[0001] The present invention relates to a flame arrester capable of arresting a flame front
advancing through a pipe line, and particularly, although not exclusively to an arrester
comprising means for attenuating a detonation in combination with means for quenching
the flame.
[0002] Flame arresters are commonly employed in pipe lines where the possibility of a backflash
exists.
[0003] Backflash can occur where there is present a combination of three factors, namely:
a flow of a flammable air/hydrocarbon gas mixture; confinement of the mixture within
a pipe or other structure; and means for igniting the gas mixture. A typical example
exists in the case of a flare line extending from an oilfield storage tank. A flammable
gas mixture flows from the tank head-space through the line to a flare stack having
an outlet to the atmosphere. The mixture leaving the flare stack outlet is normally
kept lit. If the flow velocity at the stack is not sufficiently high, the flame can
"backflash" or burn upstream through the pipe line. If the flame front reaches the
tank, the latter can explode.
[0004] As stated, flame arresters have long been emplaced in such lines to snuff out or
quench the flame front before it reaches an installation (such as the storage tank)
where serious harm could be done.
[0005] Commonly, a flame arrester comprises a flanged tubular housing which is connected
into the line to form an integral component thereof. An "element" is positioned within
the bore or chamber of the housing to extend transversely fully across the bore diameter.
[0006] The element functions to quench the flame front.
[0007] In structure, the element usually comprises a matrix having a multiplicity of small
diameter, elongate channels extending therethrough in the direction of the pipe axis.
The matrix usually consists of metal. One typical element, for example, comprises
a long flat sheet of aluminum, referred to as the "core". A second similar sheet is
crimped in sawtooth fashion and the apexes of the crimps are in contact with the upper
surface of the core sheet. The product is then spirally wound to produce a cylindrical
element. An element of this type is commonly referred to as a "spiral wound crimped
ribbon" element.
[0008] As stated, the channels of the element are minute in width or diameter. More specifically,
the channel diameter is selected to be smaller than the "quenching diameter". The
quenching diameter is the largest diameter at which a flame within the channel would
be extinguished under static flow conditions. The determination of the quenching diameter
is commonly carried out in the industry in accordance with the practice outlined in
"Progress in Combustion Science and Technology", Potter, A.E. Jr., Volume 1, pages
145-181 (1960).
[0009] In principle then, a flame arrester element is provided with small enough channels,
established by determination in accordance with standard industry practice, so that
sufficient heat will be removed from a flame, by conductance through the matrix material,
to cause the flame to be extinguished.
[0010] Unfortunately, in practice, flame arresters do from time to time fail to arrest the
flame and explosions do occur as a result, even though they have been designed in
accordance with established and industry-accepted practice.
[0011] The reason for failure, in applicant's view, is that the conventional flame arresters
are only capable of coping with a limited part of the spectrum of flame propagation
conditions to which they may be exposed, when used outside existing standards.
[0012] Flame propagation can occur in two modes, deflagration and detonation.
[0013] Deflagration is a combustion wave that propagates by the transfer of heat and mass
to the unburned gas ahead of it. Associated flame front overpressures can range from
0 to 10 or 20 times the initial value (which is commonly atmospheric pressure). Flame
velocities are usually subsonic for deflagrations.
[0014] Detonation is a combustion wave that propagates by shock compression-induced ignition.
Detonations travel supersonically, with Mach numbers of 5 to 10. Detonation overpressures
typically reach 15 to 50 times the initial value.
[0015] Under a suitable and complex combination of circumstances (including gas composition,
length of run from the ignition source, and flame front turbulence-creating factors
such as bends and the like), an advancing flame front can accelerate and change from
the deflagration mode to the detonation mode. Detonation is evidenced by a rapid and
sharp escalation in the pressure accompanying the flame front, said peak pressurewave
being in spaced relationship in front of the flame front. A typical pressure/distance
plot based on a burn involving detonation in a pipe is set forth in Figure 2, following
below, and shows the spectrum of pressure change that occurs as a flame front transition
takes place between modes.
