Guinault GA100V40D1100

Length 3300
Width 1880
Height 1765
Weight 2100

The Ground power unit produces 400Hz and 28VDC
power to supply the aircraft during a stop on the ground.
The unit can be operated for maintenance and handling purposes.

The engine, driving the alternator, settles the frequency
of the alternative generation.
The electronic speed regulation ensures the stability
of the performances in continuous working and during transiants,
as per GPU performances and ain compliance
with the standards in force

When the alternator is driven by the engine at its nominal power,
the alternator supplies the power required by the aircraft,
up to the dimensioning nominal power and admissible overloads.
The voltage regulator ensures the stability
of the performances in continuous working
and during the load transients, in compliance with the standards in force

Technical data:
Distribution according to request : 1 (or 2)×400 Hz circuit (s), 1×28VCC circuit, 1×50 Hz circuit
Nominal power of the 400 Hz generation : 100 kVA at p.f. 0,8
admissible overload on the 400 Hz generation : 112 kVA at p.f. 0,8 during 5mn
Nominal power of the 28 VCC generation : 600A permanent
admissible overloads on the 28 VCC generation : 800A functional overloads / 2400A at instantaneous peak
Nominal power of the 50 Hz generation : 2.2 kVA at p.f. 0,8
Diesel engine : IVECO type NEF45 TM2 at 2182 rpm
400 Hz GUINAULT alternator type AS250M150V3
GUINAULT transformer rectifier unit (TRU) type RS493
Operating temperature : - 20°C to + 50°C