Liquid fuel combustion apparatus

A liquid fuel combustion apparatus comprises a combustion cylinder, a fuel reservoir, a housing, a blower and an electrical ignition heater. The reservoir is disposed inside the cylinder to store a liquid fuel supplied from outside of the cylinder. The housing is disposed outside the cylinder to create a space therebetween and has an end wall opposite to an end wall of the cylinder. The blower is disposed outside, and in a spaced apart relation to, the housing and supply air to the space. The heater is supported by the end walls and ignite liquid fuel stored in the reservoir.

BACKGROUND OF THE INVENTION 
This invention relates to a liquid fuel combustion apparatus and in 
particular to a liquid fuel combustion apparatus in which an air supply 
and discharge are forcedly effected. 
Recently, various pot-type liquid fuel combustion apparatus of the forced 
air-supply/discharge variety have been developed. In these apparatus, an 
air supply means, such as blower, supply air for combustion into a fuel 
vapor after causing liquid fuel, such as kerosene, stored in a liquid 
reservoir to be heated by the ignition of an ignition heater to produce a 
fuel vapor. And a mixed gas which consists of the combustion air and the 
fuel vapor is burned in a blue flame. 
A portion of the liquid fuel combustion apparatus includes a combustion 
cylinder having a circumferential wall with a number of air holes and an 
end wall by which one end of the combustion cylinder is blocked. The 
apparatus also have a housing arranged apart from the outer surface of the 
combustion cylinder to surround the outer surface of the combustion 
cylinder. The housing includes and end wall which is disposed opposite to 
the end wall of the combustion cylinder. 
With the liquid fuel combustion apparatus, the air supply means for 
supplying the combustion air is fixed to the end wall of the housing to 
provide a rigid unit. The air supply means supplies the combustion air, 
through a small opening on the end wall of the housing, into a space 
between the inner surface of the housing and the outer surface of the 
combustion cylinder. For this reason, the ignition heater and the other 
communication component parts for permitting communication between an 
inside of the combustion cylinder and an outside of the housing have to be 
arranged on the circumferential wall of the combustion cylinder. It is 
necessary in such arrangement to form a plurality of openings for 
inserting the ignition heater and the other communication parts on the 
circumferential wall of the housing. The longer the circumferential length 
of the openings, the greater the difficulties encountered in sealing said 
openings. Since the opening for inserting the heater have the longest 
circumferential length, the seal member applied to the opening for the 
heater is naturally complicated. In the mounting of the seal member, a 
cumbersome operation is required. The openings must, after the ignition 
heater and the other communication component parts are inserted, be 
hermetically sealed by a seal member so that any combustion air may not 
leak out. Where the air supply means is constituted of a high static 
pressure type blower utilizing a turbo-fan, it is necessary to further 
enhance the extent of sealing of the sealing member with respect to the 
cutout and thus a structure of the seal member becomes complicated. The 
complexity of the structure of the seal member and the cumbersomeness of 
assembling result in a high cost of the combustion apparatus as a whole. 
Since the air supply means is rigidly fixed to the housing such that it 
provides a rigid unit, the total axial length of the air supply means and 
housing becomes of necessity longer. Where the combustion apparatus is 
used in combination with another device, the manner in which it is 
combined with the other device is restricted, it being difficult to 
provide a compact structure. 
SUMMARY OF THE INVENTION 
It is accordingly the object of this invention to provide a liquid fuel 
combustion apparatus which permits a simpler structure and easier 
assembling of a seal member, requires no particular design consideration 
for the seal member even if an air supply means for producing high static 
pressure is used, and can provide a compact unit with a wider choice of 
design combination.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS 
FIG. 1 shows a liquid-fuel combustion apparatus 10 according to one 
embodiment of this invention. The apparatus 10 includes a cylindrical 
housing 12 which is horizontally arranged in the longitudinal direction. A 
combustion cylinder 16 having its one end closed by an end wall 14 is 
arranged in a coaxially, spaced-apart relation within the housing 12. In 
this embodiment, the end wall 14 of the housing 12 is formed of a flat 
plate. The combustion cylinder 16 comprises a first circumferential wall 
portion 18 located near the end wall 14, a second circumferential wall 
portion 20 extending from an open end (i.e. the other end) thereof toward 
the middle portion thereof and having a smaller diameter than that of the 
first circumferential wall portion 20, and a third circumferential wall 
portion 22 having a tapered shape and merging with the first and second 
circumferential wall portions. The combustion cylinder 16 as a whole has a 
length shorter than that of the housing 12. A first flange 24 is outwardly 
projected on the outer marginal surface of the open end of the combustion 
cylinder 16. The outer diameter of the first outer flange 24 is made 
smaller than the inner diameter of the housing 12. The first outer flange 
24 is contacted with the inner surface of an inner flange 26 inwardly 
projected at one end of the housing 12 and secured there by bolts. A 
second outer flange 28 is projected on the outer marginal surface of the 
other end of the housing 12. An end wall 30 formed of a flat plate is 
secured by bolts to the outer surface of the second outer flange 28. The 
end wall 30 is disposed parallel to the end wall 14 of the combustion 
cylinder 16. 
