Military COTS VI BRICK VTM Family

Not Recommended for New Designs / End of Life - Please see below
MIL-COTS VTM®
MT036 SERIES
S
®
C
US
C
NRTL
US
Current Multiplier
Features
Size:
1.91 x 1.09 x 0.37 in
48,6 x 27,7 x 9,5 mm
• -55°C to 100°C baseplate operation
• 3 MHz effective switching frequency
• Isolated 1 to 50 Vout
• Low weight – 1.10 oz (31.3 g)
• High density
• 1 µs transient response
• Small footprint
• Up to 96.5% efficiency
• ZVS / ZCS Sine Amplitude Converter
Product Overview
The VI Brick® VTM Current Multiplier
provides extremely fast, efficient, and quiet
fixed ratio voltage division (or current
multiplication). With twelve voltage division
ratios from 1:1 to 1:32, the isolated
VI Brick VTM provides the user with the
flexibility to supply up to 100 A or 120 W at
any output voltage from 1 to 50 Vdc in a
package occupying ~ 2 square inches.
The Military COTS VI Brick VTMs are
optimized for use with the Military
Pre-Regulator Module to implement a
Factorized Power Architecture (FPA).
Together, the PRM® + VTM set provides the
full functionality of a DC-DC converter, but
with breakthrough performance and
flexibility in a rugged, miniature package.
The companion VI Brick PRM for the MT036
family of VI Brick VTMs is the 28 Vdc input
MR028A036M012FP, which operates from
an input range of 16-50 Vdc (the data sheet
is available at vicorpower.com). The VTM can
also be used as a standalone POL product.
By factorizing the DC-DC power conversion
into its essential elements – isolation and
transformation on the one hand, and the
output voltage control and regulation on
the other – and arranging those functions
in a sequence that maximizes system
performance, FPA offers a fundamentally
new and significantly improved approach to
power conversion.
The VI Brick VTM’s fast dynamic response
and low noise eliminate the need for bulk
capacitance at the load, substantially
increasing the POL density while improving
reliability and decreasing cost.
Product Status
Part Number
MT036A011M100FP
MT036A015M080FP
MT036A022M055FP
MT036A030M040FP
MT036A045M027FP
MT036A060M020FP
MT036A072M017FP
MT036A090M013FP
MT036A120M010FP
MT036A180M007FP
MT036A240M005FP
MT036A360M003FP
Product Status
Replaced By
EOL
EOL/NRND
EOL/NRND
EOL/NRND
EOL/NRND
EOL/NRND
EOL/NRND
EOL/NRND
EOL/NRND
EOL/NRND
EOL/NRND
EOL/NRND
none
MVTM36Bx015M080A00
MVTM36Bx022M055A00
MVTM36Bx030M040A00
MVTM36Bx045M027A00
MVTM36Bx605M020A00
MVTM36Bx072M017A00
MVTM36Bx090M013A00
MVTM36Bx120M010A00
MVTM36Bx180M007A00
MVTM36Bx240M005A00
MVTM36Bx360M003A00
NRND = Not Recommended for New Designs
MIL-COTS VTM®
Rev 1.1
vicorpower.com
Page 1 of 13
01/2014
800 927.9474
MT036 SERIES
Not Recommended for New Designs / End of Life - Please see First Page
SPECIFICATIONS
Absolute Maximum Ratings
Parameter
+In to -In
+In to -In
PC to -In
VC to -In
+Out to -Out
Isolation voltage
Output current
Peak output current
Output power
Peak output power
Operating temperature
Storage temperature
Values
-1.0 to 60
100
-0.3 to 7.0
-0.3 to 19.0
Model specific
2,250
Model specific
1.5 • Iout
120
180
-55 to +100
-65 to +125
Unit
Vdc
Vdc
Vdc
Vdc
Vdc
Vdc
A
A
W
W
°C
°C
Notes
For 100 ms
Input to output
Continuous
For 1 ms
Continuous
For 1 ms
M-Grade; baseplate
M-Grade
Note: Stresses in excess of the maximum ratings can cause permanent damage to the device. Operation of the device is not implied at these or any other conditions
in excess of those given in the specification. Exposure to absolute maximum ratings can adversely affect device reliability.
