Flanged ladder seal

Fluid reaction surfaces (i.e. – impellers) – Specific working member mount – Blade received by continuous circumferential channel

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Details

416193A, 416218, F01D 530

Patent

active

048758302

ABSTRACT:
In a compressor rotor assembly of an axial flow gas turbine engine, wherein the rotor disk has a circumferential blade retaining slot for receiving the root of each blade of a row of blades, a ladder seal is provided between the slot and the blade platforms to limit the leakage of working medium gases from the flow path and through the slot. During engine operation, the seal moves radially outwardly into sealing relation with the underside surface of each platform. At the same time, radially inwardly extending flanges of the seal move radially outwardly into sealing relation with the sidewalls of the disk slot.

REFERENCES:
patent: 902915 (1908-11-01), Roth
patent: 922581 (1909-05-01), Hanzlik et al.
patent: 2717554 (1955-09-01), Stalker
patent: 2948505 (1960-08-01), Sonder
patent: 3972645 (1976-08-01), Kasprow
patent: 4464096 (1984-08-01), Trousdell et al.

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