TCW Technologies IBBS-12v-3ah-CRT-V Скачать руководство пользователя страница 6

                       p/n 725.0002  REV 3.0 

 

© 2023 TCW Technologies, LLC. 

 

5. 

The Back-up Power Master switch must be utilized to turn the back-up battery 

system off when not in use.  The back-up power master switch gives the pilot the ability to 
turn the back-up battery system off.  In some installations this may be the only means to 
shut down the connected equipment.  
 

6. 

The IBBS unit has a low voltage warning output, pin 3.   This pin may be used to 

drive an LED indicator or to provide a digital signal to indicate the main input bus is in a 
low voltage condition.   When the main input bus (connected to pin 5) falls below about 11 
volts this output will drive to a low state.   Maximum current sourced into this pin is 25 
milliamps. 
 

7. 

 The IBBS unit has in internal battery monitor connection, pin 2.  This pin allows the 

voltage state of the internal battery to be monitored with a separate volt meter or an 
analog input of a monitor system.  This pin will only report internal battery voltage when 
the unit is enabled by turning the Back-up Master switch ON.  A fully charged battery back 
will indicate about 13-14.7 volts on this pin. 

 

 

Important note:  the meter utilized to measure pin 2 must have an input impedance 
>100k ohms otherwise it will load down pin 2 and provide an artificially low voltage 
reading. 

 
 

When used with the 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 the IBBS product.  It is essential to ensure the wires do not inadvertently 
short together during installation.  Remember, the IBBS pack is a back-up source of 
power and is ready to deliver output power even when the aircraft electrical system is in 
the off state. 
 

9. 

    When using the IBBS product to provide back-up power to an electronic ignition 

system it MUST be used to back-up one and only one electronic ignition module.  Do not 
use one IBBS to back up both electronic ignition modules in a dual electronic ignition 
system.   Follow the instructions per the electronic ignition manufacture.   Do not connect 
any other loads to the IBBS when using the IBBS to power an electronic ignition module. 
Do not use the IBBS system to back-up a dual ignition system having only a single power 
input that feeds both ignition system.  Do not use a single IBBS system to back-up two 
electronic ignition systems. 

 

 
 
 

Manufacturer/model 

Volts 2 input location 

Garmin   G3x system    GEA 24 

J244, Pin 28 

Advanced Flight Systems 5000 series: 

Expansion Port   Pin 13 

Содержание IBBS-12v-3ah-CRT-V

Страница 1: ...by integrating all of the key elements in a single enclosure The IBBS system provides back up power to critical electronic loads such as EFIS GPS Autopilots Radios Electronic Ignition systems and engi...

Страница 2: ...lots JPI and EI engine monitors SureFly electronic ignitions Lycoming EIS electronic ignitions and ElectroAir electronic ignitions IBBS must be installed using the current aircraft standards and pract...

Страница 3: ...mance Specifications and potential limitations and ratings under various conditions including environmental and application installations See Item 3 below for installation location limitations Install...

Страница 4: ...rt The vent port must be routed to the bottom or side exterior of the aircraft via the vent hose Locate a suitable flat location measuring at least 3 3 x 12 in area or in an existing avionics rack for...

Страница 5: ...atically transfers the load current on the output pins to the internal back up battery source Pin 5 nominal current draw is 3 3 amps during charging Pin 4 provides power to an internal battery heater...

Страница 6: ...ve an input impedance 100k ohms otherwise it will load down pin 2 and provide an artificially low voltage reading When used with the following EFIS systems wire pin 2 to the Volts2 input of the EFIS o...

Страница 7: ...Power Master Switch The IBBS has one input switch connection as identified in the wiring diagrams Back up Power Master This switch enables back up power from the IBBS system to be available on the ou...

Страница 8: ...Low Temperatures 18 C 75 of effective nominal capacity 30 C 70 of effective nominal capacity 45 C 45 of effective nominal capacity Servicing The internal battery in the IBBS system is replaceable howe...

Страница 9: ...test ensures the transfer circuit and back up battery are properly working 4 Verify the low voltage warning light is indicating a low voltage condition 5 Turn on the Aircraft Master Switch ensure the...

Страница 10: ...p n 725 0002 REV 3 0 2023 TCW Technologies LLC 10 3 Land aircraft as soon as practical to resolve the loss of main electrical power...

Страница 11: ...nstallation approval The internal battery is not field replaceable The IBBS unit must be returned to TCW Technologies LLC for all repair and servicing requirements Endurance testing 1 Turn off the Air...

Страница 12: ...FAA approved revision The use of alternate models will require a new FAA installation approval The internal battery is not field replaceable The IBBS unit must be returned to TCW Technologies LLC for...

Страница 13: ...and ensure aircraft engine 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 n...

Страница 14: ...d transient load 30 second duration max Battery Internal sealed Li Fe PO4 nominal 12 8 volts Charger Integral high performance fast charger with cell balancing and thermal monitoring Surge Protection...

Страница 15: ...erational Performance Standards for Rechargeable Lithium Battery Systems Environmental Qualification RTCA DO 160 g B2BBBSC1EYXXFSZB IX XXXXAZ ZC TT MA3H3L3XXAX Power input 14 volts nominal 1 8 amps ch...

Страница 16: ...0 temp variation 5 Category B Humidity 6 Category B operational shock 7 Category B vibration 8 Category S curve C explosion 9 Category E waterproofness 10 Category Y fluid susceptibility 11 Category x...

Страница 17: ...ss View from back of aircraft wiring harness 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 sw...

Страница 18: ...p n 725 0002 REV 3 0 2023 TCW Technologies LLC 18 IBBS unit mounting footprint 11 16in 2 00in Mounting holes 0 188 4 plcs All dimensions in inches IBBS unit height 3 2 C G at center of all axis...

Страница 19: ...aus PA USA IBBS 12V 3AH CRT V Input 13 16 volts DC Output 12 volts 5amps INTEGRATED Back up Battery SYSTEM Back up power output 20 awg Main Aircraft Bus charge sense pass thru Pin Function 15 pin Male...

Страница 20: ...Power Master 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 gro...

Страница 21: ...nfo 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 NOTES 7 11 8 13 14 15 output output output ww...

Страница 22: ...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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