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p/n 725.0001  REV 1.5 

 

     © 2021 TCW Technologies, LLC. 

Alternately, a ground-based charger is available from TCW Technologies LLC., model # 
IBBS-12v-CHARGER-LI-FE.     This charger may be used for recharging the IBBS unit as 
well as keeping it fully charged during long term product storage.  (9 months or longer) 
 

Battery Capacity:

 

The IBBS provides an energy capacity of 6 amp-hours at 12.8 volts when the system is fully 
charged and operated at 25 C°.   Depending on various conditions including operating and 
storage temperature and age of the battery pack, the capacity of the system will vary. With a 
fully charged battery, the following average performance can be expected in terms of 
operating duration.  The operating duration is for an output voltage down to 9.0 volts. (end 
point voltage).  The battery is also rated for at least 500 shallow discharge cycles, this is 
defined as a10 minute discharge operation at 6 amps followed by 30 minutes of recharge 
time.  
 
Nominal Current Draw                 

Duration  

 

Effective Nominal Capacity 

Total connected load all outputs 
 
1.5  amps  

 

 

 

240 minutes   

 

6 amp-hrs 

 

3.0 amps   

 

 

 

110 minutes   

 

5.5 amp hrs. 

6.0 amps   

 

 

 

55 minutes   

 

5.5 amp-hrs 

8.0 amps   

 

 

 

37 minutes                

5.0 amp hrs. 

 
Capacity at Low Temperatures:    
 
-18 C°      75% of effective nominal capacity 
-30 C°  

70% of effective nominal capacity  

-40 C° 

45% of effective nominal capacity 

 

 

 

Servicing: 

The internal battery in the IBBS system is replaceable; however, the IBBS product must be 
returned to TCW Technologies, LLC. for this service.  Battery life depends strongly on many 
factors including operating and storage temperature, number of discharge cycles and depth 
of discharge.  The battery capacity should be checked at least annually for suitable back-up 
power operation of the connected equipment.  When the battery capacity no longer meets 
the operating criteria of the aircraft it must be replaced.  Contact TCW Technologies, LLC. 
regarding battery replacement. 
 

Storage beyond 9 months: 

If the IBBS unit is to be stored without connection to the aircraft for a period greater than 9 
months it must be connected to a source of DC power to maintain the bat

tery’s charge.   Only 

connections to the ground terminal and the main power terminal are required.   Connect Pin 
5 (main power) and Pin 9 (ground) of the IBBS to any source of regulated DC power at 14-15 
volts with a current capability of at least 3.3 amps to accomplish full recharging.  Ensure the 
IBBS unit is in an ambient temp of 0-40 C° for ground-based charging.   Charger model 
IBBS-12v-CHARGER-Li-Fe is available from TCW Technologies, LLC. to simplify this 
activity. 

 
 
 

Содержание IBBS-12v-6ah-CRT

Страница 1: ...back up power to critical electronic loads such as EFIS GPS Autopilots Radios and engine monitor systems Integral to the IBBS is a lithium iron phosphate battery pack and a matched charging system to...

Страница 2: ...ElectroAir electronic ignitions IBBS must be installed using the current aircraft standards and practices as shown in AC 43 13 2A 1B IBBS products are covered by US Patent 8 189 305 Table of Contents...

Страница 3: ...he IBBS must be connected to the back up power input of the respective device For equipment having only a single power input terminal the IBBS pass thru power function must be utilized This is typical...

Страница 4: ...aths feeding the connected loads These pins are internally wired in parallel it is recommended to populate all three pins join the wires together and feed all of these inputs from the pass thru power...

Страница 5: ...he following EFIS systems wire pin 2 to the Volts2 input of the EFIS or engine monitor as follows 8 Complete the installation of the wiring harness and connector prior to attaching the connector to th...

Страница 6: ...aircraft bus falls below 11 volts Pin 1 is pulled to ground when the back up master switch is turned on this enables the IBBS system If the back up power master switch is enabled and normal aircraft p...

Страница 7: ...city at Low Temperatures 18 C 75 of effective nominal capacity 30 C 70 of effective nominal capacity 40 C 45 of effective nominal capacity Servicing The internal battery in the IBBS system is replacea...

Страница 8: ...Master Switch ensure the connected equipment remains energized The low voltage warning light should go out If a separate avionics bus is utilized this may need to be turned ON to continue the operatio...

Страница 9: ...from the IBBS product 4 Measure and record at least the following information The time until the first piece of connected equipment no longer functions or the time until the output of back up power s...

Страница 10: ...h 2 Select engine operation based on the use of only the electronic ignition module provided with back up battery power 3 PULL the circuit breaker feeding pins 4 5 of the IBBS system confirm engine co...

Страница 11: ...gine is properly returned to the off position by following normal run and shut down procedures 10 After completing these tests recharge the IBBS product by operating the system normally for up to 1 5...

Страница 12: ...volts Charger Integral high performance fast charger with cell balancing and thermal monitoring Surge Protection 34 volt active clamp 1500w 10 1000uS waveform Wiring 15 pin male D sub on product Encl...

Страница 13: ...e Lithium Battery Systems Environmental Qualification RTCA DO 160 F B2BBBSC1XYXXFSZB IX XXXXAZ ZC TT MA3H3L3XXAX DO 160 G Section 14 cat S Section 8 cat S c1 Section 7 cat B Section 22 cat A3H3L3 Powe...

Страница 14: ...wiring harness View from back of connector Pin Function 5 PWR in charge sensing 2 Batt info 3 Low Volt Warn 12 Output 13 Output 14 Output 15 Output 6 Pwr pass thru input 1 Enable backup switch 9 Groun...

Страница 15: ...725 0001 REV 1 5 2021 TCW Technologies LLC 15 Product mounting footprint 4 mounting holes 0 190 1 50 7 25 2 290 7 70 Top View 0 225 All dimensions in inches Product height 2 75 C G at center of all a...

Страница 16: ...12V 6AH CRT Input 10 15 volts DC Output 12 volts 8 amps INTEGRATED Back up Battery SYSTEM Back up power output 20 awg 10 amp Main Aircraft Bus charge sense pass thru Pin Function 15 pin Male Dsub on u...

Страница 17: ...er Battery Info Back up power output 20 awg 22 awg 22 awg 20 awg 20 awg 20 awg 1 6 9 10 2 5 12 main power input 15 pin female Dsub connector 3 Low Voltage Warning LED NOTE Use redundant ground pins 9...

Страница 18: ...0 awg 20 awg 1 6 9 10 2 5 12 Main power input 15 pin female Dsub connector 3 Low Voltage Warning LED NOTES 7 11 10 amp 8 13 14 15 output output output Back up power input 3 Use of power pins will powe...

Страница 19: ...00 ft 15 000 temp variation 5 Category B Humidity 6 Category B operational shock 7 Category B vibration 8 Category S curve C explosion 9 Category X waterproofness 10 Category Y fluid susceptibility 11...

Страница 20: ...designed and manufactured RETURN OR REPLACED COMPONENTS any item to be replaced under this Warranty must be returned to TCW Technologies in Emmaus PA or such place as TCW may designate freight prepaid...

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