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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Bibliographic Details
Main Author GALLARDO, JR.; VICENTE C
Format Patent
LanguageEnglish
Published 23.06.1981
Subjects
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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.
Bibliography:Application Number: US19790049780