초록 ▼

A blade for a Kaplan turbine has substantially linear touching lines for contacting, in the closed position of the guide blade array, adjacent guide blades, the contact lines being linear or curved and running generally parallel to the pivot axis of the blade. The trailing side of the blade extends

A blade for a Kaplan turbine has substantially linear touching lines for contacting, in the closed position of the guide blade array, adjacent guide blades, the contact lines being linear or curved and running generally parallel to the pivot axis of the blade. The trailing side of the blade extends progressively inwardly and with a progressively increasing distance from the touching line on the trailing side.

대표청구항 ▼

[ I claim:] [1.] A Kaplan-turbine guide vane having a leading side and a trailing side with respect to liquid flow therepast and a vane longitudinal axis at an intermediate location between said leading and trailing sides and about which said vane is rotatable, said vane widening from a leading edge

[ I claim:] [1.] A Kaplan-turbine guide vane having a leading side and a trailing side with respect to liquid flow therepast and a vane longitudinal axis at an intermediate location between said leading and trailing sides and about which said vane is rotatable, said vane widening from a leading edge at said leading side toward said intermediate location and narrowing from said intermediate location toward a trailing edge of the vane, said vane being positioned in an array of such vanes centered on a turbine axis such that, upon rotation of the vanes of said array about the respective longitudinal axes into a closed position, each of said vanes contacts adjacent vanes at a first touching line (E1) on said leading side and a second touching line (E2) on said trailing side of the respective vane, said touching lines of each vane extending generally in the same direction as the respective longitudinal axis and said first touching line lying along an inside surface of each vane and the second touching line lying along an outside surface of each vane relative to said turbine axis, each of said vanes having a twist of the respective trailing side over at least a third of the length of the respective vane with the respective trailing side along the twist being turned progressively inwardly toward said turbine axis with a progressive increase in a distance between said second touching line and the trailing edge of the respective vane.