GB2084903A - Atomising liquid fuel - Google Patents

Atomising liquid fuel Download PDF

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Publication number
GB2084903A
GB2084903A GB8130918A GB8130918A GB2084903A GB 2084903 A GB2084903 A GB 2084903A GB 8130918 A GB8130918 A GB 8130918A GB 8130918 A GB8130918 A GB 8130918A GB 2084903 A GB2084903 A GB 2084903A
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GB
United Kingdom
Prior art keywords
oil
mixing chamber
ports
burner
atomiser
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB8130918A
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GB2084903B (en
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Central Electricity Generating Board
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Central Electricity Generating Board
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Filing date
Publication date
Application filed by Central Electricity Generating Board filed Critical Central Electricity Generating Board
Priority to GB8130918A priority Critical patent/GB2084903B/en
Publication of GB2084903A publication Critical patent/GB2084903A/en
Application granted granted Critical
Publication of GB2084903B publication Critical patent/GB2084903B/en
Expired legal-status Critical Current

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Classifications

    • 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
    • F23D11/101Burners 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 medium and fuel meeting before the burner outlet
    • F23D11/102Burners 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 medium and fuel meeting before the burner outlet in an internal mixing chamber
    • F23D11/103Burners 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 medium and fuel meeting before the burner outlet in an internal mixing chamber with means creating a swirl inside the mixing chamber

Abstract

An atomiser for use in an oil burner comprises a cap 16 screwed onto a body member 10 to define an annular mixing chamber 15 with a plurality of exit ports 14 to give a conical spray of oil droplets. One of the oil and the atomising fluid may be fed through a central passage through the body and the other through an annular passage or passages into the mixing chamber. The oil ports are arranged to produce toroidal recirculation in the annular mixing chamber and the atomising fluid is injected into the mixing chamber at a plurality of positions to give good mixing. <IMAGE>

