IAE V2500
The IAE V2500 is a two-shaft high-bypass turbofan engine which powers the Airbus A320 family, the McDonnell Douglas MD-90, and the Embraer KC-390.
The engine's name is a combination of the Roman numeral V, symbolizing the five original members of the International Aero Engines consortium, which was formed in 1983 to produce the V2500 engine. The 2500 represents the 25,000 lbf produced by the original engine model, the V2500-A1 variant. FAA type certification for the V2500 was granted in 1988.
The maintenance, repair, and operations market for V2500 is close to billion as of 2015.
Development
based the 10-stage HP compressor on a scale-up of the RC34B eight-stage research unit used in the RB401-06 Demonstrator Engine, but with two additional stages added added to the front and rear of the compressor spool. Pratt & Whitney developed the combustor and the 2-stage air-cooled HP turbine, while the Japanese Aero Engine Corporation provided the LP compression system. MTU Aero Engines were responsible for the 5-stage LP turbine and Fiat Avio designed the gearbox.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. In early 2012, the 5,000th V2500 engine was delivered to SilkAir, and IAE achieved 100 million flying hours. Six years later, in June 2018, over 7,600 engines were delivered and the V2500 achieved 200 million flight hours on 3100 aircraft in service.
Variants
V2500-A1
The original version, has 1 fan stage, 3 LP booster stages, 10 HPC stages, 2 HPT stages, and 5 LPT stages. This engine promised better fuel burn on the Airbus 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. First entered service with Adria Airways.V2500-A5
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 thrust, to meet the requirements of the larger Airbus A321. Soon, Airbus offered derated versions of the V2500-A5 on the Airbus A319 and Airbus A320, enabling the same engine hardware to be used across all Airbus A320 family aircraft, with the exception of the Airbus A318. The vast majority of V2500s are of the A5 variety.V2500-D5
This engine retains the turbomechanical configuration of the V2500-A5, but is fitted with different mounting hardware and accessory gearboxes to facilitate installation on the McDonnell Douglas MD-90.V2500-E5
This engine retains the turbomechanical configuration of the V2500-A5, but is fitted with different mounting hardware and accessory gearboxes to facilitate installation on the Embraer KC-390.Derated versions
A number of derated, Stage 4 noise compliant engines have been produced from the -A5 configuration, including:- The thrust V2524-A5 for the Airbus A319
- The thrust V2527-A5 for the Airbus A320
- The thrust V2525-D5 for the McDonnell Douglas MD-90-30. Engine Turbine and Accessory on the side instead of bottom to accommodate lateral mounting. Also has an option in the cockpit to add 3,000 pounds additional thrust for "hot and high" conditions
- The thrust V2533-A5 for the Airbus A321
- The thrust V2531-E5 for the Embraer KC-390
V2500SelectOne
V2500SelectTwo
On March 15, 2011, IAE announced an upgrade option of V2500 SelectOne Engines to the SelectTwo Program. It offers reduced fuel consumption due to a software-upgrade and Reduced Ground Idle, and is available since 2014 for the V2500-A5 variants.Applications
- Airbus A320ceo family
- Embraer KC-390
- McDonnell Douglas MD-90
Specifications
- Rotor speed: LP: 5,650 RPM, HP: 14,950 RPM
- Control: Dual channel FADEC
Variant | Certification | Take-Off Thrust | Weight | T/W | BPR | Comp. | Application |
V2500-A1 | 1 June 1988 | 4.68 | 5.4:1 | 35.8:1 | Airbus A320 | ||
V2527E-A5 | 14 August 1995 | 4.50 | 4.8:1 | 32.8:1 | Airbus A320 | ||
V2527-A5 | 21 November 1992 | 4.44 | 4.8:1 | 32.8:1 | Airbus A320 | ||
V2527M-A5 | 24 May 1999 |