Patent ID: 7788896

Claim:
A turbine compressor comprising; a compressor section comprising a proximal end, a distal end, a bore, a threaded hollow cylinder, a first end, the first end coupling to the compressor section, a second end, the second end coupling to a turbine section and an intake port adapted to receive a substance; the turbine section comprising a proximal end, a distal end, a bore and an exhaust port adapted to release a substance; a combustion section coupling to the compressor section and the turbine section, the combustion section having at least one ignition device, a grooved shaft extending from a portion of the compressor section through the combustion section with the grooved shaft (i) being rotatably coupled to the compressor section and the turbine section, (ii) having a support mechanism, and (iii) having a generally helically-shaped groove; and a bushing substantially surrounding the compressor section bore and the turbine section bore.