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The generator operation principle is identical to that
of the main or auxiliary generation. The generator
output characteristics are:
- three phase 115/200V. 400Hz (12000RPM)
- output power: 5KVA continuously
CSM/G CONTROL UNIT SUPPLY
Battery 2 (during transient configuration) and then
the Permanent Magnet Generator supplies the Constant
Speed Motor/Generator control unit and the exciter
field through a voltage regulation module.
The voltage regulation module maintains the Point Of
Regulation (POR) at a nominal voltage value (115V).
TMUELAS02-T01 LEVEL 3
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AC GENERATION - EMERGENCY GENERATION D/O
TMUELAS02-P01 LEVEL 3
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AC GENERATION - EMERGENCY GENERATION D/O
GENERATOR OPERATION CONTROL
As the Emergency AC generator parameters are correct,
the Emergency Generator Line Contactor is supplied by
the Constant Speed Motor/Generator control unit.
The Emergency AC generator has priority to supply the
AC and DC ESSential Buses (Contactors 3XC1 and 3XC2
are de-energized by relay 12XE).
TMUELAS02-T02 LEVEL 3
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AC GENERATION - EMERGENCY GENERATION D/O - GENERATOR OPERATION CONTROL
TMUELAS02-P02 LEVEL 3
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AC GENERATION - EMERGENCY GENERATION D/O
GENERATOR MONITORING
The Constant Speed Motor/Generator operation is
monitored by the red FAULT light.
The FAULT light activation is controlled by either
Battery Charge Limiter (BCL1 or 2).
During transient configuration or if the generator is
faulty, there is no ESS TR output, thus the fault light
comes on.
TMUELAS02-T03 LEVEL 3
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AC GENERATION - EMERGENCY GENERATION D/O - GENERATOR MONITORING
TMUELAS02-P03 LEVEL 3
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SELF EXAMINATION
With the Main Landing Gear not compressed, and
after AC Bus 1 and 2 failures, when does the RAT
and EMER GEN FAULT light come on?
A - When the static inverter is lost.
B - When the AC and DC ESS buses are lost.
C - When the ESS TR is lost.
When does the CSM/G supply the DC and AC ESS buses?
A - When AC Bus 1 or 2 is lost.
B - When the Emergency Generator parameters
are correct.
C - As soon as BAT 2 is lost.
TMUELAS02 LEVEL 3
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24 - ELECTRICAL POWER
24-24-00 EMERGENCY ELECTRICAL POWER LOGIC
DESCRIPTION
CONTENTS:
Emergency Generation Automatic Operation
Emergency Generation Manual Operation In Flight
Emergency Generation Manual Operation On Ground
Emergency Generator Test
Self Examination
TMUELE502 LEVEL 1
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EMERGENCY ELECTRICAL POWER LOGIC DESCRIPTION
EMERGENCY GENERATION AUTOMATIC OPERATION
If AC BUS 1 and 2 are lost above a given airspeed
(100Kts), the Ram Air Turbine will extend
automatically.
As the AC generator is not yet available, the AC ESS
BUS and DC ESS BUS are respectively supplied by the
STATIC INVERTER and BATTERY 2.
The activation of the emergency generator via the blue
hydraulic system takes place only if the landing gear
is not compressed.
When the EMER GEN is available, it supplies the AC ESS
　
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