US 4,124,329 AGranted

Axial-flow reversible turbine

OwnerViktor I. Romanov, Felix I. Kirzner +1inventors

InventorsViktor I. Romanov, Felix I. Kirzner, Yakov K. Soroka

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Abstract

An axial-flow reversible turbine comprises a nozzle assembly and a wheel rotor mounted consecutively in the direction of the flow of the working medium and provided with two-section blades. One section of said blades forms the flow duct of the direct-rotating turbine and the other section, the flow duct of the counter-rotating turbine. The flow duct of the direct-rotating turbine incorporates a valve in the form of variable-incidence airfoil vanes intended to deny the access of the working medium into said duct. The inside diameter of the flow duct of the counter-rotating turbine is larger than the outside diameter of the flow duct of the direct-rotating turbine. The gas flow ducts of the direct- and counter-rotating turbines communicate with each other through a cylindrical bushing with ports. Said bushing is installed coaxially with the wheel rotor at the inlet of the flow into the flow duct before the nozzle assembly and its inside diameter is substantially equal to the outside diameter of the flow duct of the direct-rotating turbine. The bushing is provided with a band arranged along its periphery and being sufficiently wide for overlapping the ports. The band has a device for moving it radially to at least two fixed positions in one of which it fits around the outside circumference of the gas flow duct of the counter-rotating turbine and in the other position it fits around the outside circumference of the gas flow duct of the direct-rotating turbine.

An axial-flow reversible turbine comprising:

a casing;
a nozzle assembly accommodated in said casing and having two-section blades for controlling the rate of flow of the working medium through said turbine;
a wheel rotor with two-section blades for converting the kinetic energy of the flow of the working medium into mechanical work and mounted in the direction of the flow of the working medium after said nozzle assembly;
one section of said blades of said nozzle assembly and of said wheel rotor forming the flow duct of the direct-rotating turbine and the other section of said blades of said nozzle assembly and said wheel rotor forming the flow duct of the counter-rotating turbine, the inside diameter of said flow duct of the counter-rotating turbine being larger than the outside diameter of said flow duct of the direct-rotating turbine;
a valve in the form of variable-incidence airfoil vanes intended to deny access of the working medium into said flow duct of the direct-rotating turbine and located in said casing at the entrance into said flow duct;
a cylindrical bushing with ports for intercommunicating said flow ducts and installed in said casing coaxially with said wheel rotor at the entrance of the flow into said flow duct before said nozzle assembly and having an inside diameter substantially equal to the outside diameter of said flow duct of the direct-rotating turbine;
an entrance to said flow duct;
a band sufficiently wide for overlapping said ports and arranged along the periphery of said bushing;
a device for moving said band radially to at least two fixed positions in one of which it fits around the outside circumference of said flow duct of the counter-rotating turbine whereas in the other position it fits around the outside circumference of said entrance of said flow duct of the direct-rotating turbine, said device being installed on the external surface of said casing and connected with said band, said flow duct being a combination of the annular channel, nozzle vanes and turbine blades.

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Abstract

Claims4