Patent US3609497A successfully refreshed from Google Patents.
US4216652A
Expired / Lapsed
US
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Integrated, replaceable combustor swirler and fuel injector
Assignee: Rolls Royce Corp
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Filing: 1978-06-08
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Granted: 1980-08-12
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Expires: 1998-06-08
Abstract
Abstract An air blast fuel supply system for a gas turbine engine comprises a floating swirler separated from the fuel injector and means for radially supporting both the swirler and fuel injector for free radial movement with respect to a combustor dome; a fuel atomization lip on the floating swirler is located in spaced overlying relationship to a tangential fuel director to form an annular fuel film at the outlet of the fuel injector and an outer annular air flow directing lip on the floating swirler directs inlet air flow against the fuel film as it leaves the atomization lip. The fuel injector includes a nozzle tube that slips to permit free axial movement of said fuel injector with resepct to the dome and wherein the tangential fuel director maintains the annular fuel film throughout axially shifted positions of said nozzle tube. This allows the fuel nozzle to be inserted through a small opening in the engine case while maintaining the integrated relationship with the swirler attached to the combustor. The fuel atomization lip has an outlet edge thereon and an outer annular air flow directing lip has outlet edge thereon maintained at a constantly fixed dimensional relationship therebetween throughout axial shifted positions of the nozzle tube whereby the fuel break-up point for atomization of fuel and air remains the same with respect to the combustor during engine operation.
Inventors
- 👤 Avrum S. Herman
- 👤 Samuel B. Reider
- 👤 Cecil H. Sharpe
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 20:20
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/42; F23R3/60; F23C; F23C7/00; F23C7/002; F23C7/004; F23D; F23D11/00; F23D11/10; F23D11/12; F23R3/28; F23R3/283
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
225 words
An air blast fuel supply system for directing air and fuel into a combustor having a fixed dome thereon comprising: a floating swirler and fuel injector nozzle, means for radially supporting both said swirler and fuel injector nozzle for free radial movement and axial restraint with respect to said dome, means for defining a tangential fuel director movably supported for axial movement on said fuel injector nozzle, a fuel atomization lip fixed on said floating swirler and located in spaced overlying relationship to said tangential fuel director to form an annular fuel film at the outlet of said fuel injector nozzle, means including an annular air flow directing lip fixed on said floating swirler to direct inlet air flow against the fuel film to atomize it as it leaves said atomization lip, said tangential fuel director and fuel atomization lip maintaining said annular fuel film throughout axially shifted positions of said tangential fuel director with respect to said fuel atomization lip, said fuel atomization lip having an outlet edge thereon and said outer air flow directing lip having an outlet edge thereon maintained at a constantly fixed dimensional relationship therebetween throughout axial shifted movements of said tangential fuel director whereby the fuel break-up point for atomization of fuel and air from said fuel nozzle remains the same with respect to the combustor during engine operation.
Claim 2
Dependent Claim
225 words
An air blast fuel supply system for directing air and fuel into a combustor having a fixed dome thereon comprising: a floating swirler and fuel injector nozzle, means for radially supporting both said swirler and fuel injector nozzle for free radial movement and axial restraint with respect to said dome, means for defining a tangential fuel director movably supported for axial movement on said fuel injector nozzle, a fuel atomization lip fixed on said floating swirler and located in spaced overlying relationship to said tangential fuel director to form an annular fuel film at the outlet of said fuel injector nozzle, means including an annular air flow directing lip fixed on said floating swirler to direct inlet air flow against the fuel film to atomize it as it leaves said atomization lip, said tangential fuel director and fuel atomization lip maintaining said annular fuel film throughout axially shifted positions of said tangential fuel director with respect to said fuel atomization lip, said fuel atomization lip having an outlet edge thereon and said outer air flow directing lip having an outlet edge thereon maintained at a constantly fixed dimensional relationship therebetween throughout axial shifted movements of said tangential fuel director whereby the fuel break-up point for atomization of fuel and air from said fuel nozzle remains the same with respect to the combustor during engine operation.
Claim 3
Dependent Claim
268 words
An air blast fuel supply system for directing air and fuel into a combustor having a fixed dome thereon comprising: a floating swirler and fuel injector nozzle, means for radially supporting both said swirler and fuel injector nozzle for free radial movement with respect to said dome, said last mentioned means including a dome support ring with a recessed radial shoulder, said swirler having a shroud with a radial flange slidably supported by said shoulder and a removable locator ring secured to said support ring for removably axially retaining said swirler in place, means for defining a tangential fuel director movably supported for axial movement on said fuel injector nozzle, a fuel atomization lip fixed on said floating swirler and located in spaced overlying relationship to said tangential fuel director to form an annular fuel film at the outlet of said fuel injector nozzle, means including an annular air flow directing lip fixed on said floating swirler to direct inlet air flow against the fuel film to atomize it as it leaves said atomization lip, said tangential fuel director and fuel atomization lip maintaining said annular fuel film throughout axially shifted positions of said tangential fuel director with respect to said fuel atomization lip, said fuel atomization lip having an outlet edge thereon and said outer air flow directing lip having an outlet edge thereon maintained at a constantly fixed dimensional relationship therebetween throughout axial shifting movement of said tangential fuel director whereby the fuel break-up point for atomization of fuel and air from said fuel nozzle remains the same with respect to the combustor during engine operation.
Claim 4
Dependent Claim
268 words
An air blast fuel supply system for directing air and fuel into a combustor having a fixed dome thereon comprising: a floating swirler and fuel injector nozzle, means for radially supporting both said swirler and fuel injector nozzle for free radial movement with respect to said dome, said last mentioned means including a dome support ring with a recessed radial shoulder, said swirler having a shroud with a radial flange slidably supported by said shoulder and a removable locator ring secured to said support ring for removably axially retaining said swirler in place, means for defining a tangential fuel director movably supported for axial movement on said fuel injector nozzle, a fuel atomization lip fixed on said floating swirler and located in spaced overlying relationship to said tangential fuel director to form an annular fuel film at the outlet of said fuel injector nozzle, means including an annular air flow directing lip fixed on said floating swirler to direct inlet air flow against the fuel film to atomize it as it leaves said atomization lip, said tangential fuel director and fuel atomization lip maintaining said annular fuel film throughout axially shifted positions of said tangential fuel director with respect to said fuel atomization lip, said fuel atomization lip having an outlet edge thereon and said outer air flow directing lip having an outlet edge thereon maintained at a constantly fixed dimensional relationship therebetween throughout axial shifting movement of said tangential fuel director whereby the fuel break-up point for atomization of fuel and air from said fuel nozzle remains the same with respect to the combustor during engine operation.
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) | 1983-08-12 | 1984-02-11 | 1984-08-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-08-12 | 1988-02-11 | 1988-08-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-08-12 | 1992-02-11 | 1992-08-12 | $7700.00 | Window Closed / Lapsed |