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A vane cluster for a turbine engine compressor or turbine includes a shroud 12 with a nonlinear slot 26 extending therethrough to divide the shroud into thermally independent shroud segments 24. The slot is bordered by matching nonlinear surfaces 28 that are easy and inexpensive to produce with conv

A vane cluster for a turbine engine compressor or turbine includes a shroud 12 with a nonlinear slot 26 extending therethrough to divide the shroud into thermally independent shroud segments 24. The slot is bordered by matching nonlinear surfaces 28 that are easy and inexpensive to produce with conventional wire EDM equipment. The nonlinear profile of the slots effectively resists fluid leakage.

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1. A vane cluster, comprising:an outer shroud; a radially inner shroud; at least two airfoils extending between the shrouds; one and only one of the shrouds having a slot residing between neighboring airfoils end extending nonlinearly from a radially inner surface of the shroud to a radially outer s

1. A vane cluster, comprising:an outer shroud; a radially inner shroud; at least two airfoils extending between the shrouds; one and only one of the shrouds having a slot residing between neighboring airfoils end extending nonlinearly from a radially inner surface of the shroud to a radially outer surface of the shroud to define shroud segments, the slot having a generally constant width. 2. The cluster of claim 1 wherein the nonlinear slot comprises at least two slot portions with a juncture therebetween, each juncture corresponding to a change of angular orientation.3. The cluster of claim 2 comprising at least three slot portions with at least two changes of angular orientation.4. The cluster of claim 3 wherein the changes of angular orientation define an accumulated angular change of at least about 180 degrees.5. The cluster of claim 1 wherein the nonlinear slots comprises a curved portion.6. The cluster of claim 1 wherein the nonlinear slot comprises at least two straight line segments.7. The cluster of claim 1 wherein the shroud having a nonlinear slot extending therethrough is the inner shroud.8. The cluster of claim 1 wherein a nonlinear slots is present between each and every neighboring airfoil of the cluster.9. The cluster of claim 1 wherein the slot is formed by electro-discharge machining.10. The cluster of claim 1 wherein the slot is defined by a kerf arising from material removal from an otherwise unitary shroud.11. The cluster of claim 1 wherein the slot is formed by removing material from an otherwise unitary shroud.12. The cluster of claim 1 wherein the shroud has a unitary prefinished state arid a severed finished state.13. The cluster of claim 1 wherein the nonlinear slot is the exclusive means for resisting fluid leakage through the slot.