Aircraft Factfile and Recognition Guide - Boeing 787


Background

       
       

In the late 1990s, Boeing began considering a replacement for the 767 when sales weakened due to competition from the Airbus A330-200. As sales of the Boeing 747-400 also slowed, the company proposed two new aircraft, the 747X, and the Sonic Cruiser. The 747X, competing with the Airbus A380, would have lengthened the 747-400 and improved efficiency by using a composite supercritical wing. The Sonic Cruiser would have achieved higher speeds (approximately Mach 0.98) while burning fuel at the same rate as the existing 767.

Market interest for the 747X was tepid, but the Sonic Cruiser had brighter prospects. Several major airlines in the United States, including Continental Airlines, initially showed enthusiasm for the Sonic Cruiser concept, although they also expressed concerns about the operating cost. However, by decreasing travel time they would be able to increase customer satisfaction and aircraft utilization.

The September 11, 2001 attacks upended the global airline market. Airlines could not justify large capital expenditures, and increased petroleum prices made them more interested in efficiency than speed. The worst-affected airlines, those in the United States, were considered the most likely customers of the Sonic Cruiser. Boeing offered airlines the option of using the airframe for either higher speed or increased efficiency, but the high projected airframe costs caused demand to slacken further. Then the company officially canceled the Sonic Cruiser on December 20, 2002, and switched tracks by announcing an alternative product, the 7E7, on January 29, 2003, naming the executives to run the new jetliner program.

The replacement for the Sonic Cruiser project was dubbed the "7E7" (with a development code name of "Y2"). The "E" was said to stand for various things, depending upon the audience. To some, it stood for "efficiency", to others it stood for "environmentally friendly". In the end, Boeing claimed it merely stood for "Eight", after the aircraft was eventually rechristened "787". A public naming competition was also held, for which out of 500,000 votes cast online the winning title was Dreamliner.

On April 26, 2004, the Japanese airline All Nippon Airways (ANA) became the launch customer for the 787, then known as the 7E7, by announcing a firm order for 50 aircraft with deliveries to begin in late 2008. ANA's order included 30 787-3, 290–330 seat, one-class domestic aircraft, and 20 787-8, long-haul, 210–250 seat, two-class aircraft for regional international routes such as Tokyo Narita–Beijing. The aircraft will allow ANA to open new routes to mid-sized cities not previously served, such as Denver, Moscow, and New Delhi.

Early concept images of the 787 included rakish cockpit windows, a dropped nose and a distinctive "shark-fin" vertical stabilizer. The final styling of the aircraft was more conservative, the fin appearing visually similar to those of aircraft currently in service. The nose and cockpit windows were also changed to a more conventional form.

The 787-3 and 787-8 were to be the initial variants, with the 787-9 entering service in 2010. Boeing initially priced the 787-8 variant at US$120 million, a low figure that surprised the industry. In 2007, the list price was $146–151.5 million for the 787-3, $157–167 million for the 787-8 and $189–200 million for the 787-9. Customer-announced orders and commitments for the 787 reached 237 aircraft during the first year of sales, with firm orders numbering 677 by the 787's premiere on July 8, 2007, and well before entry into service. This makes the 787 the fastest-selling wide-body airliner ever before entry into service.

The 787 uses the same technology proposed for the Sonic Cruiser in a more conventional configuration. Boeing claims the 787 will be near to 20% more fuel-efficient than the 767. One third of the efficiency gain will come from the engines, another third from aerodynamic improvements and the increased use of lighter weight composite materials, and the final third from advanced systems. The most notable contribution to efficiency is the new electrical architecture which replaces bleed air and hydraulic power sources with electrically powered compressors and pumps, as well as completely eliminating pneumatics and hydraulics from some subsystems (e.g., engine starters or brakes). Technology from the Sonic Cruiser and 787 will be used as part of Boeing's project to replace its entire airliner product line, an endeavor called the Yellowstone Project (of which the 787 is the first stage).

Boeing selected two engine types, the General Electric GEnx and Rolls-Royce Trent 1000, to power the 787, both placed in pods. Significantly, this leaves Pratt & Whitney, which normally has an entrant in the market, unable to offer one of its engines to 787 customers. According to United Technologies Corporation CEO George David, Pratt & Whitney "couldn't make the business case work for that engine." For the first time in commercial aviation, both engine types will have a standard interface with the aircraft, allowing any 787 to be fitted with either a GE or Rolls-Royce engine at any time. Engine interchangeability makes the 787 a more flexible asset to airlines, allowing them to change easily from one manufacturer's engine to the other's if required. The engine market for the 787 is estimated at US$40 billion over the next 25 years. The launch engine for all three current 787 variants is the Rolls-Royce Trent 1000. Airbus has offered the competing A350 powered by a development of the Rolls Royce Trent turbofan, the Trent XWB.

