| General Information |
| Type |
D-18T |
| Isp |
9000sec |
| Isp (sea level) |
8000sec |
| Burn Time |
3375sec |
| Chambers |
1 |
| Weight and size |
| Dry Weight |
4100kg |
| Length |
5.4m |
| Width |
2.937m |
| Height |
2.792m |
| Takeoff regime |
| Thrust |
23430kg |
| Specific fuel consumption |
0.350kg/kgf/h |
| Turbine inlet temperature |
1600°K |
| Cruising regime (ISA conditions) |
| Altitude |
11000km |
| Speed |
Mach 0.75 |
| Thrust |
4860kg |
| Pressure ratio |
27.5 |
| Bypass ratio |
5.7 |
| Specific fuel consumption |
0.570kg/kgf/h |
| Turbine inlet temperature |
1395°K |
D-18 by Lotarev
(G.A.Ivchenko
-Progress Design Bureau)
32k photo, courtesy of
Rick Slobodian
The D-18T engine was selected in
1984
to power world mightiest transport planes - An-124 Ruslan and
An-225 Mria.
The advantages of the engine:
- High takeoff thrust
- Low specific fuel consumption
- High reliability (meeting the FAR and BCAR airworthiness requirements)
- Long-term service life
- Low levels of noise and contaminants emission (meeting ICAO standards)
- Ease of maintenance and high repairability.
- The engine is equipped with the efficient thrust reverser installed in the fan duct.
Three-shaft modular engine became a base model for entire line of XXI century
aircraft engines with static thrust up to 30t. Gas dynamic quality and high thermal cycle
parameters of the D-18T allow to use it as a heart of
gas
turbine installations with shaft power of 25 to 30MW.
| Engine Modules: |
| Fan fairing |
Fan wheel |
Fan shaft with bearing |
| Fan casing |
Fan stator blades |
Intermediate pressure compressor |
| Main module |
Thrust reverser |
Combustion chamber |
| HP turbine rotor |
Turbine bearing cases |
IP turbine rotor |
| Fan turbine |
Rear bearing assembly |
Rear mount |
| Exhaust cone |
Exhaust nozzle |
|
D-18T engine is manufactured by the
Zaporozhye Motorostroitel Industrial
Association in cooperation with ZMDB "Progress".
| D-18T |
1984 |
bypass turbojet |
32,430kg (??27,500kg) 229,5kN |
|
| D-18TM |
? |
bypass turbojet |
25,000kg |
|
| D-18TP |
? |
bypass turbojet |
27,500kg |
|