A number of air holes 32 are bored in multi-stages over the length of the 
second circumferential wall portion 20 of the combustion cylinder 16 and 
the air holes in each stage are arranged at an equal pitch in the 
circumferential direction of the second circumferential wall portion 20 of 
the combustion cylinder 16. A first flame stabilizing baffle 34 having a 
disc like shape is disposed near the open end of the combustion cylinder 
16 and concentrically within the second circumferential wall portion 20 of 
the combustion cylinder 16 and has an outer diameter smaller than the 
inner diameter of the second circumferential wall portion 20. The first 
stabilizing baffle 34 is fixed to the second circumferential wall portion 
20 by a plurality of radially projecting support bars 36. A second flame 
stabilizing baffle 38 having a hollow disc like shape is disposed within 
and concentrical with the second circumferential wall portion 20 of the 
combustion cylinder 16 such that it is located midway between the fixed 
position of the first flame stabilizing baffle 34 and a position of an 
intersection with the third circumferential wall portion 22. The second 
flame stabilizing baffle 38 has an outer diameter smaller than the inner 
diameter of the second circumferential wall portion. The second flame 
stabilizing baffle 38 is secured, like the first flame stabilizing baffle, 
to the second circumferential wall portion 20 by a plurality of support 
bars 40. 
A fuel supply pipe 42 is inserted through the upper portion of the end wall 
14 of the combustion cylinder 16 such that it extends in a direction 
substantially transverse to the end wall 14. The fuel supply pipe 42 is 
supportingly fixed in a water-tight fashion to the end wall 14 by a 
conventional means such as welding. One end of the fuel supply pipe 42 
extends toward the interior (hereinafter referred to as a fuel evaporation 
region 43) of the first and third circumferential wall portion. The other 
end of the fuel supply pipe 42 is inserted out through the end wall 30 of 
the housing 12 such that it extends in a direction transverse to the end 
wall 30. The other end of the fuel supply pipe 42 further extends through 
a fuel pump 44 into a fuel tank 46 where is connected. The fuel supply 
pipe 42 permits liquid fuel stored in the fuel tank 46 to be supplied drop 
by drop into the fuel evaporation region 43. In this case, an amount of 
liquid fuel supply is varied by varying an amount of discharge from the 
fuel pump 44. 
A fuel reservoir 48 is located at the lowest portion of the fuel 
evaporation region 43 such that it is defined by the lower inner surfaces 
of the first and third circumferential wall portion 18 and 22 and lower 
inner surface of the end wall 14. The liquid fuel so supplied is stored in 
the fuel reservoir 48. 
An overflow tube 50 extends through the lower portion of the end wall 14 in 
a manner to be substantially perpendicular to the end wall 14, and fixed 
in a water-tight fashion to the end wall 14 by a conventional means such 
as welding etc. One end of the overflow tube 50 is made flush with the 
inner surface of the end wall 14. The inserting position of the overflow 
tube 50 is located at a level lower than an intersection of the second and 
third circumferential wall portion 20 and 22. The other end of the 
overflow tube 50 extends out through the end wall 30 in a manner to be 
perpendicular to the end wall 30 of the housing 12, and is connected to 
the top of a discharge oil tank 51. Since the mount of the liquid fuel 
once stored in the fuel reservoir 48 is regulated by the overflow tube 50 
to a predetermined level, no liquid fuel flows into the interior 
(hereinafter referred to as a combustion region 52 of the second 
circumferential wall portion of the combustion cylinder 16). 
An ignition means attaching tube 54 extends through the end wall 14 in a 
manner to be perpendicular to the end wall 14 and is located in a position 
higher than the fixed position of the overflow tube 50. The attaching tube 
54 is supportingly fixed, in a water-tight fashion, to the end wall 14 by 
a conventional means such as welding. One end of the attaching tube 54 is 
made flush with the inner surface of the end wall 14 and a packing is 
fixed to the other end of the attaching tube 54. The attaching tube 54 is 
attached to the inner surface of the end wall 30 of the housing 12 with 
the packing in between. A hole is formed in a location where the other end 
of the attaching tube 54 is contacted with the end wall 14 and has a 
diameter equal to the inner diameter of the attaching tube 54. An ignition 
means 56 is constituted of a bar-like, electrical ignition heater and 
inserted through said hole into the attaching tube 54. One end of the 
ignition means 56 which constitutes a ignition portion is located above 
the fuel reservoir 48. The heater of the ignition means 56 is covered by a 
fuel absorption net 58 which is fixed to the end wall 14. When current is 
supplied to the ignition means 56 the liquid fuel drawn by the net 58 from 
the fuel reservoir 48 is heated and lighted. An opening 59 is formed at 
the central portion of the end wall 30 of the housing 12. An air 
conduction tube 60 for combustion is fitted on the edge of the front 
surface of the end wall 30 which regulates the opening 59 and extends 
outwardly. A bellows tube 62 is connected at one end to the air conduction 
tube 60 and at the other end to an air supply means 64 such as a blower. 
