Honeywell International Inc.

Garrett Transportation I Inc.

Mohamed Tahyry

Francis Abel

Pierre Barthelet

Lorrain Sausse

Arnaud Gerard

Giorgio Figura

Olivier Espasa

Vincent Eumont

Bassam Chammas

Emmanuel Bouvier

Jean-Michel Geoffroy

Nicolas Gaineton

Romain Chicot

A turbocharger having a variable-nozzle turbine formed by pivotable vanes supported by a nozzle ring includes a locator that is radially elastically deformable and is disposed between a radially outwardly facing surface of the center housing and an opposing surface of the nozzle ring for radially locating the nozzle ring relative to the center housing. At least one vent is defined in either a radially outermost surface of the locator or the surface of the nozzle ring to allow pressure communication between spaces on axially opposite sides of the locator.

Variable-nozzle turbine with means for radial locating of variable-nozzle cartridge

A variable-vane assembly for a variable nozzle turbine comprises a nozzle ring supporting a plurality of vanes affixed to vane arms that are engaged in recesses in the inner edge of a unison ring. The unison ring is rotatable about the axis of the nozzle ring so as to pivot the vane arms, thereby pivoting the vanes in unison. A plurality of guide pins for the unison ring are inserted into apertures in the nozzle ring and are rigidly affixed therein such that the guide pins are non-rotatably secured to the nozzle ring with a guide portion of each guide pin projecting axially from the face of the nozzle ring. Each guide portion defines a shoulder radially overlapping the inner edge of the unison ring such that the unison ring is restrained by the guide pins against excessive movement in both radial and axial directions.

Variable-vane assembly having fixed guide pins for unison ring

Growing community of inventors

Epinal, France

Mohamed Tahyry