODEL
Figure 4. Negative Feedback Terms
There are two significant Negative Feedback Terms that affect MOSFET performance, the DRF100, and all the
DRF devices. They are the effect of Miller Capacitance (CNET) and Source Lead Inductance (VLS). Figure 4
shows the location of these two Negative Feedback Terms and the equations that describe their effects on MOSFETs
and the DRF Series Devices. We have little control over the CNET term; however we can ensure, by design, that the
Driver IC has sufficient output voltage swing and power margin to drive all the RF MOSFETs we may choose to
use. In addition we have taken great care to minimize the VLS and LG terms in all of the DRF Devices. LG and RG
impact Bandwidth and switching speed. LD in most DRF devices is between 5 and 15nH in the Drain circuit. This
has very little effect on most circuits operating below 50MHz.
Referring to Figure 4, as the current rises in the MOSFET at turn on, the Voltage at Node 3, MOSFET Source (Die)
also rises. This is a negative feedback term to the Gate Drive at Node 2. The magnitude is driven by the inset
equation for (VLS).
At the same time, the voltage at the Drain (Die), Node 1, falls. This falling voltage produces a negative feedback
term to the Gate (Die) Node. The magnitude of this “Miller Feedback” is given by the inset formula (CNET). In short
it presents an increase in effective input capacitance which is voltage and time dependent. The time dependency is
determined by the rate of change of the drain voltage.
Miller Capacitance is a function of Silicon Die design - the bigger the die, the larger the Miller effect. The Source,
Gate and Drain lead inductance are byproducts of the geometry of the package design.
As we integrate Figure 3 and Figure 4 into a Hybrid, we cross from the discreet components, as illustrated in Figure
4, to a multi-chip module design. In that process it is important to minimize all parameters that will limit
performance of the hybrid.
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Application Note 1815
May 2013
Loop Inductance
LOAD
This section discusses how package inductance and circuit stray
inductance are formed, and how to minimize them.
The parasitic loop for an RF Output is schematically illustrated in
Figure 5. The Source V1 is the square wave output to the RF Network
and the load. The mechanical geometry forms a current loop that is
very critical to Circuit Operation. The smaller the loop, the lower the
stray inductance.
W
+
-
Figure 5. Current Loop in an RF Loop
Δ B Field Excluded from metal plane
Cross
Sectional
Area
Δ Current
V1
B Field can only form in the
open area, A.
W
L≈
Δ B Field
B Field
Figure 6. Loop Inductance
µo N2 A
W
Current flowing in the metal
sheet
Figure 7. Loop Inductance
Figures 6 and 7 illustrate the output loop inductance of an RF Power Output Stage. From Equation 1 we see that the
stray inductive term is directly proportional to the Cross Sectional Area. Therefore, if we minimize the Cross
Sectional Area we will reduce the loop inductance proportionally. In addition, if we increase the width W we will
also reduce the Loop Inductance. See the equation below.
Equation 1
μ N 2A
L= 0
W
Where:
L= Inductance, H
µ0 = Permeability of Free Space, 1.26 x 10-6 H m-1
N2 = (Number of turns)2 = 1
A = Cross Sectional Area, m2
W = Width, m
Equation 1 shown at the left is simplified but accurate
enough for our discussion. Looking at this equation, we
see the only two terms that we can change are terms A
and W. See Equation 2. In the process of Printed Circuit
design it is essential that A/W is minimized in order to
optimize circuit Performance.
Equation 2
L:
A
W
For the RF Output Section this loop inductance is a very critical, geometry and layout-driven, parameter. The
smaller the better. This lower inductance drives the ring frequency higher with lower amplitude. If the loop
inductance is too large ringing on the top of the Drain voltage waveform can have severe consequences, such as HV
breakdown, reduced power output, higher harmonics and loss of stability. The PCB layout must incorporate this
understanding. This will be discussed in more detail later in the Hybrid section and in the Push-Pull and Half-Bridge
sections.
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Application Note 1815
May 2013
Mechanical
The DRF family of RF Hybrid Devices incorporates one or two RF Driver Integrated Circuits and one or two RF
Power MOSFETs. The DRF Series devices are designed to allow their user to focus on the Output RF elements in
the design with little need to address the RF Driver. For this discussion we will start with the Flangeless Discrete
Devices. Figure 8 illustrates the construction of the Legacy Devices and the New Flangeless devices. The principal
physical difference between the two, is the Copper Tungsten Flange, used on legacy devices. This leads to a
difference in the Thermal Impedance, Power Cycle Capability as well as Electrical and RF performance. There is
also the cost differential between the two technologies.
Mounting Holes are
located in the Lid
Fiberglass reinforced
Plastic Lid. Ultem
2300
Ceramic Lid
RF Die
.010in. gold
plated Kovar
lead frame
.005in. Copper
gold plated
lead frame
RF Die
BeO
Substrate
Refractory Lead
Frame Attach
BeO
Substrate
Copper
Tungsten Flange
Refractory
Substrate
Attach
Mounting Holes
are located in
the Flange
Legacy Device
Flangeless Device
Figure 8. Legacy and New Flangeless Construction
4-40 Screw 4-6 in./lb
Split Ring /
Belleville Washer
RF Die
Compressive
Force
.005in. Boss
BeO SUBSTRATE
HEAT SINK
Thermal Compound
Device Lead
Figure 9. Flangeless Power Device
Compression
Lid Ultem 2300
In Figure 8 we see both the
Flangeless and the legacy Flanged
device. There are only three
obvious components that they
share: the lead frame, the die and
the substrate. The compression
mechanics of the package design
are less obvious. Referring to
Figure 9, when the two 4-40 screws
are tightened, the 0.005in. Bosses
at the two ends of the package lid,
force the package to flex.
These Bosses contact the heat sink first. As torque is applied to the mounting screws, the lid begins to flex and in so
doing applies a constant pressure to the substrate, pressing it hard onto the heat sink. The two green arrows in Figure
9 illustrate this pressure. The side walls of the plastic lid have been removed in this sectioned view of the package.
The side walls are thick and tall so that the pressure applied along the complete perimeter of the BeO substrate is
close to the same. The lid is constructed with a fiberglass reinforced plastic, Ultem 2300, an exceedingly strong high
temperature material.
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Application Note 1815
May 2013
Thermal
Figure 10 illustrates the VRF154 Thermal Profile and Figure 11 the MRF154, a flanged device with similar
mechanical construction. The Thermal Profile illustrates one of the differences between the Flangeless and the
Flanged device. They both start at 25°C and end at 175°C, however it is the point-by-point delta in these two plots
as they move between limits that illustrates the different in the specific heat of the packages.
225
1 Die
2 Solder
3 Metal 1
4 BeO
5 Metal 2
6 Thermal Compound
7 Heat Sink Surface
200
175
150
Tj
225
Chart Legend
125
200
175
150
Tj
125
100
100
75
75
50
50
25
0
1
2
3
4
5
6
7
8
25
j
DELTA T+ THS
( TJ − THS)
PD:=
Rθ JHS
3
PD = 1. 782 × 10
RθJC = 0. 052
PD:=
0
1
4
j
DELTA T+ THS
( TJ − THS)
Rθ JHS
2
3
VRF154
Figure 12. VRF154
VRF154
RθJC =.06
RθJHS =.193
PD = 908W
PDC = 1.23KW
6
3
PD = 1.601 × 10
Rθ JHS= 0. 084
Figure 10. VRF154 Thermal Profile
5
7
8
RθJC = 0. 036
Rθ JHS= 0. 094
Figure 11. MRF154 Thermal Profile
MRF154
MRF154
RθJC =.130
RθJHS =.199
PD = 880W
PDC = 1.28KW
Figure 13. MRF154
The most important point is that the new VRF154 Flangeless Design, Figure 12, and the MRF154 legacy design,
Figure 13, are very similar in thermal performance. In electrical performance they are, for all practical purposes,
identical. As was true for the previous section, the cost is different. For the VRF154 and the MRF154, this
difference is substantial.
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Application Note 1815
May 2013
Power Calculations
These calculations are for the Driver portion of the DRF family of devices. The driver power consumption is low but
not insignificant. This necessitates a design step for the proper operation of any of the DRF Series Hybrids,
DRF12XX, DRF13XX and DRF14XX.
Driver Power Loss
P = C NET × VGS 2 × f
Miller Capacitance
CNET must include the driver Coss and the CIss , Crss of the MOSFET used in the Hybrid. This is given in the Data
Sheet. In the case of the DRF100, use only the COSS of the Driver and the load power.


