Shroud assembly having C-clip retainer

Information

  • Patent Grant
  • 6435820
  • Patent Number
    6,435,820
  • Date Filed
    Wednesday, August 25, 1999
    25 years ago
  • Date Issued
    Tuesday, August 20, 2002
    22 years ago
Abstract
Disengagement of the C-clip in turbine shroud assemblies is prevented by providing a C-clip retainer. The shroud assembly includes a shroud support having a hook and at least one shroud having a mounting flange. A C-clip overlaps the hook and the mounting flange to clamp the shroud to the shroud support, and the retainer is secured to the shroud support and located so as to engage the C-clip. The retainer engages the C-clip in such a manner so as to limit aft axial movement of the C-clip, thereby eliminating C-clip back-off.
Description




BACKGROUND OF THE INVENTION




This invention relates generally to gas turbine engines and more particularly to shroud assemblies utilized in the high pressure turbine section of such engines.




A gas turbine engine includes a compressor that provides pressurized air to a combustor wherein the air is mixed with fuel and ignited for generating hot combustion gases. These gases flow downstream to one or more turbines that extract energy therefrom to power the compressor and provide useful work such as powering an aircraft in flight. A turbine section commonly includes a stationary turbine nozzle disposed at the outlet of the combustor for channeling combustion gases into a turbine rotor disposed downstream thereof. The turbine rotor includes a plurality of circumferentially spaced apart fan blades extending radially outwardly from a rotor disk that rotates about the centerline axis of the engine.




The turbine section further includes a shroud assembly located immediately downstream of the turbine nozzle. The shroud assembly closely surrounds the turbine rotor and thus defines the outer boundary for the hot combustion gases flowing through the turbine. A typical shroud assembly comprises a shroud support which is fastened to the engine outer case and which in turn supports a plurality of shrouds. The shrouds are held in place, in part, by arcuate retaining members commonly referred to as C-clips. Specifically, the C-lips hold the aft end of the shrouds in place against the shroud hangers via an interference fit.




The interference fit normally provides excellent retention of the shrouds. However, there can be a tendency for the C-clips to back off in some instances because of a thermal ratcheting phenomenon. That is, although the shrouds and C-clips are segmented to accommodate for thermal expansion, there is a possibility that the thermal loads within the shroud assembly can overcome the interference fit clamp loads. In some cases, there may be enough of a gap between the C-clip aft face and the adjacent nozzle outer band to allow for C-clip disengagement. Such disengagement could result in severe hardware damage.




Accordingly, there is a need for a shroud assembly design that eliminates C-clip back-off.




SUMMARY OF THE INVENTION




The above-mentioned needs are met by the present invention which provides a shroud assembly including a shroud support having a hook and at least one shroud having a mounting flange. A C-clip overlaps the hook and the mounting flange to clamp the shroud to the shroud support, and a retainer is secured to the shroud support and located so as to engage the Clip. The retainer engages the C-clip in such a manner so as to limit aft axial movement of the C-clip, thereby eliminating C-clip back-off.




Other objects and advantages of the present invention will become apparent upon reading the following detailed description and the appended claims with reference to the accompanying drawings.











DESCRIPTION OF THE DRAWINGS




The subject matter which is regarded as the invention is particularly pointed out and distinctly claimed in the concluding part of the specification. The invention, however, may be best understood by reference to the following description taken in conjunction with the accompanying drawing figures in which:





FIG. 1

is an axial sectional view of the shroud assembly of the present invention.





FIG. 2

is an isometric view of a retention plate from the shroud assembly of FIG.


1


.





FIG. 3

is a fragmentary sectional view showing a second embodiment of the shroud assembly of the present invention.





FIG. 4

is a fragmentary sectional view showing a third embodiment of the shroud assembly of the present invention.





FIG. 5

is a fragmentary sectional view showing a fourth embodiment of the shroud assembly of the present invention.











DETAILED DESCRIPTION OF THE INVENTION




Referring to the drawings wherein identical reference numerals denote the same elements throughout the various views,

FIG. 1

shows a shroud assembly


110


of the present invention in closely surrounding relation with turbine blades


112


carried by a rotor disk (not shown) in the high pressure turbine section of a gas turbine engine. The shroud assembly


110


includes a plurality of arcuate shrouds


114


(only one shown in

FIG. 1

) arranged in an annular array so as to encircle the turbine blades


112


. The shrouds


114


are held in position by a shroud support


116


which, in turn, is supported by the engine outer case (not shown) in a conventional manner.