Variants

The 787-8 is the base model of the 787 family with a length of 186 feet (57 m) and a wingspan of 197 feet (60 m) and a range of 7,650 to 8,200 nautical miles (14,200 to 15,200 km) depending on seating configuration. The 787-8 seats 210 passengers in a three class configuration. The variant will be the first of the 787 line to enter service in 2010. Boeing is targeting the 787-8 to replace the 767-200ER and 767-300ER, as well as expand into new non-stop markets where larger planes would not be economically viable. The bulk of 787 orders are for the 787-8. On December 8, 2009, United Airlines announced an agreement for 25 Boeing 787-8s with an option for 50 more.

       

The 787-3 will be a 290-seat (two-class) short-range version of the 787 targeted at high-density flights, with a range of 2,500 to 3,050 nautical miles (4,650 to 5,650 km) when fully loaded. It is designed to replace the Airbus A300/Airbus A310 and Boeing 757-300/Boeing 767-200 on regional routes from airports with restricted gate spacing. It will use the same fuselage as the 787-8, though with some areas of the fuselage strengthened for higher cycles. The wing will be derived from the 787-8, with blended winglets replacing raked wingtips. The change decreased the wingspan by roughly 25 feet (7.6 m), allowing the 787-3 to fit into more domestic gates, particularly in Japan.

This model will be limited in its range by a reduced Maximum Take-Off Weight (MTOW) of 364,000 lb (163,290 kg). (Actual range is calculated by the remaining available weight for fuel after the aircraft empty weight and payload are subtracted from the MTOW). A full load of passengers and cargo would limit the amount of fuel it could take on board, as with the 747-400D. This is only viable on shorter, high-density routes, such as Tokyo to Shanghai, Osaka to Seoul, or London to Berlin. Many airports charge landing fees based on aircraft weight; thus, an airliner rated at a lower MTOW, though otherwise identical to its sibling, would pay lower fees.

The 787-9 will be the first variant of the 787 with a "stretched" (lengthened) fuselage, seating 250–290 in three classes with a range of 8,000 to 8,500 nautical miles (14,800 to 15,750 km). This variant differs from the 787-8 in several ways, including structural strengthening, a lengthened fuselage, a higher fuel capacity, a higher maximum take-off weight (MTOW) and the same wingspan as the 787-8. The targeted date for entry into service (EIS), originally planned for 2010, was scheduled for early 2013 in December 2008. Boeing is targeting the 787-9 to compete with both passenger variants of the Airbus A330 and to replace their own 767-400ER. Like the 787-8, it will also open up new non-stop routes, flying more cargo and fewer passengers more efficiently than the 777-200ER or A340-300/500.

Boeing has stated that it is likely to develop another version, the longer 787-10, with a seating capacity between 290 and 310.  It would compete with the Airbus A350-900 and would supersede the 777-200ER.  In addition, it could also compete with the A330-300 and A340-300.  This variant has not officially been launched but would be a "matter of when."  The 787-10 will be a stretched version of the 787-9 and sacrifice some range to add extra seat and cargo capacity.

Specifications

Model 787-3 787-8 787-9
Cockpit crew Two
Seating, typical 290-330
317 (2-class)
210-250
242 (3-class)
250-290
280 (3-class)
Length 186 ft (56.7 m) 206 ft (62.8 m)
Wingspan 170 ft 6 in (52.0 m) 197 ft 3 in (60.1 m)
Height 55 ft 6 in (16.9 m)
Fuselage dimensions Width: 18 ft 11 in (5.77 m)
Height: 19 ft 5 in (5.92 m)
Cabin width 18 ft (5.49 m)
Cargo capacity 4,400 cu ft (125 m3)
28ื LD3
5,400 cu ft (153 m3)
36ื LD3
Empty weight 223,000 lb (101,000 kg) 242,000 lb (110,000 kg) 254,000 lb (115,000 kg)
Maximum take-off weight (MTOW) 375,000 lb (170,000 kg) 502,500 lb (228,000 kg) 547,000 lb (248,000 kg)
Cruising speed Mach 0.85 (903 km/h, 561 mph, 487 knots, at 40,000 ft/12,200 m)
Maximum speed Mach 0.89 (945 km/h, 587 mph, 510 knots, at 40,000 ft/12,200 m)
Maximum range, fully loaded 2,500–3,050 nmi (4,630–5,650 km; 2,880–3,510 mi) 7,650–8,200 nmi (14,200–15,200 km; 8,800–9,440 mi) 8,000–8,500 nmi (14,800–15,700 km; 9,210–9,780 mi)
Maximum fuel capacity 12,830 US gal (48,600 L; 10,700 imp gal) 85,964 lb 33,528 US gal (127,000 L; 27,900 imp gal) 224,638 lb 33,428 US gal (127,000 L; 27,800 imp gal) 224,638 lb
Service ceiling 43,000 ft (13,100 m)
Engines (ื2) General Electric GEnx or Rolls-Royce Trent 1000
Thrust (ื2) 53,000 lbf (240 kN) 64,000 lbf (280 kN) 71,000 lbf (320 kN)

Sources: Wikipedia Boeing 787


ฉ 2005-2010 Steven Holzinger