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Encyclopedia > GP7000

The Engine Alliance GP7000 (known as the GP7200 for a brief time period) is a new turbofan jet engine that will incorporate advanced technologies of proven wide-body products, originally from the world's No.1 and No.3 aero-engine manufacturers, GE Aircraft Engines and Pratt & Whitney, but now to also include Snecma Moteurs of France (a CFM International partner with GE), who has recently joined the GP7000 program. Snecma has 20 percent of General Electric’s share of the GP7000 engine program, or 10% as a whole. Schematic diagram of high-bypass turbofan engine CFM56-3 turbofan, lower half, side view. ... General Electric Aircraft Engines (GEAE) is the top supplier of aircraft engines in the world and offers engines for the majority of commercial aircraft. ... Pratt & Whitney is an American aircraft engine manufacturer whose products are widely used in both civil and military aircraft. ... Snecma Moteurs of France is one of the worlds major aircraft engine suppliers. ...


Originally intended to power Boeing Commercial Airplanes' cancelled 747X, the engine has since been pushed for Airbus' A380-800 superjumbo. It is built on the GE90 core and the PW4000 low-pressure system. Boeing Commercial Airplanes (BCA), based in Renton Washington, is a unit of The Boeing Company, consisting of the Seattle-based former Boeing Airplane Company (the civil airliner division), as well as the Long Beach-based Douglas Aircraft division of the former McDonnell Douglas Corporation. ... The Boeing 747, commonly called a Jumbo Jet, is among the most recognizable jet airliners, and is among the largest passenger airliners. ... Airbus S.A.S. is a commercial aircraft manufacturer based in Toulouse, France. ... The Airbus A380 is a double-deck, four-engined airliner manufactured by EADS (Airbus S.A.S.). It is the largest passenger airliner in the world. ... NASA GE90 airflow simulation General Electric GE90 is a family of high-bypass turbofan engines built by General Electric for the Boeing 777, with thrust ranging from 74,000 to 115,000 lbf (329 to 512 kN). ... The Pratt & Whitney PW4000 is a family of high-bypass turbofan aircraft engines with certified thrust ranging from 52,000 to 99,040 lbf (230 to 441 kN). ...


The competing Rolls-Royce plc Trent 900 was named as the lead engine for the then-named A3XX in 1996 and was initially selected by almost all A380 customers. However the GE/PW engine increased its share of the A380 engine market to the point where it will now power 48% of the super-jumbo fleet. This disparity in sales was resolved in a single transaction, with Emirates' order of 45 GP7000-powered A380-800s, comprising over one third of A380 sales (as of 2005). Emirates has traditionally been a Rolls-Royce customer. A380 aircraft powered by the GP7200s will have A380-86X model numbers as 6 is the code for Engine Alliance engines. Rolls-Royce plc is a British aircraft engine maker; the second-largest in the world, behind General Electric Aviation. ... Rolls-Royce Trent 900 on A380 prototype Rolls Royce Trent is a family of high-bypass turbofan engines manufactured by Rolls-Royce. ... Boeing 777-300ER “Emirates” redirects here. ... 2005 is a common year starting on Saturday of the Gregorian calendar. ... The Engine Alliance, a 50/50 joint venture between General Electric and Pratt & Whitney, was formed in August 1996 to develop, manufacture, sell, and support a family of modern technology engines for new high-capacity, long-range aircraft. ...


Ground testing of the engine began in April 2004 and the engine was run for the first time on an A380 on August 14, 2006. [1] The Federal Aviation Administration certified the engine for commercial operation on January 4, 2006. [2] On August 25, 2006, an A380-861 test aircraft (MSN 009) made the first flight of an Engine Alliance powered A380. The flight began and ended at Toulouse and lasted about four hours. Tests were performed on the engines flight envelope, cruise speed, and handling. A day earlier, the same aircraft performed rejected takeoff tests on the engines. 2004 : January - February - March - April - May - June - July - August - September - October - November - December Deaths in April • 18 Ratu Sir Kamisese Mara • 19 Norris McWhirter • 22 Pat Tillman • 24 Estée Lauder Other recent deaths Ongoing events EU Enlargement Exploration of Mars: Rovers Haiti Rebellion Reconstruction of Iraq – Occupation & Resistance Israeli... August 14 is the 226th day of the year in the Gregorian calendar (227th in leap years), with 139 days remaining. ... For the Manfred Mann album, see 2006 (album). ...   FAA redirects here. ... January 4 is the 4th day of the year in the Gregorian calendar. ... For the Manfred Mann album, see 2006 (album). ... A rejected takeoff or RTO is the situation in which it is decided to abort the takeoff of an airplane. ...

Contents

Major customers

Emirates are Islamic territories ruled by Emirs (q. ... Air France (Compagnie Nationale Air France) is a subsidiary of Air France-KLM. Before its merger with KLM, it was the national airline of France, employing 71,654 people (as of January 2005). ... United Parcel Service Inc. ... ILFC (International Lease Finance Corporation, though the abbreviation is the more common usage) is an aircraft lessor headquartered in Los Angeles, California. ... Korean Air (KSE: 003490) is the largest airline based in South Korea. ...

GP7270 Characteristics

General characteristics

  • Type: two-spool turbofan engine
  • Length: 474 cm (187 in)
  • Diameter: 316 cm (124 in), fan tip 295 cm (116 in)
  • Dry weight: 6712 kg (14,798 lb)

Components

  • Compressor: hollow-titanium, 24 swept wide-chord hollow titanium fan blades, by-pass ratio of 8.7:1; five-stage low-pressure axial compressor; nine-stage high-pressure axial compressor
  • Combustors: low-emissions single annular combustor
  • Turbine: two-stage high pressure turbine, boltless architecture, single crystal blades, split blade cooling and thermal barrier coatings, axial flow; six-stage low-pressure axial flow

Performance

  • Power output:
  • Overall pressure ratio: 43.9
  • Thrust-to-weight ratio: 46.3 N/kg (4.73 lbf/lb) assuming 17,230 lb engine and 81,500 lbf of thrust

Sources Schematic diagram of high-bypass turbofan engine CFM56-3 turbofan, lower half, side view. ... An animation of an axial compressor. ... A ring of can type combustors circles the mid section of this gas turbine. ... A Siemens steam turbine with the case opened. ... Bold text The compression ratio is a single number that can be used to predict the performance of any engine (such as an internal-combustion engine or a Stirling Engine). ... Thrust-to-weight ratio (where weight means weight at the Earths surface) is a dimensionless parameter characteristic of rocket and jet engines, and of vehicles propelled by such engines (typically space launch vehicles and jet aircraft). ...

  • FAA certificate data sheet
  • Engine Alliance GP7000, Teal Group Corporation
  • [2]

References

External links



 
 

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