Reaction-jet turbine

F - Mech Eng,Light,Heat,Weapons – 15 – B

Patent

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Details

170/33, 121/73

F15B 13/02 (2006.01)

Patent

CA 2010337

REACTION-JET TURBINE Abstract of the Disclosure A reaction-jet turbine has a rotor in the form of a shaft having at least one axial passage, and at least one gas dynamic supply device in the form of a supply pipe positioned coaxially with the shaft in a spaced relation to the end thereof. At least one jet pipe is cantilevered to the shaft and has at the distal end thereof a thrust nozzle communicating with an end inlet of the axial passage so as to form a continuous gas duct. The outlet portion of the supply pipe is made in the form of a supply nozzle having the minimum cross-sectional area thereof which is smaller than the minimum cross-sectional area of the thrust nozzle, the ratio between these areas ensuring a shook wave in the entry zone of the axial passage of the shaft.

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