US3682390A - Liquid atomizing devices - Google Patents

Liquid atomizing devices Download PDF

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Publication number
US3682390A
US3682390A US36802A US3682390DA US3682390A US 3682390 A US3682390 A US 3682390A US 36802 A US36802 A US 36802A US 3682390D A US3682390D A US 3682390DA US 3682390 A US3682390 A US 3682390A
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Prior art keywords
passages
blades
passage means
air
supplied
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Expired - Lifetime
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US36802A
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Alan Gillingham Cheshire
Harold Place
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ZF International UK Ltd
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Lucas Industries Ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/02Spray pistols; Apparatus for discharge
    • B05B7/10Spray pistols; Apparatus for discharge producing a swirling discharge
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B7/00Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
    • B05B7/02Spray pistols; Apparatus for discharge
    • B05B7/04Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge
    • B05B7/0416Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid
    • B05B7/0433Spray pistols; Apparatus for discharge with arrangements for mixing liquids or other fluent materials before discharge with arrangements for mixing one gas and one liquid with one inner conduit of gas surrounded by an external conduit of liquid upstream the mixing chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour

Definitions

  • This invention relates to a liquid atomizing device intended particularly for use in the burners of gas turbine engines.
  • a liquid atomizing device in accordance with the invention comprises a tubular body through which air is. caused to flow in use, an air swirler at the downstream end of said body including a plurality of blades inclined to the axis of said body, a plurality of passages being formed in said blades and extending adjacent the respective trailing edges thereof, each such passage communicating with one or more transverse holes in the associated blade, and passage means whereby liquid can be supplied to said passages, with the arrangement being such that in use, liquid supplied to said passages is injected transversely into the swirling air stream through said holes.
  • FIG. 1 is a view of a liquid atomizing device in accordance with the invention, the view being partially in longitudinal section,
  • FIG. 2 is an end view of the device, also partially in section and FIG. 3 is a developed cross-section on line 3--3 in FIG. 2.
  • the device shown includes a tubular body comprising an outer sleeve 11 and an inner sleeve 12 between which there is defined an annular passage means 13 communicating with an inlet 14 ina support 15 for the body 10.
  • a tubular body comprising an outer sleeve 11 and an inner sleeve 12 between which there is defined an annular passage means 13 communicating with an inlet 14 ina support 15 for the body 10.
  • the support 15 i.e., the end which will be downstream 10 so that air flowing through the body 10 is given a swirling motion thereby to create a conically expanding air flow pattern immediately downstream of the body.
  • Each of the blades 17 is formed with a drilling 18 extending adjacent the trailing edge of the associated blade with such drilling communicating at its outer end with the annular passage 13.
  • One or more cross bores 19 is or are formed in each of the blades 17 to communicate with the drilling 18 therein.
  • there is an air swirler 16 comprising a plurality of blades 17 which are inclined to the axis of the body shown, there are three such cross bores in each blade and these open onto the face of the blade which will, in use, be at high pressure, as will be evident from FIG. 3.
  • liquid is injected into the swirling air stream through the holes fonned by the cross bores 19. It is intended that such an arrangement will be effective in atomizing the liquid over a wide range of liquid supply pressures and air flow rates through the body 10. Such a characteristic is required in the burners of a gas turbine engine to ensure effective atomization during starting when the fuel pressure is low and the air flow rate through the body 10 will similarly be low.
  • llAliaur t ue atomizing device or positioning man airstream comprising a tubular body which is open at both ends and through which air is caused to flow in use, an air swirl at the downstream end of said body including a plurality of blades inclined to the axis of said body, a plurality of passages being formed in said blades and extending adjacent the respective trailing edges thereof, a hole opening onto the face of each blade which is, in use, at high pressure, said passages communicating with said holes, and passage means whereby liquid fuel can be supplied to said passages, the arrangement being such that in use, liquid fuel supplied to said passages is injected transversely into the swirling airstream through said holes, the body comprising an outer sleeve and an inner sleeve which between them define said passage means.
  • each said passage communicates at its outer end with the said passage means.

Abstract

A liquid atomizing device in which a tubular body is open at both ends and has inclined blades mounted within one end to impart a swirling motion to air passing through the body. Fuel is supplied through passages which open on to the downstream edges of the blades, with the fuel being injected transversely into the swirling airstream.

