[0001] This invention relates to heating apparatus and is particularly concerned with a
space heater useful for heating large spaces, such as factory interiors.
[0002] According to the invention, heating apparatus comprises a fuel injection device arranged
to discharge fuel into a combustion region for combustion by a burner, means operable
to supply fuel in a liquid state under pressure to a gasifying means from which the
fuel is supplied to the injection device in a state such that it emerges into the
combustion region in a substantially gasified state, and igniter means operable to
ignite the gasified fuel for burning in the combustion region.
[0003] Preferably, the gasifying means is a heater for raising the temperature of the fuel
to a value at which the fuel emerges from the injection device in a substantially
gasified state.
[0004] The burner is preferably provided with a plurality of burner nozzles to which distinct
fuel supplies are connected, in use, one nozzle being connected to said gasified fuel
supply. The other nozzle may be connected to a separate gas supply, enabling either
or both of said supplies to be used, as required.
[0005] In a preferred arrangement, flow means are provided to produce a flow of external
air into the combustion region.
[0006] In one typical arrangement, the combustion region is formed adjacent the inlet end
of an elongate combustion conduit, from the outlet end of which heated air and combustion
products are expelled by a first flow means, further flow means being provided adjacent
said outlet end and being operable to enhance gas flow along the conduit from the
inlet end to the outlet end.
[0007] Preferably, both of the flow means, and conveniently also the fuel supply means,
typically a pump, are driven from a single motive device which may conveniently be
an electric motor.
[0008] The invention will now be described, by way of example, with reference to the accompanying
drawings, in which:-
Figure 1 is an end view of one form of space heating apparatus of the invention;
Figure 2 is a side view of the apparatus of Figure 1;
Figure 3 illustrates an alternative form of space heating apparatus incorporating
alternative fuel supplies, and
Figure 4 illustrates, to an enlarged scale, one form of the burner used in the apparatus
of the invention.
[0009] Referring to Figures 1 and 2, the space heating apparatus shown therein has a casing
1 which supports a generally U-shaped burner tube, of which the inlet end is illustrated
at 2 and the outlet end at 3. Mounted on the upper part of the casing 1 is an air
inlet fan 4 which draws in air as indicated by the arrows A, and expels it along a
duct 5 connecting the fan to the inlet end 2 of the burner tube. The housing 1 also
mounts an exhaust fan 6 connected by a duct 12 to the outlet end 3 of the burner tube
and acting to draw exhaust gases towards the outlet 3.
[0010] The fans 4 and 6 are both connected to a single drive means in the form of an electric
motor 7 disposed therebetween and mounted on the casing 1. Drive from the motor 7
is transmitted via the inlet fan 4 to a fuel pump 8 from which fuel oil is fed, in
the illustrated arrangement, to a fuel heater 9 and thence to a burner injector nozzle
10. A pair of igniter electrodes 11 are disposed in the vicinity of the burner 10.
[0011] The sizes and operating characteristics of the fans 4 and 6 are chosen so that they
provide the correct ratio between inlet air and exhaust gas flow when driven at the
same speed by the motor 7. It would, however be possible to drive the fans at different
speeds, using suitable gear transmissions, or to provide suitable throttling means
for the fans which may be adjustable to enable the flow rate ratio to be varied. Similarly,
the pump 8 is such as to provide a suitable flow rate at a desired pressure when driven
at the same speed as the fans from a common drive shaft, as in the illustrated arrangement
It would, however be possible to drive the pump via a gear transmission which may
provide a variable ratio.
[0012] Oil fed to the heater 9 is heated to raise its temperature above atmospheric boiling
point and the feed pressure produced by the pump 8 is chosen so that the heated oil
emerging from the burner nozzle 10 vaporises as it enters the combustion tube. The
fan 4 produces sufficient air flow to provide a combustible mixture when mixed with
the gasified fuel and the combustible mixture is ignited by the electrodes 11. Swirl
inducing vanes 10A are provided prior to the electrodes in conventional manner. Once
ignited, the combustion becomes self sustaining and the function of the electrodes
is then changed so that they become conducting probes which provide a continuous check
on the existence and/or nature of the flame. The exhaust fan 6 draws the combustion
products from the burner along the combustion tube and these are expelled, as indicated
by the arrow B, either along a flue to atmosphere, or for re-direction into the inlet
of the fan 4 or into a heat exchanger in which the heat may be recovered for further
use. The heater operates under the control of an electronic control unit E.