 ΔV − ΔVGS   
C NET = C ISS(MOSFET) + C RSS(MOSFET)  DS
   + C OSS(DRIVER)
ΔVGS
  



Let:
Driver COSS =2500pF
Driver Power Outputs and Power Grounds
.181in
CISS(MOSFET) = 1890pF (Load to Driver)
CRSS(MOSFET) = 75pF (Load to Driver)
∆VDS = 400V
∆VGS = 15V
Output MOSFETs
.043in
VDD = 15V
f =13.56MHz
RθJSH = 2.53°C/W


 400V − 15V   
C NET = 1890pF + 75pF
   + 2500pF
15V

  


CNET = 1890pF + 1925pF + 2500pF=6315pF
Power Loss in the Driver is:
P = 6315pF × 15 2 × 13.56MHz
P = 19.26W
Driver VDD Current
I DRIVER =
P
19.26W
=
= 1.284A
VDD
15V
Operating Temperature
ΔT = R θJHS × P
Driver signal inputs
Figure 14. Internal Thermal Image of Driver Die
The heat distribution in the Driver Die is illustrated
in Figure 14. As we see the Output MOSFET
Section of the die is the hottest. The balance of the
die generates very little heat. Therefore the DRF100
datasheet uses the 0.181in x 0.043 in. area for the
thermal power dissipation specification. Assuming a
45°C heat sink, the Junction Temperature will be
94°C. This is well below the 150°C rating of the
device.
∆T = 2.53°C/W X 19.26W ≈ 49°C
For a DRF device, the total Driver Power of 19.26W must be added to the power loss that will be dissipated in
the Power MOSFET(s) during operation. The Heat sink must be designed accordingly.
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Application Note 1815
May 2013
DRF Hybrids
DRF100 Driver Die Operation
R1
.25
+Vdd
1
7
V1
3V
C2
6u
V2
5
A2
INVERTER
R6
1K
18
IN
VCC
VEE
13
C4
3p
D2
1N 4148
A1
XNOR
14
9
15
R5
200
6
3
C1
1p
R4
.12
L1
.1n
25
R7
1K
D1
1N 4148
R3
4000
R2
1800
X3A
54ALS08
X1
PPG100
19
R9
200
22
11
A3
BUFFER
16
X2
MAX9010
R8
.15
X3B
54ALS08
OUT
8
L2
.15n
12
C3
2.5n
10
20
R11
.35
23
4
R10
1000K
X5
PPG100
X4
PPG100
SG
X6
PPG100
21
GND
2
D3
1N 4148
R13
2000K
FN
D4
1N 4148
5
C5
3p
R12
1000K
Figure 15. DRF100 Equivalent SPICE Sub-Circuit Diagram
DRF100 Driver Die Sub Circuit Diagram
The DRF SPICE Sub Circuit Diagram is illustrated in Figure 15 above. X2, the MAX9010 model, is used as the
input comparator. The Switching Speed is a close match to the DRF100 input, however, the Hysteresis has been
altered to more closely model the DRF100 performance. The XOR gate A1 is used to provide the Invert Function of
the FN pin. Inverters A2 and A3 are used to create the Device Delay. Gates X3A and X3B provide the drive for the
differential pair X4 and X5. These two devices provide the drive and signal timing for the Half-Bridge Output
devices X1 and X6. L2, C3 and R11 model the output characteristics of the DRF100. All parameters of the DRF100
Model are accurate with respect to the device performance, with the exception of the DC idle current. The
specification is ≅ 2mA however the model idle current is ≅ 4mA. It should be noted that the SPICE Model of Figure
15 will not function if the Reference Ground is not at DC=0 and dV/dt =0 and the Anti-Ring function is not
modeled.
Power GND
1uF
1uF
1uF
1uF
1uF
1uF
Current Loops
Internal By pass Capacitors
Transparent Case Outline,
Fiberglass reinforced
Ultem 2300
This section is replicated
in all DRF Devices
GN
D
GN
D
OU
T
Q4
Q6
ES
D
ES
D
ES
D
U14
N
OU
T
Q4
Q5
Q6
U11P
U5P
U14P
U5N
U11P
U14P
U11P
U7
U11P
U8
Driver IC
VDD
U5N
U5P
U3
U10P
U2
BeO Substrate
U9
U5P
GND +V FN IN SG +V
GND
U6
U12
FN
P
D
INV
P
D
IN
P
D
SG
U11
N
U11
N
U11
N
U11
N
U10
N
U4P
U4
N
U5P
U5
N
U5N
U1
Gold plated
Copper leads
GN
D
GN
D
Q3
U14P
U14
N
U14
N
VDD
OU
T
OU
T
ES
D
Power GND OUTPUT
ES
D
ES
D
ES
D
VDD
VDD
U12
Kelvin Signal Ground
Figure 16. DRF100 Internal View
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Application Note 1815
May 2013
Referring to the discussion of inductive loops on Page 4, the Internal High Speed bypassing capacitors and the
Coplanar Current Loop are illustrated in Figure 16. The symmetry of the Coplanar Loop, minimizing the area and
the opposing currents, provides for a reduction in apparent inductance. Locating the internal High-Speed By-Passing
within this loop enables the fast turn on and off performance of the driver. Moving the capacitors outside of the
package would severely compromise the switching speed by increasing the Loop Inductance as previously stated.
We will see that reducing the cross-sectional area, balanced and opposed current flows via circuit symmetry are
necessary to reduce inductive strays and therefore increase the system operating RF Frequency.
DRF100 Test Circuit
The Test Circuit for the DRF100 is shown in Figure 17 and the Fixture is shown in Figure 4.
In Figure 17 we see that both VDD pins 2 and 6
are heavily bypassed. This is recommended for
optimum operation performance and stability.
The FN pin can be bypassed for increased
noise immunity in the Non-Inverting mode. In
the Inverting Mode this is not necessary. The
control signal is applied to the IN pin via a
BNC connector. This signal is terminated in
50Ω for the test circuit, however this input can
be terminated in 500Ω to 1KΩ depending on
circuit requirements and noise immunity
requirements.
Figure 17. DRF100 Test Circuit
PCB Cutout for DRF100 Mounting, see notes on heat sinking
+15V
+15V RTN
Load , RL=50Ω and CL=3nF
User Configurable Area
Figure 18 is an illustration of the
DRF100 Evaluation Board. +15V,
the VDD supply and the Ground
for the supply are shown as red and
green banana connectors. A large
portion of the PCB, red dashed
rectangle, was allocated for circuit
development. The PCB is a Full
Ground Plane layout. This platform
was used in the design and
parameter extraction of the device.
R1
C1-3
CL
BNC
C4
R2
Microsemi
DRF100
RL
C5-7
R3
Note By-Passing
Capacitors
location near +V
Inputs
Both Outside traces
are a ground
connection.
All traces within the Blue
dashed line are isolated
from ground.
Figure 18. DRF100 Test Board
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Application Note 1815
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The suggested PCB layout for the DRF100 is illustrated in Figure 18. The external by-passing for the DRF100 Vdd
inputs are placed symmetrically on the PCB, and illustrated in the red circle. All the supporting driver components
must be kept in a close group as illustrated in the Figure. No power DC or RF traces should pass through this area
and no control or low voltage power for the DRF100 should pass through the high power RF section.
DRF1200
The DRF1200 is the second in the DRF Series of devices. In the DRF1200 the RF Driver die, used in the DRF100,
is combined with a High Voltage RF Power MOSFET. This combination gives the designer an RF Hybrid which
allows the control of ≈ 1KW of RF power with ≈ 10W of RF drive (see power calculations section). This is a power
gain of ≈ 20db. Figure 19 shows the circuit diagram of the DRF1200.
FN
High
High
Low
Low
U1
IN
High
Low
High
Low
MOSFET
ON
OFF
OFF
ON
Table 2
.
Figure 19. DRF1200 Circuit Diagram
All previous discussions of the DRF100 apply to the input section of the DRF1200. In the following section, the
DRF1200 design and testing guidelines are addressed. Table 2 illustrates the truth diagram for the DRF1200.
Figure 20 is an internal view of the DRF1200.
10
9
SOURCE
GND
8
SOURCE
GND
BeO Substrate .040in. Thick
Low Inductance Output
Loop
DRAIN
Low Inductance Driver Output
Loop (Charge)
Low Inductance Driver Output
Loop (Discharge)
Low Inductive Loop ByPass Capacitors
Transparent Case Outline,
Fiberglass Renforced Ultem2300
1uF
1uF
1uF
1uF
1uF
1uF
Solder Dam
Leads Not To Scale
SOURCE
SOURCE
+V FN IN SG +Vcc
GND
GND
1
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2 3 4 5 6
7
Figure 20. DRF1200 Internal View
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Application Note 1815
May 2013
There are three important features that must be addressed. The first is the Driver CI Output Loop, for the MOSFET
gate charge and discharge, is illustrated in red. Much care has been taken to reduce the magnitude of the inductance
between the Driver and the MOSFET. The lower the value of this stray parameter the higher the operating frequency
will be.
