US4761959A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Adjustable non-piloted air blast fuel nozzle
Assignee: Honeywell International Inc
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Filing: 1987-03-02
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Granted: 1988-08-09
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Expires: 2007-03-02
Abstract
Abstract A fuel nozzle for injecting atomized fuel into an air stream at an adjustable angle with respect to its longitudinal axis is described incorporating a support flange, a fuel supply tube, a nozzle tip body at the end of the fuel supply tube and a sheath between the support flange and the nozzle tip body for directing air to the nozzle tip body. A second sheath enclosing the first sheath is provided wherein each has a slot opening which may be positioned with respect to the support flange for admitting air into and where the size of the opening may be controlled by rotating the outer sheath with respect to the inner sheath to provide an adjustable overlap of the slot openings. The invention overcomes the problem of injecting fuel into the combustor of a jet engine at an angle which may be adjustable over a predetermined range to enhance combustion of the fuel. The invention further overcomes the problem of injecting or capturing a predetermined amount of compressor discharge air for subsequent flow to the nozzle tip.
Inventors
- 👤 Russell P. Romey
- 👤 Lonny R. Greer
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 21:15
CPC Classifications
F; F23; F23D; F23D11/00; F23D11/10; F23D11/106; F23D11/107; F23R; F23R3/00; F23R3/28; F23R3/283; F23D2900/00; F23D2900/11101
Claims Analysis
Total Claims: 17
Claim 1
Independent Claim
323 words
An apparatus for atomizing fuel in air and for injecting said fuel and air into an air stream at a first angle φ with respect to a first longitudinal axis which is adjustable over a predetermined angular range comprising: a support flange for mechanically supporting a fuel supply tube and a first sheath, a nozzle tip body spaced a predetermined distance from said support flange and having an air inlet and a fuel inlet and an outlet for expelling atomized fuel outward from and along a second longitudinal axis of said nozzle tip body, said fuel inlet concentric with a pivot axis of said nozzle tip body, said nozzle tip body pivot axis positioned transverse to said first and second longitudinal axes, said fuel supply tube having a first end adjustably connected to said fuel inlet of said nozzle tip body to supply fuel thereto and to support and hold said nozzle tip body with its second longitudinal axis at said angle within said predetermined angular range by positioning said nozzle tip body around said pivot axis, said first longitudinal axis passing through said support flange and through said nozzle tip body, an internal air cap having an outer surface with portions thereof conforming to the surface of revolution, said outer surface surrounding said nozzle tip body and attached thereto to direct air through said nozzle tip body via said air inlet, said first sheath having a cylindrical shape concentric with said first longitudinal axis, having a slot opening for admitting air inside said sheath, said sheath extending a predetermined distance from said support flange, an external air cap having an inside surface with portions thereof conforming to the surface of revolution and having a first opening for mating with an opening at the end of said sheath and a second opening to permit said nozzle tip body to expel atomized fuel at positions within said predetermined angular range about said pivot axis.
Claim 2
Independent Claim
323 words
An apparatus for atomizing fuel in air and for injecting said fuel and air into an air stream at a first angle φ with respect to a first longitudinal axis which is adjustable over a predetermined angular range comprising: a support flange for mechanically supporting a fuel supply tube and a first sheath, a nozzle tip body spaced a predetermined distance from said support flange and having an air inlet and a fuel inlet and an outlet for expelling atomized fuel outward from and along a second longitudinal axis of said nozzle tip body, said fuel inlet concentric with a pivot axis of said nozzle tip body, said nozzle tip body pivot axis positioned transverse to said first and second longitudinal axes, said fuel supply tube having a first end adjustably connected to said fuel inlet of said nozzle tip body to supply fuel thereto and to support and hold said nozzle tip body with its second longitudinal axis at said angle within said predetermined angular range by positioning said nozzle tip body around said pivot axis, said first longitudinal axis passing through said support flange and through said nozzle tip body, an internal air cap having an outer surface with portions thereof conforming to the surface of revolution, said outer surface surrounding said nozzle tip body and attached thereto to direct air through said nozzle tip body via said air inlet, said first sheath having a cylindrical shape concentric with said first longitudinal axis, having a slot opening for admitting air inside said sheath, said sheath extending a predetermined distance from said support flange, an external air cap having an inside surface with portions thereof conforming to the surface of revolution and having a first opening for mating with an opening at the end of said sheath and a second opening to permit said nozzle tip body to expel atomized fuel at positions within said predetermined angular range about said pivot axis.