Description

United States Patent Cheshire et a1.
[54] LIQUID ATOMIZING DEVICES [72] Inventors: Alan Gillingham Cheshire, Bumley,
Lancashire; Harold Place, Accn'ngton; both of Englandj a v [73] Assignee: Joseph Lucas (Industries) Limited [22] Filed: May 13, 1970 [21] Appl. No.: 36,802
[52] US. Cl ..239/399 [51] Int. Cl. ..B05b 7/10 [58] Field of Search ..239/399, 403, 400
[56] References Cited UNITED STATES PATENTS Zink ..239/4oo x [151 3,682,390 [4s] Aug. 8, 1972 3,231,201 1/1966 Jackson ..239/399 2,815,982 12/1957 Blearnaster ..239/403X Primary Examiner-Allen N. Knowles Assistant Examiner-Thomas C. Culp, Jr. Attomey-Holman & Stern ABSTRACT A liquid atomizing device in which a tubular body is open at both ends and has inclined blades mounted within one end to impart a swirling motion to air passing through the body. Fuel is supplied through passages which open on to the downstream edges of the blades, with the fuel being injected transversely into the swirling airstream.
2Clains,3DrawingFigures LIQUID ATOMIZING DEVICES BACKGROUND OF THE INVENTION This invention relates to a liquid atomizing device intended particularly for use in the burners of gas turbine engines.
SUMMARY OF THE INVENTION A liquid atomizing device in accordance with the invention comprises a tubular body through which air is. caused to flow in use, an air swirler at the downstream end of said body including a plurality of blades inclined to the axis of said body, a plurality of passages being formed in said blades and extending adjacent the respective trailing edges thereof, each such passage communicating with one or more transverse holes in the associated blade, and passage means whereby liquid can be supplied to said passages, with the arrangement being such that in use, liquid supplied to said passages is injected transversely into the swirling air stream through said holes.
BRIEF DESCRIPTION OF THE DRAWINGS An example of the invention isshown in the accompanying drawings in which FIG. 1 is a view of a liquid atomizing device in accordance with the invention, the view being partially in longitudinal section,
FIG. 2 is an end view of the device, also partially in section and FIG. 3 is a developed cross-section on line 3--3 in FIG. 2.
DETAILED DESCRIPTION OF THE DRAWINGS The device shown includes a tubular body comprising an outer sleeve 11 and an inner sleeve 12 between which there is defined an annular passage means 13 communicating with an inlet 14 ina support 15 for the body 10. At the end of the body remote from the support 15 (i.e., the end which will be downstream 10 so that air flowing through the body 10 is given a swirling motion thereby to create a conically expanding air flow pattern immediately downstream of the body.
Each of the blades 17 is formed with a drilling 18 extending adjacent the trailing edge of the associated blade with such drilling communicating at its outer end with the annular passage 13. One or more cross bores 19 is or are formed in each of the blades 17 to communicate with the drilling 18 therein. In the example in use), there is an air swirler 16 comprising a plurality of blades 17 which are inclined to the axis of the body shown, there are three such cross bores in each blade and these open onto the face of the blade which will, in use, be at high pressure, as will be evident from FIG. 3.
Thus, in use, liquid is injected into the swirling air stream through the holes fonned by the cross bores 19. It is intended that such an arrangement will be effective in atomizing the liquid over a wide range of liquid supply pressures and air flow rates through the body 10. Such a characteristic is required in the burners of a gas turbine engine to ensure effective atomization during starting when the fuel pressure is low and the air flow rate through the body 10 will similarly be low.
Having thus described our invention what we claim as ew d, e ir to secureb Lette Patentis;
llAliaur t ue atomizing device or positioning man airstream, comprising a tubular body which is open at both ends and through which air is caused to flow in use, an air swirl at the downstream end of said body including a plurality of blades inclined to the axis of said body, a plurality of passages being formed in said blades and extending adjacent the respective trailing edges thereof, a hole opening onto the face of each blade which is, in use, at high pressure, said passages communicating with said holes, and passage means whereby liquid fuel can be supplied to said passages, the arrangement being such that in use, liquid fuel supplied to said passages is injected transversely into the swirling airstream through said holes, the body comprising an outer sleeve and an inner sleeve which between them define said passage means.
2. The device as claimed in claim 1 in which each said passage communicates at its outer end with the said passage means.

Claims (2)

1. A liquid fuel atomizing device for positioning in an airstream, comprising a tubular body which is open at both ends and through which air is caused to flow in use, an air swirl at The downstream end of said body including a plurality of blades inclined to the axis of said body, a plurality of passages being formed in said blades and extending adjacent the respective trailing edges thereof, a hole opening onto the face of each blade which is, in use, at high pressure, said passages communicating with said holes, and passage means whereby liquid fuel can be supplied to said passages, the arrangement being such that in use, liquid fuel supplied to said passages is injected transversely into the swirling airstream through said holes, the body comprising an outer sleeve and an inner sleeve which between them define said passage means.
2. The device as claimed in claim 1 in which each said passage communicates at its outer end with the said passage means.
US36802A 1970-05-13 1970-05-13 Liquid atomizing devices Expired - Lifetime US3682390A (en)

