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ROTOR AIRFOILS TO CONTROL TIP LEAKAGE FLOWS
ROTOR AIRFOILS TO CONTROL TIP LEAKAGE FLOWS
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机译:旋翼机翼可控制提示泄漏流量
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摘要
A rotor blade (24) for a gas turbine engine includes a bowed surface (43) on a tip region (40) of the suction side (32) thereof. The curvature of the bowed surface (43) progressively increases toward the tip (36) of the blade (24). The bowed surface (43) results in a reduction of tip leakage through a tip clearance (50) from the pressure side (30) to the suction side (32) of the blade (24) and reduces mixing loss due to tip leakage.
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