GE 90 engine Info
The following is mindless information for those who have nothing to do today. (I'm having a slow day too)
The first General Electric-powered Boeing 777 was delivered to British Airways on November 12, 1995;
[11] the aircraft, with two GE90-77Bs, entered service five days later.
[12] Initial service was affected by
gearbox bearing wear issues, which caused the airline to temporarily withdraw its 777 fleet from
transatlantic service in 1997.
[12] British Airways' aircraft returned to full service later that year,
[13] and General Electric subsequently announced engine upgrades.
Records[edit]
According to the
Guinness Book of Records, at 127,900 pounds-force (569 kN)f, the engine holds the record for the highest thrust (although rated at 115,300 pounds-force (513 kN)f). This thrust record was accomplished inadvertently as part of a one-hour, triple-red-line engine stress test. In order to accommodate the increase in torsional stresses an entirely new steel alloy (GE1014) had to be created and then machined to extreme tolerances.
[14] The new record was set during testing of a GE90-115B development engine at GE Aviations' Peebles Test Operation, which is an outdoor test complex outside Peebles, Ohio. It eclipsed the engine's previous Guinness world record of 122,965 pounds-force (546.98 kN).
[15]
On November 10, 2005, the GE90 entered the Guinness World Records for a second time. The GE90-110B1 powered a 777-200LR during the world's longest flight by a commercial airliner, though there were no fare-paying passengers on the flight, only journalists and invited guests. The 777-200LR flew 13,422 miles (21,601 km) in 22 hours, 42 minutes, flying from
Hong Kong to
London "the long way": over the Pacific, over the continental U.S., then over the Atlantic to London.
[16] (The longest flight by a commercial airliner with passengers is 18.5 hours, flown by an
Airbus A340-500 aircraft on a daily
non-stop flight from New York to Singapore on
Singapore Airlines. See
Singapore Airlines Flight 21)
Variants
GE90-76B rated at 76,000 lbf (338.1 kN)
GE90-77B rated at 77,000 lbf (342.5 kN)
GE90-85B rated at 85,000 lbf (378.1 kN)
GE90-90B rated at 90,000 lbf (400.3 kN)GE90-92B rated at 92,000 lbf (409.2 kN)
GE90-94B rated at 93,700 lbf (417 kN)
GE90-110B1 rated at 110,100 lbf (489.3 kN)
GE90-115B rated at 115,300 lbf (514 kN)
Specifications (GE90-115B)[edit]
General characteristics
- Type: axial flow, twin-shaft, bypass turbofan engine
- Length: 287 in (7,290 mm)[19]
- Diameter: overall: 135 in (3.429 m);[19] fan: 128 in (3.251 m)
- Dry weight: 18,260 lb (8,283 kg)[19]
Components
- Compressor: axial: 1 wide chord swept fan, 4 low pressure stages, 9 high pressure stages
- Turbine: axial: 6 low pressure stages, 2 high pressure stages
Performance