US4050241A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Stabilizing dimple for combustion liner cooling slot
Assignee: General Electric Co
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Filing: 1975-12-22
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Granted: 1977-09-27
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Expires: 1995-12-22
Abstract
Abstract A combustion liner cooling slot is provided with a plurality of circumferentially spaced stabilizing dimples disposed in an annular lip adapted to facilitate attachment of a cooling fluid to the combustion liner in a protective film barrier. The stabilizing dimples are characterized by a depressed portion having a dimple ceiling of constant radial height and further having a decreasing circumferential width portion.
Inventors
- 👤 Thomas L. DuBell
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 13:11
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/02; F23R3/04; F23R3/06; F23R3/08; F23M; F23M5/00; F23M5/08; F23M5/085; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
157 words
In a combustor liner film cooling slot of the variety including an annular space extending circumferentially of the liner and defined between overlapping portions of telescoping liner segments, a cooling fluid plenum substantially circumscribing the liner, means for transferring cooling fluid from the plenum to the space, means for exhausting fluid from the space onto the liner, and an overhanging lip extending substantially axially downstream of the space for facilitating attachment of the fluid to the liner in a protective film barrier, the improvement comprising: a stabilizing dimple disposed within said lip, the dimple including a substantially radially depressed portion, the depressed portion having a first radial height proximate its upstream extremity, a second radial height at its downstream extremity, said second radial height being greater than said first radial height, said depressed portion further including an intermediate segment intermediate said upstream and downstream extremities and having a radial height substantially equal to said second radial height.
Claim 2
Dependent Claim
157 words
In a combustor liner film cooling slot of the variety including an annular space extending circumferentially of the liner and defined between overlapping portions of telescoping liner segments, a cooling fluid plenum substantially circumscribing the liner, means for transferring cooling fluid from the plenum to the space, means for exhausting fluid from the space onto the liner, and an overhanging lip extending substantially axially downstream of the space for facilitating attachment of the fluid to the liner in a protective film barrier, the improvement comprising: a stabilizing dimple disposed within said lip, the dimple including a substantially radially depressed portion, the depressed portion having a first radial height proximate its upstream extremity, a second radial height at its downstream extremity, said second radial height being greater than said first radial height, said depressed portion further including an intermediate segment intermediate said upstream and downstream extremities and having a radial height substantially equal to said second radial height.
Claim 3
Dependent Claim
38 words
The invention in claim 1 wherein said depressed portion is further comprised of a first circumferential width proximate its upstream extremity and a second circumferential width proximate its downstream extremity, the first width being greater than the second.
Claim 4
Dependent Claim
44 words
The invention as set forth in claim 2 wherein said intermediate segment is disposed immediately upstream and adjacent to said downstream extremity, said intermediate segment and said downstream extremity cooperating to form a dimple ceiling of constant radial height downstream of said upstream extremity.
Claim 5
Dependent Claim
65 words
The invention as set forth in claim 3 further including a plurality of said stabilizing dimples so characterized, said dimples spaced circumferentially about said lip, each of said dimples cooperating with adjacent dimples to define a flow channel for the passage of cooling air from said space to said liner, said flow channel having consecutive downstream cross-sectional areas of increasing magnitude in the downstream direction.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1980-09-26 | 1981-03-28 | 1981-09-27 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-09-26 | 1985-03-28 | 1985-09-27 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-09-26 | 1989-03-28 | 1989-09-27 | $7700.00 | Window Closed / Lapsed |