Method and device for assembling and adjusting variable capacity turbine
AssigneeMitsubishi Heavy Industries, Ltd.
InventorsYasuaki Jinnai, Takashi Mikogami, Koji Matsumoto
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AssigneeMitsubishi Heavy Industries, Ltd.
InventorsYasuaki Jinnai, Takashi Mikogami, Koji Matsumoto
Estimating the term…
The invention provides a method and device of assembling and adjusting a variable capacity turbine, which simplifies assembling process resulting in reduction of man-hours and costs of assembling and adjustment, and makes it possible that the nozzle vane setting of the adjustable nozzle mechanism is done with high accuracy without influenced by the accuracy in dimensions of the constituent parts such as nozzle vane and annular link mechanism and that the adjustable nozzle vane mechanism is adjusted whenever necessary even after the turbine is assembled. The invention is characterized in that a plurality of nozzle vanes are temporarily encircled and bound with a binding member capable of binding/releasing such as belt, etc. in a state the vanes are perfectly closed with the vanes contacting to each other, then the nozzle pin fixed to each of the nozzle vanes and supported free of rotation in the nozzle mount is fixed by staking or the like to the lever plate constituting the connection part of the annular link mechanism with the vanes in the temporarily bound state.
A method of assembling and adjusting a variable capacity turbine having a plurality of nozzle vanes disposed along the circumferential direction of a turbine rotor in the inner radius side of the spiral scroll formed in the turbine casing and supported free of rotation on the supporting part of the nozzle mount, the turbine rotor being supported in the turbine casing for rotation around the rotation axis;
A device for assembling and adjusting a variable capacity turbine having a plurality of nozzle vanes disposed along the circumferential direction of a turbine rotor in the inner radius side of the spiral scroll formed in the turbine casing and supported free of rotation on the supporting part of the nozzle mount, the turbine rotor being supported in the turbine casing for rotation around the rotation axis;
Dependencies are inferred from the claim text.