US5085575A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for premixed combustion of a liquid fuel
Assignee: ABB Asea Brown Boveri Ltd
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Filing: 1990-12-19
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Granted: 1992-02-04
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Expires: 2010-12-19
Abstract
Abstract In a premixed type of combustion of a liquid fuel at high pressure, the injection of the fuel (4c, 4d) and its evaporation with a gaseous medium (5) is undertaken, in order to prevent premature ignition of the liquid/gaseous mixture in the burner itself, at a location where the droplets of the fuel from the fuel nozzles (4a, 4b) are screened from the flame radiation from the flame front of the burner. As soon as the fuel (4c, 4d) is pre-evaporated, i.e. leaves the duct (7a, 7b) via the inlet slot (1d, 2d) in the direction of the internal space (3) of the burner as a mixture (6), it absorbs practically no flame radiation.
Inventors
- 👤 Jakob Keller
- 👤 Jurgen Haumann
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 17:06
CPC Classifications
F; F23; F23C; F23C7/00; F23C7/002; F23D; F23D11/00; F23D11/36; F23D11/40; F23D11/402; F23C2900/00; F23C2900/07002
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
207 words
A method for premixed combustion of a fuel in a burner having a first partial conical body having a longitudinal centerline and a second partial conical body having a longitudinal centerline, said first and second partial conical bodies being positioned adjacent one another with the respective centerlines thereof in parallel offset relation so as to form a substantially conical core body having two longitudinally extending tangential inlet openings for feeding into an internal space of the core body, said burner further including a duct communicating with each of said inlet openings and at lest one liquid fuel nozzle in each said duct, said method comprising the steps of: discharging liquid fuel from each of said nozzles; and permitting said fuel to be vaporized in the respective ducts to form a gaseous fuel in the respective ducts, the gaseous fuel entering the internal space of the core body and being discharged and combusted to form a flame fremont at a large diameter end of said core body, wherein said ducts are positioned external to said core body such that said partial conical bodies screen the discharged liquid from radiation feronm the flame front and such that only the evaporated gaseous fuel enters the radiation region of the flame.
Claim 2
Independent Claim
207 words
A method for premixed combustion of a fuel in a burner having a first partial conical body having a longitudinal centerline and a second partial conical body having a longitudinal centerline, said first and second partial conical bodies being positioned adjacent one another with the respective centerlines thereof in parallel offset relation so as to form a substantially conical core body having two longitudinally extending tangential inlet openings for feeding into an internal space of the core body, said burner further including a duct communicating with each of said inlet openings and at lest one liquid fuel nozzle in each said duct, said method comprising the steps of: discharging liquid fuel from each of said nozzles; and permitting said fuel to be vaporized in the respective ducts to form a gaseous fuel in the respective ducts, the gaseous fuel entering the internal space of the core body and being discharged and combusted to form a flame fremont at a large diameter end of said core body, wherein said ducts are positioned external to said core body such that said partial conical bodies screen the discharged liquid from radiation feronm the flame front and such that only the evaporated gaseous fuel enters the radiation region of the flame.
Claim 3
Dependent Claim
20 words
Method as claimed in claim 1, wherein the evaporation of the fuel is carried out with an air/exhaust gas mixture.
Claim 4
Dependent Claim
20 words
Method as claimed in claim 1, wherein the ratio between the recycled exhaust gas and the added air is 0.7.
Claim 5
Dependent Claim
194 words
A burner for premixed combustion of a fuel, comprising: a first partial conical body having a longitudinal centerline; a second partial conical body having a longitudinal centerline, said fist and second partial conical bodies being positioned adjacent one another with respective centerlines thereof in parallel offset relation so as to form a substantially conical core body having two longitudinally extending tangential inlet openings for feeding into an internal space of the core body; a duct communicating with each of said inlet openings; and at least one liquid fuel nozzle in each said duct, said nozzles being positioned such that fuel discharged from each of said nozzles is vaporized in the respective ducts to form a gaseous fuel in he respective ducts, the gaseous fuel entering the internal space of the core body and being discharged and combusted to form a flame front at a large diameter end of said core body, wherein said ducts are positioned external to id core body such that said partial conical bodies comprise means for screening the discharged liquid from radiation from the flame front such that only the evaporated gaseous fuel enters the radiation region of the flame.
Claim 6
Dependent Claim
194 words
A burner for premixed combustion of a fuel, comprising: a first partial conical body having a longitudinal centerline; a second partial conical body having a longitudinal centerline, said fist and second partial conical bodies being positioned adjacent one another with respective centerlines thereof in parallel offset relation so as to form a substantially conical core body having two longitudinally extending tangential inlet openings for feeding into an internal space of the core body; a duct communicating with each of said inlet openings; and at least one liquid fuel nozzle in each said duct, said nozzles being positioned such that fuel discharged from each of said nozzles is vaporized in the respective ducts to form a gaseous fuel in he respective ducts, the gaseous fuel entering the internal space of the core body and being discharged and combusted to form a flame front at a large diameter end of said core body, wherein said ducts are positioned external to id core body such that said partial conical bodies comprise means for screening the discharged liquid from radiation from the flame front such that only the evaporated gaseous fuel enters the radiation region of the flame.
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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) | 1995-02-03 | 1995-08-05 | 1996-02-04 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1999-02-03 | 1999-08-05 | 2000-02-04 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2003-02-03 | 2003-08-05 | 2004-02-04 | $7700.00 | Window Closed / Lapsed |