THE AIRCRAFT GAS TURBINE ENGINE HAVING A LOW PRESSURE TURBINES WITH CLOSED ROTATION AND ADJUSTABLE DIVISION OF A TORQUE, AND ALSO THE ASSISTANT COMMUNICATOR HELD MEETING.

摘要

The assembly has a low pressure turbine with a flowpath and located aft of a high pressure spool (33). The low pressure turbine has counter rotatable low pressure inner and outer rotatable turbines. A single direction rotation booster has a row of booster blades connected to a low pressure outer shaft and axially located aft and downstream of a fan blade row (15).