Turbo shaft engine with acoustical compression flow amplifying ramjet

A turbo shall engine for amplifying the flow rate of an air stream, comprising:

• a blower housing defining a chamber and a blower inlet port for receiving an incoming air stream into said chamber;
• a turbine blower assembly rotatably mounted in said chamber and having a plurality of blades positioned for rotation by said incoming air stream;
• a gas turbine having a primary air duct defining an air intake and an opposed outlet port, said air intake connected to said blower housing for receiving said incoming air stream, said gas turbine adapted to compress said incoming air stream and to ignite an admixture of fuel and said compressed incoming air stream so as to amplify the flow rate of said incoming air stream, said gas turbine adapted to exhaust said amplified air stream through said outlet port;
• and
• an exhaust channel having a first open end coupled to said outlet port for receiving said amplified air stream, said exhaust channel adapted to transfer said amplified air stream through said blower housing and defining an outlet opening for exhausting said amplified air stream from said blower housing, said blades of said turbine blower assembly positioned between said inlet port and outlet openings for rotation by said amplified air stream.