Vane ring for a turbine engine having retention devices

Patent metadata

Field	Value
Publication number	US-10267168-B2
Application number	US-201414571976-A
Country	US
Kind code	B2
Filing date	Dec 16, 2014
Priority date	Dec 23, 2013
Publication date	Apr 23, 2019
Grant date	Apr 23, 2019

Abstract

An engine including a turbine section with a number of vane assemblies attached to a support housing. The assemblies are secured to the support housing with fasteners and retaining clips for the fasteners.

First claim

What is claimed is:

1. A retaining clip for an engine component, comprising:
an arcuate plate extending less than half annularly between a first end and a second end and defining an outer surface that faces radially outward, the arcuate plate including (i) a first mounting tab positioned adjacent to the first end, (ii) a second mounting tab positioned adjacent to the second end, and (iii) at least two lobes extending radially outward from the outer surface, each lobe including a first curved surface and a second curved surface, the first curved surface and the second curved surface of each lobe being connected to and extending radially outwardly from the outer surface and defining therebetween a mounting slot positioned between the first mounting tab and the second mounting tab,
wherein the arcuate plate is configured to deflect elastically between an unloaded curvature in which the arcuate plate defines a first radius and a loaded curvature in which the arcuate plate defines a second radius that is greater than the first radius.

2. The retaining clip of claim 1 , wherein the arcuate plate is a metallic plate.

3. The retaining clip of claim 1 , wherein:
the arcuate plate further includes an inner surface that faces radially inward,
the first mounting tab includes a first flange extending radially inward from the inner surface, and
the second mounting tab includes a second flange extending radially inward from the inner surface.

4. The retaining clip of claim 3 , wherein the mounting slots are positioned along the outer surface.

5. The retaining clip of claim 1 , wherein the arcuate plate is biased in the unloaded curvature.

6. The retaining clip of claim 1 , wherein the arcuate plate further includes a first slot defined in the first end and a second slot defined in the second end.

7. A turbine, comprising:
a circular housing including a mounting bracket positioned on an outer circumference of the circular housing,
a vane nozzle segment positioned on the outer circumference of the circular housing,
a mounting pin including a head and a body extending from the head, the body extending through a bore defined in the mounting bracket and the vane nozzle segment to secure the vane nozzle segment to the circular housing, and
a retaining clip positioned in a slot defined in the mounting bracket, the retaining clip adapted to exert a radial spring load on the mounting pin relative to the circular housing to retain the mounting pin in the bore defined in the mounting bracket and the vane nozzle segment,
wherein the head of the mounting pin is positioned in a mounting slot defined in the retaining clip, wherein the mounting slot is radially open.

8. The turbine of claim 7 , wherein the retaining clip extends from a first end to a second end and defines an arc length between the first end and the second end that is less than the outer circumference of the circular housing.

9. The turbine of claim 7 , wherein:
the mounting bracket is a first mounting bracket positioned between a second mounting bracket and a third mounting bracket, and
the retaining clip includes a first tab that is engaged with the second mounting bracket and a second tab that is engaged with the third mounting bracket.

10. The turbine of claim 7 , wherein:
the retaining clip includes a radially-outward surface, and
the mounting slot is defined between a first curved surface and a second curved surface, the first curved surface and the second curved surface being connected to, and extending outwardly from, the radially-outward surface.

11. The turbine of claim 7 , wherein the retaining clip is a metallic plate.

12. The turbine of claim 7 , wherein the body of the mounting pin is unthreaded.

13. A turbine, comprising:
a circular housing including a mounting bracket positioned on an outer circumference of the circular housing,
a vane nozzle segment positioned on the outer circumference of the circular housing,
a mounting pin including a head and a body extending from the head, the body extending through a bore defined in the mounting bracket and the vane nozzle segment to secure the vane nozzle segment to the circular housing, and
a retaining clip positioned in a slot defined in the mounting bracket, the retaining clip exerting a radial spring load on the mounting pin to retain the mounting pin in the bore defined in the mounting bracket and the vane nozzle segment,
wherein the head of the mounting pin is positioned in a mounting slot defined in the retaining clip,
wherein the mounting bracket is a first mounting bracket positioned between a second mounting bracket and a third mounting bracket, and the retaining clip includes a first tab that is engaged with the second mounting bracket and a second tab that is engaged with the third mounting bracket,
wherein:
the retaining clip includes a radially-inward side that faces the circular housing and a radially-outward side positioned opposite the radially-inward side,
the mounting slot is defined in the radially-outward side, and
the first tab and the second tab are positioned on the radially-inward side of the retaining clip.

14. The turbine of claim 13 , wherein the retaining clip includes a second mounting slot defined in the radially-outward side.

15. The turbine of claim 14 , further comprising:
a fourth mounting bracket positioned on the outer circumference of the circular housing between the first mounting bracket and the second mounting bracket, and
a second mounting pin including a head and a body extending from the head, the body of the second mounting pin extending through a bore defined in the fourth mounting bracket and the vane nozzle segment to secure the vane nozzle segment to the circular housing,
wherein the head of the second mounting pin is positioned in the second mounting slot of the retaining clip.

16. A method of attaching a vane nozzle segment to a turbine housing, the method comprising:
sliding a mounting pin into the vane nozzle segment and the turbine housing, and then
advancing a retaining clip into a slot defined in the turbine housing such that the retaining clip exerts a radial spring load on the mounting pin relative to the turbine housing to retain the mounting pin in the vane nozzle segment and the turbine housing, the retaining clip extending from a first end to a second end and defining an arc length between the first end and the second end that is less than an outer circumference of the turbine housing.

17. The method of claim 16 , further comprising:
sliding a second mounting pin into the vane nozzle segment and the turbine housing, and
advancing the retaining clip into a second slot defined in the turbine housing to position a head of the second mounting pin in a mounting slot defined in the retaining clip.

18. The method of claim 17 , further comprising engaging a first mounting bracket of the turbine housing with a first tab of the retaining clip and engaging a second mounting bracket of the turbine housing with a second tab of the retaining clip to prevent further circumferential movement of the retaining clip.

Assignees

• Rolls Royce Corp

Inventors

• Bulgrin Charles A
• Westphal William
• Tamaddoni Michael

Classifications

• Y10T29/49321

  Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member · CPC title

• F01D25/28

  Supporting or mounting arrangements, e.g. for turbine casing · CPC title

• F01D25/246

  Fastening of diaphragms or stator-rings · CPC title

• F01D9/04

  forming ring or sector · CPC title

• Y02T50/672

  Cross-Sectional Technologies · mapped topic