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4276867A (en) * 1979-03-19 1981-07-07 Metzenthin Dieter W Fuel atomizing device
US5647200A (en) * 1993-04-08 1997-07-15 Asea Brown Boveri Ag Heat generator
US5772422A (en) * 1996-08-27 1998-06-30 Pvi Industries, Inc. Burner array for water heating apparatus
US6227185B1 (en) * 1999-03-01 2001-05-08 Edward J. Spracher Air intake conduit fuel metering device
US6363724B1 (en) 2000-08-31 2002-04-02 General Electric Company Gas only nozzle fuel tip
US6438961B2 (en) 1998-02-10 2002-08-27 General Electric Company Swozzle based burner tube premixer including inlet air conditioner for low emissions combustion
US20030121266A1 (en) * 2001-12-21 2003-07-03 Roberto Modi Main liquid fuel injection device for a single combustion chamber, having a premixing chamber, of a gas turbine with low emission of pollutants
US6655145B2 (en) * 2001-12-20 2003-12-02 Solar Turbings Inc Fuel nozzle for a gas turbine engine
US6820424B2 (en) * 2001-09-12 2004-11-23 Allison Advanced Development Company Combustor module
US20050045745A1 (en) * 2003-08-13 2005-03-03 Unilever Home & Personal Care Usa, Division Of Conopco, Inc. Domestic spray device
US20050223710A1 (en) * 2004-04-07 2005-10-13 Creighton Sherman C Swirler
US20070074517A1 (en) * 2005-09-30 2007-04-05 Solar Turbines Incorporated Fuel nozzle having swirler-integrated radial fuel jet
US7232080B2 (en) 2003-08-13 2007-06-19 Unilever Home & Personal Care Usa Division Of Conopco, Inc. Nozzle for a spray device

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2531316A (en) * 1946-08-09 1950-11-21 John S Zink Multiple fuel burner
US2815982A (en) * 1953-11-06 1957-12-10 William R Graham Apparatus for dispelling fog
US3231201A (en) * 1963-04-29 1966-01-25 Magic Servant Products Company Burner assembly

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2531316A (en) * 1946-08-09 1950-11-21 John S Zink Multiple fuel burner
US2815982A (en) * 1953-11-06 1957-12-10 William R Graham Apparatus for dispelling fog
US3231201A (en) * 1963-04-29 1966-01-25 Magic Servant Products Company Burner assembly

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4276867A (en) * 1979-03-19 1981-07-07 Metzenthin Dieter W Fuel atomizing device
US5647200A (en) * 1993-04-08 1997-07-15 Asea Brown Boveri Ag Heat generator
US5772422A (en) * 1996-08-27 1998-06-30 Pvi Industries, Inc. Burner array for water heating apparatus
US6438961B2 (en) 1998-02-10 2002-08-27 General Electric Company Swozzle based burner tube premixer including inlet air conditioner for low emissions combustion
US6227185B1 (en) * 1999-03-01 2001-05-08 Edward J. Spracher Air intake conduit fuel metering device
US6363724B1 (en) 2000-08-31 2002-04-02 General Electric Company Gas only nozzle fuel tip
US6453673B1 (en) 2000-08-31 2002-09-24 General Electric Company Method of cooling gas only nozzle fuel tip
US6460326B2 (en) 2000-08-31 2002-10-08 William Theodore Bechtel Gas only nozzle
US6820424B2 (en) * 2001-09-12 2004-11-23 Allison Advanced Development Company Combustor module
US6655145B2 (en) * 2001-12-20 2003-12-02 Solar Turbings Inc Fuel nozzle for a gas turbine engine
US20030121266A1 (en) * 2001-12-21 2003-07-03 Roberto Modi Main liquid fuel injection device for a single combustion chamber, having a premixing chamber, of a gas turbine with low emission of pollutants
US6834506B2 (en) * 2001-12-21 2004-12-28 Nuovo Pignone Holding S.P.A. Main liquid fuel injection device for a single combustion chamber, having a premixing chamber, of a gas turbine with low emission of pollutants
US20050045745A1 (en) * 2003-08-13 2005-03-03 Unilever Home & Personal Care Usa, Division Of Conopco, Inc. Domestic spray device
US7191959B2 (en) * 2003-08-13 2007-03-20 Unilever Home & Personal Care Usa Division Of Conopco, Inc. Domestic spray device
US7232080B2 (en) 2003-08-13 2007-06-19 Unilever Home & Personal Care Usa Division Of Conopco, Inc. Nozzle for a spray device
US20050223710A1 (en) * 2004-04-07 2005-10-13 Creighton Sherman C Swirler
US7334410B2 (en) * 2004-04-07 2008-02-26 United Technologies Corporation Swirler
US20070074517A1 (en) * 2005-09-30 2007-04-05 Solar Turbines Incorporated Fuel nozzle having swirler-integrated radial fuel jet
US7703288B2 (en) * 2005-09-30 2010-04-27 Solar Turbines Inc. Fuel nozzle having swirler-integrated radial fuel jet

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