MAX KINGSLEY-JONES / SINGAPORE
Boeing plans to retain the General Electric CF6-80C2 for its latest 747-400 development after confirming its aim to launch in June. But Rolls-Royce is pushing for its new Trent 600 to be offered on the aircraft. Dubbed the 747-400X Quiet Longer Range (QLR), the model's development schedule calls for service entry in March 2004, equipped with the 63,300lb-thrust (280kN) CF6-80C2B9F.
Talks are being held with R-R about a Trent 600-powered version, and the UK manufacturer says it could meet a mid-2004 in-service date. Boeing has been working with all three 747 engine suppliers - GE, R-R and Pratt & Whitney - but GE is leading the programme. The R-R RB211 is not powerful enough for the QLR, so R-R is proposing its 63,000lb-thrust Trent 600, derived from the Trent 500.
Boeing vice president 747 programme Jeff Peace says: "[Trent 600] timing isn't right due to engine/airframe integration issues, such as the availability of a strut."
The QLR project, which Boeing says is now at "offerable" status, comprises aerodynamic changes, increased weights, more powerful, acoustically treated engines and a new interior (Flight International, 12-18 February). Passenger and freighter versions are offered, and Boeing is believed to have presented the aircraft to Cathay Pacific and Singapore Airlines.
At take-off weights of up to 396,900kg (875,000lb), the QLR will offer slightly better (+3%) range performance than the current 747-400, and complies with stringent QC2 departure noise limits at London Heathrow. If QC2 compliance is not needed, the aircraft can operate at its new structural maximum take-off weight of 417,800kg to provide between 5% and 15% more range (see table).
Using a predetermined departure profile, Peace says the thrust rating will be used to its maximum level to achieve rapid acceleration and lift-off, then the thrust will be manually reduced to pre-determined levels to reduce noise.
"The Trent 600 would provide better performance and noise margins," says R-R executive vice president airlines Charles Cuddington.
The wing will be modified with a new raked wingtip, and a trailing-edge wedge on new outboard double-slotted flaps, which combine to improve aerodynamic efficiency and provide a 1-2% reduction in fuel consumption.
TABLE: Boeing 747-400XQLR specification | |
Wingspan | 68.7m |
Maximum take-off weight | 417,800kg |
Maximum fuel capacity | 248,700 litres |
Range (at QC2 compliance)* | 13,900km |
Range (Maximum/416 pax)** | 14,920km |
Range (Maximum/250 pax)** | 15,840km |
Cruise speed Mach | 0.86 |
Engine thrust (GE engine) | 63,300lb |
*396,900kg MTOW ** 417,800kg MTOW Freighter version has MTOW of 412,800kg, maximum range of 9,530km with payload of 112,800kg Source: Boeing |
Source: Flight International