[0016] When flame propagation incurs detonation, two undesirable results can occur, namely:
- combustion may be initiated on the protected or upstream side of a conventionally
designed element; and
- the element may be structurally damaged and thereafter lose some of its arresting
capability.
[0017] These problems associated with detonation have been acknowledged in the prior art
literature.
[0018] In reviewing the literature, applicant noted two different theories of interest given
to explain the failure of arresters when exposed to detonation. One theory suggested
that the high pressure of detonation would propel hot gas through the channels at
such high velocity that the conventionally designed element would be incapable of
cooling the gas sufficiently. On reaching the upstream end of the element, the still-hot
gas would combine with the unburned gas and heat it so that spontaneous ignition would
occur. The other theory suggested that the high pressure would densify the flammable
gas mixture in the channels so that flame advancing through the channels would create
so much heat that the matrix heat sink would be incapable of preventing the flame
from reaching the upstream end of the channels.
[0019] Two modifications of an arrester element readily suggest themselves from these theories,
as a means for coping with the high pressure failures. More particularly, one could:
- reduce the width of the channels; or
- further elongate the channels;
to thereby increase the heat-removal capability of the element.
[0020] Reducing the channel width or diameter is a solution of only limited applicability
or practicality. As the channel diameter is reduced, the pressure drop across the
element increases. Choking a vent line in this fashion is undesirable. So that leaves
elongation of the channels as an avenue to explore.
[0021] Applicant constructed and tested an element having a channel length 16 times that
of a commercially available element designed in accordance with conventional practice.
When subjected to detonation conditions, this extended element still failed over a
significant portion of the flame propagation spectrum. Thus channel elongation does
not appear to solve the problem of failure at high pressure, at least in a practical
and feasible fashion.
[0022] Another possible modification for the element has been suggested in the prior art,
to improve quenching capability. This involves providing channels which are tortuous
in configuration and have alternating sections of expanded and reduced diameter. Channels
of this design cause the flame front to move turbulently.
[0023] Applicant tested elements having such turbulence-creating channels and found that
they do provide improved quenching. However, when subjected to the high pressures
approaching or accompanying detonation conditions, the elements still failed with
some regularity.
[0024] So there is still a need for a flame arrester which is improved with respect to handling
the full spectrum or range of flame propagation conditions, including detonation.
[0025] In accordance with preferred embodiments of the present invention, a detonation attenuator
is provided within the housing of a flame arrester. The attenuator is positioned in
front of the quenching element, to receive and reflect part of the central portion
of the detonation wave back into the pipe. Only a portion of the detonation wave passes
around the attenuator and accompanies the flame to the element. By incorporating an
attenuator of successful design , an arrester is provided which has been tested and
shown to be much improved in coping with a full spectrum of flame propagation conditions.
[0026] Preferably, the modified flame arrester involves, in combination:
- A housing whose internal chamber has a greater cross-sectional area than that of
the pipe line, so there is expansion of the shock wave/flame front as it enters the
chamber; and
- A generally cup-shaped attenuator or member, positioned in line with and adjacent
to the housing flame front inlet, for receiving and reflecting part of the detonation
wave back down the pipe. The attenuator side wall is inwardly spaced from the longitudinal
wall of the housing to thereby form an annular passage connecting the flame front
inlet with the quenching element. The peripheral portion of the shock wave/flame front
train passes through this passage to the element, wherein the flame is quenched.
[0027] The combination may have the following advantages:
- The element is protected by the attenuator from structural damage from detonation,
to a much improved extent. In test runs without an attenuator, the element was rendered
ineffective after as few as 3 detonations. When tested with the attenuator in place,
the same type of element was able to withstand as many as 25 detonations without significant
damage;
- The combined components performed to quench detonations. When tested under similar
conditions against several commercially available flame arresters, the new arrester
was successful in quenching on every run while the other units failed on some runs,
as shown later in this specification. Stated otherwise, the present arrester performed
successfully over the full spectrum of wave propagation at the test conditions; and
- In applications where the flame arrester is used in situations where the flow and
the potential flame front approach from the same direction, the attenuator can serve
to protect the element from velocity erosion or degradation from collision by solid
objects in the line. Velocity erosion occurs when fine particles carried in a high
velocity gas flow strike the element.
