US4499735A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Segmented zoned fuel injection system for use with a combustor
Assignee: United States Department of the Air Force
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Filing: 1984-02-09
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Granted: 1985-02-19
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Expires: 2004-02-09
Abstract
Abstract A segmented, zoned fuel injection system for use within the entrance area of a combustor. The fuel injection system has a plurality of spray bars formed as part of closely-spaced apart segments. The spray bars are zoned to permit additional control of profile and flow rate of fuel injected into the combustor. This design permits radial profile control within the combustor, maintains higher efficiency at low fuel flows and easy replacement and/or maintenance of the components thereof.
Inventors
- 👤 George W. Moore
- 👤 Robert G. Carroll
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 04:19
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/28; F02; F02C; F02C7/00; F02C7/22; F02C7/228; F23R3/34
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
274 words
A removable fuel injection system for use in conjuction with a combustor, said fuel injection system comprising: a plurality of circumferentially spaced-apart segments, each of said segments being in the form of a wedge-shaped plate; means for mounting each of said circumferentially spaced-apart plates adjacent one another and adjacent the entrance of said combustor so as to form an annular-shaped body; each of said plates including means for injecting fuel into said combustor and means for permitting gas to flow into said combustor; said fuel injecting means being in the form of a plurality of radially spaced-apart tubular-shaped, circumferential spray bars, all of said spray bars lying in substantially the same radial plane; each of said spray bars having a plurality of sets of fuel injecting orifices therein, said orifices of each of said sets of orifices being disposed in a circumferential, spaced-apart relationship with respect to one another, and a plate located within the interior of each of said tubular-shaped spray bars for dividing each of said spray bars into a pair of separate fuel injecting zones; said gas flow permitting means being in the form of a plurality of sets of openings of preselected size, said openings of each of said sets of openings being disposed in a circumferential, spaced-apart relationship with respect to one another, and each of said sets of said openings and spray bars being alternately spaced-apart in the radial direction; and means operably connected to each of fuel injecting zones for providing a regulated amount of fuel to each of said zones, whereby the amount and location of said fuel being injected into said combustor can be controlled.
Claim 2
Dependent Claim
274 words
A removable fuel injection system for use in conjuction with a combustor, said fuel injection system comprising: a plurality of circumferentially spaced-apart segments, each of said segments being in the form of a wedge-shaped plate; means for mounting each of said circumferentially spaced-apart plates adjacent one another and adjacent the entrance of said combustor so as to form an annular-shaped body; each of said plates including means for injecting fuel into said combustor and means for permitting gas to flow into said combustor; said fuel injecting means being in the form of a plurality of radially spaced-apart tubular-shaped, circumferential spray bars, all of said spray bars lying in substantially the same radial plane; each of said spray bars having a plurality of sets of fuel injecting orifices therein, said orifices of each of said sets of orifices being disposed in a circumferential, spaced-apart relationship with respect to one another, and a plate located within the interior of each of said tubular-shaped spray bars for dividing each of said spray bars into a pair of separate fuel injecting zones; said gas flow permitting means being in the form of a plurality of sets of openings of preselected size, said openings of each of said sets of openings being disposed in a circumferential, spaced-apart relationship with respect to one another, and each of said sets of said openings and spray bars being alternately spaced-apart in the radial direction; and means operably connected to each of fuel injecting zones for providing a regulated amount of fuel to each of said zones, whereby the amount and location of said fuel being injected into said combustor can be controlled.
Claim 3
Dependent Claim
40 words
A fuel injection system as defined in claim 1 wherein said means for providing said regulated amount of fuel to each of said zones of said spray bars in one of said plates comprises a separate conduit and a valve.
Claim 4
Dependent Claim
326 words
A combustor for a gas turbine engine comprising: an inner liner; an outer liner, said inner liner and outer liners being disposed with respect to each other so as to define therebetween an annular-shaped combustion chamber, said combustion chamber having an inlet at one end thereof; and a removable fuel injection system located adjacent said inlet end of said combustion chamber, said fuel injection system being formed of a plurality of circumferentially spaced-apart segments, each of said segments being in the form of a wedge-shaped plate; means for mounting each of said circumferentially spaced-apart plates adjacent one another and adjacent the entrance of said combustor so as to form an annular-shaped body; each of said plates including means for injecting fuel into said combustor and means for permitting gas to flow into said combustor; said fuel injecting means being in the form of a plurality of radially spaced-apart, tubular-shaped, circumferential spray bars, all of said spray bars lying in substantially the same radial plane; each of said spray bars having a plurality of sets of fuel injecting orifices therein, said orifices of each of said sets of orifices being disposed in a circumferential, spaced-apart relationship with respect to one another, and a plate located within the interior of each of said tubular-shaped spray bars for dividing each of said spray bars into a pair of separate fuel injecting zones; said gas flow permitting means being in the form of a plurality of sets of openings of preselected size, said openings of each of said sets of openings being disposed in a circumferential, spaced-apart relationship with respect to one another, and each of said sets of said openings and spray bars being alternately spaced-apart in the radial direction; and means operably connected to each of said fuel injecting zones for providing a regulated amount of fuel to each of said zones, whereby the amount and location of said fuel being injected into said combustor can be controlled.
Claim 5
Dependent Claim
326 words
A combustor for a gas turbine engine comprising: an inner liner; an outer liner, said inner liner and outer liners being disposed with respect to each other so as to define therebetween an annular-shaped combustion chamber, said combustion chamber having an inlet at one end thereof; and a removable fuel injection system located adjacent said inlet end of said combustion chamber, said fuel injection system being formed of a plurality of circumferentially spaced-apart segments, each of said segments being in the form of a wedge-shaped plate; means for mounting each of said circumferentially spaced-apart plates adjacent one another and adjacent the entrance of said combustor so as to form an annular-shaped body; each of said plates including means for injecting fuel into said combustor and means for permitting gas to flow into said combustor; said fuel injecting means being in the form of a plurality of radially spaced-apart, tubular-shaped, circumferential spray bars, all of said spray bars lying in substantially the same radial plane; each of said spray bars having a plurality of sets of fuel injecting orifices therein, said orifices of each of said sets of orifices being disposed in a circumferential, spaced-apart relationship with respect to one another, and a plate located within the interior of each of said tubular-shaped spray bars for dividing each of said spray bars into a pair of separate fuel injecting zones; said gas flow permitting means being in the form of a plurality of sets of openings of preselected size, said openings of each of said sets of openings being disposed in a circumferential, spaced-apart relationship with respect to one another, and each of said sets of said openings and spray bars being alternately spaced-apart in the radial direction; and means operably connected to each of said fuel injecting zones for providing a regulated amount of fuel to each of said zones, whereby the amount and location of said fuel being injected into said combustor can be controlled.
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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) | 1988-02-19 | 1988-08-20 | 1989-02-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-02-19 | 1992-08-20 | 1993-02-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-02-19 | 1996-08-20 | 1997-02-19 | $7700.00 | Window Closed / Lapsed |