Attachment device for removable components in hot gas paths in a turbine engine

• US 7,334,960 B2
• Filed: 06/23/2005
• Issued: 02/26/2008
• Est. Priority Date: 06/23/2005
• Status: Expired due to Fees

• Current Assignee: Siemens Energy Incorporated (Siemens AG)
• Original Assignee: Siemens Power Generation, Inc.
• Inventors: Glessner, John C., Dahlke, Stefan, Nicosia, Robert O., Moraes, Ricardo F.
• Primary Examiner(s): Stodola; Daniel P.
• Assistant Examiner(s): Ferguson; Michael P.
• Application Number:
  US11/165,366
• Publication Number:
  US 20070031188A1
• Time in Patent Office: 978 Days
• Field of Search: 403/348, 403/349, 403/350, 403/351, 403/352, 403/335, 403/336, 403/337, 607/96, 607/98, 285/376, 285/401
• US Class Current: 403/348
• CPC Class Codes: F16B 2200/503 the flange being separate from the elements to be connected
• CPC Class Codes: F16B 2200/506 bolted or riveted
• CPC Class Codes: F16B 5/10 by means of bayonet connections F16B5/0092 takes precedence; fastening devices locking by rotation F16B21/02
• CPC Class Codes: F23R 3/60 Support structures; Attaching or mounting means
• CPC Class Codes: Y10T 403/7005 Lugged member, rotary engagement
• CPC Class Codes: Y10T 403/7009 Rotary binding cam or wedge

Abstract

An attachment device for coupling one or more removable turbine components to a carrier of a turbine engine. The attachment device may include a securement structure rotatable about an axis of rotation and including one or more arms for grasping an arm extending from a support structure. A fastener may extend from the support structure and be inserted into a fastener receiving recess in the securement structure for preventing the securement structure from rotating and becoming disengaged from the support structure. The attachment device may also include a fastener retaining device for preventing the fastener, which may be a threaded bolt, from becoming disengaged from the attachment device, traveling downstream in a turbine, and damaging a turbine assembly.

Claims

1. An attachment device for attaching turbine components to form a hot gas path within the components, comprising:

a support structure comprising an annular flange having inner and outer surfaces with at least one axially extending fastener receiving recess for containing a fastener and at least one retention arm extending from the support structure, wherein the at least one retention arm defines at least one recess;

a securement structure concentrically aligned with the support structure about an axis of rotation, comprising an annular flange having inner and outer surfaces with at least one axially extending fastener receiving recess and at least one retention arm extending from the body of the securement structure and configured to be inserted into the at least one recess formed from the retention arm of the support structure to grasp the at least one retention arm of the support structure after the securement structure has been rotated about an axis the rotation, wherein the outer surface of the securement structure forms a hot gas path outer surface; and

at least one fastener movably coupled to the support structure, a head of the fastener disposed between the outer surface of the support structure and the inner surface of the securement structure, such that the fastener is moveable between a position in which the fastener extends into the at least one fastener receiving recess of the securement structure thereby preventing rotation of the securement structure relative to the support structure and a position in which the fastener is contained within the at least one fastener receiving recess in the support structure enabling the securement structure to be rotated about the axis of rotation;

an orifice in the flange of the securement structure that extends through the hot gas path outer surface and enables a tool to be inserted through the hot gas path outer surface from within the hot gas path to engage and move the at least one fastener between positions, and enable the securement structure to be removed in the hot gas path;

wherein the orifice in the flange of the securement structure is sized to prevent the head of the at least one fastener from passing through the orifice and releasing the fastener into the hot gas path.

2. The attachment device of claim 1, further comprising a fastener retaining device for preventing the fastener from being removed from the attachment device.

3. The attachment device of claim 2, wherein the fastener retaining device comprises a wall in the securement structure that prevents the fastener from being removed from the attachment device.

4. The attachment device of claim 1, wherein the support structure includes a central aperture enabling combustor gases to pass through the support structure and wherein the at least one retention arm extending from the support structure comprises a plurality of retention arms positioned around a perimeter of the central aperture.

5. The attachment device of claim 4, wherein the securement structure includes a central aperture enabling combustor gases to pass through the securement structure and wherein the at least one retention arm extending from the securement structure comprises a plurality of retention arms positioned around a perimeter of the central aperture.