[0028] According to one aspect of the invention, there is provided a flame arrester for
arresting the advance of a flame front through a pipe line, comprising: a generally
tubular housing adapted to be connected with the pipe line, whereby the housing forms
an integral component thereof, said housing forming an inlet for a flame front advancing
through the pipe line and an outlet, said housing thus forming an open-ended chamber;
element means, positioned in the chamber at its outlet end and extending transversely
across the housing chamber, for quenching the flame attempting to pass therethrough;
and a generally cup-shaped member, positioned in the chamber in line with and adjacent
to, the inlet, for receiving the central portion of a detonation wave entering the
chamber and reflecting part of it back into the pipe line.
[0029] Preferably, the side wall of the cup-shaped member is spaced inwardly from the longitudinally
extending wall of the housing, to form an annular passage therewith.
[0030] Preferably, the width of the mouth of the cup-shaped member is greater than the width
of the housing inlet, whereby the cup-shaped member encircles the inlet.
[0031] According to a second aspect of the present invention, there is provided a flame
arrester for arresting the advance of a flame front through a pipe line, comprising:
a generally tubular housing, said housing being adapted to be connected with the pipe
line whereby the housing forms an integral component thereof, said housing forming
an inlet for a flame front advancing through the pipe line, said housing further forming
an open-ended chamber of expanded diameter relative to the pipe line with which it
is to be used;
element means, positioned in the housing at its outlet end and extending transversely
fully across the housing chamber, for quenching the flame attempting to pass therethrough,
said element means comprising a matrix forming a multiplicity of discrete channels
extending therethrough generally in the direction of the longitudinal axis of the
housing, each such channel having a width less than the diameter required for quenching
a flame front in the deflagration mode; and
detonation attenuating means for receiving the central portion of a detonation wave
entering the chamber and reflecting it, said means being positioned in the chamber
at its inlet end and comprising a generally cup-shaped member having its mouth directed
toward the inlet, said cup-shaped member having its side wall inwardly spaced from
the longitudinally extending wall of the housing to form an annular passage therewith,
the width of the mouth of the cup-shaped member being greater than the width of the
inlet whereby the cup-shaped member encircles the inlet, the first end of the cup-shaped
member being spaced from the adjacent end wall of the housing, whereby a peripheral
portion of the flame front may enter the annular passage and reach the element means.
[0032] Preferably, the element means comprises a stack of expanded metal sheets, each such
sheet having a multiplicity of generally diamond-shaped openings having long and short
widths, the sheets being alternately juxtapositioned so that a sheet has its opening
long dimension rotated at about 90
o relative to the next adjacent sheet.
[0033] According to a third aspect of the present invention, there is provided a flame arrester
for arresting the advance of a flame front through a pipe line, comprising:
a generally tubular housing, said housing being adapted to be connected with the pipe
line, whereby the housing forms an integral component thereof, said housing forming
an inlet for a flame front advancing through the pipe line and an outlet, said housing
thus forming an open-ended chamber;
element means, positioned in the chamber at its outlet end and extending transversely
across the chamber, for quenching the flame attempting to pass therethrough; and
a generally cup-shaped member, positioned in the chamber in line with and adjacent
to but spaced from the inlet, said cup-shaped member being positioned between the
inlet and the element means said member having a solid end wall extending transversely
across the inlet and a side wall, said side wall being spaced inwardly from the longitudinally
extending wall of the housing, to form an annular passage therewith, said cup-shaped
member having its mouth directed towards the inlet, said cup-shaped member being operative
to receive the central portion of a detonation wave entering the chamber and to reflect
part of it back into the pipe line.
[0034] According to another aspect of the present invention, there is provided a flame arrestor
including any integer disclosed in the first aspect in combination with any integer
disclosed in the second aspect and/or in combination with any integer disclosed in
the third aspect.
