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US4437314A Expired / Lapsed US ⏱️ 0.0 years remaining

Atomizer nozzle for continuous fuel injection

Assignee: Kloeckner Humboldt Deutz AG
•
Filing: 1981-07-08
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Granted: 1984-03-20
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Expires: 2001-07-08
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Abstract

Abstract An atomizer nozzle for continuous fuel injection is provided. The nozzle can serve as a main injection nozzle or as an igniter for combustion chambers, and is provided with a single-hole fuel nozzle, and an annular gap for possible additional air supply located coaxially therebefore. The chamber or space between the nozzle opening and the annular gap is connected by pressure equalization openings with the combustion chamber behind or after the annular gap. The pressure equalization openings are represented and defined by individual spacers between the fuel nozzle body and the air nozzle ring.

Inventors

  • 👤 Karl-Heinz Collin

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 14:49
CPC Classifications
F; F23; F23D; F23D11/00; F23D11/10; F23D11/106

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 329 words
An atomizer nozzle arrangement specifically used for continuously injecting fuel into a combustion chamber of a gas turbine engine, wherein the nozzle atomizes the fuel without utilizing moving parts and with minimum utilization of intake air, the nozzle arrangement comprising in combination: an air intake communicating with the combustion chamber; a vaporizor tube within the combustion chamber; a nozzle body positioned within the vaporizor tube in spaced relating therewith to define a space therebetween through which space a portion of the intake air passes; the nozzle body having a bore therethrough for delivering fuel therethrough, the bore having a fuel outlet of a smaller diameter than the bore, from which outlet a spray of fuel is ejected; a circular chamber in the nozzle body and positioned downstream from the outlet, through which chamber the spray of fuel passes, the chamber having a back wall through which the outlet of the bore passes; an annular body having a hollow interior and disposed in the circular chamber in spaced relation to the back wall of the chamber to define a space between the back wall of the chamber and annular body; the hollow annular body having an axial opening coincident with the axis thereof which opening is aligned with but spaced from the outlet of the bore and through which the spray of fuel and air from said hollow annular body pass; the hollow annular body having a front wall and a rear wall each of which have concave portions adjacent the axial opening; an opening communicating the space between the back wall of the chamber and the annular body with the space between the vaporizor tube and nozzle body for pressure equalization; an air supply conduit connected radially with the interior of the hollow annular body for supplying pressurized air thereto, and means for interrupting air flow through the air supply conduit so that the air supply can be stopped when the temperature of the combustion chamber reaches operating temperature.
Claim 2
Dependent Claim 329 words
An atomizer nozzle arrangement specifically used for continuously injecting fuel into a combustion chamber of a gas turbine engine, wherein the nozzle atomizes the fuel without utilizing moving parts and with minimum utilization of intake air, the nozzle arrangement comprising in combination: an air intake communicating with the combustion chamber; a vaporizor tube within the combustion chamber; a nozzle body positioned within the vaporizor tube in spaced relating therewith to define a space therebetween through which space a portion of the intake air passes; the nozzle body having a bore therethrough for delivering fuel therethrough, the bore having a fuel outlet of a smaller diameter than the bore, from which outlet a spray of fuel is ejected; a circular chamber in the nozzle body and positioned downstream from the outlet, through which chamber the spray of fuel passes, the chamber having a back wall through which the outlet of the bore passes; an annular body having a hollow interior and disposed in the circular chamber in spaced relation to the back wall of the chamber to define a space between the back wall of the chamber and annular body; the hollow annular body having an axial opening coincident with the axis thereof which opening is aligned with but spaced from the outlet of the bore and through which the spray of fuel and air from said hollow annular body pass; the hollow annular body having a front wall and a rear wall each of which have concave portions adjacent the axial opening; an opening communicating the space between the back wall of the chamber and the annular body with the space between the vaporizor tube and nozzle body for pressure equalization; an air supply conduit connected radially with the interior of the hollow annular body for supplying pressurized air thereto, and means for interrupting air flow through the air supply conduit so that the air supply can be stopped when the temperature of the combustion chamber reaches operating temperature.
Claim 3
Dependent Claim 53 words
The atomizer nozzle arrangement of claim 1 wherein the annular body is secured to the back wall of the nozzle body by a plurality of screws and wherein the space between the annular body and back wall of the chamber is created by space washers disposed between the annular body and back wall.

References Cited (Backward Citations)

US1430327A Cited
US986663A Cited
CH122807A Cited
US1629253A Cited
US1864647A Cited
US1849125A Cited
US2103328A Cited
US2157265A Cited
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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) 1987-03-20 1987-09-19 1988-03-20 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1991-03-20 1991-09-19 1992-03-20 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1995-03-20 1995-09-19 1996-03-20 $7700.00 Window Closed / Lapsed

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