The Loop is composed of two nested loops, one or the right and one on the left. These current loops are magnetically
coupled and form a Coplanar Line. Following the red line on the right from the Tail to the Point of the arrow, during
Turn-On of the MOSFET, the current flow is from the Source and the power ground, through the By-Pass
Capacitors into the Driver IC, then out of the driver IC and into the Gate of the MOSFET. During Turn-Off of the
MOSFET, the currents flow in the opposite direction. During both Turn-On and Turn-Off the two currents are
forced by topology to flow in opposite directions. Given this flow and the level of the coupling between the two
loops, the Inductance is effectively reduced.
The second, the MOSFET Output Loops shown in blue, operate in the same manner, as the Driver Loops.
The third, the compressed layout of components, aids in reducing internal stray inductance.
The combination of these features allows the DRF1200 to have switching speeds of ≈ 5 ns and operate at
frequencies of ≈ 30MHz.
Figure 21 illustrates the schematic diagram of the DRF1200 Test Circuit and Figure 22 the DRF1200 Evaluation
Switching Board.
Figure 21. DRF1200 Test Circuit
In Figure 21, the input circuits of the DRF1200 have the same requirements as the DRF100 and therefore are
identical. Pin 8 and Pin 10 are the power grounds. It should be noted that Pins 1, 7, 8 and 10 are common points and
connected inside of the DRF1200. The Output Pin 9 is connected to the resistor RL. The value of this resistor is
sized such that when Vds is at Maximum, the Ids will also be at the specified Maximum. This is true for all DRF
Testing.
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Application Note 1815
May 2013
o = One Plated Through Hole
X = 5 Plated Through Holes
Full Ground Plane PCB
GND
+15V
Area for User Circuit
Development
Cutout for Device
Vdd By-Pass
Capacitors 2 Places
R2 R1
X
o
o
o
o
o
o
GND
o
1
X
C11
C10
X
2
200Ω
+VDS
R6
200Ω
C13
C12
XX
MICROSEMI
DRF1200
BNC
R4 R3
o
J2
X
X
Control
Signal input
o
C1
X
3
X
4
C2
J1
o
o
o
o
o
o
o
o
4 Traces for user
Circuit Development
Jumper Connecting By-Pass Capacitors to
Ground, 2 Places
NO CONTROL SIGNAL or LV POWER TRACE TO
THE RIGHT OF THIS LINE
Figure 22. DRF1200 Switching PCB
Figure 22 is the DRF1200 Switching PCB. This layout was used for device characterization. Also illustrated is the
suggested PCB layout for the DRF1200 driver input side.
Spice simulations will be used throughout the text for ease of discussion and as an illustrative tool. All circuits
discussed have been realized in bench hardware, the models include appropriate strays and predict the bench
data with reasonable accuracy.
Figure 23 illustrates the DRF1200 in a Class-E RF Generator circuit (see relevant publications at end of text). The
circuit is a Single-Ended, Non-Linear, fixed Frequency design, capable of generating > 1KW of RF output power
with 12.1W input power, about 20db gain. The power is most commonly controlled by adjusting the DC Supply
(VDs).
Circuit Parameters have been adjusted for the Highest Efficiency and Highest Power Output while limiting the
MOSFETs junction temperature to a maximum of ≈ 100°C and limiting the Drain to Source Margin to a positive
number or zero. These are defined as the Boundary Conditions. This term will be referenced later in the text. All
values shown in the following text were acquired with these constraints. The DRF1200 model in Figure 23 is a
template for all devices in the DRF series.
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Application Note 1815
May 2013
VDs
300
WV1
ARF467 MOSFET Die
used in the DRF1200
4
IV1
*
Matching Network
V4
X1
ARF467FL
DRF1200
L4
.15e-9
V14
V5
L2
5u
5
8
VG
7
V6
6
C4
480p
R4
.1
15
C6
11p
11
R6
.01
R5
.01
IR5
R8
.35
9
2
C5
5p
1
R3
50
C3
710p
L3
690e-9
10
C7
2.5n
WV3
R2
.1
C2
5p
13
R7
.15
V9
C1
129p
*
V3
Simplified Driver IC SPICE Model
Tran Generators = PULSE
WR3
*
Circuit Performance
Vsupply
+300V
Pout
1252W
Pin
1328W
PLoss
76W
Eff
94.3%
Pulse Gate Drive PW=17ns
Ths
45°C
TjX1
91°C
Vds Margin
53V
Drain Z=6Ω
Out Z=50Ω
Table 3
Figure 23. Class-E RF Generator using the DRF1200
Table 3 lists the performance for the RF Generator of Figure 23 which is typical for this topology utilizing the
DRF1200 (see Application Note 1811, DRF1200 13.56MHz Reference Design Kit, Microsemi website).
1 V9
2 V1
16.0
Plot1
V1, V9 in volts
12.0
Figure 24 illustrates the input gate drive at V14 and
the signal on the Gate of the Device at (VGs). V9 is
the input gate drive and V1 is the signal on the gate
structure of the MOSFET die. Circuit stray
inductance L4, the Resistance R7, and the Miller
Effect are responsible for the distortion of this
Square wave input drive.
8.00
4.00
2
1
0
18.42u
18.46u
18.50u
18.54u
TIME in seconds
18.58u
Figure 24. Gate Drive
1.20k
30.0
800
20.0
400
V14 in volts
Plot1
V5 in volts
1 V14
2 V5
10.0
0
0
-400
-10.0
2
1
18.42u
18.46u
18.50u
TIME in seconds
18.54u
Figure 25 shows the Gate Drive (V14) and the
Drain wave form (V5). The Resonant tank circuit
L3, C3 and C4-C6 filter the V5 wave form to create
a sine wave output. These components also match
the load impedance of 50Ω to the much lower drain
output impedance at V5.
18.58u
Figure 25. Gate V1 and Drain V5
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13/32
Application Note 1815
May 2013
DRF1300
The DRF1300 is the third in the DRF Series of devices. In the DRF1300, the RF Driver die used in the DRF100 is
combined with a High Voltage RF Power MOSFET in a Push Pull Configuration. This combination gives the
designer an RF Hybrid which allows the control of ≈ 2KW of RF power with ≈ 20W of RF drive, this is a power
gain of ≈ 20db. Figure 26 shows the circuit diagram of the DRF1300.
Drain 17
Common 1, 7
Source 16, 18
8, 12
FN
HIGH
HIGH
IN
HIGH
LOW
MOSFET
ON
OFF
LOW
LOW
HIGH
LOW
Table 4
OFF
ON
Drain 15
9
10
11
Source 14, 16
Common 7, 13
Figure 26. DRF1300 Circuit Diagram
All previous discussions of the DRF100 apply to the input section of the DRF1300. In the following section, the
DRF1300 design and testing guidelines are addressed. Table 4 illustrates the truth diagram for the DRF1300.
Figure 27 is an internal view of the DRF1300. The DRF1300 is, in essence, two DRF1200s in the same package;
these two devices are completely independent.
18
17
16
15
14
GND
DRAIN A
GND
DRAIN B
GND
BeO Substrate .080in. Thick
Low Inductance
Output Loop
Low Inductance
Driver Output Loop
Low Inductive Loop ByPass Capacitors
1uF
1uF
1uF
1uF
1uF
1uF
1uF
1uF
1uF
1uF
1uF
1uF
Transparent Case
Outline, Fiberglass
Renforced Ultem2300
Leads Not To Scale
GND
1
+V FN IN SG +V
2
3
4
5
6
GND
7
+V FN IN SG +V
8
9 10 11
12
GND
13
Figure 27.
DRF1300 Internal View
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14/32
Application Note 1815
May 2013
There are three important features that must be addressed. The first is the Driver CI Output Loop, illustrated in red.
Much care has been taken to reduce the magnitude of the inductance between the Driver and the MOSFET. The
lower the value of this stray parameter, the higher the operating frequency will be.
The Loop is composed of two nested loops, one on the right and one on the left. These current loops are
magnetically coupled and form a Coplanar Line. Following the red line on the right from the Tail to the Point of the
arrow, during Turn-On of the MOSFET the current flow is from the Source and the power ground, through the ByPass Capacitors into the Driver IC, then out of the driver IC and into the Gate of the MOSFET. During Turn-Off of
the MOSFET, the currents flow in the opposite direction. During both Turn-On and Turn-Off, the two currents are
forced by topology to flow in opposite directions. Given this flow and the level of the coupling between the two
loops, the Inductance is effectively reduced.
