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Planform view of a 787-9 showing its 9.6 wing aspect ratio and 32° wing sweep Front view of a Vietnam Airlines 787-10, the fuselage is 19 ft (5.8 m) wide and 19 + 1 ⁄ 2 ft (5.94 m) high while the fan has a 9.3 ft (2.8 m) diameter. The Boeing 787 Dreamliner is a long-haul, widebody, twin-engine jetliner, designed with lightweight structures ...
The Rolls-Royce Trent 1000 is a high-bypass turbofan engine produced by Rolls-Royce, one of the two engine options for the Boeing 787 Dreamliner, competing with the General Electric GEnx. It first ran on 14 February 2006 and first flew on 18 June 2007 before a joint EASA/FAA certification on 7 August 2007 and entered service on 26 October 2011.
The first flight with one of these engines took place on 22 February 2007, using a Boeing 747-100, fitted with one GEnx engine in the number 2 (inboard left hand side) position. By fall 2019, General Electric was offering the GEnx-2B, developed for the 747-8, for the revised 767-XF variant based on the 767-400ER, but needed enough volume to ...
A cross-section comparison of Airbus A380 (double-deck the full length) and Boeing 747-400 (double-deck only in the front section) The production of the large Boeing 747-8 and Airbus A380 four-engine, long-haul jets has come to an end as airlines are now preferring the smaller, more efficient Airbus A350, Boeing 787 and Boeing 777 twin-engine ...
The 747-8's vertical tail unit is largely unchanged, with a height of 63 ft 6 in (19.35 m). [118] The General Electric GEnx is the only engine available for the 747-8. Unlike the GEnx introduced on the 787, the 747 engine variant provides bleed air and features a smaller diameter to fit on the 747 wing. [126]
The ANA flight from Ube in west Japan to Tokyo was canceled after the right engine of the Boeing 787 failed to start. ANA's Dreamliners are powered by Rolls' Trent 1000 engines.
Rolls-Royce MT30. The Rolls-Royce Trent is a family of high-bypass turbofans produced by Rolls-Royce. It continues the three spool architecture of the RB211 with a maximum thrust ranging from 61,900 to 97,000 lbf (275 to 431 kN). Launched as the RB-211-524L in June 1988, the prototype first ran in August 1990.
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