Variable nozzle mechanism and variable-displacement type exhaust turbocharger
US-2018340467-A1 · Nov 29, 2018 · US
US10995629B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10995629-B2 |
| Application number | US-201816200934-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 27, 2018 |
| Priority date | Nov 30, 2017 |
| Publication date | May 4, 2021 |
| Grant date | May 4, 2021 |
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A variable nozzle mechanism in which a nozzle mount has a first surface which has a minimum clearance in a direction of an axis with respect to a lever side facing surface in an opposing region facing the lever side facing surface in the direction of the axis, and a second surface which is disposed adjacent to the first surface in a circumferential direction of the nozzle mount and has a clearance in the direction of the axis with respect to the lever side facing surface larger than the clearance in the direction of the axis between the first surface and the lever side facing surface.
Opening claim text (preview).
What is claimed is: 1. A variable nozzle mechanism, comprising: a first annular member; a plurality of nozzle vanes which are provided to face the first annular member, disposed in an annular fluid flow channel for guiding a working fluid from a scroll flow channel formed on an outer circumferential side of a turbine rotor to the turbine rotor, rotatable relative to the first annular member, and configured to adjust the flow passage area of the fluid flow channel; a plurality of vane shafts which are inserted through support holes penetrating through the first annular member and support the respective nozzle vanes one by one; a plurality of levers which are disposed outside the fluid flow channel and extend from the respective vane shafts radially outward of the first annular member; and a second annular member which is provided to be rotatable with respect to the first annular member around a central axis of the first annular member to support the plurality of levers, and rotates the nozzle vanes together with the levers relative to the first annular member, wherein a circumferential direction of the first annular member is the same as a rotation direction of the second annular member, wherein each of the levers has a lever side facing surface which faces the first annular member in the direction of the central axis, and wherein the first annular member has a first surface which has a minimum clearance in the direction of the central axis with respect to the lever side facing surface in an opposing region that faces the lever side facing surface in the direction of the central axis, and a second surface which is disposed adjacent to the first surface in the circumferential direction of the first annular member and has a clearance in the direction of the central axis with respect to the lever side facing surface that, when the lever side facing surface faces the second surface, is greater than the clearance in the direction of the central axis between the first surface and the lever side facing surface. 2. The variable nozzle mechanism according to claim 1 , wherein the first surface and the second surface are arranged alternately in the circumferential direction so as to form an annular shape. 3. The variable nozzle mechanism according to claim 1 , wherein a recessed portion which is recessed in the direction of the central axis is provided in the opposing region of the first annular member, and the second surface is provided on an inner surface of the recessed portion. 4. The variable nozzle mechanism according to claim 1 , wherein a protruding portion which protrudes in the direction of the central axis and is separate from or integral with the first annular member is provided in the opposing region of the first annular member, and the first surface is provided on a surface of the protruding portion. 5. The variable nozzle mechanism according to claim 1 , wherein the lever further includes an engaging portion which is engaged with and supported by the second annular member at an outer end portion in the radial direction, and the lever side facing surface is provided in the engaging portion. 6. The variable nozzle mechanism according to claim 1 , wherein the lever further comprises: an engaging portion which is engaged with and supported by the second annular member at an outer end portion in the radial direction, and a fixing portion which fixes the vane shaft at an inner end portion in the radial direction, and the lever side facing surface is provided between the engaging portion and the fixing portion. 7. The variable nozzle mechanism according to claim 1 , wherein the first surface is provided along the lever side facing surface, and the second surface gradually approaches to the lever side facing surface to be connected to the first surface as it goes toward a front side in a rotational direction of the second annular member which is a direction in which an opening of a nozzle vane of the plurality of nozzle vanes increases. 8. A rotating machine comprising the variable nozzle mechanism according to claim 1 . 9. The variable nozzle mechanism according to claim 1 , wherein when the nozzle vanes are arranged at the position of full opening, the lever side facing surface faces the first surface.
for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line (F01D17/167 takes precedence) · CPC title
for radial admission · CPC title
the axes being inclined in relation to each other · CPC title
in turbochargers · CPC title
by means of nozzle vanes · CPC title
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