Exhaust-gas turbine of a turbocharger

Rotary kinetic fluid motors or pumps – With lubricating – sealing – packing or bearing means having...

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4152082, F01D 904

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active

059645741

ABSTRACT:
The object of the invention is to provide a nozzle ring for the exhaust-gas turbine of a turbocharger which, in addition to an improved service life, also guarantees a constant efficiency.
According to the invention, this is achieved in that an radial expansion gap (20) is formed between the turbine casing (2) and the nozzle ring (11), and at least one seal (22) is arranged in the expansion gap (20). To this end, an encircling groove (21) accommodating the seal (22) is formed in at least one of the fastening elements (16, 17) of the nozzle ring (11) or in at least one of the components (3, 4, 5) which surround the fastening elements (16, 17).

REFERENCES:
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patent: 1922017 (1933-08-01), Guy
patent: 2447942 (1948-08-01), Imbert et al.
patent: 3068638 (1962-12-01), Birmann
patent: 3737247 (1973-06-01), Horning
patent: 4242040 (1980-12-01), Swearingen
patent: 4679984 (1987-07-01), Swihart et al.
patent: 5059091 (1991-10-01), Hatfield
patent: 5249920 (1993-10-01), Sheperd et al.
"Kolbenring-Handbuch"; pp. 174-175; undated.
"Fey Lamellenringe"; pp. 4-5; undated.

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