| FULL NAME | INTEGRATED DRIVE GENERATOR 23 |
DESCRIPTION
GP-23 is a primary source of constant frequency AC power of the aircraft electrical system. It consist of an alternator driven by a hydromechanical constant speed drive. The constant speed drive provides the alternator shaft rotational speed of 12000 rpm.
CHARACTERISTICS
| Rated power | 60 kVA |
| Working fuel temperature | -40…+160 °С |
| Environment temperature | -60…+185 °С |
| The frequency of the input revolutions | 4700-8480 rpm |
| Working fuel | ИПМ-10, Турбоникоил 210А |
| AC current frequency | 400±4 Hz |
| Rated current voltage | 120/208 V |
| Altitude | 22 000 m |
| Mass | 52 kg |
| Overall dimensions | 544×270 mm |
INTEGRATION
| Aircraft | An-72 |
| Aircraft | An-124 |
| Aircraft | An-225 |
| Aircraft | Tu-22 |
| Aircraft | Tu-26 |