Turbomachine blade tip shroud with parallel casing configuration
Embodiments of the present invention include a turbomachine having a turbomachine blade (22) and a stationary structural component (23). The turbomachine blade (22) includes a tip shroud (50) having a leading edge portion (54) where the leading edge portion has a first surface. The stationary struct...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | Embodiments of the present invention include a turbomachine having a turbomachine blade (22) and a stationary structural component (23). The turbomachine blade (22) includes a tip shroud (50) having a leading edge portion (54) where the leading edge portion has a first surface. The stationary structural component (23) is disposed about the turbomachine blade (22) and includes a corresponding portion (56) corresponding to the leading edge portion (54) of the tip shroud (50), where the corresponding portion (56) has a second surface, where the first surface and the second surface have generally parallel contours. |
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