Abstract: Vibration induced compressor vane failure from tip leakage vortex bursting is eliminated or minimized. By securing the vane at opposite ends to inner and outer stationary casings, tip leakage is entirely avoided hence avoiding the mechanism for inducing vibration. By contouring the inner surface of the flow path to converge the flow in a downstream direction with a cantilevered compressor vane having a vane tip spaced from the inner casing surface, airflow lift off is precluded or minimized maintaining the flow attached to the flowpath surfaces with consequent avoidance of tip vortex induced vibration.

Abstract: A compressor radial bleed manifold and compressor case assembly includes a compressor case having one or more bleed flow exit passages therein; and a discrete bleed manifold mounted on the compressor case and having one or more inlet passages extending radially between a manifold plenum and the one or more exit passages in the mounting boss for bleeding compressor air into the manifold plenum.