Description

SPECIFICATION Fuel atomisers for oil burners This invention relates to oil fuel atomisers for use in oil burners.
A common practice in oil burners for large boilers is to use atomisers of the Yiet type in which a number of ports are arranged at an angle to the burner axis to produce a hollow conical spray. Each exit port has a co-axial atomising fluid port for injection of the atomising fluid (which may be steam or air) and also has an oil port entering at an angle. A degree of mixing between the atomising fluid and oil takes place in the exit port and the two phase mixture then expands out of the exit port to form a spray. One of the problems with this type of atomiser is that the jet of oil from the oil port tends to impinge on the opposite side of the exit port where it forms a thick film.
This thick film can persist through the exit port to the end thereof and hence lead to the formation of relatively large oil droplets.
In British Patent Specification No, 1470671 there is described an atomiser in which the oil is introduced into the exit ports either axisymmetrically (that is symmetrical with regard to the axis of the exit port) through an annular port or symmetrically through a number of discrete oil ports. This arrangement prevents the formation of a thick asymmetric oil film. In the construction described in the aforementioned specification the ports are formed as a number of inserts which are mounted in a unitary body. This construction gives a significant improvement in performance over a Y-jet but there can be problems in the cleaning of this type of atomiser.
In accordance with the present invention a multi-jet atomiser for an oil burner comprises a body having a plurality of exit ports leading outwardly from an annular mixing chamber to form a conical spray, means for injecting oil through oil inlet ports into the mixing chamber, the oil being injected at each inlet port in a direction to produce a toroidal recirculation in the annular mixing chamber with the injected oil from each inlet port passing close to an exit port at approximately right angles to the axis of that exit port and means for injecting an atomising fluid into the mixing chamber at a plurality of positions in a wall of the mixing chamber.
With this construction, the atomising fluid is injected into a turbulent recirculating flow region through ports in the wall of the mixing chamber opposite the exit ports. The atomising fluid thus becomes well mixed with the oil and carries part of the recirculating mixture into the exit ports in the appropriate directions to pass through these ports and to expand outwardly therefrom as a fine spray.
Conveniently there is provided a plenum chamber or a plurality of plenum chambers through which the oil is fed into the aformentioned oil inlet ports.
The aforementioned annular mixing chamber preferably has a curved surface opposite each oil injection port shaped to direct the impinging oil around a curved path towards the axis of the burner assembly and hence to promote the toroidal recirculation.
The aforesaid means for injecting an atomising fluid into the mixing chamber may be at a plurality of positions in a wall of the mixing chamber opposite the exit ports.
The mixing chamber may have walls shaped to guide the injected oil in a direction across the exit ports and thence around in a recirculatory path over the wall opposite the exit ports.
Conveniently the annular mixing chamber and, if provided, the plenum chamber or chambers are constituted by regions between the end of a main burner body element containing a central atomising fluid passage extending axially through the body element to atomising fluid injection ports in the end thereof and a cap which is secured, e.g.
threaded, onto the main burner body element and which has the aforesaid exit ports.
Alternatively the main burner body element may contain a central oil passage extending axially through the body element to said oil inlet ports. In this case the atomising fluid is passed through passages around the central oil passage.
The following is a description of a number of embodiments of the invention, reference being made to the accompanying drawings in which: Figure 1 is a front elevation of an atomiser for an oil burner; Figure 2 is a section along the line 2-2 of Fig. 1 through the front part of the burner, showing the atomiser; and Figures 3, 4 and 5 are sections, similar to Fig. 2, through the front parts of burners forming further embodiments of the invention.
Referring to Figs. 1 and 2, the atomiser has a main elongate body member 10 with a central passage 11 extending axially through the member 10 towards the end thereof to carry an atomising fluid, either steam or air.
This passage 11 terminates in a frusto-conical face 1 2 from which a number of ports 1 3 extend, these ports leading into an annular mixing chamber 1 5. This mixing chamber has a plurality of exit ports 14 as seen most clearly in Fig. 1. These ports 14 are formed in cap member 16, internally threaded at 17, which fits over the end of the body member 1 0. In the particular embodiment, the ports 1 3 and the ports 1 4 are at angles of about 45 to the axis of the assembly. These ports 1 3 and 14 need not necessarily be at the same angle to the axis of the assembly.The angles for the exit ports 14 would depend on the deisred cone angle of the spray. in some cases it may be preferred to make the inlet ports 1 3 parallel to the axis of the assembly.