PART NUMBERING
MT
036
A
120
M
Voltage
Transformation
Module
Input
Voltage
Designator
Package
Size
Output
Voltage
Designator
(=VOUT x10)
010
M=
P
Baseplate
Pin Style
Output
Current
Designator
(=IOUT)
Product Grade Temperatures (°C)
Grade
F
Operating
Storage
-55 to +100 -65 to +125
F = Slotted flange
T = Transverse heat sink[a]
[a] Contact
Input Specifications
Parameter
Input voltage range
Min
Typ
Max
Unit
Notes
26
36
50
Vdc
Operable down to zero V with VC voltage applied
1
V/µs
50.5
54.5
Input overvoltage turn-off
55.5
Input current
No load power dissipation
factory
(Conditions are at 36 Vin, full load, and 25°C baseplate unless otherwise specified)
Input dV/dt
Input overvoltage turn-on
P = Through hole
1.5
3.0
Vdc
57.5
Vdc
3.5
Adc
6.0
W
MIL-COTS VTM®
Rev 1.1
vicorpower.com
Page 2 of 13
01/2014
800 927.9474
Continuous
Low line to high line
Not Recommended for New Designs / End of Life - Please see First Page
MT036 SERIES
SPECIFICATIONS CONT.
Output Specifications
Parameter
(Conditions are at 36 Vin, full load, and 25°C baseplate unless otherwise specified)
Min
Typ
Unit
Note
See Table 1
Vdc
No load
K•VIN – lO•ROUT NOM
Vdc
Full load
100
Adc
26 – 50 VIN See Table 1, Page 5
150%
IMAX(A)
Max pulse width 1ms, max duty cycle 10%,
baseline power 50%
INOM(A)
Module will shut down when current limit
is reached or exceeded
Output voltage
Rated DC current
0
Peak repetitive current
DC current limit
Short circuit protection set point
Max
160%
47.4
Current share accuracy
Adc
5
10
%
Module will shut down
See Parallel Operation on Page 8
Efficiency
See Table 2, Page 5
Load capacitance
See Table 2 when used with PRM®
Output overvoltage setpoint
110%
115%
VOUT MAX
250
mV
Output ripple voltage (Typ)
No external bypass
10 µF bypass capacitor
Effective switching frequency
50
2
2.5
3.0
Line regulation
0.99K
K
Load regulation
ROUTMIN
See Figures 2 and 5
20
mV
See Figure 6
3.6
MHz
Model dependent
101K
ROUTMAX
VOUT = K•VIN at no load, See Table 1
mΩ
See Table 1
Transient response
Response time
200
ns
See Figures 7 and 8
Recovery time
1
µs
See Figures 7 and 8
MIL-COTS VTM®
Rev 1.1
vicorpower.com
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01/2014
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MT036 SERIES
SPECIFICATIONS (CONT.)
Environmental Qualifications
Vibration
MIL-STD-810F method 514.5, procedure I, category 14, sine and random vibration for helicopter AH-6J main rotor with an overall level of 5.6grms,
4 hours per axis.
JESD22-B103, Condition B, 2-500Hz 3.10Grms, 30 Min
Shock
MIL-STD-810F method 516.5,Procedure I, 40 g, 15-23 ms saw tooth, 3 +/- shocks per axis, 18 total.
MIL-STD-810F method 516.5, Crash Hazard, Procedure V, 75g, 8-13 ms saw tooth, 3 +/- shocks per axis, 18 total.
JESD22-B104, Condition C 100G.s 2MS 5 shocks in each of 2 directions of 3 orthogonal axes (minimum total of 30 shocks).
Acceleration
MIL-STD 810F method 513.5 procedure I, 2-7 g (table 513.5 II Helicopter) 6 directions.
Salt Atmosphere
MIL-STD-810F Method 509.4 – 48 hr exposure.
Fungus
MIL-STD-810F Method 508.5
Terminal Strength
MIL-STD-202G, Method 211A, Test Condition A
Resistance to Solvents
MIL-STD-202G, Method 215K.
Temperature Humidity Bias (THB)
85°C / 85% RH Bias applied (500 hrs. minimum).
High Temperature Operating Life (HTOL)
JESD22-A-108-B Nom Line Full Load 1000 hrs – Product maintained at maximum operating temperature outlined in published specifications (100ºC).
Temp Cycle
JESD22-A104B -40°C to 125°C (max temperatures dictated by max and min storage specifications outlined in product published specifications),
500 cycles – Max ramp rate 15°C / minute, 8°C / min Nominal. Product tested every 250 cycles.
MIL-COTS VTM®
Rev 1.1
vicorpower.com
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MT036 SERIES
Not Recommended for New Designs / End of Life - Please see First Page
SPECIFICATIONS (CONT.)
