3-D lattice bearing support structure

Patent metadata

Field	Value
Publication number	US-11313248-B2
Application number	US-202016867363-A
Country	US
Kind code	B2
Filing date	May 5, 2020
Priority date	May 5, 2020
Publication date	Apr 26, 2022
Grant date	Apr 26, 2022

Abstract

A lattice bearing support includes a circular inner structure having a center axis and an inner radial surface, an inner rim projecting axially inward from the circular inner structure toward the center axis, a circular outer structure located outward of the circular inner structure with respect to the center axis and having an outer radial surface, an outer radial flange on the circular outer structure that projects radially outward from the outer radial surface, and a number of struts extending radially between the circular inner structure and the circular outer structure.

First claim

The invention claimed is:

1. A lattice bearing support comprising:
a circular inner structure having a center axis, the circular inner structure defining an inner radial surface;
an inner rim disposed on the circular inner structure and projecting axially inward toward the center axis;
a circular outer structure, disposed radially outward from the circular inner structure with respect to the center axis, the circular outer structure defining an outer radial surface;
an outer radial flange disposed on the circular outer structure and projecting radially outward from the outer radial surface; and
a plurality of struts disposed radially between the circular inner structure and the circular outer structure; wherein:
the plurality of struts are arranged in axial courses;
the number of axial courses ranges from 4-12;
at least some of the plurality of struts lean in a first direction relative to a radial vector projecting radially outward from the center axis;
at least some of the plurality of struts lean in a second direction relative to a radial vector projecting radially outward from the center axis; and
the first direction is opposite the second direction.

2. The lattice bearing support of claim 1 , wherein:
the inner radial surface is configured to contactingly engage an outer race of a bearing assembly; and
the inner rim defines an axial face that is configured to contactingly engage with the outer race, thereby at least partially axially supporting the lattice bearing support.

3. The lattice bearing support of claim 1 , wherein:
the outer radial flange defines a flange forward face and a flange aft face;
the flange forward face is configured to contactingly engage with a forward structure, thereby at least partially axially supporting the lattice bearing support; and
the flange aft face is configured to contactingly engage with an aft structure, thereby at least partially axially supporting the lattice bearing support.

4. The lattice bearing support of claim 1 , wherein:
each of the plurality of struts defines a strut angle relative to a radial vector projecting radially outward from the center axis; and
the strut angle of each of the plurality of struts ranges from 0-60 degrees.

5. The lattice bearing support of claim 4 , wherein the strut angle of each of the plurality of struts ranges from 10-45 degrees.

6. The lattice bearing support of claim 1 , wherein:
each of the plurality of struts has an axial cross-sectional shape that is circular;
the axial cross-sectional shape defines a diameter; and
the diameter ranges from 1-10 mm.

7. The lattice bearing support of claim 1 , wherein:
each of the plurality of struts defines an inner end near the circular inner structure and an outer end near the circular outer structure; and
a cross-sectional area of one or more struts decreases from the inner end to the outer end.

8. The lattice bearing support of claim 1 , wherein:
each of the plurality of struts defines:
an inner end near the circular inner structure;
an outer end near the circular outer structure; and
an intermediate point located between the inner end and the outer end; and

a cross-sectional area of one or more struts at the intermediate point is less than the cross-sectional area at either the inner end or the outer end.

9. The lattice bearing support of claim 1 , wherein:
one or more of the plurality of struts has an axial cross-sectional shape that is elliptical, oval, or oblong;
the axial cross-sectional shape defines a major axis and a minor axis; and
a ratio of a length of the major axis to a length of the minor axis ranges between 1-5.

10. The lattice bearing support of claim 9 , wherein the major axis is parallel to the center axis, thereby reducing a restriction to flow of a fluid through the lattice bearing support.

11. The lattice bearing support of claim 1 , comprising nickel, aluminum, titanium, copper, iron, cobalt, and/or alloys thereof.

12. The lattice bearing support of claim 1 , wherein the lattice bearing support is manufactured by one or more of additive manufacturing, hybrid additive manufacturing, hybrid additive subtractive manufacturing, subtractive manufacturing, forging, extrusion, and/or casting processes.

13. The lattice bearing support of claim 12 , wherein one or more characteristics of the plurality of struts is configured to provide a desired radial and/or axial stiffness.

14. The lattice bearing support of claim 13 , wherein the one or more characteristics is selected from the list consisting of length, girth, shape, orientation, number, and material of composition.

15. A gas turbine engine comprising one or more lattice bearing supports of claim 1 .

16. A lattice bearing support comprising:
a circular inner structure having a center axis, the circular inner structure defining an inner radial surface that is configured to contactingly engage an outer race of a bearing assembly;
an inner rim disposed on the circular inner structure and projecting axially inward toward the center axis, the inner rim defining an axial face configured to contactingly engage with the outer race, thereby at least partially axially supporting the lattice bearing support;
a circular outer structure, disposed radially outward from the circular inner structure with respect to the center axis, the circular outer structure defining an outer radial surface;
an outer radial flange disposed on the circular outer structure and projecting radially outward from the outer radial surface, the outer radial flange defining a flange forward face and a flange aft face; and
a plurality of struts disposed radially between the circular inner structure and the circular outer structure, thereby holding the circular outer structure relative to the circular inner structure; wherein:
the plurality of struts are arranged in axial courses;
the number of axial courses ranges from 4-12;
at least some of the plurality of struts lean in a first direction relative to a radial vector projecting radially outward from the center axis;
at least some of the plurality of struts lean in a second direction relative to a radial vector projecting radially outward from the center axis; and
the first direction is opposite the second direction.

17. The lattice bearing support of claim 16 , wherein:
each of the plurality of struts defines a strut angle relative to a radial vector projecting radially outward from the center axis; and
the strut angle of each of the plurality of struts ranges from 0-60 degrees.

18. The lattice bearing support of claim 16 , wherein:
the lattice bearing support comprises nickel, aluminum, titanium, copper, iron, cobalt, and/or alloys thereof;
the lattice bearing support is manufactured by one or more of additive manufacturing, hybrid additive manufacturing, hybrid additive subtractive manufacturing, subtractive manufacturing, forging, extrusion, and/or casting processes;
one or more characteristics of the plurality of struts is configured to provide a desired radial and/or axial stiffness; and
the one or more characteristics is selected from the list consisting of length, girth, shape, orientation, number, and material of composition.

Assignees

• Raytheon Tech Corp

Inventors

• Demitraszek Sr Anthony

Classifications

• F05D2220/32

  in gas turbines · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• F16C13/04

  Bearings with only partial enclosure of the member to be borne; Bearings with local support at two or more points · CPC title

• F16M2200/00

  Details of stands or supports · CPC title

• F01D25/164

  Flexible supports; Vibration damping means associated with the bearing · CPC title