[0035] For a better understanding of the invention, and to show how same may be put into
effect, reference will now be made, by way of example, to the accompanying diagrammatic
drawings, in which:
Figure 1 is a schematic side view showing a pair of flame arresters in use in a typical
application, namely in the flare and air lines of an oil storage tank;
Figure 2 is a plot of pressure versus run-up distance for a typical pressure profile
generated in a burn down a pipe line in accordance with Figure 13, said burn involving
both deflagration and detonation modes;
Figure 3 is a partly broken away side view of one form of the arrester;
Figures 4 and 5 and are end views of the arrester of Figure 3;
Figure 6 is a fully sectional plan view of the arrester of Figure 3, taken along the
line A--A;
Figure 7 is a perspective partly-broken-away view of the attenuator or cup-shaped
member of Figures 3 and 6;
Figure 8 is a perspective view of a crimped ribbon quenching element, partly broken
away to illustrate the quenching channels;
Figure 9 is a sectional side view of an arrester having a preferred form of element
consisting of a stack of expanded metal sheets;
Figure 10 is a perspective view of the element stack of Figure 9;
Figure 11 is a perspective view showing the element stack of Figure 10 in a partly
exploded form;
Figure 12 shows a fragment of two superimposed sheets of expanded metal stacked in
alternating orientation, showing the 90o rotation of the diamond-shaped openings;
Figure 13 is a schematic of the test circuit used to develop the data set forth in
the Examples;
Figures 14a to 14d are fanciful simplified representations of the arrester and the
process of detonation arrestment believed to occur in it;
Figures 15 and 16 show schematically the identical arresters, one with attenuator
and one without, used to develop the data of Example 1;
Figure 17 shows schematically an arrester, having a single element segment and provided
with a flat plate attenuator, used to develop the data of Example II;
Figure 18 shows schematically a preferred arrester having an attenuator formed with
a bent back side wall;
Figure 19 shows another alternative form of arrester; and
Figure 20 shows schematically an arrester identical to that of Figure 18 except that
the attenuator does not have the bent back side wall, said arresters of Figures 18
and 20 being used to develop the data of Table V.
[0036] The flame arrester 1 comprises a generally tubular housing 2, a quenching element
3, and a cup-shaped member or cup 4. The housing 2 is adapted to be connected into
a pipe line 5 to form a flow component thereof. The element 3 and cup 4 are positioned
within the housing 2.
[0037] The housing 2 is a multi-component assembly which consists of a flanged upstream
end member 6, a tubular middle member 7 (made up of rings), and a downstream flange
member 8. ("upstream" and "downstream" refer to the direction of flow of the gas passing
through the line 5.)
[0038] The upstream end member 6 forms a central bore or passage 9 for communication with
the bore of the upstream end of the pipe line 5. It will be noted that the member
6 is outwardly flared, so that the diameter of the bore 9 is greater than that of
the pipe line 5. The member 6 also forms suitable openings around its periphery for
receiving threaded tie rods 10 which, in cooperation with nuts 11, hold the members
6, 7, 8 together.
[0039] The downstream flange member 8 also forms peripheral openings for receiving the tie
rods 10. The member 8 forms a central threaded bore or flame inlet 12 which enables
the member to be screwed onto the threaded downstream end of the pipe line 5. This
bore 12 forms the flame front inlet for the arrester 1.
[0040] When the three members 6, 7 , 8 are assembled using the tie rods 10 and nuts 11,
the housing forms an open-ended internal chamber 13, which provides a gas flow passage
through the unit when it is connected into the pipe line 5. The diameter of this chamber
13 is greater than or expanded relative to the diameter of the pipe line bore.
[0041] The quenching element 3 is positioned in the upstream end of the housing chamber
13.
