F - Mech Eng,Light,Heat,Weapons – 15 – B
Patent
F - Mech Eng,Light,Heat,Weapons
15
B
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.
Ena Vladimir P.
Fedorenko Nikolai D.
Korolev Sergei K.
Litvinenko Viktor I.
Marochkina Irina A.
Ena Vladimir P.
Fedorenko Nikolai D.
Korolev Sergei K.
Litvinenko Viktor I.
Marks & Clerk
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