Transition duct seal

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Means to seal radial flow pump runner inlet from outlet

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415138, F04D 2908

Patent

active

047477504

ABSTRACT:
An inner wall for a transition duct between the high pressure and low pressure turbines of a multirotor gas turbine engine in which the wall structure itself is made up of multiple aligned segments which are bolted to the inner shrouds of the vane clusters of the low pressure turbine and in which the segments are secured to forward and rearward cone elements with one of said elements bolted securely to the segments and the other cone having free axial and radial movement with respect to the segments with the cone elements supporting at their inner edges a seal element to cooperate with a rotating element on a low pressure rotor.

REFERENCES:
patent: 3056583 (1962-10-01), Varadi et al.
patent: 3623736 (1971-11-01), Petrie
patent: 4397471 (1983-08-01), Feldman et al.
patent: 4553901 (1985-11-01), Laurello

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