[0042] In the embodiment shown in Figure 6, the element 3 comprises upstream and downstream
rings 14 and crossbars 15 holding four discrete element segments 16 and spacers 17
positioned between them in end-to-end formation. Each element segment 16 has a conventional
spiral-wound crimped ribbon 18 wound around a core 19 and contained within a ring
20 which is part of the housing middle member 7. The solid material (or "matrix")
of the ribbon 18 forms a multiplicity of small width, elongate, discrete channels
21. The channels 21 extend in the direction of the longitudinal axis of the housing
chamber 13. The width or diameter of these channels 21 is selected to be smaller than
the quenching diameter, when determined in accordance with standard industry practice
for the conditions involved.
[0043] It will be noted that the spacers 17 maintain a slight gap 22 between each element
segment 16. These gaps 22 provide expansion zones for gas in the channels 21 and lead
to turbulent flow of that gas.
[0044] A preferred form of quenching element is shown in Figures 9 - 12. This element comprises
a stack 30 of sheets 31 of expanded metal forming a multiplicity of diamond-shaped
channels 32. The sheets 31 are oriented in alternating fashion so that the major dimension
of the channels 32 of one sheet 31 is crosswise to the major dimension of the channels
of the next sheet. Stated otherwise, each sheet 31 is rotated 90
o relative to the next sheet in alternating fashion. This is particularly shown in
Figure 12.
[0045] Ring-like end plates 33 are provided at each end of the stack 30. Nut and bolt assemblies
34 extend through the end plates 33 and sheets 31 and hold the stack 30 together.
The tie rods 10 also extend through the assembly and clamp it against the inner shoulder
35 of the upstream end member 6.
[0046] The attenuator comprises a cup-shaped member or cup 4 having a solid end wall 41
and a tubular side wall 42. The cup 4 is fixed in place in line with and adjacent
to the flame inlet 12. More particularly, threaded rods 43 extend through the cup
end wall 41 and flange member 8. Spacers 44 cooperate with the wall 41 and member
8 to fix the cup 4 in place.
[0047] As shown, the side wall 42 of the cup 4 is inwardly spaced from the longitudinal
wall of the housing middle member 7. There is thus formed an annular passage 45 therebetween.
The mouth 4a of the cup 4 is directed towards the flame front inlet 12. It will also
be noted that the rim 46 of the cup 4 is spaced a short distance (the "stand-off")
from the downstream flange member 8. The annular passage 45 communicates with the
stand-off space 47 to form an L-shaped path past the cup 4. It will further be noted
that the diameter of the bore 48 of the cup 4 is greater than the diameter of the
flame inlet 12. Stated otherwise, the cup 4 encircles the flame inlet 12.
[0048] Before describing the observed operation of the present arrester, it is useful to
describe the nature of a detonation wave. To applicant's understanding, it comprises
three different zones or segments. These are: a shock wave, a following induction
zone, and then a reaction zone. These zones are fancifully illustrated in Figures
14a - d. The shock wave is responsible for the compression and heating of the unburned
gas. The induction zone represents the region extending back to the point at which
exothermic release begins in the hot, pressurized gas. And the reaction or flame zone
represents the region wherein exothermic reaction is initiated and completed.
[0049] Applicant's understanding of the process proceeding in the present arrester is as
follows:
[0050] When there is a detonation, the detonation wave advances through the pipe line 5.
On entering the chamber 13, the wave expands radially. The strong central portion
of the wave proceeds into the bore 48 of the cup 4 and a significant portion is reflected
by the cup 4 back down the pipe line. Only the weaker peripheral portion of the shock
wave accompanies the flame through the L-shaped passage 47, 45 to the element 3, where
the flame is quenched.
[0051] The pressure associated with the peripheral portion of the shock wave that bypasses
the attenuator is considerably lower than that associated with the central portion.
The annular or peripheral portion no longer appears to propagate as a detonation.
[0052] Applicants' tests have indicated:
- That in the absence of the attenuator, a flame front in the detonation mode will
usually penetrate through the conventionally designed quenching element and ignite
gas upstream thereof;
- That, when using the same element and test conditions but with the attenuator in
place in the arrester , the flame front does not penetrate beyond the arrester and
ignite the upstream gas;
- That, in the absence of the attenuator, the element becomes damaged in the course
of a few detonation tests; and
- That, with the attenuator in place, the same element under the same test conditions,
is not damaged.