TYPICAL WAVEFORMS & PLOTS
Ripple vs. Output Current
120
Output Ripple (mVpk-pk)
100
80
60
40
20
0
2
3
4
5
6
Output Current (A)
7
8
9
10
bypass capacitance. (MT036A120M010FP)
(MT036A120M010FP)
Efficiency vs. Output Current
Power Dissipation
6
5.5
Power Dissipation (W)
94
92
5
Efficiency (%)
4.5
90
4
3.5
88
86
84
1
Figure 2 — Sample output voltage ripple vs. output current with no POL
Figure 1 — Representative input reflected ripple current at full load
96
0
3
2.5
0
1
2
3
4
5
6
Output Current (A)
7
8
9
10
2
0
1
2
3
4
5
6
Output Current (A)
7
8
9
10
Figure 3 — Representative efficiency vs. output current. (MT036A120M010FP)
Figure 4 — Example power dissipation vs. output current. (MT036A120M010FP)
Figure 5 — Sample output voltage ripple at full load; with no POL bypass
Figure 6 — Sample output voltage ripple at full load with 4.7 µF ceramic POL
capacitance. (MT036A120M010FP)
bypass capacitance and 20 nH distribution inductance.
(MT036A120M010FP)
MIL-COTS VTM®
Rev 1.1
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MT036 SERIES
SPECIFICATIONS (CONT.)
TYPICAL WAVEFORMS
Figure 7 — Example load step with 100 µF input capacitance and no output
Figure 8 — Example load step with 100 µF input capacitance and no output
capacitance. (MT036A120M010FP)
capacitance. (MT036A120M010FP)
MIL-COTS VTM®
Rev 1.1
vicorpower.com
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MT036 SERIES
SPECIFICATIONS (CONT.)
Military Cots VTM Family Part Numbers and Ranges
K-Factor
Rated Output
Current (A)
MT036A011M100FP
1/32
MT036A015M080FP
1/24
MT036A022M055FP
Part Number
No Load Output Voltage (Vdc)
Rout (mΩ)
@26 Vin
@ 50 Vin
Min
Nom
Max
100
0.82
1.55
0.5
0.85
1.3
80
1.1
2.0
1.0
1.25
1.5
1/16
55
1.63
3.1
1.4
1.75
2.0
MT036A030M040FP
1/12
40
2.2
4.1
1.45
2.4
3.4
MT036A045M027FP
1/8
27
3.3
6.2
3.5
5.1
6.6
MT036A060M020FP
1/6
20
4.3
8.3
5.0
8.0
10
MT036A072M017FP
1/5
16.6
6.4[a]
10
6.0
9.6
12
MT036A090M013FP
1/4
13.3
6.5
12.5
6.9
9.3
11.6
MT036A120M010FP
1/3
10.0
8.7
16.6
25
31
40
MT036A180M007FP
1/2
6.7
13
25
27.5
35.7
46.4
MT036A240M005FP
2/3
5.0
17.4
33
49.3
70.6
91.8
MT036A360M003FP
1
3.3
26
50
140
170
200
Table 1 — VTM part numbers
[a]
Low line input voltage 32 V
Part Number
Typical Full Load Efficiency at nom Vout (%) Typical Half Load Efficiency at nom Vout (%) Maximum Load Capacitance (µF)
MT036A011M100FP
89.5
91.5
MT036A015M080FP
92
94
48128
27072
MT036A022M055FP
94
94.5
12032
MT036A030M040FP
94
95.0
6768
MT036A045M027FP
95.3
96.5
3008
MT036A060M020FP
95.3
96.8
1692
MT036A072M017FP
96.5
96.5
1175
MT036A090M013FP
96.3
95.5
752
MT036A120M010FP
95.5
95.5
423
MT036A180M007FP
96.0
95.2
188
MT036A240M005FP
95.0
94.8
106
MT036A360M003FP
96
96
47
Table 2 — Typical efficiency and maximum load capacitance, by part number
Control Pin Functions
VC – VTM Control
PC – Primary Control
The VC port is multiplexed. It receives the initial VCC voltage from an
upstream PRM®, synchronizing the output rise of the VTM with the
output rise of the PRM. Additionally, the VC port provides feedback to
the PRM to compensate for the VTM output resistance. In typical
applications using VTMs powered from PRMs, the PRM’s VC port
should be connected to the VTM VC port.
