Patent US4350473A successfully refreshed from Google Patents.
US4350473A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Liquid cooled counter flow turbine bucket
Assignee: United States Department of Energy
•
Filing: 1980-02-22
•
Granted: 1982-09-21
•
Expires: 2000-02-22
Abstract
Abstract Means and a method are provided whereby liquid coolant flows radially outward through coolant passages in a liquid cooled turbine bucket under the influence of centrifugal force while in contact with countercurrently flowing coolant vapor such that liquid is entrained in the flow of vapor resulting in an increase in the wetted cooling area of the individual passages.
Inventors
- 👤 James T. Dakin
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 08:44
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/14; F01D5/18; F01D5/185; F05; F05B; F05B2240/00; F05B2240/80; F05B2240/801; F05D; F05D2240/00; F05D2240/80; F05D2240/81
Claims Analysis
Total Claims: 16
Claim 1
Independent Claim
129 words
In a liquid cooled turbine bucket adapted for mounting on a rotatable turbine wheel and having a tip region at a radially outward end and an airfoil-shaped portion located radially inward to said tip region, the improvement comprising: a plurality of radially extending coolant passages disposed in said airfoil-shaped portion; means for admitting liquid into said passages at radially inwardly disposed sections of said passages; means for discharging liquid from said bucket disposed in flow communication with radially outwardly disposed sections of said passages, said liquid discharging means including a means for restricting the flow of vapor from said passages into said liquid discharging means; and means for discharging vapor from said bucket disposed in flow communication with said passages at second radially inwardly disposed sections of said passages.
Claim 2
Dependent Claim
129 words
In a liquid cooled turbine bucket adapted for mounting on a rotatable turbine wheel and having a tip region at a radially outward end and an airfoil-shaped portion located radially inward to said tip region, the improvement comprising: a plurality of radially extending coolant passages disposed in said airfoil-shaped portion; means for admitting liquid into said passages at radially inwardly disposed sections of said passages; means for discharging liquid from said bucket disposed in flow communication with radially outwardly disposed sections of said passages, said liquid discharging means including a means for restricting the flow of vapor from said passages into said liquid discharging means; and means for discharging vapor from said bucket disposed in flow communication with said passages at second radially inwardly disposed sections of said passages.
Claim 3
Dependent Claim
45 words
An improved liquid cooled turbine bucket as in claim 1 wherein said second radially inwardly disposed sections of said passages in flow communication with said vapor discharging means ae disposed radially inward of said passage sections disposed in flow communication with said liquid admitting means.
Claim 4
Dependent Claim
53 words
An improved liquid cooled turbine bucket as in claim 1 wherein said vapor discharging means includes a nozzle in vapor communication with at least a portion of said second passage sections and disposed to exhaust vapor from said bucket in a rearward direction relative to the direction of rotation of said turbine wheel.
Claim 5
Dependent Claim
38 words
An improved liquid cooled turbine bucket as in claim 3 wherein said vapor discharging means includes at least one vapor manifold in flow communication with at least a portion of said second passage sections and with said nozzle.
Claim 6
Dependent Claim
51 words
An improved liquid cooled turbine bucket as in claim 1 wherein said liquid discharging means includes a liquid manifold located in the bucket tip region in flow communication with radially outwardly disposed ends of said coolant passages and with an orifice for the discharge of liquid coolant from the turbine bucket.
Claim 7
Dependent Claim
44 words
An improved liquid cooled turbine bucket as in claim 5 wherein said liquid discharging means includes a liquid trap disposed in said tip region radially outward from and in communication with said liquid manifold intermediate said liquid manifold and said liquid coolant discharge orifice.
Claim 8
Dependent Claim
19 words
An improved liquid cooled turbine bucket as in claim 1 wherein said liquid passages are substantially circular in cross-section.
Claim 9
Dependent Claim
25 words
An improved liquid cooled turbine bucket as in claim 1 further comprising means disposed in said coolant passages for dispersing liquid flowing through said passages.
Claim 10
Dependent Claim
175 words
In a liquid cooled turbine bucket adapted for mounting on a rotatable turbine wheel and having a tip region at a radially outward end and an airfoil-shaped portion located radially inward of said tip region, the improvement comprising: a plurality of radially extending coolant passages disposed in said airfoil-shaped portion; means for admitting liquid into radially inwardly disposed sections of said passages; means for discharging liquid from said bucket including a liquid manifold located in the bucket tip region in flow communication with radially outward ends of said coolant passages, and an orifice in communication with said liquid manifold for restricting the flow of vapor into said liquid discharging means and adapted for the discharging the liquid coolant from said bucket; and means for discharging vapor from said bucket including at least one vapor manifold in flow communication with radially inward ends of said coolant passages, and a nozzle in vapor communication with said vapor manifold and disposed to exhaust vapor in a rearward direction relative to the direction of rotation of said turbine wheel.