The shroud support


116


includes an axially extending forward hook


118


and an axially extending aft hook


120


. The shroud support


116


also includes an axially extending aft flange


122


disposed at a location radially outside of the aft hook


120


. A radially outwardly extending lip


124


is formed on the distal end of the aft flange


122


. Each shroud


114


includes a base


126


having radially outwardly extending forward and aft rails


128


and


130


, respectively. A forward mounting flange


132


extends forwardly from the forward rail


128


of each shroud


114


, and an aft mounting flange


134


extends rearwardly from the aft rail


130


of each shroud


114


. The aft mounting flanges


134


of each shroud


114


are juxtaposed with the aft hook


120


of the shroud support


116


and are held in place by a plurality of retaining members


136


commonly referred to as C-clips.




The C-clips


136


are arcuate members having a C-shaped cross section and snugly overlap the aft mounting flanges


134


and the aft hook


120


so as to clamp the aft ends of the shrouds


114


in place against the shroud support


116


. Although they could be formed as a single continuous ring, the C-clips


136


are preferably segmented to accommodate thermal expansion. Typically, one C-clip


136


clamps an entire shroud plus one-half of each adjacent shroud. In which case, there are twice as many shrouds


114


as there are C-clips


136


.




The forward end of each shroud


114


is supported from the shroud support


116


via conventional shroud hangers


138


. Each shroud hanger


138


includes a first hook


140


that engages the forward hook


118


of the shroud support


116


and a second hook


142


that engages the forward mounting flange


132


of each shroud


114


.




The shroud hangers


138


are also secured to the shroud support


116


by fasteners


144


. A conventional cooling air distributor


146


is disposed between the shroud


114


and the shroud support


116


for distributing cooling air to the shrouds


114


and adjacent structure.




The shroud assembly


110


further includes a plurality of retainer plates


148


(only one shown in

FIG. 1

) arranged in an annular array and which function to limit aft axial movement of the C-clips


136


, thereby eliminating the potential of C-clip disengagement As with other components of the shroud assembly


110


, the retainer plates


148


could be formed as a single continuous ring. However, segmented plates are preferred to accommodate thermal expansion.




As best seen in

FIG. 2

, the retainer plate


148


comprises an arcuate body


150


having an interlock lip


152


extending radially inwardly from the forward inner corner thereof and a retaining flange


154


extending radially inwardly from the aft inner corner thereof. A pair of bolt holes


156


, with surrounding recesses


158


, is formed in the aft face of the arcuate body


150


. The retaining flange


154


is provided with an aft lip wear surface


160


on its aft face and one or more clearance slots


162


in its distal edge, both of which are described in more detail below.




Referring again to

FIG. 1

, the retainer plate


148


is secured to the aft end of the shroud support


116


so that the retaining flange


154


overhangs the back of the C-clip


136


and the interlock lip


152


engages the radial lip


124


formed on the aft flange


122


of the shroud support


116


. The retainer plate


148


is positioned such that the retaining flange


154


engages the aft side of the C-clip


136


. Preferably, the retainer plate


148


is secured to the shroud support


116


with bolts


164


that extend through bushings


166


disposed in the recesses


158


and the bolt holes


156


. The bolts


164


also attach a conventional flow divider


168


to the shroud support


116


.




By abutting the back of the C-clip


136


, the retaining flange


154


prevents aft axial movement of the C-clip


136


. The interlock lip


152


functions to react axial C-clip back-off load, thereby minimizing retainer plate bolt bending stress. The use of the interlock lip


152


also allows a smaller number of bolts


164


to be used. The retainer plates


148


can be sized such that each one engages multiple C-clips. Thus, the total number of retainer plates


148


will be less than the total number of C-clips


136


.




The aft lip wear surface


160


provides a contact surface for a leaf seal


170


which is disposed between the shroud assembly


110


and the nozzle outer band


172


of the adjacent stator assembly. The leaf seal


170


is attached to the nozzle outer band


172


by a plurality of circumferentially spaced pins


174


and prevents cooling air from passing between the shroud assembly


110


and the nozzle outer band


172


. The clearance slots


162


are circumferentially aligned with the leaf seal pins


174


. Thus, in the event the pins


174


travel radially outwardly because of thermal expansion of the nozzle outer band


172


, they will be received within the slots


162


, thereby avoiding any undesired interference between the pins


174


and the retaining flange


154


. The shroud assembly further includes a discourager seal


176


disposed between the radially inner surface of the C-clip


136


and the shrouds


114


for preventing the ingestion of hot gases into the cavity between the C-clip


136


and the nozzle outer band


172


.




