Turbocharger

Patent metadata

Field	Value
Publication number	US-10161305-B2
Application number	US-201214358073-A
Country	US
Kind code	B2
Filing date	Nov 13, 2012
Priority date	Nov 16, 2011
Publication date	Dec 25, 2018
Grant date	Dec 25, 2018

Abstract

A circular ring-shaped shroud plate is arranged between a scroll passage and a turbine chamber. The shroud plate has a through-hole that penetrates therethrough in a direction along an axis of a turbine shaft. A variable nozzle is supported in an openable/closable manner on the shroud plate by a shaft inserted through the through-hole. A gap between the shroud plate and a turbine housing in the direction along the axis is partitioned into a first space that communicates with an outlet of exhaust gas that faces the through-hole and is provided upstream of a turbine wheel with respect to the flow of exhaust gas, and a second space that communicates with the scroll passage, by a disc spring that is so arranged as to surround the turbine wheel.

First claim

The invention claimed is:

1. A turbocharger comprising:
a turbine housing that has a convolute scroll passage around a turbine chamber;
a turbine wheel provided on a turbine shaft, the turbine wheel rotating in the turbine chamber and being rotationally driven when exhaust gas that has flowed along the scroll passage after being discharged from an engine is blown onto the turbine wheel;
an annular support member arranged between the scroll passage and the turbine chamber, the annular support member having through-holes at a plurality of spots around the turbine wheel, the through-holes penetrating in a direction along an axis of the turbine shaft;
a plurality of variable nozzles that are openable and closeable, the variable nozzles being supported on the support member by shafts inserted through the respective through-holes, and making variable a flow velocity of exhaust gas blown onto the turbine wheel through changes in opening degrees of the variable nozzles; and
an annular sealing member arranged so as to surround the turbine wheel, the annular sealing member partitioning a gap between the support member and the turbine housing in the direction along the axis into a first space communicating with an outlet of exhaust gas, the annular sealing member facing the through-holes and being provided upstream of the turbine wheel with respect to flow of exhaust gas, wherein exhaust gas passing through the outlet is blown onto the turbine wheel to rotationally drive the turbine wheel, and a second space communicating with the scroll passage, and
wherein the turbocharger further includes a flow path conveying exhaust gas from the through-holes to a portion upstream of the turbine wheel such that exhaust gas flowing through the flow path is used to rotationally drive the turbine wheel, the flow path including a passage establishing communication between the first space and operational ranges of the variable nozzles where each of the plurality of variable nozzles turns together with a corresponding one of the shafts, the operational ranges of the variable nozzles including regions of the variable nozzles located downstream of the shafts with respect to the flow of exhaust gas where each of the variable nozzles turns together with a corresponding one of the shafts, and wherein at least one of the variable nozzles is configured to extend past the outlet and to reach a bulge portion of the turbine housing towards the turbine chamber.

2. The turbocharger according to claim 1 , wherein the bulge portion extends toward a side of a bearing housing, the bearing house rotatably supports the turbine shaft and is located between the support member and the turbine wheel in a state of being spaced apart from the support member, and the passage is constituted by a space between the support member and the bulge portion.

3. The turbocharger according to claim 1 , further comprising:
an annular plate that is arranged opposite the support member across the variable nozzle, the annular plate being integrally coupled to the support member, wherein
the sealing member is constituted by a disc spring, the disc spring is arranged so as to surround the turbine wheel in the gap, the disc spring is in contact with the support member at one of an outer peripheral edge portion of the disc spring and an inner peripheral edge portion of the disc spring, and the disc spring is in contact with the turbine housing, at the outer peripheral edge portion of the disc spring and the inner peripheral edge portion of the disc spring, wherein the disc spring is in an elastically deformed state such that a dimension of the disc spring in the direction along the axis decreases, the disc spring urges the support member toward a side of a bearing housing that supports the turbine shaft, presses the annular plate against the bearing housing, and partitions the gap into the first space and the second space.

Assignees

• Ikegami Hiroaki
• Uesugi Tsuyoshi
• Toyota Motor Co Ltd
• Toyota Jidoshokki Kk

Inventors

• Ikegami Hiroaki
• Uesugi Tsuyoshi

Classifications

• F01D17/165 Primary

  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

• F02B43/02 Primary

  Engines characterised by means for increasing operating efficiency · CPC title

• F02C6/12

  Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure · CPC title

• F05D2220/40

  in turbochargers · CPC title