| V2500 | |
|---|---|
 | |
| The V2500-A5/D5/E5 has one fan, four low- and ten high-pressure compressor stages, and two high- and five low-pressure turbine stages. | |
| Type | Turbofan |
| Manufacturer | International Aero Engines |
| First run | 1987 |
| Major applications | |
| Number built | Over 7,600 (June 2018)[1] |
TheIAE V2500 is a two-shafthigh-bypass turbofan engine built byInternational Aero Engines (IAE) which powers theAirbus A320 family, theMcDonnell Douglas MD-90, and theEmbraer C-390 Millennium.[2]
The engine's name is a combination of theRoman numeralV, symbolizing the five original members of the International Aero Engines consortium, formed in 1983 to produce the engine, and2500, which represents the 25,000-pound-force (110 kN) thrust produced by the original engine model, the V2500-A1.FAAtype certification for the V2500 was granted in 1988.
Themaintenance, repair, and operations market for the V2500 is close toUS$3 billion as of 2015.[3]
Rolls-Royce based the ten-stage high-pressure compressor on an eight-stage run in theRB401 in the mid 1970's followed by a nine-stage run in theRJ.500. The V.2500 would use ten stages, with the first four with variable stators, giving a pressure ratio of 20:1.[4] A single-stage booster was also part of the original configuration. Serious handling problems (inability to accelerate without surging) with this arrangement resulted in a redesigned compression system. The pressure ratio was reduced to 16:1 which needed a fifth variable stage and revised blading in the rear stages.[5] Two extra booster stages were required to restore the original overall pressure ratio.[6] A fourth booster stage would be added after the initial variant entered service.Pratt & Whitney developed the combustor and the two-stage air-cooled high-pressure turbine, while theJapanese Aero Engine Corporation provided the low-pressure compression system.MTU Aero Engines were responsible for the five-stage low-pressure turbine andFiat Avio designed the gearbox.[7]
In 1989, its unit cost was US$4.7 million.[8] The 4,000th V2500 was delivered in August 2009 to the Brazilian flag carrier TAM and installed on the 4,000th Airbus A320 family aircraft, an A319.[9] In early 2012, the 5,000th V2500 engine was delivered to SilkAir, and IAE achieved 100 million flying hours.[7] Six years later, in June 2018, over 7,600 engines were delivered and the V2500 achieved 200 million flight hours on 3,100 aircraft in service.[1]
The original version, has one fan stage, three low- and ten high-pressure compression stages, and two high- and five low-pressure turbine stages. This engine promised better fuel burn on theAirbus A320 than the competing CFM56-5A; however, initial reliability issues, coupled with insufficient thrust for the larger A321, prompted the development of the improved V2500-A5 variant. It first entered service withCyprus Airways.
A fourth booster stage was introduced into the engine basic configuration to increase core flow. This, together with a minor fan diameter and airflow increase, helped to increase the maximum thrust to 33,000 lbf (147 kN) thrust, to meet the requirements of the largerAirbus A321.[10] Soon, Airbus offered derated versions of the V2500-A5 on theAirbus A319 andAirbus A320, enabling the same engine hardware to be used across allAirbus A320 family aircraft, with the exception of theAirbus A318. The vast majority of V2500s are of the A5 variety.
This engine retains the configuration of the V2500-A5 but is fitted with different mounting hardware and accessory gearboxes to facilitate installation on theMcDonnell Douglas MD-90.
This engine retains the configuration of the V2500-A5 but is fitted with different mounting hardware and accessory gearboxes to facilitate installation on theEmbraer KC-390.
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A number of de-rated engines compliant with Stage 4 noise regulations have been produced from the -A5 configuration, as well as two variants with significant increase in thrust, thus expanding the thrust range from 23,500 lbf to 33,000 lbf:
On October 10, 2005, IAE announced the launch of the V2500Select—later called V2500SelectOne—with a sale toIndiGo Airlines to power 100 A320-series aircraft. The V2500SelectOne is a combination performance improvement package and aftermarket agreement. In February 2009, Pratt & Whitney upgraded the first V2500-A5 to the SelectOne Retrofit standard; the engine was owned by US Airways and had been in use since 1998.
On March 15, 2011, IAE announced an upgrade option of V2500 SelectOne Engines to the SelectTwo Program.[11] It offers reduced fuel consumption due to a software upgrade and Reduced Ground Idle (RGI),[12] and is available since 2014 for the V2500-A5 variants.
Data from Type Certificate Data Sheet[13]
| Variant | Certification | Take-OffThrust | Weight | T/W | BPR[14] | Comp.[14] | Application[14] |
|---|---|---|---|---|---|---|---|
| V2500-A1[14] | 1 June 1988 | 110.31 kN (24,800 lbf) | 2,404 kg (5,300 lb) | 4.68 | 5.4:1 | 35.8:1 | Airbus A320 |
| V2527E-A5 | 14 August 1995 | 4.50 | 4.8:1 | 32.8:1 | |||
| V2527-A5 | 21 November 1992 | 108.89 kN (24,480 lbf) | 4.44 | ||||
| V2527M-A5 | 24 May 1999 | 133.00 kN (29,900 lbf)} | 5.43 | ||||
| V2522-A5 | 10 June 1996 | 102.48 kN (23,040 lbf) | 4.18 | 4.9:1 | Airbus A319 | ||
| V2524-A5 | |||||||
| V2530-A5 | 29 November 1992 | 140.56 kN (31,600 lbf) | 5.73 | 4.6:1 | 35.2:1 | Airbus A321 | |
| V2533-A5 | 14 August 1996 | 4.5:1 | |||||
| V2531-E5[15] | 20 June 2015 | 139.36 kN (31,330 lbf) | 5.68 | 4.7:1 | 36.2:1 | Embraer KC-390 | |
| V2525-D5 | 29 November 1992 | 111.20 kN (25,000 lbf) | 2,595 kg (5,721 lb) | 4.20 | 4.8:1 | 34.5:1 | McDonnell Douglas MD-90 |
| V2528-D5 | 124.55 kN (28,000 lbf) | 4.71 | 4.7:1 | 35.2:1 |
Comparable engines
Related lists
Hurt by problems with the V.2500 turbofan and the shelving of its SuperFan derivative, International Aero Engines is seeking to restore confidence in the company and its engine.
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