Sealing device and method for turbomachinery

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

Reexamination Certificate

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Details

C277S415000

Reexamination Certificate

active

07435049

ABSTRACT:
A compliant seal for use between rotating blades and a static shroud surrounding the rotating blades in a steam or gas turbine is disclosed. The seal includes a tip surface, substantially resistant to wear due to rubbing by the tip of the rotating blades, and an elastic biasing member, comprising a biasing element. The wear-resistant surface is thus biased against the tips of the rotating blades to seal a gas path between the rotating blades and the static shroud.

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patent: 6439844 (2002-08-01), Turnquist et al.
patent: 6536773 (2003-03-01), Datta
patent: 2002/0192074 (2002-12-01), Turnquist et al.

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