|
Technical data
The AE3007 turbofan engine is a high bypass (5:1),
two spool, axial-flow engine, flat rated at 7,580 pounds
of thrust, uninstalled, sea level static to 113°F
ambient temperature.
The design features include:
- wide-chord single-stage direct-drive fan
- 14-stage axial-flow compressor with inlet guide
vanes (IGVs) and five variable-geometry-stator stages
- full annular type combustion liner with 16 fuel
nozzles and two high tension igniters
- two-stage HP turbine driving the HP compressor
- three-stage LP turbine to drive the fan
- dual aircraft mounted, fully-redundant FADECs
- accessory-drive gearbox for engine-driven accessories
and air system for aircraft pressurisation, engine
starting, and cross bleed starts
| Engine |
EIS |
Power |
Applications |
Seats |
Range
(nm)* |
| AE3007A |
1997 |
7,580lb
34kN |
ERJ 145ER |
50 |
1060 |
 |
|
|
|
|
|
| AE3007A1 |
1998 |
7,580lb
34kN |
ERJ 145LR |
50 |
1550 |
|
|
|
|
|
|
| AE3007A1/1 |
1998 |
7,580lb 34kN |
ERJ 145LR |
50 |
1550 |
|
|
|
|
|
|
| AE3007A1P |
1999 |
7,580lb
34kN |
ERJ 145LR |
50 |
1550 |
|
|
|
|
|
|
| AE3007A1P |
2002 |
7,580lb
34kN |
Legacy - Executive |
50 |
1550 |
|
|
|
|
|
|
| AE3007A1E |
2002 |
8,110lb
36kN |
ERJ 145XR |
50 |
2000 |
|
|
|
|
|
|
| AE3007A1E |
2002 |
8,110lb
36kN |
Legacy |
50 |
2000 |
|
|
|
|
|
|
| AE3007A1/3 |
2001 |
7,201lb
32kN |
ERJ 140 |
44 |
1630 |
|
|
|
|
|
|
| AE3007A1/3 |
1999 |
7,201lb
32kN |
ERJ 135LR |
37 |
1700 |
|
|
|
|
|
|
| AE3007A1/3 |
2001 |
7,201lb
32kN |
Legacy |
37 |
- |
|
|
|
|
|
|
| AE3007A3 |
1999 |
7,000lb
31kN |
ERJ 135 |
37 |
1400 |
|
|
|
|
|
|
| AE3007C |
2002 |
6,442lb
30kN |
Citation X |
- |
3300 |
|
|
|
|
|
|
| AE3007C1 |
2002 |
6,764lb
37kN |
Citation X |
- |
3300 |
|
|
|
|
|
|
| AE3007H |
- |
8,290lb
37kN |
Global Hawk |
- |
- |
|
|
|
|
|
|
| *Aircraft Manufacturer's Data |
|
