IP Library Granted Patent US 11,530,615
Granted Patent B1
US 11,530,615 · App. 17/653,110 · Granted Dec 20, 2022

Method for constructing a fixed-vane ring for a nozzle of a turbocharger turbine

Inventors: Yunbin Gong (Shanghai, CN); Jianfeng Du (Shanghai, CN); Zhiqiang Li (Shanghai, CN); Guijun Yang (Shanghai, CN)
Assignee: Garrett Transportation I Inc.
F01D9/041B23P15/04F05D2230/60
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Quick Facts
Patent No.
US 11,530,615
App. No.
17/653,110
Granted
Dec 20, 2022
Kind
B1
Abstract

A method for constructing a nozzle ring for a turbocharger turbine nozzle includes the steps of: providing a nozzle ring in the form of an annular flat disk, the nozzle ring having a first face and an opposite second face; forming a plurality of circumferentially spaced circular bores extending through the nozzle ring from the first face to the second face; providing a plurality of vanes, each vane having a circular vane shaft extending from one end of the vane; inserting the vane shafts respectively into the bores in the nozzle ring from said first face thereof and orienting each vane to achieve a desired setting angle for the vane; and rigidly affixing the vane shafts to the nozzle ring to fix the vanes at the desired setting angles.

Claims (9)

1. A method for constructing a fixed-vane ring for a nozzle of a turbocharger turbine, comprising the steps of:

providing a nozzle ring comprising an annular flat disk, the nozzle ring having a first face and an opposite second face, an annular groove being formed in the second face;

forming a plurality of circumferentially spaced circular bores extending through the nozzle ring from the first face to the second face, the bores being located within said annular groove in the second face of the nozzle ring;

providing a plurality of vanes, each vane comprising an airfoil portion and a circular vane shaft extending from one end of the airfoil portion;

inserting the vane shafts respectively into the bores in the nozzle ring from said first face thereof, each vane being oriented at a desired setting angle; and

rigidly affixing the vane shafts to the nozzle ring to fix the vanes at the desired setting angles.

2. The method of claim 1 , wherein the rigidly affixing step comprises riveting the vane shafts to the nozzle ring.

3. The method of claim 1 , wherein the rigidly affixing step comprises welding the vane shafts to the nozzle ring.

4. The method of claim 1 , wherein the nozzle ring is provided to be constructed of a first material, and the vanes are provided to be constructed of a second material that is different from the first material.

Assignments (2)
SECURITY AGREEMENT (AMENDMENT NO. 3) Recorded Jun 7, 2023
From: GARRETT TRANSPORTATION I INC.
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 063904/0932 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 1, 2022
From: GONG, YUNBIN; DU, JIANFENG; LI, ZHIQIANG; YANG, GUIJUN
To: GARRETT TRANSPORTATION I INC.
Reel/Frame 059139/0454 →