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BQ24262_15 Datasheet, PDF (24/56 Pages) Texas Instruments – bq2426x 3-A, 30-V, Host-Controlled Single-Input, Single-Cell Switched-Mode Li-Ion Battery Charger With Power-Path Management and USB-OTG Support
Not Recommended for New Designs : bq24260, bq24261
bq24260, bq24261, bq24261M, bq24262
SLUSBU4D – DECEMBER 2013 – REVISED APRIL 2015
www.ti.com
Device Functional Modes (continued)
9.4.16 External NTC Monitoring (TS)
The I2C interface allows the user to easily implement the JEITA standard for systems where the battery pack
thermistor is monitored by the host. Additionally, the bq24260/1/1M/2 provides a flexible, voltage based TS input
for monitoring the battery pack NTC thermistor. The voltage at TS is monitored to determine that the battery is at
a safe temperature during charging. The JEITA specification is shown in Figure 13.
1.0 C
Charging Current 0.5 C
4.25 V
VBAT 4.15 V
4.1 V
Portion of spec not covered by TS
Implementation on bq2426x
T1
(0°C)
Cold
T2
(10°C)
Cool
T3 T4
(45°C) (50°C)
Warm
T5
(60°C)
Hot
Figure 13. Charge Current During TS Conditions
To satisfy the JEITA requirements, four temperature thresholds are monitored; the cold battery threshold (TNTC <
0°C), the cool battery threshold (0°C < TNTC < 10°C), the warm battery threshold (45°C < TNTC < 60°C) and the
hot battery threshold (TNTC > 60°C). These temperatures correspond to the VCOLD, VCOOL, VWARM, and VHOT
thresholds in the EC table. Charging is suspended and timers are suspended when VTS < VHOT or VTS > VCOLD.
When VCOOL < VTS < VCOLD, the charging current is reduced to half of the programmed charge current. When
VHOT < VTS < VWARM, the battery regulation voltage is reduced by 140mV from the programmed regulation
threshold. The TS function is disabled by connecting TS directly to DRV (VTS > VTSOFF).
The TS function is voltage based for maximum flexibility. Connect a resistor divider from DRV to GND with TS
connected to the center tap to set the threshold. The connections are shown in Figure 14. The resistor values are
calculated using the following equations:
RLO =
VDRV
´ RCOLD
´ RHOT
´
é
ê
ë
1
VCOLD
-
1ù
ú
VHOT û
RHOT
´
é
ê
VDRV
ù
é
- 1ú - RCOLD ´ ê
VDRV
ù
- 1ú
ë VHOT û
ë VCOLD û
(1)
RHI =
VDRV
VCOLD
-1
1
1
RLO + RCOLD
24
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