Gas turbine engine rotor blading sealing device

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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415116, F01D 1108

Patent

active

055932789

ABSTRACT:
The disclosed invention relates to a sealing device for the rotor blades of a gas turbine engine which permits real time adjustment to be made of the clearances between the rotor blade tips and the sealing structure. The sealing shroud around the turbine wheel is formed of sectors, each sector being attached to a monolithic short response time ring and a monolithic long response time ring. Ventilating air from upstream of the turbine wheel is directed onto the rings such that the sectors are caused to radially expand or contract in compliance with the expansion or contraction of the tips of the rotor blades during stabilized and transient engine operational modes. A small positive clearance between the sealing sectors and the blade tips is maintained throughout the range of the engine's operation.

REFERENCES:
patent: 4050843 (1977-09-01), Needham
patent: 4304093 (1981-12-01), Schulze
patent: 4363599 (1982-12-01), Cline
patent: 4487016 (1984-12-01), Schwarz
patent: 4513567 (1985-04-01), Deveau

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