GP7000
The GP7000 is developed, manufactured and marketed by Engine Alliance, a joint venture of GE Aviation and Pratt & Whitney. Other partner sharing in this engine program are MTU, Snecma and Techspace Aero. MTU has taken on responsibility for the development and manufacture of the low-pressure turbine and the turbine center frame. The company also manufactures components for the high-pressure turbine.
The GP7000 engine family powers long-haul aircraft. Flight certification of the GP7000-powered Airbus A380 was obtained in late 2007. The aircraft entered revenue service in August 2008 and is setting a new benchmark in terms of reliability, fuel consumption and noise emissions in its class.
| Technical Data |
|
|
Thrust |
340 kN |
|
Bypass ratio |
9:1 |
|
Pressure ratio |
43.9:1 |
|
Length |
4740 mm |
|
Fan Diameter |
2950 mm |
Facts – GP7000
- Two-shaft turbofan
- Five stage low-pressure compressor
- Nine stage high-pressure compressor
- Two-stage high-pressure turbine
- Six-stage low-pressure turbine
- High fuel efficiency at cruise
- Low noise
- Low weight
Development
- Low-pressure turbine
- Turbine center frame
Production
- High-pressure turbine
- Low-pressure turbine
- Turbine center frame
MTU share
22,5%
Applications & Partners
![]() |
||
| Airbus A380 |
Partners
- General Electric
- Pratt & Whitney
- Snecma Moteurs
- Techspace Aero

Print