In addition to eliminating the potential of C-clip disengagement, the shroud assembly


110


of the present invention provides further advantages in that it requires no modification to the shrouds


114


, C-clips


136


or shroud hangers


138


, and only limited modification of the shroud support


116


. Furthermore, the present invention permits simplified lip weld repair because just the retainer plate


148


, and not the entire shroud assembly


110


, needs to be removed for repair.




Turning to

FIG. 3

, a shroud assembly


210


in accordance with a second embodiment of the present invention is shown. The shroud assembly


210


is similar to the first embodiment in that it includes a plurality of arcuate shrouds


214


(only one shown in

FIG. 3

) supported by a shroud support


216


. The shroud support


216


has an axially extending aft hook


220


formed on its aft end, and each shroud


214


includes an aft rail


230


from which an aft mounting flange


234


extends rearwardly. The aft mounting flanges


234


of each shroud


214


are juxtaposed with the aft hook


220


and are held in place by a plurality of C-clips


236


which overlap the aft mounting flanges


234


and the aft hook


220


so as to clamp them together.




The shroud assembly


210


further includes a plurality of retainer plates


248


(only one shown in

FIG. 3

) attached to the aft end of the shroud support


216


by bolts


264


. Like the retainer plate


148


of the first embodiment, the retainer plate


248


of the second embodiment comprises an arcuate body


250


having an interlock lip


252


extending radially inwardly from the forward inner corner thereof and a retaining flange


254


extending radially inwardly from the aft inner corner thereof. As before, the interlock lip


252


engages a radial lip


224


formed on the distal end of an aft flange


222


extending from the shroud support


216


.




The retainer plate


248


differs from that of the first embodiment in that the retaining flange


254


is configured differently. Instead of overhanging the back of the C-clip


236


, the retaining flange


254


terminates at a point radially outside of the C-clip


236


. An aft lip wear surface


260


is formed on the aft face of the retaining flange


254


to present a contact surface for a leaf seal


270


. A retaining lip


237


is formed on the radially outer surface of the C-clip


236


, near its aft side. The retainer plate


248


is positioned on the shroud support


216


so that the retaining flange


254


engages the retaining lip


237


. By abutting the back of the retaining lip


237


, the retaining flange


254


prevents aft axial movement of the C-clip


236


.




By locating the contact point closer to the center of gravity of the retainer plate


248


, this embodiment provides for lower retainer plate bending moment, which can be a factor when high axial C-clip back-off loads are involved. Furthermore, because the retaining flange


254


is considerably shorter than that of the first embodiment, clearance between the retainer plate


248


and the leaf spring pins


274


is not an issue. Thus, the retaining flange


254


does not need clearance slots formed therein.




Referring to

FIG. 4

, a shroud assembly


310


in accordance with a third embodiment of the present invention is shown. The shroud assembly


310


is quite similar to that of the second embodiment It includes a plurality of arcuate shrouds


314


(only one shown in

FIG. 4

) supported by a shroud support


316


. The shroud support


316


has an axially extending aft hook


320


formed on its aft end, and each shroud


314


includes an aft rail


330


from which an aft mounting flange


334


extends rearwardly. The aft mounting flanges


334


of each shroud


314


are juxtaposed with the aft hook


320


and are held in place by a plurality of C-clips


336


which overlap the aft mounting flanges


334


and the aft hook


320


so as to clamp them together.




The shroud assembly


310


further includes a plurality of retainer plates


348


(only one shown in

FIG. 4

) attached to the aft end of the shroud support


316


by bolts


364


. Each retainer plate


348


comprises an arcuate body


350


having an interlock lip


352


extending radially inwardly from the forward inner corner thereof and a retaining flange


354


extending radially inwardly from the aft inner corner thereof. As before, the interlock lip


352


engages a radial lip


324


formed on the distal end of an aft flange


322


extending from the shroud support


316


.




The retainer plates


348


and C-clips


336


of the third embodiment are slightly different from that of the second embodiment. The retaining flange


354


terminates at a point radially outside of the C-clip


336


and has a forwardly extending abutment lip


355


formed on its distal end. An aft lip wear surface


360


is formed on the aft face of the retaining flange


354


to present a contact surface for a leaf seal


370


. A retaining lip


337


is formed on the radially outer surface of the C-clip


336


, but unlike the retaining lip


237


of the second embodiment, the retaining lip


337


is located near the forward side of the C-clip


336


. The retainer plate


348


is positioned on the shroud support


316


so that the abutment lip


355


engages the retaining lip


337


. By abutting the back of the retaining lip


337


, the retaining flange


354


prevents aft axial movement of the C-clip


336


.




