Turbine housing of turbocharger

Rotary kinetic fluid motors or pumps – Including thermal expansion joint – Radially sliding

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415187, F28F 700

Patent

active

046936688

ABSTRACT:
Mated engaging grooves are formed at opposing surfaces of sections into which a turbine housing main body is divided with respect to the axial direction of a turbine. A partition wall is fitted in the mated engaging grooves, leaving a clearance in the radial direction. The end of the partition wall on the side of the gas inlet of the turbine housing main body is made into contact with the side surface or surfaces of a partition wall supporting member disposed at the gas inlet such that the partition wall supporting member is in coplanar relationship with a flange surface of the turbine housing main body, whereby thermal deformations in the direction of the gas flow at the gas inlet of the partition wall are permitted and the gas-tightness is ensured at the gas inlet of the turbine housing.

REFERENCES:
patent: 2801043 (1957-07-01), Spotz et al.
patent: 2944785 (1960-07-01), Sampietro
patent: 3270495 (1966-09-01), Connor
patent: 3331302 (1967-07-01), Baumann et al.
patent: 3394919 (1968-07-01), Catterfeld
patent: 4384821 (1983-05-01), Mains et al.

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