The Primary Control (PC) port is a multifunction port for controlling the
VTM as follows:
In applications where a VTM is being used without a PRM, 14 V must
be supplied to the VC port for as long as the input voltage is below 26 V
and for 10 ms after the input voltage has reached or exceeded 26 V. The
VTM is not designed for extended operation below 26 V. The VC port
should only be used to provide VCC voltage to the VTM during startup.
Disable – If PC is left floating, the VTM output is enabled. To
disable the output, the PC port must be pulled lower than 2.4 V,
referenced to -In. Optocouplers, open collector transistors or relays
can be used to control the PC port. Once disabled, 14 V must be
re-applied to the VC port to restart the VTM.
Primary Auxiliary Supply – The PC port can source up to 2.4 mA
at 5 Vdc.
MIL-COTS VTM®
Rev 1.1
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MT036 SERIES
SPECIFICATIONS (CONT.)
General Specifications
Parameter
Min
Typ
Max
Unit
Notes
MTBF (MT036A120M010FP)
MIL-HDBK-217F
5,046,701
Hours
25°C, GB
908,153
50°C NS
711,584
65°C AIC
Isolation specifications
Voltage
2,250
Vdc
Input to output
pF
Input to output
10
MΩ
Input to output
2,250
Vdc
Input to case / ouput to case
Capacitance
3,000
Resistance
Voltage
Agency approvals
cTÜVus
UL /CSA 60950-1, EN 60950-1
CE Mark
Low voltage directive
Mechanical
See Mechanical Drawings, Figures 12, 13
Weight
1.10/31.3
oz /g
Length
1.91/48,6
in / mm
Baseplate model
Width
1.09/27,7
in / mm
Baseplate model
Height
0.37/9,5
in / mm
Baseplate model
Dimensions
Thermal
Over temperature shutdown
125
130
135
°C
Thermal capacity
23.8
Ws /°C
Baseplate-to-ambient
7.7
°C / W
Baseplate-to-ambient; 1000 LFM
2.9
°C / W
Baseplate-to-sink; flat, greased surface
0.40
°C / W
Baseplate-to-sink; thermal pad
0.36
°C / W
Junction temperature
Auxiliary Pins
Parameter
Min
Typ
Max
Unit
DC voltage
4.8
5.0
5.2
Vdc
Module disable voltage
2.4
2.5
Notes
Primary Control (PC)
Module enable voltage
Current limit
2.4
Disable delay time
Vdc
2.5
2.6
Vdc
VC voltage must be applied when module is
enabled using PC
2.5
2.9
mA
Source only
µs
PC low to Vout low
10
VTM Control (VC)
External boost voltage
12
External boost duration
6
19
10
Vdc
Required for VTM start up without PRM®
ms
Vin > 26 Vdc. VC must be applied continuously
if Vin < 26 Vdc.
MIL-COTS VTM®
Rev 1.1
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MT036 SERIES
PIN / CONTROL FUNCTIONS
+In / -In DC Voltage Ports
The VTM input should not exceed the maximum specified. Be aware of this
limit in applications where the VTM is being driven above its nominal output voltage. If less than 26 Vdc is present at the +In and -In ports, a continuous VC voltage must be applied for the VTM to process power. Otherwise
VC voltage need only be applied for 10 ms after the voltage at the +In and
-In ports has reached or exceeded 26 Vdc. If the input voltage exceeds the
overvoltage turn-off, the VTM will shutdown. The VTM does not have
internal input reverse polarity protection. Adding a properly sized diode in
series with the positive input or a fused reverse-shunt diode will provide
reverse polarity protection.
TM – For Factory Use Only
VC – VTM Control
The VC port is multiplexed. It receives the initial VCC voltage from an
upstream PRM®, synchronizing the output rise of the VTM with the output
rise of the PRM. Additionally, the VC port provides feedback to the PRM to
compensate for the VTM output resistance. In typical applications using
VTMs powered from PRMs, the PRM’s VC port should be connected to the
VTM VC port.
Figure 9 — VI Brick VTM pin configuration (viewed from pin side)
In applications where a VTM is being used without a PRM, 14 V must be
supplied to the VC port for as long as the input voltage is below 26 V and
for 10 ms after the input voltage has reached or exceeded 26 V. The VTM is
not designed for extended operation below 26 V. The VC port should only be
used to provide VCC voltage to the VTM during startup.
PC – Primary Control
The Primary Control (PC) port is a multifunction port for controlling the
VTM as follows:
Disable – If PC is left floating, the VTM output is enabled. To
disable the output, the PC port must be pulled lower than 2.4 V,
referenced to -In. Optocouplers, open collector transistors or relays
can be used to control the PC port. Once disabled, 14 V must be
re-applied to the VC port to restart the VTM.