Like the second embodiment, this configuration provides for lower retainer plate bending moment Furthermore, the forward location of the retaining lip


337


greatly reduces the stress impact on the C-clip with respect to the second embodiment.




Turning to

FIG. 5

, a shroud assembly


410


in accordance with a fourth embodiment of the present invention is shown. As in the previous embodiments, the shroud assembly


410


includes a plurality of arcuate shrouds


414


(only one shown in

FIG. 5

) supported by a shroud support


416


. The shroud support


416


has an axially extending aft hook


420


formed on its aft end, and each shroud


414


includes an aft rail


430


from which an aft mounting flange


434


extends rearwardly. The shroud support


416


also includes an axially extending aft flange


422


disposed at a location radially outside of the aft hook


420


. The aft mounting flanges


434


of each shroud


414


are juxtaposed with the aft hook


420


and are held in place by a plurality of C-clips


436


which overlap the aft mounting flanges


434


and the aft hook


420


so as to clamp them together.




An aft lip wear surface


460


is formed on the back side of the aft flange


422


to present a contact surface for a leaf seal


470


. A retaining lip


437


is formed on the radially outer surface of the C-clip


436


and is preferably located near the forward side of the C-clip


436


. The shroud assembly


410


differs from the previously described embodiments in the type of retainer used. Specifically, the retainer plate is replaced with a split ring


478


disposed within an annular slot


423


formed in the radially inner surface of the aft flange


422


. The slot


423


is axially positioned so that the spilt ring


478


engages the back side of the retaining lip


437


. The split ring


478


is preferably a


720


degree ring that fits into the slot


423


with a tight tolerance. Thus, the spilt ring


478


is axially fixed with respect to the shroud support


416


and accordingly prevents aft axial movement of the C-clip


436


by virtue of its abutting relationship with the retaining lip


437


.




The foregoing has described a shroud assembly having a retainer that eliminates C-clip back-off. While specific embodiments of the present invention have been described, it will be apparent to those skilled in the art that various modifications thereto can be made without departing from the spirit and scope of the invention as defined in the appended claims.



