Systems and methods for a variable geometry turbine nozzle

Patent metadata

Field	Value
Publication number	US-10519799-B2
Application number	US-201715828681-A
Country	US
Kind code	B2
Filing date	Dec 1, 2017
Priority date	Nov 21, 2014
Publication date	Dec 31, 2019
Grant date	Dec 31, 2019

Abstract

Various systems and methods are described for a variable geometry turbine. In one example, a nozzle vane includes a stationary having a first cambered sliding surface and a sliding vane having a second cambered sliding surface where the second cambered sliding surface includes a flow disrupting feature in contact with the first sliding cambered surface. The sliding vane may be positioned to slide in a direction from substantially tangent along a curved path to an inner circumference of the turbine nozzle and selectively uncover the flow disrupting feature.

First claim

The invention claimed is:

1. A method for a turbine nozzle, comprising:
during a first condition, moving an actuation block coupled to a nozzle vane of the turbine nozzle from a first position to a second position to open the nozzle vane and move the nozzle vane against a shroud-side wall of the turbine nozzle; and
during a second condition, moving the actuation block from the second position to a third position, the first position between the second position and the third position, and then back to the first position to close the nozzle vane and move the nozzle vane back against the shroud-side wall.

2. The method of claim 1 , wherein the first condition includes when engine load is greater than a threshold load and wherein the second condition includes when engine load is less than the threshold load.

3. The method of claim 1 , wherein the actuation block is shaped as a rhomboid.

4. The method of claim 1 , wherein the actuation block is coupled to the nozzle vane through a pivotable yoke and rotatable shaft, the pivotable yoke surrounding two oppositely facing sides of the actuation block.

5. The method of claim 4 , wherein moving the actuation block includes moving the actuation block in a circumferential direction relative to a central axis of a turbine wheel, the turbine nozzle surrounding the turbine wheel and sharing the central axis with the turbine wheel, and consequentially moving the pivotable yoke in the circumferential direction and an axial direction, the axial direction defined in a direction of the central axis.

Assignees

• Ford Global Tech Llc

Inventors

• Sun Harold Huimin
• Zhao Ben
• Hu Leon
• Yi Jianwen James
• Curtis Eric Warren
• Zhang Jizhong

Classifications

• F05D2210/30

  Flow characteristics · CPC title

• 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

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title

• F02B37/24 Primary

  by using pumps or turbines with adjustable guide vanes · CPC title

• F05D2220/40

  in turbochargers · CPC title