Granted Patent B1

US 12,392,347 · App. 18/443,905 · Granted Aug 19, 2025

Inventors: Chao Zhang (Vaughan, CA); Rambod Larijani (Mississauga, CA)

Assignee: Pratt & Whitney Canada Corp.

F04D17/10F04D29/284

Abstract

Claims (23)

1. A method of producing a centrifugal compressor impeller, the impeller including a hub with a rotational axis, a forward surface, and an aft surface, the aft surface extending between an outer radial surface of the impeller and a bore centered on the rotational axis, the method comprising:

analyzing the impeller to determine a stress field having tangential stress data values and radial stress data values as a function of radial position within the impeller hub and as a function of axial position within the impeller hub;

determining biaxiality ratio (BR) data using the determined tangential stress data values and the determined radial stress data values;

determining a peak von Mises creep strain location on the impeller;

contouring the aft surface at the peak von Mises creep strain location using the radial stress data values and the BR data, the contouring including providing a hub thickness aligned with the peak von Mises creep strain location so that the impeller hub has a localized area of decreased radial stress data values at the peak von Mises creep strain location; and

producing the impeller with the aft surface.

2. The method of claim 1 , wherein a portion of the aft surface has a concave arcuate contour that defines a rear cavity.

3. The method of claim 2 , wherein the step of contouring the aft surface step includes contouring at least a portion of the rear cavity.

4. The method of claim 1 , wherein the step of contouring the aft surface includes providing the hub thickness aligned with the peak von Mises creep strain location so that the impeller hub has a localized area of decreased BR data values at the peak von Mises creep strain location.

5. The method of claim 4 , wherein the step of contouring the aft surface includes providing the hub thickness aligned with the peak von Mises creep strain location so that the impeller hub has a localized area of decreased von Mises stress (S VM ) values at the peak von Mises creep strain location.

6. The method of claim 1 , wherein the step of contouring the aft surface includes providing a hub thickness that has a first region of radial stress data values, a second region of radial stress data values, and a third region of radial stress data values, wherein the first region of radial stress data values is disposed at a first radius from the rotational axis, the second region of radial stress data values is disposed at a second radius from the rotational axis, and the third region of radial stress data values is disposed at a third radius from the rotational axis, wherein the second radius is greater than the first radius, and the third radius is greater than the second radius, and wherein the radial stress data values in the second region are lower than the radial stress data values in both the first region and the third region, and wherein the determined von Mises peak creep strain is disposed at the second radius.

7. A method of producing a centrifugal compressor impeller, the impeller including a hub with a rotational axis, a forward surface, and an aft surface, the aft surface extending between an outer radial surface of the impeller and a bore centered on the rotational axis, the method comprising:

analyzing the impeller to determine a stress field having tangential stress data values and radial stress data values as a function of radial position within the impeller hub and as a function of axial position within the impeller hub;

determining biaxiality ratio (BR) data using the determined tangential stress data values and the determined radial stress data values;

determining a peak von Mises creep strain location on the impeller;

contouring the aft surface at the peak von Mises creep strain location using the radial stress data values and the BR data, wherein the contouring includes providing a hub thickness aligned with the peak von Mises creep strain location so that the impeller hub has a localized area of decreased BR data values at the peak von Mises creep strain location; and

producing the impeller with the aft surface.

8. A method of producing a centrifugal compressor impeller, the impeller including a hub with a rotational axis, a forward surface, and an aft surface, the aft surface extending between an outer radial surface of the impeller and a bore centered on the rotational axis, the method comprising:

analyzing the impeller to determine a stress field having tangential stress data values and radial stress data values as a function of radial position within the impeller hub and as a function of axial position within the impeller hub;

determining biaxiality ratio (BR) data using the determined tangential stress data values and the determined radial stress data values;

determining a peak von Mises creep strain location on the impeller;

contouring the aft surface at the peak von Mises creep strain location using the radial stress data values and the BR data, wherein the contouring includes providing a hub thickness aligned with the peak von Mises creep strain location so that the impeller hub has a localized area of decreased von Mises stress (S VM ) values at the peak von Mises creep strain location; and

producing the impeller with the aft surface.

Assignments (1)

References Cited (20)