[0053] The invention is supported and illustrated by the following examples:
Example 1
[0054] This example shows that a flame arrester having an attenuator and a conventional
quenching element, successfully arrested an air/propane flame front at both deflagration
and detonation conditions. The burn runs were carried out in the test assembly shown
in Figure 13.
Test Conditions: |
quenching element: |
aluminum crimped metal ribbon, 0.050 inch crimp height, round spiral wound, 8 inch
path length; |
downstream (burn end) piping: |
straight run, 35 feet, 3" schedule 80 steel pipe, threaded to arrester, 10 ignition
location points tapped into pipe, for use with a spark plug ignitor; |
housing detail: |
chamber 7" long with 8" diameter; |
gas mixture: |
4.6% propane-air; |
[0055] The test procedure was as follows:
- The propane and air were metered into the down-stream pipe;
- The mixture composition was monitored with a gas chromatograph to ensure propane
concentration accuracy;
- The pipe system was purged with the mixture and ignited. Different runs were ignited
at different distances from the arrester. (Ignition location was important to all
of these tests. The explosion pressures experienced by the flame arrester tended to
increase as the burn distance was increased. More particularly, starting from the
ignition point closest to the flame arrester, the deflagration pressure increased
with increasing distance from the flame arrester flame inlet. After a certain point
(ignition location #7), a flame front passed through the deflagration/detonation transition
zone with only detonations occurring when longer run-up distances were thereafter
used.)
- Flame arrester failure (i.e. flame propagation on the protected side) was determined
by flame ionization sensors, as shown in Figure 13.
[0056] The test results were as follows.
[0057] Having reference to Figure 15, there is shown a schematic of an arrester A in accordance
with the invention, having a cup-shaped attenuator. The arrester A was repeatedly
tested as set forth in Table I on the test circuit of Figure 13 and the flame was
quenched on every test.

[0058] Having reference to Figure 16, there is shown a schematic of an arrester B otherwise
identical to arrester A but absent the attenuator. It was only tested for detonations
and failed as shown in Table II.

[0059] The attenuation of impinging shock waves was verified using quick response pressure
transducers located as shown on Figure 13. The strength of the inlet shock was determined
by pressure measurement P1 on the inlet pipe immediately prior to entry into the flame
arrester. The attenuated pressure P2 was measured just before the quenching element.
Typical results were as follows:
TABLE III
Ignition Location |
P1(psig) |
P2(psig) |
#10 |
410 |
180 |
#8 |
710 |
350 |
Example II
[0060] This example compares burn test run results when an arrester having a flat disc,
in accordance with Figure 17, was used. With the flat disc in place as the attenuator,
the results were as follows:
TABLE IV
Ignition location: |
#10 |
Number of ignitions: |
5 |
Number of failures: |
5 |
[0061] A further embodiment of the attenuator is illustrated in Figure 1 . In this embodiment,
the sidewall 60 of the cup 61 is partly turned back to create an annular confined
zone 62 for trapping a peripheral portion of the shock wave. The arrester of Figure
18 corresponded with that of Figure 20, except for the shape of the attenuator.
[0062] The modified entrance or mouth of this cup improves quenching of detonations. This
was demonstrated by severe condition runs initiated from the ignition location (#10)
most distant from the arrester and having a flame accelerator in the line. The results
of testing two arresters, shown in Figures 18 and 20, were as follows:
TABLE V
Arrester Design |
Ignition Location |
Number of Ignitions |
Number of Failures |
Figure 18 |
#10 |
10 |
0 |
Figure 20 |
#10 |
5 |
3 |
[0063] Figure 19 shows another alternative form of arrester.
[0064] More particularly, Figure 19 shows an arrester 70 having a tubular housing 71 closed
at its upper end by a wall 72. A cylindrical element 73 is created by wrapping coiled
expanded metal 74 around a support spool 75. The spool 75 has structural support bars
76 that run parallel to its axis. The expanded metal diamonds are all oriented in
the same direction throughout the depth of the element 73. The cup 77 is situated
in the space 78 formed by the hollow spool 75. The mouth 79 of the cup 77 is open
toward the flame inlet 80.
