Multi-spool turbofan engine with turbine bleed

In a multi-spool by-pass turbofan engine comprising a low pressure spool having a fan at a forward end and a low pressure turbine at an aft end thereof, and a high pressure spool having a high pressure compressor at a forward end in fluid flow communication with the fan on said low pressure spool and a high pressure turbine at the aft end thereof, a combustor in fluid flow communication between the high pressure compressor and the high pressure turbine on said high pressure spool, a combustion gas duct between the high and low pressure turbines on said high and low pressure spools, respectively, a by-pass duct extending from the fan on said low pressure spool to a point aft of the high pressure turbine on said high pressure spool, and an alternator driven by the high pressure spool of said engine, the improvement comprising:

• a plurality of circumferentially spaced poppet valves in said combustion gas duct immediately aft of the high pressure turbine on said high pressure spool;
• and
• a plurality of flow diverters connected to said poppet valves, respectively, and movable into said combustion gas duct upon opening of said valves, said poppet valves being individually openable at engine idle conditions to provide a fluid flow path from said high pressure turbine through said valves to said by-pass duct so as to increase the expansion ratio across the high pressure turbine to produce a relatively high RPM thereof at idle conditions while concomitantly reducing the expansion ratio across the low pressure turbine to reduce the speed of said low pressure spool and of the fan thereon thereby reducing air mass flow to the high pressure compressor on said high pressure spool and minimizing fuel consumption at idle speed.