Attenuating shroud support

• US 5,181,826 A
• Filed: 11/23/1990
• Issued: 01/26/1993
• Est. Priority Date: 11/23/1990
• Status: Expired due to Fees

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Rock, Peter J.
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): Lee, Michael S.
• Application Number:
  US07/617,244
• Time in Patent Office: 795 Days
• Field of Search: 415/114, 415/115, 415/116, 415/117, 415/134, 415/135, 415/139, 415/173.1, 415/173.3, 415/173.6
• US Class Current: 415/173.1
• CPC Class Codes: F01D 11/18 using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion

Abstract

A shroud support for a gas turbine engine includes a mounting flange mountable to a casing, a hanger for supporting a turbine shroud, and an annular coupling joining the mounting flange to the hanger. The coupling includes a set of circumferentially spaced apertures defining a set of beams therebetween, with the beams being sized and configured for attenuating radial distortion from the mounting flange transmitted to the hanger. In a preferred embodiment of the invention, the coupling includes a frustum which includes the apertures and beams.

Claims

1. A turbine shroud support comprising:

an annular mounting flange having a radially outer end fixedly mountable to a casing, and a radially inner end;

an annular hanger spaced radially inwardly from said mounting flange for supporting a turbine shroud;

an annular coupling fixedly joining said mounting flange to said hanger, and including a plurality of circumferentially spaced apertures defining a plurality of beams therebetween, said beams being sized and configured for reducing axial force and axial moment transmitted from said mounting flange to said hanger for attenuating radial distortion transmitted to said hanger from said mounting flange.

2. A shroud support according to claim 1 wherein said coupling includes a frustum having a base fixedly joined to said mounting flange, and a top joined to said hanger, and said apertures extend between said base and said top to define said beams extending from said base to said top.

3. A shroud support according to claim 2 wherein said beams are equiangularly spaced from each other.

4. A shroud support according to claim 3 wherein said frustum includes a centerline axis and said beams extend radially outwardly relatively to said frustum centerline axis and perpendicularly to said base.

5. A shroud support according to claim 2 wherein said beams each have a length, width, and thickness preselected for providing flexibility of said frustum for attenuating said transmitted radial distortion.

6. A shroud support according to claim 2 wherein said coupling further includes a tubular cylinder disposed coaxially between said frustum and said hanger, and having a proximal end fixedly joined to said frustum top, and a distal end fixedly joined to said hanger.

7. A shroud support according to claim 6 wherein said hanger includes an aft rail fixedly joined to said cylinder distal end, a base fixedly joined to said aft rail for supporting said shroud, and a forward rail fixedly joined to said base and spaced generally parallel to said aft rail.

8. A shroud support according to claim 7 wherein said frustum includes a centerline axis and said beams extend radially outwardly relative to said frustum centerline axis and perpendicularly to said base and said top, and equiangularly from each other.

9. A shroud support according to claim 8 wherein said beams each have a length, width, and thickness preselected for providing flexibility of said frustum for attenuating said transmitted radial distortion.

10. A shroud support according to claim 9 wherein said frustum has a cone angle relative to said frustum centerline axis of about 53°

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