Turbine engine with a fire chamber and a helical fan

A turbine engine system, comprising:

• a fire chamber, having:
• a first cylindrical body having a first central axis;
• a first elongated hollow shaft extending co-axially along the first central axis, the first elongated hollow shaft extending along the first central axis;
• a plurality of wings fixedly secured to an exhaust plate and the first elongated hollow shaft;
• a plurality of combustion chambers disposed within a thickness of the first cylindrical body;
• a plurality of fuel injectors extending through the thickness of the first cylindrical body in a direction perpendicular to the first central axis and in gaseous communication with the plurality of combustion chambers;
• and
• a plurality of spark plug injectors extending through a bottom surface of the first cylindrical body and in a direction parallel with the first central axis and in gaseous communication with the plurality of combustion chambers;
• a plurality of cooling chambers disposed within the thickness of the first cylindrical body and positioned between the plurality of combustion chambers, wherein a cooling chamber of the plurality of cooling chambers is positioned adjacent to a combustion chamber of the plurality of combustion chambers, wherein compressed air is injected into the cooling chamber;
• and
• a helical fan, having:
• a cylindrical body having a second central axis;
• a second elongated hollow shaft extending co-axially along the second central axis and in gaseous communication with the first elongated hollow shaft;
• and
• a plurality of blades extending from an inner wall of the cylindrical body to an outer surface of the second elongated hollow shaft.