Outer diffuser case for a gas turbine engine

Patent metadata

Field	Value
Publication number	US-10100675-B2
Application number	US-201514958287-A
Country	US
Kind code	B2
Filing date	Dec 3, 2015
Priority date	Dec 9, 2014
Publication date	Oct 16, 2018
Grant date	Oct 16, 2018

Abstract

An outer diffuser case of a diffuser case assembly for use in a gas turbine engine may have a housing orientated about an engine axis, a forward flange projecting radially outward from the housing, a mid-flange spaced axially aft of the forward flange and projecting radially inward from the housing, and an aft flange projecting radially outward from the housing. The mid flange is spaced axially between the forward and aft flanges and is configured to detachably engage an inner diffuser case of the case assembly. The forward flange is configured to detachably engage a high pressure compressor and the aft flange is configured to detachably engage a high pressure turbine of the engine.

First claim

The invention claimed is:

1. An outer diffuser case for use in a gas turbine engine, the outer diffuser case comprising:
a housing orientated about an axis;
a forward flange projecting radially outward from the housing and configured to detachably engage a high pressure compressor;
an aft flange spaced axially downstream from the forward flange, projecting radially outward from the housing, and configured to detachably engage a high pressure turbine; and
a mid-flange spaced axially between the forward and aft flanges and projecting radially inward from the housing, and wherein the mid flange is configured to detachably engage an inner diffuser case;
wherein the housing has an axial length within a range of 39.200 to 39.210 cm, and an outer diameter proximate to the forward flange within a range of 51.864 to 51.890 cm.

2. The outer diffuser case set forth in claim 1 , wherein the housing is cone shaped and diverges in a downstream direction, increasing in diameter from an upstream end to a downstream end.

3. The outer diffuser case set forth in claim 2 , wherein the housing diverges in the downstream direction by about 2.5 degrees with respect to the axis.

4. The outer diffuser case set forth in claim 1 , wherein the housing has a minimum wall thickness proximate to the aft flange within a range of 0.305 to 0.330 cm.

5. The outer diffuser ease set forth in claim 1 , wherein the aft flange carries ninety circumferentially spaced bolt holes, and each of the spaced bolt holes has a center positioned at a distance of about 28.912 cm from the axis.

6. The outer diffuser case set forth in claim 1 , wherein the forward flange carries 81 circumferentially spaced bolt holes, and each of the spaced bolt holes has a center positioned at a distance of about 27.441 cm from the axis.

7. The outer diffuser case set forth in claim 1 , wherein the housing includes a rearward projecting, annular, lip disposed downstream of the aft flange.

8. The outer diffuser case set forth in claim 7 , wherein the lip has a base portion and a reinforcement portion projecting radially outward from the base portion and directly adjacent to the aft flange.

9. An outer diffuser case for use in a gas turbine engine, the outer diffuser case comprising:
a housing orientated about an axis;
a forward flange projecting radially outward from the housing and configured to detachably engage a high pressure compressor;
an aft flange spaced axially downstream from the forward flange, projecting radially outward from the housing, and configured to detachably engage a high pressure turbine; and
a mid-flange spaced axially between the forward and aft flanges and projecting radially inward from the housing, and wherein the mid flange is configured to detachably engage an inner diffuser case;
wherein the aft flange carries ninety circumferentially spaced bolt holes, and each of the spaced bolt holes has a center positioned at a distance of about 28.912 cm from the axis; and
wherein the aft flange has a thickness within a range of 0.610 to 0.762 cm.

10. An outer diffuser case for use in a gas turbine engine, the outer diffuser case comprising:
a housing orientated about an axis;
a forward flange projecting radially outward from the housing and configured to detachably engage a high pressure compressor;
an aft flange spaced axially downstream from the forward flange, projecting radially outward from the housing, and configured to detachably engage a high pressure turbine; and
a mid-flange spaced axially between the forward and aft flanges and projecting radially inward from the housing, and wherein the mid flange is configured to detachably engage an inner diffuser case;
wherein the aft flange carries ninety circumferentially spaced bolt holes, and each of the spaced bolt holes has a center positioned at a distance of about 28.912 cm from the axis; and
wherein the aft flange has an outer diameter within a range of 59.830 to 59.957 cm.

11. An outer diffuser case for use in a gas turbine engine, the outer diffuser case comprising:
a housing orientated about an axis;
a forward flange projecting radially outward from the housing and configured to detachably engage a high pressure compressor;
an aft flange spaced axially downstream from the forward flange, projecting radially outward from the housing, and configured to detachably engage a high pressure turbine; and
a mid-flange spaced axially between the forward and aft flanges and projecting radially inward from the housing, and wherein the mid flange is configured to detachably engage an inner diffuser case;
wherein the forward flange carries 81 circumferentially spaced bolt holes, and each of the spaced bolt holes has a center positioned at a distance of about 27.441 cm from the axis; and
wherein the forward flange has a thickness within a range of 0.508 to 0.660 cm.

12. An outer diffusser case for use in a gas turbine engine, the outer diffuser case comprising:
a housing orientated about an axis;
a forward flange projecting radially outward from the housing and configured to detachably engage a high pressure compressor;
an aft flange spaced axially downstream from the forward flange, projecting radially outward from the housing, and configured to detachably engage a high pressure turbine; and
a mid-flange spaced axially between the forward and aft flanges and projecting radially inward from the housing, and wherein the mid flange is configured to detachably engage an inner diffuser case;
wherein the forward flange carries 81 circumferentially spaced bolt holes, and each of the spaced bolt holes has a center positioned at a distance of about 27.441 cm from the axis; and
wherein the forward flange has an outer diameter within a range of 28.824 to 28.964 cm.

13. An outer diffuser case for use in a gas turbine engine, the outer diffuser case comprising:
a housing orientated about an axis;
a forward flange projecting radially outward from the housing and configured to detachably engage a high pressure compressor;
an aft flange spaced axially downstream from the forward flange, projecting radially outward from the housing, and configured to detachably engage a high pressure turbine; and
a mid-flange spaced axially between the forward and the aft flanges and projecting radially inward the housing, and wherein the mid flange is configured to detachably engage an inner diffuser case;
wherein the housing includes a rearward projecting, annular, lip disposed downstream of the aft flange;
wherein the lip has a base portion and a reinforcement portion projecting radially outward from the base portion and directly adjacent to the aft flange; and
wherein the base portion includes a distal end that projects axially rearward further than the reinforcement portion, the base portion has an outer diameter within a range of 54.562 to 54.587 cm, and the reinforcement portion projects axially rearward from the aft flange by a distance within a range of 0.749 to 0.775 cm and has an outer diameter with a range of 54.747 to 54.757 cm.

14. An outer diffuser case for use in a gas turbine engine, the outer diffuser case comprising:
a cone-shaped housing orientated about an axis, the housing including a lip; and
an aft flange projecting radially outward from the housing, and configured to detachably engage a high pressure turbine, wherein the lip generally projects rearward from the aft flange;
wherein the lip has a base portion and a reinforcement portion projecting radially outward from the base portion and directly adjacent to the aft flange; and
wherein the base portion includes a dital end that projects axially rearward

Assignees

• United Technologies Corp

Inventors

• Eastwood Jonathan J
• Hyland Dave J
• Dale Timothy

Classifications

• F01D25/243 Primary

  Flange connections; Bolting arrangements (F01D25/265 takes precedence) · CPC title

• 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

• F01D25/34

  Turning or inching gear · CPC title

• F01D25/30

  Exhaust heads, chambers, or the like · CPC title

• F01D25/26

  Double casings; Measures against temperature strain in casings · CPC title