Ceramic radial flow turbine heat shield with turbine tip seal

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Between blade edge and static part

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Details

4151734, 4151736, 415178, F01D 1108

Patent

active

061557803

ABSTRACT:
A turbine engine includes a rotatable turbine having a peripheral tip and a backface. A heat shield is positioned adjacent the backface and includes an integral ring extending from a peripheral edge of the heat shield to a position spaced radially outwardly from the peripheral tip of the rotatable turbine to form a tip clearance between the ring and the peripheral tip. The turbine comprises a material having a coefficient of thermal expansion at least approximately four times greater than the coefficient of thermal expansion of the heat shield such that the turbine expands toward the ring as a result of heat within the engine, thereby reducing the tip clearance to minimize air flow along the backface and improve efficiency of the engine.

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patent: 5297928 (1994-03-01), Imakire et al.
patent: 5630702 (1997-05-01), Marmillac et al.
patent: 5855112 (1999-01-01), Bannai et al.

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