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US3841787A Expired / Lapsed US ⏱️ 0.0 years remaining

Axial flow turbine structure

Assignee: Westinghouse Electric Corp
•
Filing: 1973-09-05
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Granted: 1974-10-15
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Expires: 1993-09-05
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Abstract

Abstract An axial flow gas turbine having inner and outer casings, the inner casing being supported within the outer casing by horizontal keying members therebetween. Arrays of stationary integral vane segments and adjacent arcuate blade ring segments are supported inwardly from and interlocked with the inner casing by arcuate segmented support members. The arcuate segmented support members are each fixedly attached at their centermost point to the inner casing. This arrangement permits thermal expansion between mating members with respect to each other. The employment of individually locked stationary integral vane segments and arcuate blade ring segments provide an arrangement where blade path leakage harmonics are limited to the number of such segments in each of their respective planes across the turbine, thus eliminating the deleterious effects created by even harmonics of two stationary half blade segment structures.

Inventors

  • 👤 A Scalzo

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 23:22
CPC Classifications
F; F01; F01D; F01D25/00; F01D25/24; F01D25/246; F01D9/00; F01D9/02; F01D9/04; F01D9/042; F05; F05D; F05D2240/00; F05D2240/10; F05D2240/11

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 281 words
An axial flow turbine comprising: an outer generally cylindrical casing, a generally coaxial inner casing, said outer and said inner casings generally defining a plenum chamber therebetween, an annular array of stationary blades disposed within said inner casing having an outer shroud portion, a rotor having an array of rotatable blades on its periphery, said rotatable blades being coaxial and adjacent said stationary blades, an array of arcuate blade ring segments disposed radially outwardly of said rotatable blades, said array of stationary blades comprising arcuate integral vane segments thereof, said stationary blades being supported from said inner casing by arcuate support segments, said arcuate support segments and said inner casing having a track and channel interlock arrangement therebetween, said arcuate support segments and said outer shroud portion of said stationary integral vane segments having a track and channel interlock arrangement therebetween, each arcuate support segment being fixedly attached at one point on its periphery to the inner casing to permit circumferential thermal expansion of said segments, said array of arcuate blade ring segments being supported radially outwardly of said rotatable blades by arcuate support segments having track and channel interlock arrangements with the inner casing and also having a track and channel interlocking support arrangement between an edge of each of said ring segments and the downstream edge of adjacent upstream stationary integral vane segments, said inner casing being supported within said outer casing by generally horizontal keying members, said keying members being received in keyways within said outer casing, and at least two generally vertically disposed pins disposed between each inner casing member and said outer casing providing vertical alignment of said inner casing member with respect to said turbine.
Claim 2
Dependent Claim 281 words
An axial flow turbine comprising: an outer generally cylindrical casing, a generally coaxial inner casing, said outer and said inner casings generally defining a plenum chamber therebetween, an annular array of stationary blades disposed within said inner casing having an outer shroud portion, a rotor having an array of rotatable blades on its periphery, said rotatable blades being coaxial and adjacent said stationary blades, an array of arcuate blade ring segments disposed radially outwardly of said rotatable blades, said array of stationary blades comprising arcuate integral vane segments thereof, said stationary blades being supported from said inner casing by arcuate support segments, said arcuate support segments and said inner casing having a track and channel interlock arrangement therebetween, said arcuate support segments and said outer shroud portion of said stationary integral vane segments having a track and channel interlock arrangement therebetween, each arcuate support segment being fixedly attached at one point on its periphery to the inner casing to permit circumferential thermal expansion of said segments, said array of arcuate blade ring segments being supported radially outwardly of said rotatable blades by arcuate support segments having track and channel interlock arrangements with the inner casing and also having a track and channel interlocking support arrangement between an edge of each of said ring segments and the downstream edge of adjacent upstream stationary integral vane segments, said inner casing being supported within said outer casing by generally horizontal keying members, said keying members being received in keyways within said outer casing, and at least two generally vertically disposed pins disposed between each inner casing member and said outer casing providing vertical alignment of said inner casing member with respect to said turbine.
Claim 3
Dependent Claim 43 words
An axial flow turbine arrangement as recited in claim 1 wherein said support segments for said ring segments are fixedly attached at one point to said casing to permit circumferentially directed thermal expansion of said support segments with respect to its adjacent components.
Claim 4
Dependent Claim 29 words
An axial flow turbine arrangement as recited in claim 1, wherein a biased arcuate member provides sealing means between the plenum chamber and the axial hot fluid flow path.
Claim 5
Dependent Claim 41 words
An axial flow turbine arrangement as recited in claim 1, wherein said turbine comprises a plurality of annular arrays of stationary blades and a plurality of rotatable blades, each annular array of stationary blades being supported by said arcuate support arrangement.

References Cited (Backward Citations)

US2919891A Cited
US3427000A Cited
US3519366A Cited
US3542483A Cited
US3529904A Cited
US3529903A Cited
US3689174A Cited
US3781125A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1977-10-14 1978-04-15 1978-10-15 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1981-10-14 1982-04-15 1982-10-15 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1985-10-14 1986-04-15 1986-10-15 $7700.00 Window Closed / Lapsed

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