The second, the MOSFET Output Loops shown in blue, operate is the same manner as the Driver Loops.
The third is that compressing the layout of components further aids in reducing internal stray inductance.
The combination of these features allows the DRF1300 to have switching speeds of ≤ 5 ns and operate at
frequencies of up to 30MHz.
The DRF1300 is assembled with adjacent MOSFET die and adjacent driver die. This means that the two MOSFET
die are selected based on their location on the silicon wafer, side-by-side. This will not provide an exact match of
functional parameters but very close. The driver dies are selected in the same manner with similar results. Overall
the DRF1300 will have all parameters of the left side and the right side of the device nearly a match.
U2
U2
U2
Figure 28. DRF1300 Test Circuit
Figure 28 is a schematic diagram of the DRF1300 Test Circuit. A 5V max signal input is applied to either J1 or J2.
Using the Signal Ground (SG) for the BNC shielding provides a Kelvin connection for the input increasing noise
immunity. The driver supply from the +15V (VCC) input is applied to U1 Vdd pins 2 and 6 that are both externally
and internally connected to help balance pulse currents in the hybrid. The same applies for U2 Vdd pins 8 and 12.
U1 section and the U2 section do not share an internal power connection. Connecting the Jumper JP1 will cause the
U1 side of the DRF1300 to operate in the Inverting mode, while JP2 provides this function for the U2 side. The
output sections as configured have 50Ω resistive pull-up circuits with on board filtering for the High Voltage power
supply. Electrical performance data is captured with a test circuit similar to Figure 29.
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15/32
Application Note 1815
May 2013
GND
+15V
Vdd Bypass
Capacitors 2 Places
X= 9 Plated Thru Holes
to Ground Plane
Cutout for Device
Area for User Circuit
Development
GND
+15V
Vdd Bypass
Capacitors 2 Places
Full Ground Plane
1
X
C11 C12
X
BNC
R6
X
X
GND
2
R5
Micerosemi
DRF1300
BNC
X
X
+Vds
X
R7
R8
X
4 Traces for User
Circuit Development
3
C13 C14
X
X
X
4
No Control Signal or LV Power
Trace to the Right of this Line .
Figure 29. DRF1300 Evaluation Switching
Figure 29 is an illustration of the DRF1300
BNC Evaluation Switching PCB. The user configurable area is illustrated by
the dashed red line. For example, this area can be modified to be a Push-Pull Class-D RF Generator.
DRF1300 Push-Pull RF Generator 2.8KW
DRF1300
V15
V1
X1
ARF300
17 L2
8
5n
19
27
16
IV2
WV2
26
16
5
25
R8
.05
V2
14
Simplified Driver
IC SPICE Model
L8
R15 5n
L9
.15e-9
L7
10n
2
X3
ARF300
23
X2
XFMR-TAP
RATIO = .5
R4
.15
23
23
23
C6
15p
L6
2u
6
22
23
23
R9
500
26
*
WR9
C4
235p
R6
.05
20
12
R5
50
21
*
WR5
R10
.05
25
25
.15
V3
23
L5
2u
Y18
V16
27
V12
C3
.01u
L4
293n
23
L3
2u
R16
.001
C5
10u
*
27
*
R7
.10
4
50Ω
WR4
V6
25Ω
27
R3
.001
V4
C2
15p
IR3
R2
.35
V2
165
4
Matching Network
6.25Ω
C1
2.5n
13
ARF300 MOSFET Die
used in the DRF1300
17
15
1
7
R1
.15
V13
R14
.15
*
L1
V1
Tran Generators = PULSE .15e-9
Y17
24
6.25Ω
25
C7
15p
Push-Pull Transformer
V Ratio = 1:2
No transformer Loses
are Modeled
3
10
C8
2.5n
V9
V3
Tran Generators = PULSE
R11
.15
9
11
18
R13
.35
IR12
R12
.001
Figure 30. DRF1300 Push-Pull RF Generator
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16/32
Application Note 1815
May 2013
Figure 30 illustrates the DRF1300 in a push-pull Class-D circuit configuration.
Table 5 lists the performance. In this mode of operation, the MOSFETs X1 and X3
are gated in an alternating pattern. This applies power to alternate windings of the
transformer X2. The transformer primary to secondary ratio is 1:2, which translates
to a reduction of 4:1 in impedance, Load to MOSFET Drain, 50Ω Load to 6.26Ω
Drain. The RF Driver IC is modeled in Figure 30 in the yellow highlighted areas,
X1 for the High Side Switch and 3X for the Low Side switch. The largest difficulty
in a push-pull Class-D circuit design is the design of the transformer. This is also
true for the SPICE model. In a push-pull Class-D circuit configuration, it should be
noted that the simulations are less precise due to the transformer model. This being
said, the circuit model is still instructive for the completeness of understanding.
Figure 31 shows the Gate and Drain waveform timing. Illustrated at (A) on the
Drain waveform is a small discontinuity in the Rate of Rise, which is the result of
slightly more inductance than necessary for resonance. However this small
inductance makes a noticeable increase in Efficiency, see Application Note 1808.
T1 and T2 illustrate the gate on time. Figure 32 illustrates the relationship between
the nDrain waveform and the RF sine wave on the output load R5.
1 V15
800
300
12.0
400
Volts
V15 in volts
1 V6
16.0
V1 in volts
Pout
2859W
Pin
3459W
PLoss
561W
Eff
Pulse Gate
Drive
Ths
83.6%
25°C
Tj X3
101°C
PW=25ns
TjX1
101°C
Vds Margin
138V
Drain Z=6Ω Out Z=50Ω
Table 5
2 V1
400
200
Circuit Performance
Vsupply
+165V
8.00
A
2 V12
Bipolar Square Wave
on V6
Sine Wave Output on
V12
0
1
-400
100
4.00
2
1
2
0
-800
0
48.92u
T1
T2
Figure 31. Gate and Drain Waveforms
48.96u
49.04u
49.00u
TIME in seconds
49.08u
Figure 32. Transformer and Output Waveforms
DRF1400
The DRF1400 is the fourth in the DRF Series of devices. In the DRF1400, the RF Driver die used in the DRF100 is
combined with two High Voltage RF Power MOSFETs in a Half Bridge Topology. This combination gives the
designer an RF Hybrid which allows the control of ≈ 5KW of RF power with ≈ 20W of RF drive. This is a power
gain of > 24db. Figure 33 shows the circuit diagram of the DRF1400 and Table 6 illustrates the truth diagram for the
DRF1400.
FN
HIGH
HIGH
LOW
LOW
IN
MOSFET
HIGH
ON
LOW
OFF
HIGH
OFF
LOW
ON
Table 6
Figure 33. DRF1400 Circuit Diagram
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17/32
Application Note 1815
May 2013
The DRF1400 is assembled with adjacent MOSFET die and adjacent driver die. This means that the two MOSFET
die are selected based on their location on the silicon wafer, side-by-side. This will not provide an exact match of
functional parameters but very close. The driver die are selected in the same manner with similar results. Overall the
DRF1400 will have all parameters of the left side and the right side of the device nearly a match.
DRAIN
OUTPUT
SOURCE
MOSFET Current
Loop
Power MOSFET
Driver Current
Loops
Driver IC
1uF
1uF
1uF
1uF
1uF
1uF
1uF
1uF
1uF
1uF
1uF
1uF
Integrated By-Pass
Capacitors
GD +VD FN IN SG +VD GD
GS +VS FN IN SG +VS GS
Figure 34. DRF1400 Internal View
Figure 34 is an internal view of the DRF1400, the Half Bridge topology in the DRF Family. The input Driver and
MOSFET circuitry are virtually identical to the DRF1200. The current loops are magnetically coupled and form a
Coplanar Line. Following the red line on the right from the Tail to the Point of the arrow, during Turn-On of the
MOSFET the current flow is from the Source and the power ground, through the Bypass Capacitors into the Driver
IC, then out of the driver IC and into the Gate of the MOSFET. During Turn-Off of the MOSFET the currents flow
in the opposite direction. During both Turn-On and Turn-Off, the two currents are forced by topology to flow in
opposite directions. Given this flow and the level of the coupling between the two loops, the Inductance is
effectively reduced as in DRF1300. However, the MOSFET Output Loops shown in blue do not operate in the same
manner as the DRF1200 and DRF1300. Here, there is no symmetry, which leads to increased inductance in the drain
source loop. This increased inductance is offset by the typically high voltage operation of the Half Bridge Topology.
In addition this inductance will subtract from the value of the Output Network Inductor (see output network on Page
24). The DRF1400 is capable of switching speeds of ≤ 5 ns and operate at frequencies of up to 30MHz.
