|
NAME and MAIN TECHNICAL
SPECIFICATIONS |
|
Name |
Basic types of helicopters |
Gear ratio |
Rotor shaft rotation speed, RPM |
N/ Мt
being transferred |
Weight |
|
Intermediate
gearbox
8А-1515-000
|
Mi-8, Mi-8МТ,
Mi-14, Mi-17, Mi-24
and modifications |
1 |
2575 |
184 kW
max 442 kW
|
24,4 |
|
Tail gearbox
246-1517-000
|
Mi-8, Mi-8МТ,
Mi-14, Mi-17, Mi-24
and modifications |
0,4318 |
n1=2575
n2=1112 |
184 kW
max 442 kW
|
58,7 |
|
Wobble plate
8-1950-000
|
Mi-8, Mi-8МТ,
Mi-14, Mi-17
and modifications |
- |
192 |
- |
122 |
|
Wobble plate
24-1940-000
|
Mi-24/25/35
and modifications |
- |
192 |
- |
122 |
|
Tail rotor shaft
8А-1516-000
|
Mi-8, Mi-8МТ,
Mi-14, Mi-17
and modifications |
1 |
2589 |
Мt.=575 N×m
Мt.max=1380 N×m
|
57 |
|
Tail rotor shaft
24-1526-000
|
Mi-24/25/35
and modifications |
- |
n1=3237
n2=2575 |
Мt.1=930 N×m Мt.max1=1425 N×m
Мt.2=905 N×m Мt.max2=1530 N×m |
49,7 |
|
Drive gearbox
24-1512-000
|
Mi-24/25/35
and modifications |
0,795
1,857 |
n1=3237
n2=2575
n3=6011
|
53,7х2 kW
1,8 kW
consumed |
51,3 |
|
Intermediate gearbox
90-1515-000
|
Mi-26
and modifications |
1 |
2685
|
1272 kW
max 2868 kW
|
135 |
|
Tail gearbox
90-1517-000
|
Mi-26
and modifications |
4,848 |
n1=2685
n2=554 |
1272 kW
max 2868 kW
|
348,5 |
|
|
