[0001] This invention relates to gas burner tips.
[0002] There are furnace burner arrangements in which combustion air is discharged in a
vortex through a ring of burner tips from which combustion gas is discharged. Frequently,
this vortex is unstable in that it precesses about the axis resulting in circumferential
variations in air flow. A consequence is that the combination of the gas with air
is not regular, resulting in combustion pulsations. If the acoustic frequency of the
furnace is such that Rayleigh's criterion is satisfied, then the combustion pulsations
may be sustained, leading to excessive furnace vibrations.
[0003] The present invention arose from a consideration of this problem and of ways in which
more regular combustion might be obtained.
[0004] According to the present invention, there is provided a gas burner tip in the form
of a cylinder closed at one end except for an opening in an end wall that is oblique
to the cylindrical surface and having an opening of smaller area lying wholly in the
part of the cylindrical wall that is defined by a diametrical plane across which the
end wall lies symmetrically.
[0005] An embodiment of the invention will now be described with reference to the accompanying
drawings in which
Figure 1 shows a gas burner tip in side view;
Figure 2 shown the burner tip of Figure 1 from above; and
Figure 3 illustrates an end view, from inside the furnace, of a burner mounted at
an opening in a furnace wall.
[0006] The tip A shown in Figure 1 has a barrel 1 of which the outer diameter is about 27mm.
Its length is about 70mm and at the lower end is a mounting flange 2. Centrally, at
its upper end, there is a ridge 3 about 8mm wide and flat end walls 4 and 5 slope
down symmetrically from the sides of the ridge 3 at about 45°.
[0007] In one of the end walls 5 is a circular opening 8 of just over 20mm diameter. A circular
opening 9 of smaller diameter, 15mm, is formed in the cylindrical wall of the barrel
about half way between the ridge 3 and the top of the flange 2. The diametrical plane
of the barrel 1 that contains the centre of the opening 8 is displaced from that which
contains the centre of the opening 9 by 22½°. The opening 9 thus lies wholly within
the diametrical plane of the barrel 1 that bisects the ridge 3 and across which the
end wall 5 lies symmetrically.
[0008] Figure 3, shows six burner tips mounted in the opening 10 in the wall of a furnace.
The boundary of they opening 10 tapers from a circle 11 in the inner face of the wall
to a circle 12 in the outer face. Ourwardly from the outer face of the furnace wall.there
extends a duct (not shown) through which air can flow to discharge through the opening
10 with a swirl in the anticlockwise direction. An oil burner 13 is arranged to discharge
centrally through the opening 10, the outlet end of the burner 14 being about mid-way
between the faces of the furnace wall.
[0009] A group of six gas burner tips A,connected to a common main (not shown) lying outside
the furnace, are disposed equi-spaced around a circle that is concentric with the
burner 14, the leading ends of the burner tips A lying forward of the oil burner 14
but rearwardly of the inner face of the furnace wall. Three of the tips, A1, are so
arranged that gas discharging from the upper opening, 8, is discharged approximately
towards the axis, but at a slight angle so that the gas has a swirl in the clockwise
direction. Gas discharging from the lower openings 9 will be more oblique to the axis
but will also swirl in the clockwise direction.
[0010] The other three tips, A2, are each disposed between two of the tips A1 and are arranged
so that gas discharging from both the openings of each will have an anticlockwise
direction of rotation and flow past, outwardly of, the tips A1.
[0011] An effect of the rotation of the gas will be to tend to constrain the air to flow
symmetrically about the axis of the burner and so tend to decouple the zone in which
gas and air is mixed and burned from the aerodynamically unstable region. The combustion
zone will tend better to resemble the combustion produced by an axial oil burner so
that gas and oil may be burned together to give a dual firing burner i.e. a burner
in which the two fuels may be burnt.
[0012] Since the combustion in the pure gas burner is similar to the oil flame, mixed firing
- with neighbouring burners using only gas and only oil - is easily attained. Also,
the detailed residual pulsation levels of the burners firing only gas and only oil
are not enhanced by burner interaction and hence the residual pulsation levels are
lower than for single-fuel firing. Dual firing broadens the air-fuel delay time involved
in the combustion, effectively dampening any tendencies to pulsate, but the periphery
of the flame is predominantly gas controlled still producing some burner interaction.
The residual pulsation levels for dual firing therefore lie between the single fuel
and mixed firing uses.
[0013] In use of the tips that have been described,the flame will tend to be removed from
the point of fuel injection so that the stabilising discs that are often provided
on gas spuds may be dispensable. A benefit of this would be the resultant lower air
velocities.
[0014] In modifications of the burner tip, it is envisaged that the opening 9 may be replaced
by two or more openings in the part of the wall that is defined by a diametrical plane
across which the end wall 5 lies symmetrically.
[0015] Other arrangements of the tips are also envisaged. In particular, all tips in a ring
may be similarly orientated in the way that the tips A1 are orientated. Whilst gas
from these tips is directed inwardly, none is directed directly to the axis, but at
an angle such as to tend to induce orderly swirl.
1. A gas burner tip in the form of a cylinder closed at one end except for an opening
in an end wall that is oblique to the cylindrical surface and having an opening of
smaller area lying wholly in the part of the cylindrical wall that is defined by a
diametrical plane across which the end wall lies symmetrically.
2. A gas burner tip as claimed in claim 1 in which the holes are both circular and
the diametrical plane containing the centre diametrical plane containing the centre
of the hole in the end wall is displaced from the diametrical plane containing the
centre of the hole in the cylindrical wall.
3 A gas burner tip as claimed in claim 2 in which the angle between the planes is
223°.
4. A gas burner comprising a cylindrical duct and means associated with the duct by
which air can be caused to flow along the duct with a swirling motion, and a plurality
of gas tips as claimed in any of claims 1 to 3 disposed concentrically around the
axis of the duct, uniformly spaced from each other and all similarly orientated so
that the gas from both openings of each is directed counter to the direction of swirl
of the air.
5. A gas burner as claimed in claim 4 in which there is interspersed with the tips
specified in claim 4 another set of tips, each disposed mid-way between an adjacent
pair of the tips specified in claim 4, the tips of the second set being all similarly
orientated so that gas from both openings of each is directed past, outwardly of the
tips specified in claim 4, and in the direction of the swirl of the air.