6. The attachment device of claim 5, wherein at least one arm of the plurality of retention arms of the securement structure is attached to the securement structure in close proximity to the central aperture and extends radially outward.

7. The attachment device of claim 6, wherein the at least one arm of the plurality of retention arms of the securement structure includes a stop extending between the at least one arm and the securement structure to facilitate insertion of the at least one retention arm of the support structure by rotating the securement structure in only a first direction.

8. The attachment device of claim 5, wherein at least one arm of the plurality of retention arms of the securement structure is attached to the securement structure and extends radially inward.

9. The attachment device of claim 4, wherein at least one retention arm of the plurality of retention arms of the support structure is attached to the support structure in close proximity to the central aperture and extends radially outward.

10. The attachment device of claim 9, wherein the at least one retention arm of the plurality of retention arms of the support structure includes a stop extending between the at least one retention arm and the support structure to facilitate insertion of the at least one retention arm of the securement structure by rotating the support structure in only a first direction.

11. The attachment device of claim 4, wherein at least one retention arm of the plurality of retention arms of the support structure is attached to the support structure and extends radially inward.

12. The attachment device of claim 1, wherein the at least one fastener comprises a plurality of fasteners positioned in the support structure.

13. The attachment device of claim 1, wherein the securement structure further comprises an outer surface that is generally opposite to the at least one retention arm of the securement structure and is configured to be substantially flush with adjacent turbine components.

14. An attachment device for attaching turbine components to form a hot gas path within the components, comprising:

a support structure comprising an annular flange having inner and outer surfaces with a central aperture, at least one axially extending fastner receiving recess for containing a fastener, and at least one retention arm positioned round a perimeter of the central aperture and extending from the support structure, wherein the at least one retention arm defines at least one recess that is generally orthogonal to an axis of rotation of the support structure;

a securement structure concentrically aligned with the support structure about the axis of rotation, comprising an annular flange having inner and outer surfaces with a central aperture, at least one axially extending fastener receiving recess, and at least one retention arm positioned around a perimeter of the central aperture, extending from the body of the securement structure, and configured to be inserted into the at least one recess formed from the retention arm of the support structure to grasp the at least one retention arm of the support structure after the securement structure has been rotated about the axis of rotation, and an outer surface that is generally opposite to the at least one retention arm of the securement structure that forms a hot gas path outer surface and configured to be substantially flush with adjacent turbine components;

at least one fastener movably coupled to the support structure , a head of the fastener disposed between the outer surface of the support structure and the inner surface of the securement structure, such that the fastener is moveable between a position in which the fastener extends into the at least one fastener receiving recess of the securement structure thereby preventing rotation of the securement structure relative to the support structure and a position in which the fastener is contained within the at least one fastener receiving recess in the support structure enabling the securement structure to be rotated;

a fastener retaining device for preventing the fastener from being removed from the attachment device and into the hot gas path once fully assembled; and

wherein the securement structure includes an orifice providing access to the at least one fastener through the hot gas so that a tool may extend through the orifice from within the hot gas path and engage and move the at least one fastener in the securement structure between positions, and wherein the orifice is sized to prevent the head of the at least one fastener from passing through the orifice and releasing the fastener into the hot gas path.

15. The attachment device of claim 14, wherein the fastener retaining device comprises a wall in the securement structure that prevents the fastener from being removed from the attachment device.

16. The attachment device of claim 14, wherein the fastener retaining device comprises a protrusion extending from the fastener for preventing the fastener from being removed from the attachment device.

17. The attachment device of claim 14, wherein the at least one arm extending from the securement structure is in close proximity to the central aperture of the securement structure and extends radially outward and the at least one arm extending from the support structure and extends radially inward.

18. The attachment device of claim 17, wherein the at least one arm extending from the securement structure includes a stop extending between the at least one arm and the securement structure to facilitate insertion of the at least one arm of the support structure by rotating the securement structure in only a first direction.

19. The attachment device of claim 14, wherein at least one arm extending from the securement structure extends radially inward and the at least one arm extending from the support structure in close proximity to the central aperture of the securement structure extends radially outward.