The Half-Bridge circuit topology
The Half-Bridge circuit topology offers the highest forward launched RF power for a given amount of silicon of any
ISM RF power topology. However there are downsides to utilization of this configuration. The Half Bridge is
complex, requires a very stable high side controller, and can operate at drain voltages approaching 800V. At this
operating point, component selection can become extremely critical.
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18/32
Application Note 1815
May 2013
+200V DC
+Vds 2,6
FN 3
AC on Common Node
IN 4
SG 5
U2 COMMON 1,7
OUTPUT 16
High Side Reference
Plane ( Floating Ground)
-200V DC
Using this circuitry we will look at
the critical circuit areas. The most
troublesome area is maintaining
control of the high side switch.
Referring to Figure 35 we see that
the Power Output (pin 16) Node in
the circuit (shown in purple) is also
the signal reference plane (Floating
Ground) for all the driver inputs
(pin 1, 2, 3, 4, 5, 6 and 7). We will
see in the following text that we will
need about -50db CMR to maintain
control of the high side switch.
Figure 35. Half-Bridge
T1
Common Mode
Choke
High Side Control
Control Input
High Side Common
Control Ground
Figure 36. Isolation Transformer
CMC to Block RF from the
LV supply
The Isolation Transformer is the
first and simplest approach for
isolation and control. Fiber-Optics
are somewhat easer to implement
and have very high CMR. The cost
is higher, however assembly is less
problematic. For this discussion we
will start with the Isolation
transformer approach.
+200V DC
15V Isolated Supply
+Vds 2,6
Control Input
FN 3
AC on Common Node
IN 4
SG 5
U2 COMMON 1,7
OUTPUT 16
CMC
High Side Reference
Plane ( Floating Ground)
Isolation
Transformer
-200V DC
Figure 37. Half Bridge with Control signal and Support Power
Figure 37 illustrates the Half Bridge of Figure 35 with the addition of the Isolation Transformer of Figure 36. We
have also included a CMC installed in the Low voltage power path. The Half Bridge of Figure 37 now includes the
three elements which require the most understanding and the most attention to detail. The isolated 15V supply will
isolate a DC potential a DC of 1KV from the secondary. However we must also provide isolation from the RF
square wave at the Output pin 16. This is accomplished with the insertion of a CMC in the DC path, Figure 37 upper
left. The input control Isolation Transformer, shown in Figure 37, must also have a CMC. Both the CMC and the
Isolation Transformer will be discussed in more detail.
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19/32
Application Note 1815
May 2013
High Side Transformer Output Section
Parasitic Coupling Capacitance
Network
High Side Switch
1
V2 Tran Generators = PULSE
4
R2
100
L1
10n
2
5
R3
5
Y2
Y1
∆
R7
500
∆
C5
1p
6
12
7
R10
1
V1
5.0
X7
PPG101
C2
1p
R6
50
17
3
R4
1
R1
1
C1
1p
V9
13
L2
50n
C6
10p
R8
1000K
V3 Tran Generators = PULSE
High Side
Reference Plane,
Half Bridge
Output Node
Figure 38 illustrates the Parasitic
Coupling Capacitance Network in the
Isolation Transformer, highlighted in
red, the secondary of the Control Signal
Coupling Transformer in the blue
highlighted box, and the High Side
Switch Driver in the green highlighted
box. The Parasitic Coupling Capacitance
Network models the coupling from the
primary of the transformer to the
secondary. With a very modest
capacitance at C5, the circuit can lose
stability. This will be catastrophic for the
Half or Full Bridge circuit.
Figure 38. Parasitic Coupling Capacitance
2 Y2#a
1 Y1
6.00
7.00
4.00
5.00
Plot1
Y1, Y1#a in volts
Plot1
Y2, Y2#a in volts
1 Y2
2.00
-2.00
2
1
3.00
2
1
0
2 Y1#a
1.00
-1.00
480n
500n
520n
540n
TIME in seconds
560n
470n
Figure 39. Y2 High Side wave form
490n
510n
530n
TIME in seconds
550n
Figure 40. Y1 High Side wave form
In Figures 39-40 we see the effect of the Parasitic Coupling from the Ground Plane to the high voltage Reference
Plane which is the output node of the Half Bridge. This coupling forces a current through the Parasitic Network
Loop, highlighted in red and shown in Figure 38. The red trace is the Y2 signal with no parasitic coupling; the blue
trace is the Y2 signal with the parasitic coupling. The level of coupling is just beginning to affect the control signal
at Y1 illustrated in Figure 40, with a C5 value of 0.25pF. This signal is about -51db from the Half Bridge output
level.
1 Y1
2 Y2#a
6.00
7.00
4.00
5.00
Plot1
Y1, Y1#a in volts
Plot1
Y2, Y2#a in volts
1 Y2
2.00
1
2
0
-2.00
2 Y1#a
2
1
3.00
1.00
-1.00
480n
500n
520n
540n
TIME in seconds
560n
Figure 41. Y2 High Side wave form
www.microsemi.com
470n
490n
510n
530n
TIME in seconds
550n
Figure 42. Y1 High Side wave form
20/32
Application Note 1815
May 2013
The level of coupling in Figure 41 is now clearly affecting the control signal at Y1 illustrated in Figure 42, which is
at -48.9db from the Half Bridge output level, with a C5 value of 0.5pF. At this point, the circuit is cross-conducting.
1 Y1
2 Y2#a
6.00
7.00
4.00
5.00
Plot1
Y1, Y1#a in volts
Plot1
Y2, Y2#a in volts
1 Y2
2.00
1
2
3.00
1.00
1
2
0
2 Y1#a
-2.00
-1.00
480n
500n
520n
540n
TIME in seconds
560n
470n
Figure 43. Y2 High Side wave form
490n
510n
530n
TIME in seconds
550n
Figure 44. Y1 High Side wave form
The level of coupling in Figure 43 is now seriously affecting the control signal at Y1 illustrated in Figure 44. This is
at -45.3db from the Half Bridge output level, the value of C5 is now 1pF. The circuit is now cross-conducting on
both the leading edge and the trailing edge.
2 Y2#a
1 Y1
6.00
7.00
4.00
5.00
Plot1
Y1#a, Y1 in volts
Plot1
Y2#a, Y2 in volts
1 Y2
2.00
1
2
0
-2.00
2 Y1#a
2
1
3.00
1.00
-1.00
480n
500n
520n
540n
TIME in seconds
560n
Figure 45. Y2 High Side wave form
470n
490n
510n
530n
TIME in seconds
550n
Figure 46. Y1 High Side wave form
The level of coupling in Figure 45 has completely disrupted the control signal at Y1 illustrated in Figure 46, which
is at -38.8db from the Half Bridge output level. The value of C5 is now at only 2pF. The circuit now is oscillating
and the switching devices most likely have been destroyed. This sequence of wave forms clearly shows that in order
to maintain system control in the RF Half Bridge we must be extremely careful in the Design and Implementation of
the isolated control circuitry. Keeping this Parasitic Capacitance as low as practical and the addition of Common
Mode Chokes can mitigate this potentially serious problem.
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21/32
Application Note 1815
May 2013
Common Mode Rejection
In order to maintain system control in an RF Half Bridge as illustrated in the preceding Figure 37, we must be
extremely careful in the Design and Implementation of the isolated control circuitry. Keeping the Parasitic
Capacitance of the Isolation Transformer as low as practical and the addition of Common Mode Chokes can help.
Figure 47 Illustrates a DC Isolated Transformer and Common Mode Choke input.
T1
Common Mode
Choke
High Side Control
Control Input
High Side Common
Control Ground
Figure 47. Ground to High Side Control
The Gate Drive is a +15V Pk pulse. This is coupled through T1 and applied to the High Side control, see Figure 47.
The Signal at this point is Bi-polar, a positive pulse with a DC offset proportional to the Pulse Width and the Duty
Cycle. Transformer coupling and CMCs were chosen for simplicity. T1 incorporates two electro static shields.
These effectively shunt the capacitive coupling to ground and improve the CMR, however they make the
transformer very difficult to build.
Common Mode Chokes (CMC)
Constructions of the CMC’s are illustrated in Figure 48. The CMC on the left should be used for both the +15V
input and the +HV VDS input. These lines are tightly twisted pairs (5-8 twists per inch). The CMC on the right
should be used for the control signal Input and on the Scope Probe Cable, when making measurements. Three to five
turns on each is sufficient. The CMC’s should be placed as close to the circuit as practical.