Claim 11
Dependent Claim
175 words
In a liquid cooled turbine bucket adapted for mounting on a rotatable turbine wheel and having a tip region at a radially outward end and an airfoil-shaped portion located radially inward of said tip region, the improvement comprising: a plurality of radially extending coolant passages disposed in said airfoil-shaped portion; means for admitting liquid into radially inwardly disposed sections of said passages; means for discharging liquid from said bucket including a liquid manifold located in the bucket tip region in flow communication with radially outward ends of said coolant passages, and an orifice in communication with said liquid manifold for restricting the flow of vapor into said liquid discharging means and adapted for the discharging the liquid coolant from said bucket; and means for discharging vapor from said bucket including at least one vapor manifold in flow communication with radially inward ends of said coolant passages, and a nozzle in vapor communication with said vapor manifold and disposed to exhaust vapor in a rearward direction relative to the direction of rotation of said turbine wheel.
Claim 12
Independent Claim
171 words
A method for cooling turbine buckets mounted on a turbine wheel and rotated about a turbine shaft, said buckets having a plurality of radially disposed coolant passages and a bucket airfoil-shaped portion, said passages terminating at their radially outward end adjacent a bucket tip region, said method comprising the steps of: providing liquid coolant to radially inwardly disposed sections of said passages; conveying liquid coolant radially upward through said passages by centrifugal force; cooling a first arcuate portion of said coolant passage walls by contact with said conveyed liquid coolant and heating said liquid coolant by said contact whereby at least a portion of said liquid coolant transitions to a vapor phase; restricting the flow of vaporized coolant into said bucket tip region; discharging liquid coolant from said tip region; conducting vaporized coolant radially inwardly through said coolant passages in contact with said conveyed liquid coolant; providing a vapor discharge means disposed in communication with radially inwardly disposed ends of said passages; and discharging vaporized coolant from said vapor discharge means.
Claim 13
Independent Claim
171 words
A method for cooling turbine buckets mounted on a turbine wheel and rotated about a turbine shaft, said buckets having a plurality of radially disposed coolant passages and a bucket airfoil-shaped portion, said passages terminating at their radially outward end adjacent a bucket tip region, said method comprising the steps of: providing liquid coolant to radially inwardly disposed sections of said passages; conveying liquid coolant radially upward through said passages by centrifugal force; cooling a first arcuate portion of said coolant passage walls by contact with said conveyed liquid coolant and heating said liquid coolant by said contact whereby at least a portion of said liquid coolant transitions to a vapor phase; restricting the flow of vaporized coolant into said bucket tip region; discharging liquid coolant from said tip region; conducting vaporized coolant radially inwardly through said coolant passages in contact with said conveyed liquid coolant; providing a vapor discharge means disposed in communication with radially inwardly disposed ends of said passages; and discharging vaporized coolant from said vapor discharge means.
Claim 14
Dependent Claim
45 words
A method for cooling turbine buckets as in claim 10 wherein a portion of the liquid coolant is entrained in the conducted flow of vaporized coolant whereby a second accurate portion of said coolant passage walls is cooled by contact with said entrained liquid coolant.
Claim 15
Dependent Claim
49 words
A method as in claim 10 wherein further comprising the steps of: dispersing the liquid coolant conveyed radially upward through said passages so as to generate liquid droplets; entraining at least a portion of said liquid droplets in the flow of vaporized coolant conducted radially inward in said passages.
Claim 16
Dependent Claim
36 words
A method for cooling turbine buckets as in claim 10 in which said vaporized coolant is discharged from said vapor discharge means in a rearward direction relative to the direction of rotation of said turbine wheel.
References Cited (Backward Citations)
US3051438A
Cited
GB979634A
Cited
US3804551A
Cited
US3816022A
Cited
US3902819A
Cited
US3856433A
Cited
US4111604A
Cited
US4134709A
Cited
GB1548154A
Cited
US4142831A
Cited
US4179240A
Cited
US4212587A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-09-20 | 1986-03-22 | 1986-09-21 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-09-20 | 1990-03-22 | 1990-09-21 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-09-20 | 1994-03-22 | 1994-09-21 | $7700.00 | Window Closed / Lapsed |