Primary Auxiliary Supply – The PC port can source up to 2.4 mA
at 5 Vdc.
+Out / -Out DC Voltage Output Ports
The output and output return are through two sets of contact locations.
The respective +Out and –Out groups must be connected in parallel with
as low an interconnect resistance as possible.
To take full advantage of the VTM, the user should note the low output
impedance of the device. The low output impedance provides fast transient response without the need for bulk POL capacitance. Limited-life
electrolytic capacitors required with conventional converters can be
reduced or even eliminated, saving cost and valuable board real estate.
MIL-COTS VTM®
Rev 1.1
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MT036 SERIES
Not Recommended for New Designs / End of Life - Please see First Page
APPLICATION NOTES & TEST CIRCUIT
Parallel Operation
In applications requiring higher current or redundancy, VTMs can be
operated in parallel without adding control circuitry or signal lines. To
maximize current sharing accuracy, it is imperative that the source and
load impedance on each VTM in a parallel array be equal. If VTMs are
being fed by an upstream PRM®, the VC nodes of all VTMs must be
connected to the PRM VC.
To achieve matched impedances, dedicated power planes within the PC
board should be used for the output and output return paths to the
array of paralleled VTMs. This technique is preferable to using traces of
varying size and length.
The VTM power train and control architecture allow bi-directional power
transfer when the VTM is operating within its specified ranges. Bi-directional power processing improves transient response in the event of an
output load dump. The VTM may operate in reverse, returning output
power back to the input source. It does so efficiently.
Anomalies in the response of the source will appear at the output of the
VTM, multiplied by its K factor of 1/8 . The DC resistance of the source
should be kept as low as possible to minimize voltage deviations on the
input to the VTM. If the VTM is going to be operating close to the high
limit of its input range, make sure input voltage deviations will not
trigger the input overvoltage turn-off threshold.
Input Fuse Recommendations
VI Bricks are not internally fused in order to provide flexibility in
configuring power systems. However, input line fusing of VI Bricks must
always be incorporated within the power system. A fast acting fuse is
required to meet safety agency Conditions of Acceptability. The input
line fuse should be placed in series with the +In port. Please see
vicorpower.com for agency approvals and fusing conditions.
Application Notes
Input Impedance Recommendations
To take full advantage of the VTM’s capabilities, the impedance of the
source (input source plus the PC board impedance) must be low over a
range from DC to 5 MHz. The input of the VTM (factorized bus) should
be locally bypassed with a 8 µF low Q aluminum electrolytic capacitor.
Additional input capacitance may be added to improve transient
performance or compensate for high source impedance. The VTM has
extremely wide bandwidth so the source response to transients is usually
the limiting factor in overall output response of the VTM.
www.vicorpower.com/application-notes
Input reflected ripple
measurement point
7 A[a]
Fuse
F1
C1
47 µF
Al electrolytic
For VTM and VI Brick application notes on soldering, thermal
management, board layout, and system design click on the link below:
+IN
C2
0.47 μF
ceramic
14 V +
–
TM
VC
PC
-OUT
R3
10 mΩ
+OUT
C3
10 µF
VTM
-IN
Notes:
1. C3 should be placed close to the load
2. R3 may be ESR of C3 or a separate damping resistor.
[a]
+
+OUT
See Input Fuse Recommendations section
Figure 10 — VI Brick® VTM test circuit
MIL-COTS VTM®
Rev 1.1
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-OUT
Load
–
MT036 SERIES
Not Recommended for New Designs / End of Life - Please see First Page
APPLICATION NOTES (CONT.)
In figures below;
K = VTM transformation ratio
RO = VTM output resistance
Vf = PRM® output (Factorized Bus Voltage)
VO = VTM output
VL = Desired load voltage
FPA ADAPTIVE LOOP
Vo = VL ± 1.0%
VC
PC
TM
IL
NC
PR
+IN
PRM-AL
VH
SC
SG
OS
NC
CD
ROS
RCD
+OUT
Vin
-IN
Factorized
Bus (Vf)
-OUT
VL (Io•Ro)
Vf =
+
K
K
+IN
TM
VC
PC
-IN
+OUT
-OUT
VTM
+OUT
-OUT
L
O
A
D
Figure 11 — The PRM controls the factorized bus voltage, Vf, in proportion to output current to compensate for the output resistance, Ro, of the VTM. The VTM
output voltage is typically within 1% of the desired load voltage (VL) over all line and load conditions.
