Technical details
Designed to power
the Airbus Military A400M military transport, the TP400 will be the most
powerful turboprop engine to enter service in the West.
Engine
characteristics
| Type
of Engine |
three-shaft
turboprop |
| Power
output |
approximately
11,000 shp at sea level |
| Pressure
ratio |
25 |
| Weight |
approx.
1,900kg (dry) |
| Length |
3,5 m
overall engine length |
| Diameter |
0,92m |
| Compressor |
5
intermediate pressure stages, 6 high pressure stages |
| Turbine |
1 high
pressure stage, 1 intermediate pressure stage,
3 low pressure stages |
The
TP400-D6 is tailored for A400M mission requirements
-
Component technology based on best
in service military and commercial practice
-
Proven
three-shaft architecture
-
Moderate
temperatures for long life
-
Modular
design for maintainability and low life cycle costs
-
Meets
future noise and emissions regulations
The
TP400 is designed for optimum maintainability
-
Full
module interchangeability
-
Quick
LRU (Line Replacement Unit) replacement
-
Dedicated
on-wing boroscope ports
-
FADEC
built-in test functions
-
Engine
replacement within 4 hours
|
