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Dream Liner (Boeing 787) | |||
Boeing Rename 7E7 Dreamliner to an official model disignation of B-787 Dreamliner which will carry 200-250 passengers on routes between 7,200
and 8,000 nautical miles (13,334-14,816 km).The airplane will use 15 to 20 percent less fuel for comparable missions than any other wide body airplane. It will also travel at speeds similar to today’s fastest wide bodies, about Mach 0.85.
Production will begin in 2005. First flight is expected in 2007 with certification, delivery and entry into service occurring in 2008. New 787DreamLiner will become the first commercial jet to be made with most of its primary structure consisting of composite materials.Some of the composite materials that will be used include graphite and toughened epoxy resin, and TiGr, a titanium/graphite composite. The graphite/epoxy material will make up the bilk of the composite materials used in the 787, while the titanium/graphite composite will be used for the wings.Titanium is a strong metal known for its light weight and durability. Graphite is a stable form of carbon. Boeing 787 (Dream Liner) will be the most advanced and efficient commercial airplane in its class and will set new standards for environmental responsibility and passenger comfort. The Engines, Boeing’s demands will intend to make B787 (Dream Liner) significantly quieter and cleaner , more fuel efficiency and cheaper to maintain. A new generation of aircraft requiring a new generation of engine. Boeing is requiring engines producing up to around 70,000 lb. of thrust. The engine manufacturers are talking about reducing the number of compressor stages, reducing bleed air or shift away from using bleed air to pressurized cabin air and shift away hydraulic systems toward nearly all electric aircraft. All of those under study and final results are still unknown. B787 will has approximately of Carbon fiber laminated composite materials around 57% of the main structure and 24% aluminum alloy, 11% titanium, and 8% steel. The 787 will have two 250kW generators to provide power for pressurization, deicing and hydraulic pumps. The 787 will have wireless IFE system, the aircraft's interior will be broken up into broadcast areas. The 787 will have 5000 psi hydraulics system. As of today (June 2005), Air Canada = 14, Air China =15, Air India = 27, Air New Zealand =2, All Nippon Airways =50, Blue Panorama =4 (Italy), China Eastern =15 , China Southern =13, Continental =10 , Ethiopian =5, First Choice =6 (UK), Hainan Airlines =8, Japan Airlines =30, Korean Airlines = 10, North West Airlines = 18, Primaris Airlines =20, Shanghai Airlines =6 , Vietnam Airlines =4 , Xiamen Airlines =3 , ANA is the first customer that selected B-787. B787 has maiden flight on 15 December 2009 and The first 787 is supposed to be delivered to All Nippon Airways of Japan by september of Year 2011 which delayed from the schedule morethan 2 years. | |||
PRELIMINARY SPECIFICATIONS OF BOEING B-787 (DreamLiner ) | |||
787-3 | 787-8 | 787-9 | |
Passengers(3 Class Config.) | 289 | 223 | 259 |
Cargo loading | n/a | 5 pallets + 5 LD3s | n/a |
Range | 3500 nm (6,500 km) | 8500 nm.(15,700 km) | 8300 nm.(15,400 km) |
Number of engine | 2 | 2 | 2 |
Engine types | GEnx, / RR Trent 1000 | GEnx, / RR Trent 1000 | GEnx, / RR Trent 1000 |
Engine Thrust | 55,000-70,000 lbs | 55,000-70,000 lbs. | 55,000-70,000 lbs. |
wing span | 168.76 ft.(51.61 m) | 192.27 ft. (58.8 m.) | 192.27 ft. (58.8 m.) |
Length | 182 ft.(56m) | 182 ft (56m.) | 202 ft.(62m) |
Operating speed | 0.85 mach (1019 km/h) | 0.85 mach (1019 km/h) | 0.85 mach (1019 km/h) |
Cruising altitude | n/a | n/a | n/a |
Max.take off weight | 299,916 lbs. | 452,500 lbs. | 500,000Lbs. |
Max.landing weight | n/a | n/a | n/a |
Operating weight empty | 242,000-252,000 lbs. | 242,000-252,000 lbs. | 242,000-252,000 lbs. |
Max.payload | n/a | n/a | n/a |
Max.fuel capacity | n/a | n/a | n/a |
cockpit B787 Dream liner | |||
1 nm.(nautical mile) = 1.15155 miles, 1 kt (knot) = 1.15155 mile / hr. 1 mach = 761 mph.(SL,ISA) |
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