Outer case with gusseted boss

Patent metadata

Field	Value
Publication number	US-9328629-B2
Application number	US-201213631770-A
Country	US
Kind code	B2
Filing date	Sep 28, 2012
Priority date	Sep 28, 2012
Publication date	May 3, 2016
Grant date	May 3, 2016

Abstract

An outer case employed in a gas turbine engine includes a plurality of support member bosses and a plurality of gusseted bosses. The plurality of support member bosses are disposed circumferentially around the outer case for receiving and securing support members that attach the outer case to an inner hub. The plurality of gusseted bosses are disposed circumferentially around the outer case and between the plurality of support member bosses.

First claim

The invention claimed is:

1. An outer case employed in a gas turbine engine, the outer case comprising:
a plurality of support member bosses disposed circumferentially around the outer case for receiving and securing support members that attach the outer case to an inner hub; and
a plurality of gusseted bosses disposed circumferentially around the outer case and between the plurality of support member bosses, wherein each of the plurality of gusseted bosses is solid and is solely connected to a single surface of the outer case.

2. The outer case of claim 1 , wherein each of the plurality of gusseted bosses include:
a flat portion extending from the surface of the outer case that is substantially parallel to an engine centerline axis; and
a curved portion extending between the surface of the outer case and the flat portion that is substantially perpendicular to the flat portion.

3. The outer case of claim 1 , wherein the plurality of gusseted bosses are axially aligned with the support member bosses.

4. A mid-turbine frame portion of a gas turbine engine comprising the outer case of claim 1 .

5. The outer case of claim 1 , wherein the plurality of gusseted bosses are located to maintain system stiffness symmetry.

6. The outer case of claim 1 , wherein the plurality of gusseted bosses are located circumferentially around the outer case to provide ovalization control of the outer case.

7. The outer case of claim 1 , wherein seven gusseted bosses are disposed circumferentially around the outer case.

8. A mid-turbine frame comprising:
an inner hub;
an outer case;
a plurality of vanes located in a gas path defined between the inner hub and the outer case;
a plurality of support members affixed between the inner hub and the outer case that transfer loads from the inner hub to the outer case;
wherein the outer case includes:
a plurality of support member bosses that receive and affix the support members to the outer case; and
a plurality of gusseted bosses disposed circumferentially around the outer case and between the plurality of support member bosses, wherein each of the plurality of gusseted bosses is solid and is solely connected to a single surface of the outer case.

9. The mid-turbine frame of claim 8 , wherein each of the plurality of gusseted bosses include:
a flat portion extending from the surface of the outer case that is substantially parallel to an engine centerline axis; and
a curved portion extending between the surface of the outer case and the flat portion that is substantially perpendicular to the flat portion.

10. The mid-turbine frame of claim 8 , wherein the plurality of gusseted bosses are axially aligned with the support member bosses.

11. The mid-turbine frame of claim 8 , wherein the plurality of gusseted bosses are positioned circumferentially around the outer case to provide ovalization control of the outer case.

12. The mid-turbine frame of claim 8 , wherein seven gusseted bosses are disposed circumferentially around the outer case.

13. A gas turbine engine comprising:
a fan section;
a compressor section located downstream from the fan section;
a combustor section;
a high pressure turbine section located downstream from the combustor section;
a low pressure turbine section located downstream for the high pressure turbine section;
a mid-turbine frame section disposed between the high pressure turbine section and the low pressure section, the mid-turbine frame section comprising:
an inner hub;
an outer case;
a plurality of vanes located in a gas path defined between the inner hub and the outer case;
a plurality of support members affixed between the inner hub and the outer case that transfer loads from the inner hub to the outer case;
wherein the outer case includes:
a plurality of support member bosses that receive and affix the support members to the outer case; and
a plurality of gusseted bosses disposed circumferentially around the outer case and between the plurality of support member bosses, wherein each of the plurality of gusseted bosses is solid and is solely connected to a single surface of the outer case.

14. The gas turbine engine of claim 13 , wherein each of the plurality of gusseted bosses include:
a flat portion extending from the surface of the outer case that is substantially parallel to an engine centerline axis; and
a curved portion extending between the surface of the outer case and the flat portion that is substantially perpendicular to the flat portion.

15. The gas turbine engine of claim 13 , wherein the plurality of gusseted bosses are axially aligned with the support member bosses.

16. The gas turbine engine of claim 13 , wherein the plurality of gusseted bosses are positioned circumferentially around the outer case to provide ovalization control of the outer case.

17. The gas turbine engine of claim 13 , wherein seven gusseted bosses are disposed circumferentially around the outer case.

Assignees

• United Technologies Corp

Inventors

• Scott Jonathan Ariel
• Farah Jorge I

Classifications

• F01D25/24

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• F01D25/162 Primary

  Bearing supports · CPC title