CFM International

CFM56

High-Bypass Turbofan In Production

Technical Specifications

Thrust
151,0 kN (34 000 lbf)
Bypass Ratio
6,0:1
Fan Diameter
1,735 m
Pressure Ratio
32,6:1
SFC
0,3300 lb/lbf·h
Dry Weight
2 380 kg
Length
2,426 m
First Run
1974
In Service
1982

Descripción general

The CFM56 is the most produced jet engine in aviation history, with more than 35,000 units delivered since its entry into service in 1982. A joint venture between GE Aerospace and Safran Aircraft Engines (formerly Snecma) under the CFM International partnership, the CFM56 family powers two of the most ubiquitous commercial aircraft families ever built: the Boeing 737 Next Generation (NG) and the Airbus A320ceo. Its combination of reliability, fuel efficiency, and low maintenance cost made it the dominant narrowbody powerplant for four decades.

The CFM56 traces its lineage to the early 1970s, when GE and Snecma signed a joint-venture agreement in 1971 to develop a new commercial turbofan for the narrowbody market. The core technology derived from GE's F101 military engine, while Snecma contributed fan and low-pressure turbine expertise. After a lengthy certification program driven partly by US export-control regulations on military-derived technology, the CFM56-2 entered airline service on the DC-8-73 in 1982. Successive variants — the -3 for the 737 Classic, -5 for the A320 family and A340, and -7B for the 737NG — continuously improved thrust, efficiency, and reliability.

Especificaciones técnicas

ParámetroValor
Empuje máximo151.0 kN (34,000 lbf)
Relación de derivación6.0:1
Diámetro del fan1.735 m (68.3 in)
Peso en seco2,380 kg (5,247 lb)
Longitud2.426 m (95.5 in)
Relación de presión total32.6:1
SFC0.330 lb/lbf·h
Primera prueba1974
Entrada en servicio1982

Variantes

The CFM56 family spans five major variants across fifty years of development. The CFM56-2 (22,000–24,000 lbf) re-engined the Douglas DC-8-73 and powers some Boeing E-3 Sentry and E-6 Mercury military aircraft. The CFM56-3 (18,500–23,500 lbf) was developed for the 737 Classic (−300/400/500), featuring a smaller fan to maintain ground clearance. The CFM56-5A/5B/5C (22,000–34,000 lbf) powers the entire A320ceo family and the A340-300/200. The CFM56-7B (19,500–33,000 lbf) is the motor exclusivo for the 737NG (−600/700/800/900ER) and remains the most numerous variant, with over 15,000 units delivered. Each successive variant brought improvements in OPR, SFC, and on-wing reliability.

Aplicaciones en aeronaves

  • Boeing 737-300: CFM56-3B1/3B2 (20,000–22,000 lbf) — variante de lanzamiento del 737 Classic
  • Boeing 737-400: CFM56-3C1 (23,500 lbf) — Classic alargado
  • Boeing 737-500: CFM56-3C1 (20,000 lbf) — Classic acortado
  • Boeing 737-600: CFM56-7B18/22 (18,500–22,700 lbf) — 737NG más pequeño
  • Boeing 737-700: CFM56-7B24/27 (24,200–27,300 lbf) — monopasillo estándar del 737NG
  • Boeing 737-800: CFM56-7B26/27 (26,300–27,300 lbf) — variante del 737 más vendida
  • Boeing 737-900ER: CFM56-7B27A (27,300 lbf) — 737NG más largo
  • Airbus A318: CFM56-5B5/9 (23,300 lbf) — miembro más corto de la familia A320
  • Airbus A319: CFM56-5A4/5B5/6 (22,000–27,000 lbf) — fuselaje estrecho más pequeño de la familia A320
  • Airbus A320-200: CFM56-5A1/5B4 (25,000–27,000 lbf) — el fuselaje estrecho por excelencia
  • Airbus A321-200: CFM56-5B3 (33,000 lbf) — variante de alto empuje para el miembro más pesado de la familia A320
  • Airbus A340-300: CFM56-5C4 (34,000 lbf) — aplicación de largo alcance con cuatro motores

Historia del desarrollo

First run in 1974 at GE's Evendale facility, the CFM56 program was nearly cancelled multiple times due to US ITAR restrictions on the F101 core technology — the US DoD initially refused to allow export of the military core to a French partner. A landmark 1979 agreement cleared the path for commercial sales. The −3 variant for the 737 Classic required a novel accessory gearbox repositioning to the side of the engine (from beneath) to preserve the 737's low ground clearance — a design decision that would echo in the LEAP-1B decades later. The CFM56-5B introduced a dual-annular combustor (DAC) option to reduce NOx emissions on the A320neo's predecessor. The −7B for the 737NG, certified in 1997, achieved unprecedented dispatch reliability rates above 99.98%, cementing CFM56's reputation. Production continues for aftermarket support and spare engines, with the LEAP family serving as the direct successor.