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(11) | EP 0 278 434 A3 |
(12) | EUROPEAN PATENT APPLICATION |
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(54) | A blade, especially a rotor blade |
(57) A rotor blade (10) particularly adapted for turbine engines comprises various injection
holes (30, 40A, 40B, 50A, 50B, 60A, 60B) on the blade tip (18) and near the blade
tip (18) and on the root plane (44) and near the root plane (44) so directed as to
reduce the tip leakage flow crossing the tip and to control the boundary layer by
means of fluid curtain and entrainment effects. |