[0013] Figure 3 illustrates an alternative form of space heater similar to that of Figures
1 and 2 but in which two distinct fuel supply sources feed fuel to respective burner
nozzles 20A, 20B of the burner 20. The burner has the usual air inlet holes 20C and
swirl inducing vanes 20D, to control the flame dimensions, in conventional manner.
Liquid fuel, such as oil, is pumped from one source through a heater 9, similar to
that in the previous embodiment, or other gasifying device and thence to the nozzle
20A which emits gasified fuel into an inlet 2 of a combustion conduit for ignition
and monitoring by electrodes 11, as previously, exhaust gas being expelled through
an outlet 3, as before. Inlet and exhaust fans may be employed as previously but are
not illustrated in this embodiment. The other fuel is gas supplied via a pressure
regulating valve 21 and an electrically controlled digital proportioning valve 22
to the other burner nozzle 20B. The valve 22 is similar in construction and operation
to that described in our copending British application entitled "Flow Control Device",
to which reference is made for a full description of the valve. It will be seen that
either or both nozzles 20A, 20B may be supplied with fuel from the respective sources
so that the two fuels may be burnt simultaneously, or the fuels may be employed alternatively
depending upon the conditions. For example, it may be economically advantageous to
use one fuel or the other over a particular period. It also enables a change to be
made from one fuel to another in the event that supply difficulties occur with one
of the fuels. It can be advantageous to supply the gasified fuel also via a proportioning
valve, which may be similar to the valve 22. This enables a controlled mixture of
fuels to be burnt with the proportions of the fuels fed to the respective burners
each being variable between 0% and 100% depending upon requirements. It is possible
to switch supplies remotely, using suitable electronic control apparatus, so that
interruption of supply from one fuel source does not cause the shut down of the heater,
as can happen in many conventional types of apparatus in which it is necessary to
change burners when a change in fuel is required. Moreover, the aforesaid fuel proportioning
may additionally or alternatively be subject to remote control from the aforesaid
or another control apparatus.
[0014] It will be understood that the apparatus of the invention may take various forms
other than those described above, such as boilers and process heaters. The liquid
fuel may be gasified by means other than the heater described above for this purpose.
Gasification may be effected, for example, by pressure reduction means, although it
may then be necessary, for the achievement or satisfactory burning, to heat the gasified
fuel prior to feeding it to the burner in order to replace the latent heat lost in
the gasifying stage.
1. Heating apparatus characterised by a fuel injection device (10, 20) arranged to
discharge fuel into a combustion region for combustion by a burner, means (8) operable
to supply fuel in a liquid state under pressure to a gasifying means (9) from which
the fuel is supplied to the injection device in a state such that it emerges into
the combustion region in a substantially gasified state, and igniter means (11) operable
to ignite the gasified fuel for burning in the combustion region.
2. Heating apparatus according to Claim 1, characterised in that the gasifying means
is a heater (9) for raising the temperature of the fuel to a value at which the fuel
emerges from the injection device (10, 20) in a substantially gasified state.
3. Heating apparatus according to Claim 1 or Claim 2, characterised in that the burner
(20) is provided with a plurality of burner nozzles (20A, 20B) to which distinct fuel
supplies are connected in use, one nozzle (20A) being connected to the gasified fuel
supply.
4. Heating apparatus according to Claim 3, characterised in that the other nozzle
(20B) is connected to a separate gas supply.
5. Heating apparatus according to any one of the preceding claims, characterised in
that flow means (4) are provided to produce a flow of external air into the combustion
region.
6. Heating apparatus according to any one of claims 1 to 4, characterised in that
the combustion region is adjacent the inlet end (2) of an elongate combustion conduit,
from the outlet end (3) of which heated air and combustion products are expelled by
a first flow means (4), further flow means (6) being provided adjacent said outlet
end (3) and being operable to enhance gas flow along the conduit from the inlet end
to the outlet end.
7. Heating apparatus according to Claim 6, characterised in that both of the flow
means (4, 6) are driven from a single motive device (7).
8. Heating apparatus according to Claim 7, characterised in that the fuel supply means
(8) is also driven from the same single motive device (7).
9. Heating apparatus according to Claim 6, wherein the first flow means (4) applies
air under positive pressure into the inlet end (2) of the combustion conduit and the
further flow means (6) draws gases from the outlet end (3) of the combustion conduit.
10. Heating apparatus according to any one of claims 3 to 9, characterised in that
respective valve means (22) are provided for varying the proportions of the two fuels
supplied to the injection device.
11. Heating apparatus according to Claim 10, characterised in that the valve means
(22) are connected to a remote controller.