SAGE 6 – Lean Burn

SAGE 6, the Lean Burn Project, started in 2011, consists of two major work streams. The first will define sub-system designs and associated verification strategies for concepts identified as most suitable for introduction into future gas turbine products. The second will focus on design and make activity to create a set of functionally representative experimental subsystems that can be integrated into a demonstration platform. It is anticipated that these hardware will be subjected to both rig testing (2013 onwards), and engine testing (2014 – 2016).

Lean Burn, critical design review of turbo machinery successfully passed (Q1 2012)