Oil from an annular region 20 around the outside of the body member 10 passes through a plurality of oil ducts 21 in the cap member 16, into an annular plenum chamber 22. From the plenum chamber, the oil is injected into a mixing chamber 1 5 through a ring of ports 23 through an upstanding part 24 in the body member 1 0. The injection from the ports 23 into the mixing chamber is in a direction such as to produce a toroidal circulation of the oil in the mixing chamber 1 5. The oil ports 23 are arranged to produce oil jets which pass close to the exit ports 1 4 at approximately right angles to the axis of the exit ports.These oil jets are directed towards a curved surface 25 of the mixing chamber, this surface being shaped so that the oil is diverted around a curved path inwardly towards the axis of the burner assembly. This shaping facilitates the recirculation of the injected oil. It will be seen that the atomising fluid is injected through the ports 1 3 into the mixing chamber at an angle to the direction of injection of the oil through ports 23. In the mixing chamber, the atomising fluid becomes well mixed with the oil. In the particular example illustrated two rows of ports 1 3 are provided for injection of the atomising fluid.
The oil is injected at ports 23 in the form of oil jets. A proportion of the recirculating mixture will emerge from the mixing chamber 1 5 through the interstices between these oil jets and will pass out through the exit ports 14 as a two-phase mixture with expands out of these ports to form a fine spray.
The plenum chamber 22 and mixing chamber 1 5 are formed as gaps between the cap member 16 and the main body member 10.
The shaping of these members 1 0, 1 6 is such that, when the cap member is screwed in position on the body member, the gaps between the cap member and body member form the mixing chamber and plenum chamber. By providing a plenum chamber 22, there need not be equal numbers of ducts 21 and ports 23 and they do not have to be accurately aligned on assembly.
The exit ports 14 have their axes defining a cone, the axis of this cone being aligned with the longitudinal axis of the burner and the apex of the cone being on that longitudinal axis. The oil spray from the plurality of exit ports 14 thus is in the general form of a hollow cone. In the mixing chamber 1 5 the atomising fluid is injected through ports on the opposite wall of the chamber, that is the wall facing the exit ports. This wall is conical.
It is not necessary in this construction however that the cap member 1 6 is angularly aligned with respect to the body element 10.
Alignment of the injection ports and exit ports is not critical and, in the particular embodiment illustrated, there are two rows of injection ports 1 3 and one row of exit ports 14.
The fluid entering the exit ports is well mixed in the mixing chamber and is forced into the exit ports. This construction gives good atomisation.
The simple construction having a cap 1 6 screwed onto the body member 10 enables the atomiser to be easily cleaned after these parts are separated.
In the above-described embodiment, the exit ports 14 are evenly spaced with their axes lying on the same cone. In some cases, however, it may be advantageous to have these exit ports on more than one cone. The ports 14 need not necessarily be evenly spaced; they may be irregularly spaced or grouped.
In Figs. 1 and 2, the atomising fluid ports are directly opposite and pointing towards the exit ports. Fig. 2 illustrates a modification of that construction and the same reference characters are used to indicate corresponding components. In Fig. 3 the atomising fluid inlets to the mixing chamber, as shown at 30, produce atomising fluid jets which tend to counter the toroidal circulation produced by the oil jets 23. This may be advantageous in some cases to enhance mixing with the oil. In this construction, because the inlets to the atomising fluid ports 30 are at a greater distance from the atomiser axis than in the arrangement of Figs. 1 and 2, it is easier to provide the requisite number of ports.
In the constructions of Figs. 1, 2 and 3, the atomising fluid is fed axially through a central passage 11 in the main burner body 10. In some cases, as shown in Figs. 4 and 5, it may be preferred to reverse the position of the oil and atomising fluid feeds, the oil feed being axially through a passage 41 and the atomising fluid being from an annular region 42 around the outside of the body member 10. This arrangement makes the incorporation of sufficient atomising fluid port area much easier by locating these ports as far as possible from the atomiser axis. The fact that the oil ports shown at 43 in Fig. 4 are now much closer to the axis is not too much of an imposition because the total oil port area is generally significantly less than the total atomising fluid port area.
Fig. 5 illustrates a modification of Fig. 4 in which the oil ports, shown at 50, are approximately parallel to the atomiser axis. The mixing chamber wall is shaped to direct the oil jets across the approach region to the exit ports. This arrangement may simplify manufacture.