Twisted Pair
INPUT
Cable EMI Suppression Core
Coaxial Cable
Signal INPUT
Cable EMI Suppression Core
Coaxial Cable
Signal
OUTPUT
CMC for +15V and
HV DC Power
Twisted Pair
OUTPUT
CMC for Scope Control
and Signals
Figure 48. Common Mode Choke (CMC)
FairRite part number 0431164181
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22/32
Application Note 1815
May 2013
Fiber Optic Control Link
The suppression of the 400-800V Common Mode Signal on the High Side Control to the Driver Circuit Input must
be on the order of -51 db for stable operation. For high power Half Bridge RF Generators, the Common Mode
Signal Slew Rate can be ≥ 100KV/µs at the high side Reference Plane. This rules out the use of low-cost Optoisolators. This would seem to indicate that we are relegated to the use of a transformer, however this is not the case.
With the modern innovations in fiber optic devices, and the reduction in cost, they are now an appealing choice to
address the High Common Mode requirements of the High Power Half Bridge, and the cost is in the same area as
the transformer solution. Illustrated in Figure 49 is a High Power Half Bridge utilizing a Fiber Optic Link for control
of the High Side Switch. It is suggested that two identical links be used, as opposed to a slower, cheaper link for the
low side switch. This maintains the Phase of the two control signals. Low Voltage supplies are not shown.
High Side Isolated
Supply
+ V Supply
High Side
Switch
Microprocess
or Control
To RF
Network
Ground Level Fiber
optic Control
Low Side
Switch
- V Supply
High Side Isolated
Supply
In Figure 49 the Microprocessor
applies the control signals to the two
fiber optic links. One assigned to the
High Side switch and the other the
Low Side switch. With this method of
signal control, all ground loops are
severed and the High CMR of the
Optical Link provides stable control
signals to the High Side switch. One
could use a cheaper optical link for the
Low Side switch; however threshold,
delay and thermal drift parameters may
be difficult to match. It is best to use
the same link for both controls.
Figure 49. High Side Fiber Optic Control
Figure 50. DC-DC Supply
Referring to Figure 50, M300 is a Switch Mode DC-DC converter that supplies +15V at 1.5A for the Driver when
operating at 13.56MHz. It also has 1KV DC isolation. The low voltage DC power path for FG1 is through CMC302
and is filtered by C303, R301 and C302, R302. DC isolation for the FG1 plane is via the DC-DC power supply
M300. C304, C305 and C306 provide local by-passing for U1 on the FG1 plane. This allows the DC to DC
converter to remain stable while the FG1 plane is slewing from +Vds to -Vsd. The operation of the DC-DC Supply
for FG2 is in the same manner.
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Application Note 1815
May 2013
N Channel – N Channel Half Bridge
Figure 51 illustrates a classical N Channel - N Channel Half Bridge RF Generator. The High Side Switch X2 and the
Low Side Switch X1 form the two active devices in the Half Bridge. X1 and X2 commutate in an alternating fashion
providing a pseudo Square Wave drive to the input of the RF Network at V1. The RF network provides an
impedance match from the Drain Impedance of X1, X2 of about 3Ω to the 50Ω load, via an L Match Network, L4
and C3. This network is also resonant at 13.56MHz so that the output at V8 is a Sine Wave. It should be noted that
the network only performs the impedance translation at the design frequency. The common design formulas account
only for a resistive source and load. Since the output devices have parasitic capacitance, the network design must be
modified to account for the stray capacitance. This is done with the addition of a series inductance (L7). A value of
L7 ≈ 10% to 25% higher than the calculated is typically required to bring the network to full efficiency. Circuit
performance is shown in Table 7.
Gate Driver
L2
25nH
V2
Tran Generators = PULSE
V21_V1
20
∆
5
R1
.15
L1
.15nH
1
X2
ARF300
IV2
Vsupply
V4_V1
High Frequency Loop
∆
4
Circuit Performance
Low Frequency Loop
RF Network Compensating
Inductance
L3
5n
10
R2
.05
V1
7
18
V8
8
13
*
12
C1
.01u
L4
139n
L7
17n
C3
930p
V11_V19
∆
14
11
L5
.15nH
C2
.02u
∆
9
Tran Generators = PULSE
V3
V1
115
WV1
WR6
X1
ARF300
IV3
2
L6
25nH
V4
115
*
IV1
V1_V19
3Ω
Output RF Network
6
*
WV4
3
R7
.01
R5
50
*
WR5
17
WR2
*
15
R4
.15
R6
.01
50Ω
Resonant at 13.56MHz
±115V
Pout
2238W
Pin
2499W
PLoss
261W
Eff
Pulse Gate
Drive
Ths
89.4%
Tj X2
100°C
TjX1
100°C
Vds Margin
270V
PW=22ns
45°C
Drain Z=3Ω
Out Z=50Ω
Table 7
IR7
Figure 51. N - N Channel Half Bridge
The Half Bridge Circuit Topology of Figure 51 contains two current loops. A low frequency loop is highlighted in
yellow, and the High Frequency Loop is highlighted in red. These loops are illustrated with near-minimum stray
inductance. Great care should be taken to achieve inductance values near the illustrated values. If we allow L2 and
L6 to reach 100nH or greater, performance will be degraded. The inductance of the Inner Loop, L3, is a very Critical
Stray Component. Values greater than a few nH can cause stability problems and excessive harmonics. Shown in
Table 8 are a set of values for variations in the three Stray Inductive terms, L2, L3 and L6 and the impact on circuit
performance.
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Application Note 1815
May 2013
Table 8. L2, L3, L6 Variations
L2=25nH L2=100nH L2=250nH
L2, L3, L6
L3=5nH
L3=20nH
L3=50nH
L6=25nH L6=100nH L6=250nH
Vsupply
±115V
±173V
±235V
Pout
2238W
1856W
816W
Pin
2499W
2116W
1060W
PLoss
261W
260W
244W
Eff
89.40%
87.7%
77.0%
Pw
26ns
26ns
26ns
Ths
45°C
45°C
45°C
Tj X2
100°C
100°C
96°C
TjX1
100°C
100°C
96°C
Vds Margin
270V
139V
5V
For Columns 2, 3 and 4, Circuit Parameters
have been adjusted for the Highest Efficiency
and Highest Power Output while not
exceeding the Boundary Conditions as stated
in the Introduction. If we allow L2 and L6 to
reach 100nH or greater, performance will be
degraded. Power Output Capability and
Efficiency are reduced significantly. The
inductance of the Inner Loop, L3, is a very
Critical Stray Component. Values greater
than a few nH can cause stability problems
and excessive harmonics.
Designing A Half Bridge Output Network
Generally, the output impedance of the half bridge – the load that will accept the maximum amount of power from it
– is nowhere near the typical 50Ω used for power measurement and coaxial cables. A tuned matching network is
used to change the output impedance of the amplifier to 50Ω.
The transistors are not ideal devices, they have a finite output capacitance, Coss. This causes the half bridge’s output
impedance to be slightly capacitive. This is important to consider, but it can be easily accommodated by the output
network if the first tuning element is a series inductor, which is usually the case.
The output impedance is calculated from the operating voltage and the allowable level of stress on the transistors. If,
for instance, the operating supply is 200 volts rail-to rail and the desired output power is 1kW, the output impedance
is calculated by Equation 1. So RL = 40Ω.
V2
Equation 1. R L = dd
POUT
The Coss is essentially in parallel with this output impedance. If the Coss is 200 pF and the operating frequency is
13.56 MHz, the output impedance is the parallel combination of RL and XCoss or 40Ω // -j58.7Ω. Converting this to
an equivalent series impedance gives RL = 27.3 –j18.6. This is the “output impedance” of the amplifier that must
now be matched to 50Ω.
Since the output of a class D amplifier contains a high amount of harmonic energy, it is convenient to employ a
matching network that is also a lowpass filter. The simplest network that will fulfill this requirement is an L-network
consisting of a series inductor and a shunt capacitor.
The first element in the matching network is an inductor that cancels the series capacitive reactance caused by Coss.
Its reactance is +j18.6Ω at 13.56 MHz or 218 nH. Now the network is calculated in Equation 2.
Equation 2. X L = R 2
R1
R R
R1
−1 = 1 2
− 1 and X C = R 1/
R2
XL
R2
R1 must always be greater than R2. Here R1 is the load (typ 50Ω) and R2 is the real part of the output impedance,
27.3Ω in our example. So the series inductance is j24.9 or 292 nH, and the shunt capacitor is –j54.8 or 214 pF.
The final network is the combined inductors, (218+292) = 510 nH, in series with the output and the shunt capacitor
of 214 pF in shunt with the output. There is one more element required. This is the blocking capacitor. It does not
form part of the matching network, but is needed to make sure there is no DC voltage on the output connector. It can
be placed in series with the inductor so as to reduce the stress on the output shunt capacitor. It must be a low loss
type because it carries the full output current of the generator, given by Equation 3.