The air supply means 64 supplies a predetermined amount of combustion air 
to a space 66 (i.e. a space of applying pressure to the combustion air) 
defined by the inner surfaces of the housing 12 and end wall 30 and the 
outer surface of the combustion cylinder 16. An air pressure in the space 
66 is once raised there and jetted at high spreads into the combustion 
region 52 through the air holes 32, creating an air stream toward the open 
end of the combustion cylinder. 
The mounting portions of the fuel supply tube 42 and overflow tube 50 with 
respect to the end wall 30 are supported by a first seal member 68 in a 
water-tight fashion, the first seal member 68 constituting one constituent 
element of a joint as shown in detail in FIG. 2. A combustion air supplied 
to the pressure applying space 66 does not leak into the outer atmosphere 
through the above-mentioned mounting portions. The first seal member 68 
comprises a pair of nuts 72, 73 threaded over an external thread 70 formed 
on the outer surface of the fuel supply tube 42 or the overflow tube 50 
and a spring washer 74 disposed between the end wall 30 and an external 
one (one nut 73 in this case) of the nuts 72, 73. The pair of nuts 72, 73 
clampingly hold the end wall 30 there between such that the spring washer 
74 is placed between the end wall 30 and the washer 73. An ignition means 
insertion hole on the end wall 30 is hermetically sealed by a cover 76 
which is fixed to the outer surface of the end wall 30. As a result, the 
liquid fuel is prevented from leaking from the fuel evaporation region 43 
through the abovementioned hole into the outer atmosphere. The cover 76 is 
in contact with the packing fixed to the other end of the ignition means 
attaching tube 54, providing a second seal member 78 for the ignition 
means 56. Therefore, there is no risk that the combustion air supplied to 
the space 66 will not leak out through the ignition means insertion hole. 
With the liquid fuel combustion apparatus so constructed, when the air 
supply means 64 and ignition means 56 are operated substantially 
simultaneously, a predetermined air stream is created toward the 
combustion region 52 in the combustion cylinder 16 and thus toward the 
open end of the combustion cylinder 16 and at the same time the ignition 
portion of the ignition means 56 is heated. With the fuel pump 44 
operated, liquid fuel is supplied from the fuel tank 46 to the fuel 
reservoir 48 in the fuel evaporation region 43. When the liquid fuel 
reaches a certain level, in the fuel reservoir 48, it is drawn by the fuel 
absorption net 58 and burned by the ignition means 56. By the fire flame 
the liquid fuel held in the fuel reservoir 48 is gasified and the flame is 
propagated to the fuel vapor and spread within the fuel evaporation 
region. 
When the temperature of an atmosphere in the fuel evaporation region 43 is 
raised, the liquid fuel supplied dropwise from the fuel supply pipe 42 is 
gasified before reaching the fuel reservoir 48, and becomes a fuel vapor. 
At this time, at the start of burning, the temperature of the liquid fuel 
stored in the fuel reservoir is relatively low and thus an amount of 
evaporation of liquid fuel is small compared with an amount of supply of 
the liquid fuel. Where the amount of supply of the liquid fuel is greater 
than that of evaporation of liquid fuel, the liquid fuel is reached near 
the level of the overflow tube 50 until the amount of evaporation of 
liquid fuel becomes great compared with the amount of supply of liquid 
fuel, a situation after the temperature of an atmosphere in the fuel 
evaporation region 43 is raised a certain time after ignition. Even if the 
amount of supply of the liquid fuel is normally relatively great, the 
liquid fuel in the fuel reservoir 48 rarely reaches the level of the 
overflow tube 50. Where the time taken from the start of fuel supply until 
the ratio between the amount of supply and the amount of evaporation is 
reversed is greater than a normal time due to some reason or others such 
as the ignition time delay, that excess portion of the liquid fuel 
supplied to the fuel reservoir is collected into the discharge oil tank 51 
through the overflow tube 50. Since, therefore, the liquid fuel is not 
flowed into the combustion region 52, it is possible to prevent fire 
accident due to abnormal burning. Now suppose that the amount of supply of 
the liquid fuel is relatively small or medium. Since in this case the time 
taken from the start of the fuel supply until the ratio between the amount 
of supply of the liquid fuel and the amount of evaporation of the liquid 
fuel is reversed becomes correspondingly small, there is rarely a chance 
that the overflow tube 50 will be required. 