Claims
  • 1. A shroud assembly comprising:a shroud support having a hook; at least one shroud having a mounting flange; a C-clip overlapping said hook and said mounting flange; and a retainer secured to said shroud support and located so as to engage said C-lip, wherein said retainer prevents aft axial movement of said C-clip.
  • 2. The shroud assembly of claim 1 wherein said retainer comprises a retainer plate having a radially inwardly extending retaining flange that engages said C-clip.
  • 3. The shroud assembly of claim 2 wherein said retaining flange has an aft lip wear surface formed thereon.
  • 4. The shroud assembly of claim 2 wherein said retainer plate has a radially inwardly extending interlock lip and said shroud support has a radially outwardly extending lip, said interlock lip engaging said radially outwardly extending lip.
  • 5. The shroud assembly of claim 2 wherein said retaining flange engages an aft side of said C-clip.
  • 6. The shroud assembly of claim 2 wherein said retaining flange has at least one clearance slot formed therein.
  • 7. The shroud assembly of claim 2 wherein said C-clip has a retaining lip formed on a radially outer surface thereof, said retaining lip engaging said retaining flange.
  • 8. The shroud assembly of claim 7 wherein said retaining lip is located near an aft side of said C-clip.
  • 9. The shroud assembly of claim 7 wherein said retaining lip is located near a forward side of said C-clip, said retaining flange having a forwardly extending abutment lip formed thereon.
  • 10. The shroud assembly of claim 1 wherein said shroud support has an annular slot formed therein and said retainer comprises a split ring disposed in said slot, said split ring engaging said C-clip.
  • 11. The shroud assembly of claim 10 wherein said split ring is a 720 degree ring.
  • 12. The shroud assembly of claim 10 wherein said C-clip has a retaining lip formed on a radially outer surface thereof, said retaining lip engaging said split ring.
  • 13. The shroud assembly of claim 12 wherein said retaining lip is located near a forward side of said C-clip.
  • 14. A shroud assembly comprising:a shroud support having a hook; at least one shroud having a mounting flange; a C-clip overlapping said hook and said mounting flange; and means for preventing aft axial movement of said C-clip.
  • 15. The shroud assembly of claim 14 wherein said means for preventing aft axial movement of said C-clip comprises a retainer plate having a radially inwardly extending retaining flange that engages said C-clip.
  • 16. The shroud assembly of claim 15 wherein said retaining flange has an aft lip wear surface formed thereon.
  • 17. The shroud assembly of claim 15 wherein said retainer plate has a radially inwardly extending interlock lip and said shroud support has a radially outwardly extending lip, said interlock lip engaging said radially outwardly extending lip.
  • 18. The shroud assembly of claim 15 wherein said retaining flange engages an aft side of said C-clip.
  • 19. The shroud assembly of claim 15 wherein said retaining flange has at least one clearance slot formed therein.
  • 20. The shroud assembly of claim 15 wherein said C-clip has a retaining lip formed on a radially outer surface thereof, said retaining lip engaging said retaining flange.
  • 21. The shroud assembly of claim 20 wherein said retaining lip is located near an aft side of said C-clip.
  • 22. The shroud assembly of claim 20 wherein said retaining lip is located near a forward side of said C-clip, said retaining flange having a forwardly extending abutment lip formed thereon.
  • 23. The shroud assembly of claim 14 wherein said shroud support has an annular slot formed therein and said means for preventing aft axial movement of said C-clip comprises a split ring disposed in said slot, said split ring engaging said C-clip.
  • 24. The shroud assembly of claim 23 wherein said split ring is a 720 degree ring.
  • 25. The shroud assembly of claim 23 wherein said C-clip has a retaining lip formed on a radially outer surface thereof, said retaining lip engaging said split ring.
  • 26. The shroud assembly of claim 25 wherein said retaining lip is located near a forward side of said C-clip.
  • 27. A shroud assembly for a gas turbine engine having a turbine rotor carrying a plurality of turbine blades, said shroud assembly comprising:an annular shroud support, said shroud support having an axially extending aft hook formed thereon; a plurality of shrouds arranged in an annular array to encircle said turbine blades, each one of said shrouds including a base having an aft rail extending outwardly therefrom, said aft rail having a mounting flange formed thereon; a plurality of C-clips overlapping said aft hook and said mounting flanges for clamping said shrouds to said shroud support; and at least one retainer secured to said shroud support and engaging said C-clips so as to prevent aft axial movement of said C-clips.
  • 28. The shroud assembly of claim 27 wherein said at least one retainer comprises a plurality of retainer plates, each retainer plate having a radially inwardly extending retaining flange that engages an aft side of at least one C-clip, and a radially inwardly extending interlock lip that engages a radially outwardly extending lip formed on said shroud support.
  • 29. The shroud assembly of claim 27 wherein each one of said C-clips has a retaining lip formed on a radially outer surface thereof, near an aft side thereof, and wherein said at least one retainer comprises a plurality of retainer plates, each retainer plate having a radially inwardly extending retaining flange that engages at least one of said retaining lips, and a radially inwardly extending interlock lip that engages a radially outwardly extending lip formed on said shroud support.
  • 30. The shroud assembly of claim 27 wherein each one of said C-clips has a retaining lip formed on a radially outer surface thereof, near a forward side thereof, and wherein said at least one retainer comprises a plurality of retainer plates, each retainer plate having a radially inwardly extending retaining flange, a forwardly extending abutment lip that engages at least one of said retaining lips formed on said retaining flange, and a radially inwardly extending interlock lip that engages a radially outwardly extending lip formed on said shroud support.
  • 31. The shroud assembly of claim 27 wherein said shroud support has an annular slot formed therein, wherein each one of said C-clips has a retaining lip formed on a radially outer surface thereof, and wherein said at least one retainer comprises a split ring disposed in said slot, said split ring engaging said retaining lips.
  • 32. In a shroud assembly comprising a shroud support having a hook, at least one shroud having a mounting flange and a C-clip,overlapping said hook and said mounting flange, a method of preventing aft axial movement of said C-clip, said method comprising:placing a retainer in engagement with said C-clip, such that said retainer blocks aft axial movement of said C-clip; and securing said retainer to said shroud support.
  • 33. The method of claim 32 wherein the step of securing said retainer to said shroud support comprises bolting said retainer to said shroud support.
  • 34. The method of claim 32 wherein the step of securing said retainer to said shroud support comprises disposing said retainer in a slot formed in said shroud support.
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH & DEVELOPMENT

The U.S. Government may have certain rights in this invention pursuant to contract numbers F33657-95-C0055 and F33657-97-C-0016 awarded by the Department of the Air Force.

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5562408 Proctor et al. Oct 1996 A
5669757 Brackett Sep 1997 A
5970716 Forrester et al. Oct 1999 A
6200091 Bromann et al. Mar 2001 B1