US4085581A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Gas-turbine combustor having an air-cooled shield-plate protecting its end closure dome
Assignee: Safran Aircraft Engines SAS
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Filing: 1976-05-27
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Granted: 1978-04-25
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Expires: 1996-05-27
Abstract
Abstract A combustion chamber for, for example, an aircraft gas turbine engine, hasn upstream end wall protected by a plate serving as a heat shield, the shield-plate being spaced from the dome and cooled by fluid flowing through orifices in the dome. The shield plate is itself formed with a plurality of small dimension orifices which create fluid jets of considerable velocity which serve to atomize any liquid fuel which may stream over the shield-plate and to increase turbulence.
Inventors
- 👤 Jacques Emile Jules Caruel
- 👤 Guy Daniel Stora
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 06:49
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/02; F23R3/04; F23R3/10; F23R3/002; F05; F05B; F05B2260/00; F05B2260/20; F05B2260/201; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
283 words
In a gas-turbine combustion chamber extending longitudinally from an upstream end which comprises: longitudinal side walls opposite one another bounding said combustion chamber; a transverse dome-shaped closure at said upstream end connecting said side walls and mechanically uniting the same to form an integral box-like structure capable of withstanding mechanical stresses; a transverse shield-plate within said chamber extending adjacent to and spaced inwardly of said dome-shaped closure to thermally screen the same, said shield-plate being so mounted with respect to said integral structure as to be substantially unaffected by mechanical stresses withstood thereby; and prevaporized fuel injecting means projecting into said combustion chamber from said dome-shaped closure through said shield-plate and having a portion bent back to discharge fuel in an upstream direction towards and onto the downstream-facing side of said shield-plate; wherein the improvement comprises means positioned between said dome-shaped closure and said shield-plate to partition the space between said dome-shaped closure and the upstream-facing side of said shield-plate into a plenum; compressed air passage means opening through said dome-shaped closure into said plenum to feed the same with compressed air and to cool said shield-plate by impact on said upstream-facing side thereof by air jets formed by said passage means; and a plurality of outwardly-inclined elemental nozzles extending through said shield-plate from said plenum and having a total cross-sectional area which is substantially smaller than the total cross-sectional area of said compressed air passage means, said elemental nozzles functioning to issue high-velocity air jets from the air located in said plenum through said shield-plate whereby any liquid fuel streaming over said downstream-facing side is atomized by said high-velocity air jets and said air jets increase local turbulence adjacent said downstream-facing side.
Claim 2
Dependent Claim
283 words
In a gas-turbine combustion chamber extending longitudinally from an upstream end which comprises: longitudinal side walls opposite one another bounding said combustion chamber; a transverse dome-shaped closure at said upstream end connecting said side walls and mechanically uniting the same to form an integral box-like structure capable of withstanding mechanical stresses; a transverse shield-plate within said chamber extending adjacent to and spaced inwardly of said dome-shaped closure to thermally screen the same, said shield-plate being so mounted with respect to said integral structure as to be substantially unaffected by mechanical stresses withstood thereby; and prevaporized fuel injecting means projecting into said combustion chamber from said dome-shaped closure through said shield-plate and having a portion bent back to discharge fuel in an upstream direction towards and onto the downstream-facing side of said shield-plate; wherein the improvement comprises means positioned between said dome-shaped closure and said shield-plate to partition the space between said dome-shaped closure and the upstream-facing side of said shield-plate into a plenum; compressed air passage means opening through said dome-shaped closure into said plenum to feed the same with compressed air and to cool said shield-plate by impact on said upstream-facing side thereof by air jets formed by said passage means; and a plurality of outwardly-inclined elemental nozzles extending through said shield-plate from said plenum and having a total cross-sectional area which is substantially smaller than the total cross-sectional area of said compressed air passage means, said elemental nozzles functioning to issue high-velocity air jets from the air located in said plenum through said shield-plate whereby any liquid fuel streaming over said downstream-facing side is atomized by said high-velocity air jets and said air jets increase local turbulence adjacent said downstream-facing side.
Claim 3
Dependent Claim
63 words
A combustion chamber as claimed in claim 1, wherein said partitioning means comprise two wall members bearing against said dome-shaped closure and engaging said shield-plate at respective intermediate locations thereof spaced from a periphery thereof, said two wall members bounding therebetween a central zone of said partitioned space forming said plenum and defining two lateral zones on both sides of said central zone.
Claim 4
Dependent Claim
56 words
A combustion chamber as claimed in claim 2, further comprising additional compressed air passage means opening through said dome-shaped closure into said two lateral zones to feed the same with compressed air and to cool said shield-plate by impact on peripheral regions of said upstream-facing side thereof by air jets formed by said additional passage means.
Claim 5
Dependent Claim
20 words
A combustion chamber as claimed in claim 1, wherein said total cross-sectional areas are in the ratio of about 1:3.
References Cited (Backward Citations)
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US3570241A
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US3899876A
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US3656298A
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Cited
US3777484A
Cited
US3916619A
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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) | 1981-04-24 | 1981-10-24 | 1982-04-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-04-24 | 1985-10-24 | 1986-04-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-04-24 | 1989-10-24 | 1990-04-25 | $7700.00 | Window Closed / Lapsed |