The liquid vapor in the fuel evaporation region 43 is once rolled, near the 
second circumferential wall portion 20, in an air stream jetted at rapid 
speeds from each air hole 32 of the second circumferential wall portion 20 
of the combustion cylinder. The liquid vapor, after being beforehand mixed 
with the air stream, the above-mentioned flame in the fuel evaporation 
region 43 is propagated and burned in a blue flame. Within the combustion 
region 52, radial blue flames directed toward the axis of the combustion 
cylinder 16 are formed at the multi-stages in the axial direction of the 
combustion cylinder. It the same time, an unburned fuel vapor is carried 
by the air stream toward the open end of the combustion cylinder 16. The 
unburned fuel vapor promotes its mixing with the air by an eddy current of 
air created near the first and second flame stabilizing baffles 34, 38 and 
is ignited by the blue flame and burned. Since the blue flame and the 
flame resulting from the burning of the unburned fuel vapor have their 
axial direction restricted by the first and second flame stabilizing 
baffles 34, 38, they are prevented from being flowen out from the open end 
of the combustion cylinder 16. The first and second flame stabilizing 
baffles 34, 38 promote through the eddy current a secondary oxidation 
process of the exhausted poisonous materials, such as hydrocarbon or 
carbon monoxide, which are produced at the burning time. As a result, the 
exhausted gas can be cleaned out. 
As set out above, since the liquid fuel combustion apparatus of this 
invention supports the ignition means between the end wall of the 
combustion cylinder and the end wall of the housing, it is possible to 
provide a simple shaped opening for the ignition means. It is also 
possible to make simpler the structure and mounting of a seal member for 
sealing off the opening. Where use is made of a high static pressure air 
supply means, no particular design consideration is necessary. As the air 
supply means is provided outside the housing such that it is spaced apart 
from the housing, it is possible to make the axial length of the housing 
shorter. According to this invention it is possible to combine the 
combustion apparatus with the other device freely and in a compact way. 
Since the air supply means is connected by the bellows tube to the 
pressure applying space the arrangement of the air supply means with 
respect to the combustion apparatus can be effected freely with a wide 
design choice. 
With the embodiment of this invention the fuel reservoir is constituted of 
a space which is defined by the end wall of the combustion cylinder and 
first and third circumferential wall portion, permitting an easier 
manufacture and assembly of the combustion cylinder including the fuel 
reservoir. As the third circumferential wall portion of the combustion 
cylinder portion is gradually tapered from the first circumferential wall 
portion toward the second circumferential wall portion, a combustion air 
stream between the fuel evaporation region 43 and the combustion region 52 
can be adjusted, thereby enhancing a combustion efficiency. 
As shown in FIG. 3 the end wall 14 of the combustion cylinder 16 is formed 
of a flat plate, and the fuel supply tube 42, overflow tube 50 and 
ignition means attaching tube 54 are substantially vertically fixed to the 
end wall 14. At the assembly time of the liquid fuel combustion apparatus 
10 the three tubes 42, 50 and 54 are perpendicularly inserted into the end 
wall 30, which is arranged parallel to the end wall of the housing 12, 
permitting a simpler structure and easy mounting of the first and second 
seal members 68, 78. The end wall 30 is readily attached and detached to 
and from the housing 12 to permit ready inspection and repairs of the 
liquid fuel combustion apparatus 10. The combustion cylinder 16 has its 
outer flange 24 axially contacted with, and fixed by bolts to, the inner 
flange 26 of the housing 12. As a result, it is possible to readly 
assemble the liquid fuel combustion apparatus as a whole. 
Although this invention is described in connection with the above-mentioned 
embodiment, it is not restricted thereto. 
As shown in FIG. 4, for example, an ignition means attaching tube 54 is 
fixed to an end wall 14 of a combustion cylinder 16 in a manner to be 
inclined with respect to the end wall 14 of the combustion cylinder 16 and 
an end wall 30 of a housing 12. The end wall 14 of the combustion cylinder 
16 may be formed of a plate with a small curvature. The end wall 30 of the 
housing 12 has not to be arranged parallel to the end wall 14 of the 
combustion cylinder 16 and may be formed of a plate with a small 
curvature. 
In place of a fuel reservoir 48 defined by the lower inner surfaces of the 
first and third circumferential wall portion 18, 22 and the lower inner 
surface of the end plate 14 a separate box may be placed within the 
combustion cylinder 16 so that a liquid fuel may be supplied dropwise from 
a fuel supply tube 42 to the box. 
The first and second seal members 68, 78 for the fuel supply tube 42, 
overflow tube 50 and ignition device attaching tube 54 are not restricted 
to those as described in connection with the embodiment and may be changed 
in a variety of ways.