In terms of volume, the most impactful commercial aero engine produced by Safran Aircraft Engines is the
CFM International CFM56 turbofan powerplant. This engine is both developed and manufactured via a 50-50
joint venture company,
CFM International, which Safran jointly owns with the American industrial conglomerate General Electric (GE). Established during the 1970s, the CFM56 was not an early success; by April 1979, the joint venture had not received a single order in five years and was allegedly two weeks away from being dissolved. Safran Aircraft Engines is also the main partner for several other engines coproduced with GE, including the
CF6-80 and
GE90. Safran Aircraft Engines is also involved in the
Engine Alliance, which manufactures the
GP7000 high-thrust turbofan engine, one of the only two powerplants certified to power the twin-decker
Airbus A380. During the 2010s, Safran started manufacturing its portion of the
LEAP engine via the CFM International joint venture; Safran and GE each assemble half of the annual volume. To cope with high demand for the LEAP engine, CFM has duplicated supply sources for 80% of parts and as well as subdivided assembly sites. Safran Aircraft Engines is also involved in
PowerJet, a joint venture business with Russian aero engine specialist
NPO Saturn; this company produces
SaM146 turbofan engine, which is used to power the
Sukhoi Superjet 100 regional jet. During 2005, a new production plant was founded in Rybinsk,
VolgAero, to manufacture components of the SaM146; additionally, parts and assemblies of other engines produced by PowerJet's two parent companies are also produced on this site. In terms of military engines, Safran Aircraft Engines produces the
Snecma M88 turbofan. This engine was developed to power the
Dassault Rafale fighter aircraft. It fulfills numerous stringent performance criteria, including a high
thrust-to-weight ratio, low fuel consumption across all flight regimes, and a long engine life. Additional considerations were afforded to both the M88's maintainability and upgrade potential (73 kN to 105 kN using the same core). Qualification of the M88-2 engine was completed during 1996 while the first production engine was delivered by the end of that year. It is of a
modular design for ease of construction and maintenance, as well as to enable older engines to be retrofitted with improved subsections upon availability, such as existing M88-2s being upgraded to M88-4E standard. In May 2010, a Rafale flew for the first time with the M88-4E engine, an upgraded variant with greater thrust and lower maintenance requirements than the preceding M88-2. engine on static display at the
Paris Air Show, 2017 In 2002, the
Europrop International (EPI) consortium was set up by four aero engine manufacturers, Safran Aircraft Engines, Germany's
MTU Aero Engines, Britain's
Rolls-Royce Holdings and Spain's
Industria de Turbo Propulsores. EPI GmbH is tasked with designing, developing, marketing, manufacturing and providing support for the
TP400-D6 turboprop engine to power the
Airbus A400M Atlas, a military airlifter manufactured by
Airbus Defence and Space. The TP400 is the most powerful turboprop in the world currently in production. During 2008, the
European Commission launched an
open rotor demonstration led by Safran within the
Clean Sky program with 65 million euros funding over eight years: a demonstrator was assembled in 2015, and ground tested in May 2017 on its open-air test rig in
Istres, aiming to reduce
fuel consumption and associated CO2 emissions by 30% compared with current
CFM56 turbofans. With its 30:1
bypass ratio, it should deliver a 15% improvement over the
CFM International LEAP already at 11:1; but
Airbus is more interested in the more conventional ultra high bypass ratio (UHBR) turbofan at 15:1, which could be introduced from 2025, offering 5% to 10% better efficiency than the LEAP and to be tested from 2020. Built around the M88's core, the fan blades are slower than the 1980s
GE36 due to the reduction gear, lowering
noise and the fan can be mounted at the engine front for under-wing configurations. The
gearbox and the blade
variable-pitch technologies were validated in 100 cycles and 70 hours of tests, including 25% at takeoff thrusts of ,
reverse thrust, and rotor imbalance with a blade weight.