Patent ID: 6783320
Filing Date: 2004-08-31
Classification: F01D,F02K,F05D,H02N

Abstract:
Pressurized gas turbine engine comprising:a) pressurized gas turbine having a plurality of gas nozzles and one or more nozzle gas ways, each gas nozzle being affixed at the perimeter of the turbine in a respective nozzle position, each of the gas nozzles having a respective axis forming an oblique angle with the direction of rotation of the perimeter of the turbine at the respective nozzle position, and each gas nozzle being hydraulically connectable to one or more sources of pressurized fluid by one or more nozzle gas ways; b) turbine engine body enclosing the turbine in a turbine chamber, the turbine engine body having an expansion chamber in the turbine chamber; and c) electrothermodynamic power convertor.