Specifications
Data from.
This engine is a dual rotor, axial flow, high bypass ratio turbofan. The 10-stage high pressure compressor is driven clockwise (Aft Looking Forward) by a 2-stage high pressure turbine. The single stage fan and 4-stage low pressure compressor are driven counterclockwise (Aft Looking Forward) by a 7-stage low pressure turbine. The engine control system includes a Full Authority Digital Engine Control (FADEC), which has an aircraft connection for digital communication. An engine monitoring unit (EMU) provides vibration level signals to the aircraft.
| Engine Model |
Arrangement | Performance | Dimensions (inch) and Weight (lb) | Certified (FAA) |
Application | Entry Into Service | Emissions | ||||||||||||||||||
| Fan diameter (in) |
Fan | LPC | HPC | LPT | HPT | Thrust Max (lbf) | Flat-Rated Temp C | Overall Pressure Ratio (OPR) |
Fan Bypass Ratio (BPR) |
Air flow (kg/s) |
SFC (max power) |
T/W Ratio |
Length | Max Envelope | Weight (Dry) |
CO | NOx | HC | |||||||
| Take-off (5 min) |
Max Cont. |
Take-off | Max Cont. |
Width | Height | ||||||||||||||||||||
| GEnx-1B54 | 111 | 1 | 4 | 10 | 7 | 2 | 57,400 | 56,300 | ISA+15 | ISA+10 | 36.0 | 4.48 | 194.0 | 139.0 | 137.0 | 12,822 | Mar 31, 2008 | B787-3 | |||||||
| GEnx-1B58 | 111 | 1 | 4 | 10 | 7 | 2 | 61,000 | 56,300 | ISA+15 | ISA+10 | 4.76 | 194.0 | 139.0 | 137.0 | 12,822 | Mar 31, 2008 | B787-3,-8 | ||||||||
| GEnx-1B64 | 111 | 1 | 4 | 10 | 7 | 2 | 67,500 | 61,500 | ISA+15 | ISA+10 | 41.0 | 5.23 | 194.0 | 139.0 | 137.0 | 12,822 | Mar 31, 2008 | B787-8,-9 | |||||||
| GEnx-1B67 | 111 | 1 | 4 | 10 | 7 | 2 | 69,400 | 61,500 | ISA+15 | ISA+10 | 43.0 | 5.41 | 194.0 | 139.0 | 137.0 | 12,822 | Mar 31, 2008 | B787-8,-9 | |||||||
| GEnx-1B70 | 111 | 1 | 4 | 10 | 7 | 2 | 72,300 | 66,500 | ISA+15 | ISA+10 | 43.0 | 9.6:1 | 5.64 | 194.0 | 139.0 | 137.0 | 12,822 | Mar 31, 2008 | B787-8,-9 | ||||||
| GEnx-2B67 | 105 | 1 | 3 | 10 | 6 | 2 | 67,400 | 58,500 | 43.0 | 8.6:1 | 185.0 | 127.0 | 127.0 | 12,400 | July 22, 2010 | B747-8 | |||||||||
Note: Data for sea level static, standard pressure, no customer bleed or customer horsepower extraction, ideal inlet, 100% ram recovery, production aircraft flight cowling, production instrumentation, fuel lower heating value of 18,400 BTU/lb.
Note: 787-3 plans were cancelled on December 13, 2010 due to low demand.
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