Claims (11)

1. A multi-jet atomiser for an oil burner comprising a body having a plurality of exit ports leading outwardly from an annular mixing chamber to form a conical spray, means for injecting oil through oil inlet ports into the mixing chamber, the oil being injected at each oil inlet port in a direction to produce a toroidal recirculation in the annular mixing chamber with the injected oil from each inlet port passing close to an exit port at approximately right angles to the axis of the exit port and means for injecting an atomising fluid into the mixing chamber at a plurality of positions in a wall of the mixing chamber.
2. A multi-jet atomiser as claimed in claim 1 wherein said means for injecting an atomising fluid into the mixing chamber are at a plurality of positions in a wall of the mixing chamber opposite the exit ports.
3. A multi-jet atomiser as claimed in claim 1 wherein the mixing chamber has walls shaped to guide the injected oil in a direction across the exit ports and thence around in a recirculatory path over the wall opposite the exit ports.
4. A multi-jet atomiser for an oil burner as claimed in any one of the preceding claims and having a plenum chamber or a plurality of plenum chambers through which the oil is fed into said oil inlet ports.
5. A multi-jet atomiser for an oil burner as claimed in any of the preceding claims wherein the annular mixing chamber is constituted by regions between the end of a main burner body element containing a central atomising fluid passage extending axially through the body element to atomising fluid injection ports in the end thereof and a cap which is secured onto the main burner body element and which has the said exit ports.
6. A multi-jet atomiser for an oil burner as claimed in any of claims 1 to 3 and having a plenum chamber or a plurality of plenum chambers through which the atomising fluid is fed into the mixing chamber.
7. A multi-jet atomiser for an oil burner as claimed in any of claims 1 to 4 or 6 wherein the annular mixing chamber is constituted by regions between the end of a main burner body element containing a central oil passage extending axially through the body element to said oil inlet ports and a cap which is secured onto the main burner body element and which has said exit ports.
8. A multi-jet atomiser as claimed in claim 5 as appendant to claim 6 wherein said cap and said main burner body element have cooperating surfaces defining said plenum chamber or chambers.
9. A multi-jet atomiser for an oil burner as claimed in any of the preceding claims wherein said annular mixing chamber has a curved surface opposite each oil inlet port shaped to direct the impinging oil around a curved path towards the axis of the burner assembly and hence to promote the toroidal recirculation.
1 0. A multi-jet atomiser as claimed in any of the preceding claims wherein said exit ports comprise a plurality of ports evenly spaced around the longitudinal axis of the burner, the axes of the ports defining a conical surface symmetrically around and with its apex on said longitudinal axis.
11. A multi-jet atomiser for an oil burner substantially as hereinbefore described with reference to Figs. 1 and 2 or Fig. 3 or Fig. 4 or Fig. 5 of the accompanying drawings.
GB8130918A 1980-10-13 1981-10-13 Atomising liquid fuel Expired GB2084903B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8130918A GB2084903B (en) 1980-10-13 1981-10-13 Atomising liquid fuel

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8032981 1980-10-13
GB8130918A GB2084903B (en) 1980-10-13 1981-10-13 Atomising liquid fuel

Publications (2)

Publication Number Publication Date
GB2084903A true GB2084903A (en) 1982-04-21
GB2084903B GB2084903B (en) 1984-05-31

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4946105A (en) * 1988-04-12 1990-08-07 United Technologies Corporation Fuel nozzle for gas turbine engine
US5014790A (en) * 1987-10-24 1991-05-14 The British Petroleum Company Plc Method and apparatus for fire control
WO2004055434A1 (en) * 2002-12-17 2004-07-01 Pratt & Whitney Canada Corp. Vortex fuel nozzle to reduce noise levels and improve mixing
JP2008096100A (en) * 2006-10-06 2008-04-24 Snecma Fuel injector for combustion chamber of gas turbine engine
CN101811101A (en) * 2010-04-23 2010-08-25 常州世方国际贸易有限公司 Atomizing nozzle and ejector thereof

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5014790A (en) * 1987-10-24 1991-05-14 The British Petroleum Company Plc Method and apparatus for fire control
US4946105A (en) * 1988-04-12 1990-08-07 United Technologies Corporation Fuel nozzle for gas turbine engine
WO2004055434A1 (en) * 2002-12-17 2004-07-01 Pratt & Whitney Canada Corp. Vortex fuel nozzle to reduce noise levels and improve mixing
JP2008096100A (en) * 2006-10-06 2008-04-24 Snecma Fuel injector for combustion chamber of gas turbine engine
CN101811101A (en) * 2010-04-23 2010-08-25 常州世方国际贸易有限公司 Atomizing nozzle and ejector thereof

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Publication number Publication date
GB2084903B (en) 1984-05-31

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PCNP Patent ceased through non-payment of renewal fee

Effective date: 20001013