Snecma Silvercrest

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The Snecma Silvercrest is a turbofan currently under development which will be manufactured by Snecma.

Announced at the 2006 NBAA convention[1]. The engine was originally designed as a 8,500- to 10,500-pound thrust turbofan[2] to power super mid-size to large cabin business jets or 40 to 60-seat regional jets with a MTOW between 45,000 and 60,000 lb[3]. Since original development the thrust range has been raised and is currently quoted as 9,500 to 12,000 pounds of thrust.

The engine architecture includes a solid wide-chord swept fan without booster, followed by a 4 axial stage + 1 centrifugal stage high pressure compressor. The overall pressure ratio is 27:1 with a core pressure ratio of "over 17". The high pressure compressor is driven by a single stage turbine, while the 40 inch fan is coupled to a 3-stage low pressure turbine[2].

The high pressure spool and combustor have been run in a core-demonstrator reaching the take-off speed of 20,300rpm[4]. A full engine demonstrator is due to run towards the end of 2008, while engine certification is pencilled in for the end of 2010 or early 2011[5] and should be available towards 2012[6]. As of january 2008, no aircraft manufacturer had selected this engine.

Turbomeca which is, like Snecma, a part of the SAFRAN Group will help to design the centrifugal compressor stage[5].

[edit] Specifications

General characteristics

  • Type: axial and centrifugal flow, twin-shaft, bypass turbofan engine (Bypass ratio: approx. 4.5[5])
  • Length: approx. 74 in[5]
  • Diameter: Fan: approx. 40 in[5]
  • Dry weight:

Components

  • Compressor: Low pressure: 1 axial fan (no booster), High pressure: 4 axial stages + 1 centrifugal stage[5]
  • Turbine: Low pressure: 3 axial stages, High pressure: 1 axial stage[5]

Performance

[edit] References

Languages