Datasheet

Ⅶ﹒Reliability test
5
Item Reference documents AEC-Q200 Test Condition Specification
1.High Temperature
MIL-STD-202 Method 108
1.Temperature:
Exposure
2.Time:1000 hours.
1.No mechanical or electrical
damage.
2.Inductance shall not change
2.Temperature Cycling JESD22 Method JA-104
2.Number of cycle:1000 cycle
3.Dwell time:30 minutes
3.Biased Humidity Test MIL-STD-202 Method 103
3.Humidity85±5% RH.
1.Temperature85±5
2.Time:1000 Hours
4.Operational Life
MIL-PRF-27-3.26/4.7.23 &
2.Time:1000 hours.
3.Apply rated current.
5.External Visual
MIL-STD-883 Method 2009
JESD22 Method JB-1006.Physical Dimensions
7.Resistance to solvents
Immerse into solvent for 3±0.5 minutes &
brush 10 times for 3 cycles.
1.No body deformation change in
appearance or obliteration of marking.
MIL-STD-202 Method 215
8.Mechanical Shock
MIL-STD-202 Method 213
1.Peak acceleration100g`s
2.Duration of pulse6ms
3.WaveformHalf-sine
9.Vibration Test MIL-STD-202 Method 204
1.Frequency and Amplitued :10-2000-10 Hz
4.DirectionX , Y , Z
3.Acceleration5g
10.Resistance To
MIL-STD-202 Method 210 &
1.Highest temperature
3.IR reflow times3 times.
Soldering Heat Test
2.Timetemp. 217):60~150 second.
11.ESD
AEC-Q200-002 or
ISO/DIS 10605
12.Solderability Test J-STD-002
1.Baking in pre-testing
150±5 / 16Hours±30 min.
More than 95% soldering coverage min on
terminations.
13.Electrical
User Spec.
1.Operating temperature
Characteriazation
2.Room temperature25.
150
1.Temperature: -55 ~ 150℃℃
1.Temperature: (Temp. rise included)150
more than ±50%.
damage.
2.Inductance shall not change
more than ±50%.
1.No mechanical or electrical
damage.
2.Inductance shall not change
more than ±50%.
1.No mechanical or electrical
damage.
2.Inductance shall not change
more than ±50%.
Inspect product
constructions, marking and
workmanship.
1.No pollution on the surface of
products.
2.Clear marking.
3.No crack.
Verify physical dimensions to
the applicable product detail
specification.
Per product specification
standard
2.Inductance shall not change
more than ±50%.
1.No mechanical or electrical
damage.
2.Inductance shall not change
more than ±50%.
1.No mechanical or electrical
damage.
2.Inductance shall not change
more than ±50%.
1.No mechanical or electrical
damage.
2.Inductance shall not change
more than ±50%.
1.No mechanical or electrical
damage.
2.Inductance shall not change
more than ±50%.
4.Velocity change12.3ft/sec
5.Direction±X, ±Y, ±Z (3times / axis )
15.Board Flex
1.Deflection speed1 mm/ sec
5.Holding time : 60 sec
AEC-Q200-005
2.Amount of deflection2 mm
3.Span90 mm
4.Direction for testBottom of PCB
16.Terminal Strength
AEC-Q200-006
After test, inductors shall be no
mechanical damage.
Test
1.Apply push force to samples
2.Force of 1.8 kg for 60±1 seconds.
1.ESD Voltage15KV
2.Mode 1150 pF / 330 Ω
3.Mode 2150 pF / 2000 Ω
4.Discharge times and polarity
3 times pos. / 3 times eng.
for each condition
2.Peak temperature240±5
3.Timetemp.217):60~150 second.
4.IR reflow times1 times.
1.No mechanical or electrical
damage.
2.Inductance shall not change
more than ±50%.
14.Flammability
1.No mechanical or electrical
damage.
2.Inductance shall not change
more than ±50%.
mounted on PCB.
-55~150℃℃
250±5
User Spec.
J-STD020D.1
MIL-STD-202 Method 304 &
2.Sweep time20 min
5.Number of sweep12 time/axis
1.No mechanical or electrical
PROD.
NAME PAGE
SMD Common Mode Filter
SPECIFICATION
PART NO.
SRF4530A SERIES
REF.:
REV.I(20160309)
BOURNS INDUCTIVE COMPONENTS