Journal of Tribology · 1994 · 11 citations · 1 references
EngineeringAerospace EngineeringMechanical EngineeringAerodynamicsMachine DesignMechanical DesignAerodynamic TestingMachine TestingMachine VibrationRotor DynamicsRotordynamicsTurbofan EnginesLabyrinth SealsLeakageLeakage PerformanceRotor Whirl InstabilityRotordynamic InstabilityRotordynamic StabilityTurbomachineryTurbomachinery Rotor Dynamics
Test results are presented for rotordynamic coefficients and leakage for three annular seals which use an anti-swirl self-injection concept to yield significant improvement in whirl frequency ratios as compared to smooth and damper seals. A new anti-swirl self-injection mechanism is achieved by deliberately machining self-injection holes inside the seal stator to partially divert inlet flow into the anti-swirl direction. The anti-swirl self-injection mechanism is used to achieve effective reduction of the tangential flow which is considered as a prime cause of rotor instability in high performance turbomachinery. Test results show that the self-injection mechanism significantly improves whirl frequency ratios; however, the leakage performance degrades due to the introduction of the self-injection mechanism. Through a series of tests, an optimum anti-swirl self-injection seal which uses a labyrinth stator surface with anti-axial flow injections is selected to obtain a significant improvement in the whirl frequency ratio as compared to a damper seal, while showing moderate leakage performance. The best whirl frequency ratio is achieved by an anti-swirl self-injection seal of 12 holes anti-swirl and 6 degree anti-leakage injection with a labyrinth surface configuration. When compared to a damper seal, the optimum configuration outperforms the whirl frequency ratio by a factor of 2.
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