Patent US4222230A successfully refreshed from Google Patents.
US4222230A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Combustor dome assembly
Assignee: General Electric Co
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Filing: 1978-08-14
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Granted: 1980-09-16
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Expires: 1998-08-14
Abstract
Abstract An improved cooling arrangement is provided for cooling a portion of a combustor dome assembly of a gas turbine engine. The improvement is comprised of an annular dome plate having a generally V-shaped cross section and including one or more circumferentially spaced apart, generally radial cooling slots within a surface which is exposed to the combustion zone.
Inventors
- 👤 Melvin Bobo
- 👤 Thomas L. DuBell
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 07:03
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/02; F23R3/04; F23R3/10
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
178 words
In a gas turbine engine combustor assembly including a pair of combustor liners radially spaced apart and forming a combustion zone therebetween, a dome assembly disposed between the liners and cooperating therewith to form an upstream end of the combustion zone, and an inlet cowl surrounding the dome assembly to define an inlet plenum upstream of the combustion zone, the improved dome assembly comprising: an annular dome plate of generally V-shaped cross section including first and second legs extending from an apex portion thereof, said apex portion being disposed adjacent to one of the liners and downstream of said legs, said first leg extending upstream from said apex portion, generally parallel to and in abutting engagement with said one of the liners, said second leg extending upstream from said apex portion at an acute angle to said first leg and forming with said apex portion a surface exposed to the combustion zone, said dome plate including one or more circumferentially spaced apart slots extending generally radially through said first leg, said apex portion, and said second leg thereof.
Claim 2
Dependent Claim
178 words
In a gas turbine engine combustor assembly including a pair of combustor liners radially spaced apart and forming a combustion zone therebetween, a dome assembly disposed between the liners and cooperating therewith to form an upstream end of the combustion zone, and an inlet cowl surrounding the dome assembly to define an inlet plenum upstream of the combustion zone, the improved dome assembly comprising: an annular dome plate of generally V-shaped cross section including first and second legs extending from an apex portion thereof, said apex portion being disposed adjacent to one of the liners and downstream of said legs, said first leg extending upstream from said apex portion, generally parallel to and in abutting engagement with said one of the liners, said second leg extending upstream from said apex portion at an acute angle to said first leg and forming with said apex portion a surface exposed to the combustion zone, said dome plate including one or more circumferentially spaced apart slots extending generally radially through said first leg, said apex portion, and said second leg thereof.
Claim 3
Dependent Claim
231 words
In a gas turbine combustor assembly including a pair of combustor liners radially spaced apart and forming a combustion zone therebetween, a dome assembly disposed between the liners and cooperating therewith to form an upstream end of the combustion zone, and an inlet cowl surrounding the dome assembly to define an inlet plenum upstream of the combustion zone, the improved dome assembly comprising: (a) an annular dome plate of generally V-shaped cross-section including first and second legs extending from an apex portion thereof, said apex portion being disposed adjacent to one of the liners and downstream of said legs, said first leg extending upstream from said apex portion generally parallel to and in abutting engagement with said one of the liners, said second leg extending upstream from said apex portion at an acute angle to said first leg and forming with said apex portion a surface exposed to the combustion zone, said dome plate including one or more circumferentially spaced apart slots extending generally radially through said first leg, said apex portion, and said second leg thereof; and (b) an annular dome panel attached to the upstream end of said second leg, having a plurality of openings intersected by said slots and extending through said dome panel for establishing fluid communication between said inlet plenum and said combustion zone, said openings being arranged to direct fluid flowing therethrough onto said surface.
Claim 4
Dependent Claim
231 words
In a gas turbine combustor assembly including a pair of combustor liners radially spaced apart and forming a combustion zone therebetween, a dome assembly disposed between the liners and cooperating therewith to form an upstream end of the combustion zone, and an inlet cowl surrounding the dome assembly to define an inlet plenum upstream of the combustion zone, the improved dome assembly comprising: (a) an annular dome plate of generally V-shaped cross-section including first and second legs extending from an apex portion thereof, said apex portion being disposed adjacent to one of the liners and downstream of said legs, said first leg extending upstream from said apex portion generally parallel to and in abutting engagement with said one of the liners, said second leg extending upstream from said apex portion at an acute angle to said first leg and forming with said apex portion a surface exposed to the combustion zone, said dome plate including one or more circumferentially spaced apart slots extending generally radially through said first leg, said apex portion, and said second leg thereof; and (b) an annular dome panel attached to the upstream end of said second leg, having a plurality of openings intersected by said slots and extending through said dome panel for establishing fluid communication between said inlet plenum and said combustion zone, said openings being arranged to direct fluid flowing therethrough onto said surface.
Claim 5
Dependent Claim
11 words
The combustor assembly of claim 2, wherein said openings are arcuate.
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) | 1983-09-16 | 1984-03-17 | 1984-09-16 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-09-16 | 1988-03-17 | 1988-09-16 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-09-16 | 1992-03-17 | 1992-09-16 | $7700.00 | Window Closed / Lapsed |