Mid-turbine frame thermal radiation shield

Patent metadata

Field	Value
Publication number	US-9303528-B2
Application number	US-201213543243-A
Country	US
Kind code	B2
Filing date	Jul 6, 2012
Priority date	Jul 6, 2012
Publication date	Apr 5, 2016
Grant date	Apr 5, 2016

Abstract

A thermal radiation shield comprises a first mounting base and a ring section. The first mounting base is disposed at a first axial end of the ring section for securing the shield ring section within a generally annular cavity defined at least in part by a hot fluid flow path boundary wall, and a radially adjacent and spaced apart cold fluid flow path boundary wall. The ring section is configured to substantially block a line of sight between the hot fluid flow path boundary wall and the cold fluid flow path boundary wall.

First claim

The invention claimed is:

1. A mid-turbine frame for a gas turbine engine, the mid-turbine frame comprising:
a radially outer case bounding an outer cold section outward of the outer case;
a radially inner case bounding an inner cold section inward of the inner case, the radially outer and inner cases defining an annular hot section therebetween;
a plurality of load spokes extending radially through the hot section and securing the outer case with the inner case;
a vane pack defining a sealed hot gas path axially traversing an annular portion of the hot section; and
a thermal radiation shield secured within a generally annular hot section cavity defined outside the sealed hot gas path, the thermal radiation shield including a first mounting base disposed at a first axial end of a shield ring section having at least one ring portion, the first mounting base secured to an aft component mounting surface, such that the shield ring section axially extends from the first mounting base towards a second opposing axial end of the shield ring section within the generally annular hot section cavity, the shield ring section substantially blocking a line of sight between an inner vane pack boundary wall and the inner case;
wherein the thermal radiation shield further comprises a second mounting base disposed at a second opposing axial end of the shield ring section; and
wherein the second mounting base includes a second flange in contact with the inner case.

2. The mid-turbine frame of claim 1 , wherein the first mounting base comprises a first flange.

3. The mid-turbine frame of claim 2 , wherein the first flange is secured to a downstream turbine rotor shield.

4. The mid-turbine frame of claim 2 , wherein the first flange is secured to the inner case.

5. The mid-turbine frame of claim 1 , wherein the second mounting base is free to thermally expand and contract proximate the inner case.

6. The mid-turbine frame of claim 1 , wherein the plurality of load spokes extend radially through a corresponding plurality of apertures in the shield ring section.

7. The mid-turbine frame of claim 1 , wherein the shield ring section is formed using a high temperature nickel alloy sheet comprising at least about 20 wt % of chromium.

8. The mid-turbine frame of claim 1 , wherein the aft component mounting surface is selected from: a portion of the inner case, and a downstream turbine rotor shield.

9. The mid-turbine frame of claim 1 , wherein the second mounting base secures the thermal radiation shield to the inner case.

Assignees

• Sanchez Paul K
• Farah Jorge I
• United Technologies Corp

Inventors

• Sanchez Paul K
• Farah Jorge I

Classifications

• F01D9/065

  Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids (see also F01D25/16, F01D25/24 and F01D25/26) · CPC title

• Y02T50/675

  Cross-Sectional Technologies · mapped topic

• F01D25/162 Primary

  Bearing supports · CPC title

• F01D25/28

  Supporting or mounting arrangements, e.g. for turbine casing · CPC title

• F05D2240/15

  Heat shield · CPC title