US4453384A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Fuel burners and combustion equipment for use in gas turbine engines
Assignee: Rolls Royce PLC
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Filing: 1981-12-22
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Granted: 1984-06-12
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Expires: 2001-12-22
Abstract
Abstract The invention relates to fuel burners and the combination of fuel burners and annular combustion equipment particularly for use in gas turbine engines. The present invention seeks to provide a fuel burner that requires a relatively small access hole in the engine casing in order to reduce stress concentrations in the casing. The fuel burner comprises a fuel feed arm and a fuel injector. The fuel feed arm and the fuel injector are cylindrical, and are arranged coaxially in end-to-end abutting relationship. The fuel feed arm has internal passages for the supply of fuel to the fuel injector, and the fuel injector has an air duct passing normally through the fuel injector for the flow of air into a cooperating combustion chamber. The fuel injector supplies fuel into the air duct to mix with the air flowing therethrough. The invention also provides combustion chamber equipment for use in conjunction with the fuel burners.
Inventors
- 👤 George Pask
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 06:34
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/28; F23R3/283; F23D; F23D11/00; F23D11/10; F23D11/12
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
315 words
Combustion equipment for a gas turbine engine comprising: an annular casing having a plurality of circumferentially arranged equi-spaced holes; an annular flame tube coaxially positioned within and spaced from said annular casing, said annular flame tube having a corresponding number of circumferentially equi-spaced holes coaxially aligned with the holes of said casing: a plurality of tubes extending radially across said annular flame tube, each tube being coaxial with the corresponding hole in the annular flame tube and the corresponding hole in the annular casing, each tube extending normal to an axis of said annular flame tube, each tube having a duct extending therethrough with an axis normal to the axis of the tube and parallel to the axis of said annular flame tube; a plurality of fuel burners, each fuel burner comprising a cylindrical fuel feed arm having a fuel passage therethrough, a fuel injector having a cylindrical body coaxial with and joined in end-to-end relationship with said cylindrical fuel feed arm, said fuel injector having a first passage in said cylindrical body communicating with said fuel feed passage in said fuel feed arm, said fuel injector having an air duct extending through said cylindrical body thereof, said air duct having an axis normal to the axes of said cylindrical body of the fuel injector and said fuel feed arm, said fuel injector having at least a second passage in said cylindrical body communicating with said first passage therein and with said air duct for injecting fuel into said air duct, each fuel burner extending coaxially through aligned holes in said annular casing and said annular flame tube and through the radial tube in said flame tube, said fuel injector of said fuel burner being positioned in said duct in said radial tube, the axis of said air duct in said cylindrical body being coincident with the axis of the duct in said radial tube.
Claim 2
Dependent Claim
315 words
Combustion equipment for a gas turbine engine comprising: an annular casing having a plurality of circumferentially arranged equi-spaced holes; an annular flame tube coaxially positioned within and spaced from said annular casing, said annular flame tube having a corresponding number of circumferentially equi-spaced holes coaxially aligned with the holes of said casing: a plurality of tubes extending radially across said annular flame tube, each tube being coaxial with the corresponding hole in the annular flame tube and the corresponding hole in the annular casing, each tube extending normal to an axis of said annular flame tube, each tube having a duct extending therethrough with an axis normal to the axis of the tube and parallel to the axis of said annular flame tube; a plurality of fuel burners, each fuel burner comprising a cylindrical fuel feed arm having a fuel passage therethrough, a fuel injector having a cylindrical body coaxial with and joined in end-to-end relationship with said cylindrical fuel feed arm, said fuel injector having a first passage in said cylindrical body communicating with said fuel feed passage in said fuel feed arm, said fuel injector having an air duct extending through said cylindrical body thereof, said air duct having an axis normal to the axes of said cylindrical body of the fuel injector and said fuel feed arm, said fuel injector having at least a second passage in said cylindrical body communicating with said first passage therein and with said air duct for injecting fuel into said air duct, each fuel burner extending coaxially through aligned holes in said annular casing and said annular flame tube and through the radial tube in said flame tube, said fuel injector of said fuel burner being positioned in said duct in said radial tube, the axis of said air duct in said cylindrical body being coincident with the axis of the duct in said radial tube.
Claim 3
Dependent Claim
57 words
Combustion equipment as claimed in claim 1 in which each fuel injector has a threaded body, the axes of each fuel injector and the corresponding threaded body being coaxial, each threaded body screwing into a corresponding nut secured to the annular flame tube, the axis of each nut being coaxial with the axis of the corresponding tube.
Claim 4
Dependent Claim
34 words
Combustion equipment as claimed in claim 2 in which the diameter of each fuel injector is substantially the same as the inside diameter of the corresponding tube extending radially across the annular flame tube.
Claim 5
Dependent Claim
47 words
Combustion equipment as claimed in claim 3 in which the diameters of each fuel feed arm and each fuel injector respectively are substantially the same as the inside diameters of the corresponding tube extending radially across the annular flame tube, and the corresponding hole in the casing.
Claim 6
Dependent Claim
77 words
Combustion equipment as claimed in claim 4 in which the annular flame tube has a head, the head having a number of equi-spaced apertures with a pot positioned coaxially inside each aperture, the axis of each aperture in the head being aligned with the corresponding axis of the duct in the tube and the corresponding axis of the air duct in the fuel injector, a number of air passages being formed between the pot and the head.
Claim 7
Dependent Claim
16 words
Combustion equipment as claimed in claim 5 in which the pots have a circular cross section.
Claim 8
Dependent Claim
13 words
Combustion equipment as claimed in claim 6 in which the pots are cylindrical.
Claim 9
Dependent Claim
16 words
Combustion equipment as claimed in claim 6 in which the pots diverge in a downstream direction.
Claim 10
Dependent Claim
32 words
Combustion equipment as claimed in claim 6 in which the upstream end of the annular flame tube has a number of equi-spaced apertures aligned with the air ducts of the fuel burners.
Claim 11
Dependent Claim
24 words
Combustion equipment as claimed in claim 9 in which each aperture in the upstream end of the annular flame tube has an air swirler.
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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) | 1987-06-12 | 1987-12-12 | 1988-06-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-06-12 | 1991-12-12 | 1992-06-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-06-12 | 1995-12-12 | 1996-06-12 | $7700.00 | Window Closed / Lapsed |