Claim 3
Dependent Claim
32 words
The apparatus of claim 1 wherein said support flange has at least one slot opening to permit rotation of said support flange with respect to a support member secured by a bolt.
Claim 4
Dependent Claim
26 words
The apparatus of claim 2 wherein said slot opening in said support flange has a center line at a predetermined distance from said first longitudinal axis.
Claim 5
Dependent Claim
18 words
The apparatus of claim 3 wherein said slot opening extends at least 45° around said first longitudinal axis.
Claim 6
Dependent Claim
18 words
The apparatus of claim 1 wherein said first end of said fuel supply tube includes a jam nut.
Claim 7
Dependent Claim
18 words
The apparatus of claim 1 wherein said predetermined angular range of angle φ extends from 45° to 80°.
Claim 8
Dependent Claim
30 words
The apparatus of claim 1 wherein said external air cap has its first opening mating with an opening of the end of said sheath to prevent air from escaping therebetween.
Claim 9
Dependent Claim
68 words
The apparatus of claim 1 wherein said portions of said inside surface of said external air cap are spaced less than a predetermined distance to said portions of said outer surface of said internal air cap to prevent the escape of air from within said sheath between said external air cap and said internal air cap at positions of said nozzle tip body within said predetermined angular range.
Claim 10
Dependent Claim
17 words
The apparatus of claim 1 wherein said surface portions conforming to the surface of revolution are spherical.
Claim 11
Dependent Claim
43 words
The apparatus of claim 1 wherein said second opening of said external air cap includes a slot opening having a center line at a predetermined distance from said pivot axis wherein said center line is in a plane normal to said pivot axis.
Claim 12
Dependent Claim
21 words
The apparatus of claim 1 wherein said external air cap further includes a set screw passing into said nozzle tip body.
Claim 13
Dependent Claim
18 words
The apparatus of claim 11 wherein said set screw passes into said nozzle body along said pivot axis.
Claim 14
Dependent Claim
51 words
The apparatus of claim 1 wherein said first sheath is surrounded by a second sheat concentric with said first longitudinal axis having a slot opening for admitting air inside said first and second sheaths at times said slot opening of said second sheath overlaps said slot opening of said first sheath.
Claim 15
Dependent Claim
31 words
The apparatus of claim 13 wherein said second sheath is cylindrical in shape and wherein said first sheath has an annular ledge for positioning said second sheath in the longitudinal direction.
Claim 16
Dependent Claim
101 words
The apparatus of claim 14 wherein said support flange includes a threaded surface concentric with said first axis for receiving a nut thereon, said nut having a cylindrical outside surface concentric with said first axis having portions closest said support flange with threads thereon, an outer sheath ring having inside threads for threading onto corresponding outside threads of said nut for compressing said second sheath between said outer sheath ring and said anular ledge whereby said second sheath may be rotated about said first longitudinal axis to provide a predetermined overlap between corresponding slot openings in said first and second sheaths.
Claim 17
Dependent Claim
76 words
The apparatus of claim 1 wherein said support flange further includes a threaded surface concentric with said first axis for receiving a nut thereon, said nut having a cylindrical surface concentric with said first axis for receiving the cylindrical inner surface of said second sheath wherein said first sheath is positioned by said second sheath concentric with said first axis and wherein said first sheath has a second end which abuts against said internal air cap.
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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) | 1991-08-09 | 1992-02-08 | 1992-08-09 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-08-09 | 1996-02-08 | 1996-08-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-08-09 | 2000-02-08 | 2000-08-09 | $7700.00 | Window Closed / Lapsed |