Method and apparatus for power generation

F - Mech Eng,Light,Heat,Weapons – 02 – C

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F02C 3/14 (2006.01) F02C 3/16 (2006.01) F02K 7/00 (2006.01) F02K 7/08 (2006.01)

Patent

CA 2144536

An apparatus (100) for generation of mechanical and electrical power. Ramjet thrust modules (102a, 102b) operate at supersonic speed (preferably Mach 3 to 4) at the distal tip ends (116a, 116b) of a low aerodynamic drag rotor (106). Rotor (106) is affixed at a hub means (114) to a power output means including central rotating upper (104a) and lower (104b) shaft portions. Escaping exhaust gases may be cooled by passing them through an enthalpy extraction section to heat a secondary fluid, Combustion gases may also be directed through a reaction turbine to utilize remaining kinetic energy to generate shaft energy.

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