MIL-COTS VTM®
Rev 1.1
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MT036 SERIES
MECHANICAL DRAWINGS
Baseplate - Slotted Flange
Heat Sink (Transverse)
Figure 12 — Module outline
Recommended PCB Pattern
(Component side shown)
Figure 13 — PCB mounting specifications
MIL-COTS VTM®
Rev 1.1
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MT036 SERIES
Vicor’s comprehensive line of power solutions includes high density AC-DC and DC-DC modules and
accessory components, fully configurable AC-DC and DC-DC power supplies, and complete custom
power systems.
Information furnished by Vicor is believed to be accurate and reliable. However, no responsibility is assumed by Vicor for its use. Vicor makes no
representations or warranties with respect to the accuracy or completeness of the contents of this publication. Vicor reserves the right to make
changes to any products, specifications, and product descriptions at any time without notice. Information published by Vicor has been checked and
is believed to be accurate at the time it was printed; however, Vicor assumes no responsibility for inaccuracies. Testing and other quality controls are
used to the extent Vicor deems necessary to support Vicor’s product warranty. Except where mandated by government requirements, testing of all
parameters of each product is not necessarily performed.
Specifications are subject to change without notice.
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“Express Limited Warranty”). This warranty is extended only to the original Buyer for the period expiring two (2) years after the date of shipment
and is not transferable.
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RESPECT TO THE PRODUCTS, INCLUDING, WITHOUT LIMITATION, ANY WARRANTIES OR REPRESENTATIONS AS TO MERCHANTABILITY, FITNESS FOR
PARTICULAR PURPOSE, INFRINGEMENT OF ANY PATENT, COPYRIGHT, OR OTHER INTELLECTUAL PROPERTY RIGHT, OR ANY OTHER MATTER.
This warranty does not extend to products subjected to misuse, accident, or improper application, maintenance, or storage. Vicor shall not be liable
for collateral or consequential damage. Vicor disclaims any and all liability arising out of the application or use of any product or circuit and assumes
no liability for applications assistance or buyer product design. Buyers are responsible for their products and applications using Vicor products and
components. Prior to using or distributing any products that include Vicor components, buyers should provide adequate design, testing and operating safeguards.
Vicor will repair or replace defective products in accordance with its own best judgment. For service under this warranty, the buyer must contact
Vicor to obtain a Return Material Authorization (RMA) number and shipping instructions. Products returned without prior authorization will be
returned to the buyer. The buyer will pay all charges incurred in returning the product to the factory. Vicor will pay all reshipment charges if the
product was defective within the terms of this warranty.
Life Support Policy
VICOR’S PRODUCTS ARE NOT AUTHORIZED FOR USE AS CRITICAL COMPONENTS IN LIFE SUPPORT DEVICES OR SYSTEMS WITHOUT THE EXPRESS
PRIOR WRITTEN APPROVAL OF THE CHIEF EXECUTIVE OFFICER AND GENERAL COUNSEL OF VICOR CORPORATION. As used herein, life support
devices or systems are devices which (a) are intended for surgical implant into the body, or (b) support or sustain life and whose failure to perform
when properly used in accordance with instructions for use provided in the labeling can be reasonably expected to result in a significant injury to the
user. A critical component is any component in a life support device or system whose failure to perform can be reasonably expected to cause the
failure of the life support device or system or to affect its safety or effectiveness. Per Vicor Terms and Conditions of Sale, the user of Vicor products
and components in life support applications assumes all risks of such use and indemnifies Vicor against all liability and damages.
Intellectual Property Notice
Vicor and its subsidiaries own Intellectual Property (including issued U.S. and Foreign Patents and pending patent applications) relating to the products described in this data sheet. No license, whether express, implied, or arising by estoppel or otherwise, to any intellectual property rights is
granted by this document. Interested parties should contact Vicor's Intellectual Property Department.
The products described on this data sheet are protected by the following U.S. Patents Numbers:
5,945,130; 6,403,009; 6,710,257; 6,911,848; 6,930,893; 6,934,166; 6,940,013; 6,969,909; 7,038,917; 7,166,898; 7,187,263; D496,906;
D505,114; D506,438; D509,472.
Vicor Corporation
25 Frontage Road
Andover, MA, USA 01810
Tel: 800-735-6200
Fax: 978-475-6715
email
Customer Service: [email protected]
Technical Support: [email protected]
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