Housing structure with improved seal and cooling

Patent metadata

Field	Value
Publication number	US-9416672-B2
Application number	US-201314052338-A
Country	US
Kind code	B2
Filing date	Oct 11, 2013
Priority date	Oct 12, 2012
Publication date	Aug 16, 2016
Grant date	Aug 16, 2016

Abstract

A housing structure for a turbo-engine, especially for a gas turbine or an aircraft engine, includes an outer housing wall and an inner housing wall, the inner and outer housing walls annularly enclosing a flow channel for the turbo-engine and being spaced apart radially from the flow channel. At least one heat shield is arranged between the inner and outer housing walls, and a bar or a fixture projects at least somewhat radially from the inner housing wall. The bar or the fixture has on at least one side a broadening element that includes a sealing face against which the heat shield is positioned in a sealing manner.

First claim

What is claimed is:

1. A housing structure for a turbo-engine having an outer housing wall and an inner housing wall, the inner and outer housing walls being spaced apart radially from one another and annularly enclosing an axial flow channel for the turbo-engine, the housing structure comprising:
a first heat shield and a second heat shield, both heat shields being disposed radially between the inner housing wall and the outer housing wall, and
a bar projecting from an inner surface of the inner housing wall at least somewhat in a radial direction and extending to a radially outer end directly abutting an inner surface of the outer housing wall, the bar including first and second broadening elements disposed, respectively, on opposing sides of the bar that face away from one another,
the first broadening element being an expansion of a first cross-section of the bar at a first radial location in a first direction transverse to the radial direction;
the second broadening element being an expansion of a second cross-section of the bar at a second radial location in a second direction transverse to the radial direction; and
wherein each of the first and second broadening elements includes a respective sealing face against which the respective first and second heat shield is positioned in a sealing manner; and
wherein each of the first and second broadening elements is disposed radially between the outer housing wall and the inner housing wall such that neither of the broadening elements contacts the outer housing wall or the inner housing wall;
wherein an inner radial side of each of the first and the second heat shields and the inner housing wall delimit, respectively, at least one inner chamber that is spaced apart from the outer housing wall; and
wherein an outer radial side of each of the first and the second heat shields and the outer housing wall delimit at least one respective outer chamber that is spaced apart from the inner housing wall; and the respective inner chambers and the respective outer chambers are sealed off from one another.

2. A housing structure in accordance with claim 1 , wherein the bar further comprises, in addition to the expansion of the cross-section of the bar at the respective first and second radial locations, a cross-section reduction at another radial location so that each of the first and second broadening elements is present only in a specific segment of the bar.

3. A housing structure in accordance with claim 1 , wherein each of the first and second broadening elements is an integral portion of the bar, the respective broadening elements being cast thereon.

4. A housing structure in accordance with claim 1 , wherein the outer housing wall includes at least one cooling air access opening into the at least one outer chamber.

5. A housing structure in accordance with claim 1 , wherein the delimitation of the respective outer chambers further includes the respective sealing faces of the respective broadening elements.

6. A housing structure in accordance with claim 1 , wherein the delimitation of the respective inner chambers further includes the respective sealing faces of the respective broadening elements.

7. A housing structure in accordance with claim 1 , wherein:
the inner housing wall is formed by at least one part of a guide vane; and
the bar is one of
a guide vane bar or
a guide ring bar or
a stator suspension.

8. A turbo-engine comprising:
a combustion chamber;
a turbine; and
a housing structure surrounding a flow channel extending between the combustion chamber and the turbine, the housing structure including
a first heat shield and a second heat shield, both heat shields being disposed radially between an inner housing wall and an outer housing wall, and
a bar projecting from an inner surface of the inner housing wall at least somewhat in a radial direction and extending to a radially outer end directly abutting an inner surface of the outer housing wall, the bar including first and second broadening elements disposed, respectively, on opposing sides of the bar that face away from one another,
the first broadening element being an expansion of a first cross-section of the bar at a first radial location in a first direction transverse to the radial direction;
the second broadening element being an expansion of a second cross-section of the bar at a second radial location in a second direction transverse to the radial direction; and
wherein each of the first and the second broadening elements includes a respective sealing face against which the respective first and second heat shield is positioned in a sealing manner; and
wherein each of the first and second broadening elements is disposed radially between the outer housing wall and the inner housing wall such that neither of the broadening elements contacts the outer housing wall or the inner housing wall;
wherein an inner radial side of each of the first and the second heat shields and the inner housing wall delimit, respectively, at least one inner chamber that is spaced apart from the outer housing wall; and
wherein an outer radial side of each of the first and the second heat shields and the outer housing wall delimit at least one respective outer chamber that is spaced apart from the inner housing wall; and the respective inner chambers and the respective outer chambers are sealed off from one another.

9. A turbo-engine in accordance with claim 8 , wherein the bar further comprises, in addition to the expansion of the cross-section of the bar at the respective first and second radial locations, a cross-section reduction at another radial location so that each of the first and second broadening elements is present only in a specific segment of the bar.

10. A housing structure for a turbo-engine having a combustion chamber, a turbine and a flow channel extending between the combustion chamber and the turbine, the housing structure comprising:
an outer housing wall;
an inner housing wall spaced radially apart from the outer housing wall, the inner and outer housing walls annularly enclosing the flow channel;
a first heat shield and a second heat shield, both heat shields being disposed radially between the inner housing wall and the outer housing wall; and
a bar projecting from an inner surface of the inner housing wall at least somewhat in a radial direction and extending to a radially outer end directly abutting an inner surface of the outer housing wall, the bar including first and second broadening elements disposed, respectively, on opposing sides of the bar that face away from one another,
each of the first and second broadening elements being an expansion of a respective cross-section of the bar at, respectively, a first radial location and a second radial location in a respective direction transverse to the radial direction, wherein the bar comprises a cross-section reduction at another respective radial location so that the respective broadening element is present only in a specific segment of the bar, and
wherein each respective broadening element includes a respective sealing face against which the respective heat shield is positioned in a sealing manner, and
wherein each of the first and second broadening elements is disposed radially between the outer housing wall and the inner housing wall such that neither of the broadening elements contacts the outer housing wall or the inner housing wall;
wherein an inner radial side of each of the first and the second heat shields and the inner housing wall delimit, respectively, at least one inner chamber that is spaced apart from the outer housing wall; and
wherein an outer radial side of each of the first and the second heat shields an

Assignees

• MTU Aero Engines AG

Inventors

• Feldmann Manfred
• Sangl Janine
• Kaltenbach Sebastian
• Lorenz Joachim

Classifications

• F05D2240/15

  Heat shield · CPC title

• F01D11/005

  Sealing means between non relatively rotating elements · CPC title

• F01D9/023 Primary

  Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings · CPC title

• F01D25/243

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

• F01D9/041 Primary

  using blades (F01D5/148 takes precedence) · CPC title