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Application Note 1815
May 2013
Equation 3. I o =
Pout
or 6A.
RL
Table 9. Excel L-Network Calculator
Table 9 is an instructive tool for the investigation of the network design, the circuit efficient and power output.
Low Frequency Loop, High Frequency Loop and Stray Inductance
Recall Table 8. Stray Inductance in most cases is detrimental to circuit performance. For the HB circuit
configuration we included a table with three sets of stray inductances. The preferred is Set (1), 25nH, 5nH, 25nH.
Set (2), 100nH, 20nH, 100nH is usable but not advised and Set (3), 250nH, 50nH, 250nH is not acceptable,
Power Output
2500
2000
1500
N-N Pulse Drive
Figure 52 illustrates Power Output vs. Stray
Inductance. For Sets 1, 2 and 3 the Power
Output is reduced by well over a 1000W.
1000
500
0
1
2
3
Stray Inductance
Figure 52. Power Output vs. Stray Inductance
95
Efficiency
90
85
N-N Pulse Drive
80
Figure 53 illustrates Efficiency vs. Stray
Inductance. For Set 2 the Efficiency is
reduced by ≈ 5%, and for Set 3 by ≈ 14%
75
70
1
2
3
Stray Inductance
Figure 53. Efficiency vs. Stray Inductance
300
Vds Margin
250
200
N-N Pulse Drive
150
100
50
Figure 54 illustrates Vds Margin vs. Stray
Inductance. The Vds Margin is reduced by
almost 100V for Set 2, and by over 200V for
Set 3.
0
1
2
3
Stray Inductance
Figure 54. Vds Margin vs. Stray Inductance
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Application Note 1815
May 2013
Figures 52, 53 and 54 illustrate the value of taking great care in the minimization of the Stray Inductance in the Low
Frequency and the High Frequency loops shown in the preceding text.
High Power
Circuit Parameters, for Figure 55, have been adjusted for the Highest Efficiency and Highest Power Output while
limiting the MOSFETs junction temperature to a maximum of ≈ 125°C and limiting the Drain to Source Margin to a
positive number or zero. These are defined as the Boundary Conditions all values shown in the following text were
acquired with these constraints, see Table 10.
Gate Driver
∆
5
L1
.15nH
1
X2
ARF300
IV2
RF Network Compensating
Inductance
L3
5n
10
R2
.05
V1
*
7
12
∆
14
18
C2
.02u
WV1
2
L6
25nH V1_V19
V4
171
*
IV1
WR2
WR6
Output RF Network
6
*
R5
50
*
WR5
17
R6
.01
3
∆
9
Tran Generators = PULSE
V3
V1
171
8
C3
930p
X1
ARF300
IV3
V8
13
11
L5
.15nH
R4
.15
C1
.01u
L4
139n
L7
16n
V11_V19
15
Vsupply
High Frequency Loop
*
20
R1
.15
V4_V1
∆
4
V21_V1
Circuit Performance
Low Frequency Loop
L2
25nH
V2
Tran Generators = PULSE
WV4
Resonant at13.56MHz
±171V
Pout
5001W
Pin
5693W
PLoss
593W
Eff
Pulse Gate
Drive
Ths
89.6%
Tj X2
125°C
TjX1
125°C
Vds Margin
155V
PW=26ns
45°C
3
R7
.01
IR7
Drain Z=3Ω Out Z=50Ω
Table 10
Figure 55. N - N Channel Half Bridge
Figure 55 is very similar to Figure 51 on Page 24, however we have changed the Boundary Conditions. We have
allowed the Junction Temperature to rise to 125°C, and the Power Output to rise to 5.01KW. This is not an
unreasonable operating point provided that the load is a 50Ω Flat Line. Once we change the load, Power must also
be altered to maintain the output devices X1 and X2 at a Tj of less than 125°C or we may damage the MOSFET
devices. Carrying this further, we can combine two Half Bridges to get 10KW. In Figure 56 we combine four
modules to get 20KW RF Output at 13.56MHz
More Power
Figure 55 illustrates a 5KW N Channel Half Bridge at 13.56MHz. In Figure 56 we have added two MOSFETs and
formed a new Series Array Half Bridge. This type of Half Bridge can be constructed to > 10KV Series Array Half
Bridge with 2MW peak power. As the Power and the Voltage increase, the working circuit be comes more and more
difficult to realize. For example, implementing the circuit of Figure 56, at operating levels of 10KV 30A and at
1MHz is difficult. However 10KV 30A at 15MHz and 30MHz is very difficult. Referring to Figure 56, as the
number of stages are increased, the mechanical length of the array may approach a multiple of one or more of the
higher order harmonics of the design frequency. This can be very problematic. At some point a Vacuum Tube may
still be the best choice.
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27/32
Application Note 1815
May 2013
Gate Driver
Low Frequency Loop
2
L1
50nH
V1
Tran Generators = PULSE
4
5
X1
ARF300
IV1
22
C1
25p
7
R13
1000k
V11_V9
15
∆
14
X2
ARF300
IV2
23
V24_V12
∆
6
R7
.15
C5
25p
L10
25n
*
C4
634p
X3
ARF300
V9_V12
25
L12
25n
32
∆
R11
1
*
WR6
R8
.01
Output RF Network
R14
1000k
V26_V19
C6
25p
WR8
R15
1000k
24
R6
50
17
WR5
12
31
30
V8
8
13
18
V9
L9
.15nH
IV3
C3
.01u
L7
191n
L8
39n
3
Tran Generators = PULSE
V2
V3
Tran Generators = PULSE
R9
1
R5
.05
9
29
27
Resonant at
13.56MHz
V7_V9
L5
.15nH
R3
.15
C2
25p
L6
25n
11
∆
R4
1
RF Network Compatsating
Inductance
V4_V7
10
16
33
26
L11
.15nH
R10
.15
IV4
C7
.05u
X4
ARF300
∆
21
R12
1000k
L4
2n
∆
∆
L2
25n
1
L3
.15nH
*
R1
1
20
R2
.15
∆
V1_V7
Low Frequency Loop
V12_V19
19
Tran Generators = PULSE
V4
V5
371
V6
371
L13
50nH
28
WV5
IV6
IV5
*
WV6
*
Figure 56. 10KW Half Bridge
The previous topology discussions are also valid for Figure 56. In fact their
effects are more intense. Control stability is very exacerbated. The CMR
required for 10KV signal with a 10ns rise time is on the order of -120db. A
Fiber optic control system is the most viable solution. The Optical Control
approach has additional benefits: System Layout, repeatability and the
potential to extract High Side Data.
Circuit Performance
Vsupply
±371V
Pout
10KW
Pin
11.258KW
PLoss
1258W
Eff
Pulse Gate
Drive
Ths
88.8%
PW=26ns
Tj= X1, X2
130°C
Tj=X3, X4
130°C
Vds Margin
154V
45°C
Drain Z=6Ω
Out Z=50Ω
Table 11
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28/32
Application Note 1815
May 2013
Very High Power
Combiners
Figure 57. Three Port Combiner
Figure 51 5KW
RF Combiner
Figure 51 5KW
RF Combiner
Figure 51 5KW
RF Combiner
Figure 51 5KW
Combiners can take many forms and their design is beyond
the scope of this article. There are two basic types –
transmission line “Wilkinson” combiner, and the
broadband ferrite-loaded combiner. Regardless of the type
used, all have several common requirements. They must
take two or more signals and combine (add) their power
together at a single output port. There must be isolation
between the inputs such that the function of one input does
not affect the others. Each input port must present a proper
load to the power sources, and the output impedance of the
combiner should be the same as each of the sources being
combined. The combining must be accomplished
efficiently. Even a 1% loss at 20kW is a considerable
heating factor.
At the other end of the signal chain, the signal splitters
divide the drive signal. Except for power handling
capability, a splitter is exactly the same as a combiner
connected in reverse.
A broadband lumped element combiner is illustrated in
Figure 57. Ports 1 and 2 are the inputs. Two in-phase
signals applied at the input will be combined at Port 3.
Since these signals are essentially in parallel, the output
impedance of Port 3 is half of the input impedance and
another matching transformer must be used to bring it back
up to the source’s impedance. The resistor is important to
the operation in two ways. If the two input signals are
exactly the same amplitude and phase, no power will be
lost in the resistor, but if there is any difference it will be
dissipated here. If there is only one input signal, half of it
will be dissipated here the other half will be delivered to
the output. If the value of the resistor is twice the input Zo,
the isolation between ports will be very high.
Figure 58. RF Combiners
Individual 2-way combiners can be combined in pairs, “echelon” fashion, to combine a larger number of sources.
The total number of input ports is always a binary number. As illustrated in the first diagram, three 2-way combiners
are used to combine four signals.
