US4845952A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Multiple venturi tube gas fuel injector for catalytic combustor
Assignee: General Electric Co
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Filing: 1987-10-23
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Granted: 1989-07-11
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Expires: 2007-10-23
Abstract
Abstract A fuel gas injector for a gas turbine engine employs a plurality of closely spaced parallel venturi tubes disposed in a pair of spaced-apart header plates. The venturi tubes are brazed to the header plates and the perimeters of the header plates are sealed to form a plenum into which pressurized gaseous fuel is supplied. Orifices lead from the plenum to throats of the venturi tubes thereby injecting the gaseous fuel at right angles into the high-velocity air stream existing at the throats of the venturi tubes. High shear is imposed on the injected fuel for providing complete mixing with the air. The high air velocity in the throats of the venturi tubes avoids flashback and flameholding. The combined flow from the plurality of venturi tubes mixes downstream thereof to provide a uniform velocity and fuel-air mixture across the flow field. This flow field is suitable for use in a catalyst bed which may be disposed downstream of the venturi tubes.
Inventors
- 👤 Kenneth W. Beebe
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 23:40
CPC Classifications
F; F23; F23C; F23C13/00; B; B01; B01F; B01F25/00; B01F25/30; B01F25/31; B01F25/312; B01F25/3121; F23D; F23D14/00; F23D14/46; F23D14/62; F23R; F23R3/00; F23R3/28; F23R3/286; F23R3/34; F23R3/40
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
111 words
A fuel injector for a combustor of a gas turbine engine comprising: a plurality of venturi tubes disposed in said combustor; said plurality of venturi tubes including means for forcing substantially all of an upstream gas flow to pass through said plurality of venturi tubes; each of said venturi tubes including a converging inlet section, a throat defining a narrowest portion, and a diverging diffuser section; each of said venturi tubes including at least one orifice through a wall of said throat; and means for feeding a fuel gas to said at least one orifice, whereby said fuel gas is injected through said wall into said gas flow at said throat.
Claim 2
Dependent Claim
111 words
A fuel injector for a combustor of a gas turbine engine comprising: a plurality of venturi tubes disposed in said combustor; said plurality of venturi tubes including means for forcing substantially all of an upstream gas flow to pass through said plurality of venturi tubes; each of said venturi tubes including a converging inlet section, a throat defining a narrowest portion, and a diverging diffuser section; each of said venturi tubes including at least one orifice through a wall of said throat; and means for feeding a fuel gas to said at least one orifice, whereby said fuel gas is injected through said wall into said gas flow at said throat.
Claim 3
Dependent Claim
39 words
A fuel injector according to claim 1, wherein said at least one orifice is disposed at about 90 degrees to said gas flow through said throat, whereby said fuel gas is injected at 90 degrees to said gas flow.
Claim 4
Dependent Claim
163 words
A fuel injector for a combustor of a gas turbine engine comprising: an upstream header plate extending across a direction of a gas flow in said combustor; a downstream header plate spaced downstream of said upstream header plate; a plurality of venturi tubes passing through said upstream and said downstream header plates; first means for sealing said plurality of venturi tubes to said upstream and downstream header plates, whereby said gas stream is forced to pass through said plurality of venturi tubes; each of said venturi tubes including a throat; second means for sealing perimeters of said upstream and downstream header plates together whereby a plenum is formed therebetween surrounding portions of said plurality of venturi tubes; means for feeding a fuel gas into said plenum; and each of said venturi tubes including at least one orifice between said plenum and a said throat, whereby said fuel gas is injectable through said at least one orifice into said gas stream at said throat.
Claim 5
Dependent Claim
163 words
A fuel injector for a combustor of a gas turbine engine comprising: an upstream header plate extending across a direction of a gas flow in said combustor; a downstream header plate spaced downstream of said upstream header plate; a plurality of venturi tubes passing through said upstream and said downstream header plates; first means for sealing said plurality of venturi tubes to said upstream and downstream header plates, whereby said gas stream is forced to pass through said plurality of venturi tubes; each of said venturi tubes including a throat; second means for sealing perimeters of said upstream and downstream header plates together whereby a plenum is formed therebetween surrounding portions of said plurality of venturi tubes; means for feeding a fuel gas into said plenum; and each of said venturi tubes including at least one orifice between said plenum and a said throat, whereby said fuel gas is injectable through said at least one orifice into said gas stream at said throat.
Claim 6
Dependent Claim
30 words
A fuel injector according to claim 3, wherein said at least one orifice includes at least three orifices spaced about a circumference of each of said plurality of venturi tubes.
Claim 7
Dependent Claim
40 words
A fuel injector according to claim 3, wherein: each of said venturi tubes includes a converging inlet section, a throat defining a narrowest portion, and a diverging diffuser section; and said at least one orifice is disposed in said throat.
Claim 8
Dependent Claim
15 words
A fuel injector according to claim 3, wherein said first means for sealing includes brazing.
Claim 9
Dependent Claim
20 words
A fuel injector according to claim 3 wherein said second means for sealing includes a sealing ring about said perimeters.
Claim 10
Dependent Claim
33 words
A fuel injector according to claim 7, wherein said second means for sealing includes brazing between said upstream header plate and said sealing ring and between said downstream plate and said sealing ring.
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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) | 1992-07-10 | 1993-01-09 | 1993-07-11 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1996-07-10 | 1997-01-09 | 1997-07-11 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2000-07-10 | 2001-01-09 | 2001-07-11 | $7700.00 | Window Closed / Lapsed |