US4472108A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Shroud structure for a gas turbine engine
Assignee: Rolls Royce PLC
•
Filing: 1982-07-07
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Granted: 1984-09-18
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Expires: 2002-07-07
Abstract
Abstract A shroud assembly is pneumatically operated to adjust the clearance between the shroud segments and the tips of the rotor blades of an associated rotor. The assembly comprises a casing to which is secured a wall member which defines a chamber whose pressure may be varied by a valve. The wall member carries shroud segments some of which define the static wall with which the rotor blades co-operate. In order to allow proper movement of the shroud segments the support means which carry the segments from the wall are arranged to be small in axial extent compared with that of the wall.
Inventors
- 👤 George Pask
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 00:39
CPC Classifications
F; F01; F01D; F01D11/00; F01D11/08; F01D11/14; F01D11/20; F01D11/22
Claims Analysis
Total Claims: 13
Claim 1
Independent Claim
254 words
A shroud assembly for a gas turbine engine comprising: an annular casing having an inner surface; a deformable annular wall member coaxial of said casing and having an inner surface and an outer surface, said outer surface of said annular wall being spaced radially inwardly from said inner surface of said annular casing, said annular wall member having axial extremities sealed to said casing to define a chamber between said inner surface of said casing and said outer surface of said annular wall, said annular wall being deformable towards and away from said casing in response to a pressure differential between said chamber and said inner surface of said annular wall member; means for varying fluid pressure within said chamber; a ring of circumferentially arranged shroud segments coaxially of and radially spaced from said inner surface of said annular wall member, said ring of circumferentially arranged shroud segments defining a boundary flow path of the engine; support means on said annular wall member for supporting said ring of circumferentially arranged shroud segments, said support means having upstream and downstream ends and further having a small axial extent therebetween when compared with an axial extent of said annular wall member, said support means extending from a section axially in the middle of said annular wall member, and said support means being arranged to allow axial movement of said ring of circumferentially arranged segments relative to said annular wall; and sealing means between said fixed casing and said upstream and downstream ends of said support means.
Claim 2
Dependent Claim
254 words
A shroud assembly for a gas turbine engine comprising: an annular casing having an inner surface; a deformable annular wall member coaxial of said casing and having an inner surface and an outer surface, said outer surface of said annular wall being spaced radially inwardly from said inner surface of said annular casing, said annular wall member having axial extremities sealed to said casing to define a chamber between said inner surface of said casing and said outer surface of said annular wall, said annular wall being deformable towards and away from said casing in response to a pressure differential between said chamber and said inner surface of said annular wall member; means for varying fluid pressure within said chamber; a ring of circumferentially arranged shroud segments coaxially of and radially spaced from said inner surface of said annular wall member, said ring of circumferentially arranged shroud segments defining a boundary flow path of the engine; support means on said annular wall member for supporting said ring of circumferentially arranged shroud segments, said support means having upstream and downstream ends and further having a small axial extent therebetween when compared with an axial extent of said annular wall member, said support means extending from a section axially in the middle of said annular wall member, and said support means being arranged to allow axial movement of said ring of circumferentially arranged segments relative to said annular wall; and sealing means between said fixed casing and said upstream and downstream ends of said support means.
Claim 3
Dependent Claim
32 words
A shroud assembly as claimed in claim 1 and in which said wall member conforms in shape to said inner surface of said casing so that said chamber is small in volume.
Claim 4
Dependent Claim
65 words
A shroud assemby as claimed in claim 1 or claim 2 in which said means for varying fluid pressure within said chamber includes valve means adapted to allow the pressure within said chamber either to approximate to that on the radially inner surface of the wall or to be at a different pressure, where the wall will be deformed towards or away from the casing.
Claim 5
Dependent Claim
34 words
A shroud assembly as claimed in claim 1 and in which said support means comprises at least one flange providing an axially facing groove in which an axially extending projection from the segments extends.
Claim 6
Dependent Claim
38 words
A shroud assembly as claimed in claim 4 in which said support means comprises two flanges axially spaced apart and which provide upstream and downstream axially facing grooves in which axially extending projections from said shroud segments extend.
Claim 7
Dependent Claim
38 words
A shroud assembly as claimed in claim 1 and in which said support means includes an auxiliary deformable wall member sealed to adjacent static structure and adapted to prevent hot engine gases escaping into the engine casing area.
Claim 8
Dependent Claim
33 words
A shroud assembly as claimed in claim 6 and comprising apertures in said auxiliary deformable wall member adapted to allow cooling air to flow to said segments from outside said auxiliary wall member.
Claim 9
Dependent Claim
17 words
A shroud assembly as claimed in claim 7 and including means for impingement cooling of said segments.
Claim 10
Dependent Claim
47 words
A shroud assembly as claimed in claim 1 in which said sealing means includes a rigidly located sealing ring between said fixed structure and one of said upstream and downstream ends of said support means, said rigidly located sealing ring supporting said support means against axial movement.
Claim 11
Dependent Claim
37 words
A shroud assembly as claimed in claim 9 in which said sealing means includes a second sealing ring which resiliently seals the other of said upstream and downstream ends of said support means against said fixed casing.
Claim 12
Dependent Claim
20 words
A shroud assembly as claimed in claim 1 including further sealing means between each pair of circumferentially arranged shroud segments.
Claim 13
Dependent Claim
21 words
A shroud assembly as claimed in claim 11 and in which there are a plurality of nested rings of said segments.
References Cited (Backward Citations)
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-09-18 | 1988-03-19 | 1988-09-18 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-09-18 | 1992-03-19 | 1992-09-18 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-09-18 | 1996-03-19 | 1996-09-18 | $7700.00 | Window Closed / Lapsed |