Using the three combiners of Figure 58 as a platform we can use some of the HB RF Generators we have discussed
to build RF Generators to higher power levels.
Figure 51 2.5KW RF Output 4 HB 3 Combiners Power Out = 10KW Good Safety Margin
Figure 55 5.0KW RF Output 4 HB 3 Combiners Power Out = 20KW medium Safety Margin
Figure 56 10KW RF Output 4 HB 3 Combiners Power Out = 40KW Low Safety Margin
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29/32
Application Note 1815
May 2013
Non reactive and Reactive loads
Load
Rs
Number
Base Line 50
1
100
2
69.5
3
40
4
28.1
Junction Temperature
250
200
175 oC
150
125 oC
100
N-N Pulse
50
N-N Sine
0
1
2
3
4
5
6
7
8
5
6
7
8
Load Number
Xs
0
0
431nH
352.6nH
174.5nH
25
0
28.1 709pF
40
390pF
69.5 317pF
Table 12
Reactive
Load
jXs
0
36.7
30
14.9
0
-14.9
-30
-36.7
Figure 59. Loads vs. Configuration
Each of these loads illustrated in Figure 59 and Table 12, present a 2:1 VSWR mismatch to 50Ω. They are equally
spaced every 45° around a 2:1 VSWR load circle. In each of the circuits, the 50Ω load is transformed through the
output matching network (i.e. L5+L6 and C2 in Figure 1) to approximately 3Ω at the Drains of transistors X1 and
X2. A load other than 50Ω is “mismatched” and its effect on the circuit is quite different. From a reliability
standpoint, keeping the load between 3-4 on the left and at or below 7 on the right is the preferred operating space.
In addition, minimizing the time spent at or above 175°C is advisable.
For a detailed discussion of N-N Pulse vs. N-N Sine drive see Microsemi Application Note 1808, ARF300-ARF301
in N-N and N-P Half Bridge RF Generators with Pulse and Sine Drive.
An output load impedance lower than 50Ω will be transformed to a higher impedance load at the devices. The
transistors can more easily supply the full output voltage to this higher impedance. Consequently, the output power
is less and the junction temperature is lower. Load impedance greater than 50Ω on the output is transformed though
the matching network to an impedance lower than 3Ω at the transistor junction. This causes the devices to be
overloaded and mistuned. This puts the full voltage on this lower impedance creating more output power at lower
efficiency which in turn causes the rise in junction temperature. Figure 59 clearly demonstrates the importance of
maintaining a proper load on the output of the RF Generator.
Conclusion
In the preceding pages we have discussed a lengthy array of topics, focused on the ISM RF power arena.
Discussions from the design of high power hybrids to the circuits’ need to exploit their maximum power
capabilities. In these pages we have discussed the design approaches for RF Power systems from 1KW to 20KW all
based on the DRF Series of Hybrid Devices. In the following section a collection of Relevant Publications is given.
Relevant Publications
Combiners
Krauss, Bostian, Raab, "Solid State Radio Engineering", John Wiley & Sons, 1980.
Dye, Granberg, "Radio Frequency Transistors: Principles and Practical Applications", Butterworth-Heinemann,
1993. Chapter 11.
H. Granberg, "Broadband Transformers and Power Combining Techniques for RF", AN-749, Motorola
Semiconductor Products Inc.
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Application Note 1815
May 2013
Thermal and Cooling
DRF Device Mounting Procedures And Power Dissipation
AAVID Thermal Technologies, Inc., Box 400, Laconia, NH 03247.
Transformers
Hilbers, A.H., Design of HF wideband power transformers, Philips Semiconductors, ECO 6907, March 1998
Hilbers, A.H., Power Amplifier Design, Philips Semiconductors, Application Note, March 1998
Hilbers, A.H., Design of HF wideband power transformers Part II, Philips Semiconductors, ECO 7213, March 1998
Sevick, J., Transmission Line Transformers, Noble Publishing, 4th Ed, 2001. ISBN: 1884932185
Fair-Rite Products Corp., PO Box J, One Commercial Row, Wallkill, NY 12589.
Chris Trask, “Designing Wide-band Transformers for HF and VHF Power Amplifiers”, QEX, Mar/Apr 2005, pp. 315.
References for Power Splitting and Combining of RF Amplifier Assemblies
Krauss, Bostian, Raab, "Solid State Radio Engineering", John Wiley & Sons, 1980.
Dye, Granberg, "Radio Frequency Transistors: Principles and Practical Applications", Butterworth-Heinemann,
1993. Chapter 11.
H. Granberg, "Broadband Transformers and Power Combining Techniques for RF", AN-749, Motorola
Semiconductor Products Inc.
Devices
N. Dye and H. Granberg, Radio Frequency Transistors – Principles and Practical Applications, Boston: ButterwrthHeinemann 1993. ISBN: 0-7506-9059-3. 0750672811 (2nd Ed., 2001)
Oxner, Edwin, Power FETS and Their Applications, Prentice-Hall, 1982. ISBN 0-13-686923-8
Matching
Gonzalez, Martin, Lopez, “Effects of Matching on RF Power Amplifier Efficiency and Output Power”, Microwave
Journal, April 1998.
RF Design
ARF300 – ARF301 In N-N and N-P Half Bridge RF Generators with Pulse and Sine Drive
Microsemi AN 1808
3KW and 5KW Half-Bridge Class-D RF Generators at 13.56MHz with 89% Efficiency and limited Frequency
Agility. IXYS RF.
PRF-1150 1KW 13.56 MHz CLASS E RF GENERATOR EVALUATION MODULE. IXYS RF
Smith Chart is a trademark and property of Analog Instruments Co., New Providence, NJ.
Sokal, HEPA-PLUS/WB v3.29, Design Automation, Inc., Lexington, MA
MIMP, Copyright Motorola, Inc. 1992, available through Motorola RF products group.
WinSMITH, v 2.0 copyright Eagleware Corp., 1998, available through Noble Publishing, Inc.
Franke and Noorani, “Lumped-Constant Line Stretcher For Testing Power Amplifier Stability”, rf Design, Mar/Apr
1983.
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Application Note 1815
January 2011
Davis and Rutledge, “Industrial Class-E Power Amplifiers With Low-cost Power MOSFETs and Sine-wave Drive”
Conf. Papers for RF Design ’97, Santa Clara, CA, Sept 1997, pp. 283-297.
M. K. Kazimierczuk and W. A. Tabisz, “Class C-E High-efficiency Tuned Power Amplifier”, IEEE Transactions on
Circuits and Systems, vol. 36, no. 3, pp. 421-428, March 1989.
R. Frey, “A push-pull 300 watt amplifier for 81.36 MHz,” Applied Microwave and Wireless, vol. 10 no. 3, pp. 3645, April 1998.
Frey, Low Cost 1000 Watt 300V RF Power Amplifier for 27.12 MHz, APT Application Note APT9701.
Frey, A 50 MHz, 250W Amplifier using Push-Pull ARF448A/B, APT Application Note APT9702.
Frey, Push-Pull ARF449A/B Amplifier for 81.36 MHz APT Application Note APT9801.
Kraus, Bostian and Raab, Solid State Radio Engineering, John Wiley & Sons, New York, 1980. ISBN 0-471-03018x
William E. Sabin, Edgar O. Schoenike, et al, Single Sideband Systems and Circuits, McGraw-Hill, 1993. ISBN0-07912038-5
Hejhall, R. “Systemizing RF Power Amplifier Design,” Motorola Semiconductor Products, Inc., Phoenix, AZ,
Application note AN282A.
Abulet, Mihai, RF Power Amplifiers, Noble Publishing, 2001. ISBN 1-884932-12-6
Filters
Blinchikoff, Zverev, Filtering in the Time and Frequency Domains, Noble Publishing, 2001, ISBN: 1884932177
Zverev, A. I., Handbook of Filter Synthesis, John Wiley & Sons, Inc, New York, 1970. ISBN: 0471986801
Cripps, Steve C. Advanced Techniques in RF Power Amplifier Design, Artech House, 2002. ISBN 1-58053-282-9
Patents
US Patent 5,187,580 “High Power Switch-Mode Radio Frequency Amplifier Method and Apparatus” Porter and
Mueller, February 16, 1993.
US Patent 5,420,537 “High Power Solid State R.F. Amplifier” Weedon, et al., May 30, 1995.
US Patent 3,919,656 “High-Efficiency Tuned Switching Power Amplifier” Nathan O. Sokal; Alan D. Sokal,
November 11, 1975.
US Patent 4,607,323 “Class E High-Frequency High-Efficiency Dc/Dc Power Converter” Nathan O. Sokal; Richard
Redl, August 19, 1986.
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32/32