Staircase blade tip
An airfoil blade tip is so configured that, when it is caused to rub against a surrounding casing, the resultant force acting on the blade tip is substantially in the tangential direction. In this way, axial forces on the airfoil are substantially reduced.
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Main Author | |
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Format | Patent |
Language | English |
Published |
23.06.1981
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Subjects | |
Online Access | Get full text |
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Summary: | An airfoil blade tip is so configured that, when it is caused to rub against a surrounding casing, the resultant force acting on the blade tip is substantially in the tangential direction. In this way, axial forces on the airfoil are substantially reduced. |
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Bibliography: | Application Number: US19790049780 |