Patent ID: 8087487

Claim:
A hybrid turbo transmission comprising: a power source providing power connected through a first axis of rotation to at least a first compressor; said at least a first compressor outputs power by means of compressed air or gas to drive a turbine or multi-stage turbines; said turbine or multi-stage turbines are connected through a second axis of rotation to a work unit; wherein said power source is a radial configured internal combustion engine configured with an air cooling system whereby; said at least a first compressor is located in front of said radial configured internal combustion engine; a second compressor is located behind said radial configured internal combustion engine; said at least a first compressor operates from ram air entering into a front of said at least a first compressor where at least a portion of said compressed ram air will enter into said radial configured internal combustion engine and at least a portion of said compressed ram air will pass though said air cooling system; warmed air that exits said air cooling system is then mixed with exhaust gas from said radial configured internal combustion engine where it is passed into said second compressor, and after the mixed exhaust and said warmed air exits said second compressor it is transferred back for use in said at least a first compressor.