Preliminary optimization of a common rail direct injection diesel alternative to the AE2100 class turboshafts

It is shown that a CRDID (Common Rail Direct Injection Diesel) turbo compound design is a highly over constrained problem. Very few options are available to the designer, even from the metallurgical point of view. The process of the preliminary design is fully described and the preliminary performance evaluation is fully described. A comparison with the original turbo shaft installation of a Hercules C130J aircraft is performed and the results are analyzed. The CRDID turbo compound seems an extremely convenient option since it can halve the fuel consumption, with increased safety and reduced logistical problems. CRDID emissions, with SCR (Selective Catalytic Reduction) may easily reach the automotive Euro 6 standard. ©2006-2015 Asian Research Publishing Network (ARPN).