[0065] In this configuration, the cup 77 acts to reduce the amount of pressure piling that
results from the reflection of the incoming shock wave from the housing end wall 72.
[0066] The reader's attention is directed to all papers and documents which are filed concurrently
with or previous to this specification and which are open to public inspection with
this specification, and the contents of all such papers and documents are incorporated
herein by reference.
[0067] All of the features disclosed in this specification (including any accompanying claims,
abstract and drawings), and/or all of the steps of any method or process so disclosed,
may be combined in any combination, except combinations where at least some of such
features and/or steps are mutually exclusive.
[0068] Each feature disclosed in this specification (including any accompanying claims,
abstract and drawings), may be replaced by alternative features serving the same,
equivalent or similar purpose, unless expressly stated otherwise. Thus, unless expressly
stated otherwise, each feature disclosed is one example only of a generic series of
equivalent or similar features.
[0069] The invention is not restricted to the details of the foregoing embodiment(s). The
invention extends to any novel one, or any novel combination, of the features disclosed
in this specification (including any accompanying claims, abstract and drawings),
or to any novel one, or any novel combination, of the steps of any method or process
so disclosed.
1. A flame arrester 1 for arresting the advance of a flame front through a pipe line
5, comprising:
a generally tubular housing 2, said housing 2 being adapted to be connected with the
pipe line 5, whereby the housing 2 forms an integral component thereof, said housing
2 forming an inlet 12 for a flame front advancing through the pipe line 5 and an outlet,
said housing 2 thus forming an open-ended chamber 13;
element means 3, positioned in the chamber 13 at its outlet end and extending transversely
across the chamber 13, for quenching the flame attempting to pass therethrough; and
a generally cup-shaped member 4, positioned in the chamber 13 in line with and adjacent
to the inlet 12, for receiving the central portion of a detonation wave entering the
chamber 13 and reflecting part of it back into the pipe line 5.
2. A flame arrester as set forth in claim 1 wherein:
a side wall 42 of the cup-shaped member 4 is spaced inwardly from a longitudinally
extending wall of the housing 2, to form an annular passage 45 therewith.
3. A flame arrester 1 as set forth in claim 1 or claim 2, wherein:
the width of a mouth 48 of the cup-shaped member 4 is greater than the width of the
housing inlet 12, whereby the cup-shaped member 4 encircles the inlet 12.
4. A flame arrester 1 for arresting the advance of a flame front through a pipe line
5, comprising:
a generally tubular housing 2, said housing 2 being adapted to be connected with the
pipe line 5 whereby the housing 2 forms an integral component thereof, said housing
2 forming an inlet 12 for a flame front advancing through the pipe line 5, said housing
2 further forming an open-ended chamber 13 of expanded diameter relative to the pipe
line 5 with which it is to be used;
element means 3, positioned in the housing 2 at its outlet end and extending transversely
substantially fully across the housing chamber 13, for quenching the flame attempting
to pass therethrough, said element means 3 comprising a matrix forming a multiplicity
of discrete channels 21 extending therethrough generally in the direction of the longitudinal
axis of the housing 2, each such channel 21 having a width less than the diameter
required for quenching a flame front in the deflagration mode; and
detonation attenuating means for receiving the central portion of a detonation wave
entering the chamber 13 and reflecting it, said means being positioned in the chamber
13 at its inlet end 12 and comprising a generally cup-shaped member 4 having its mouth
40 directed toward the inlet 12, said cup-shaped member 4 having its side wall 42
inwardly spaced from the longitudinally extending wall of the housing 2 to form an
annular passage 45 therewith, the width of the mouth of the cup-shaped member 4 being
greater than the width of the inlet 12 whereby the cup-shaped member 4 encircles the
inlet 12, the first end of the cup-shaped member being spaced from the adjacent end
wall 7 of the housing 2, whereby a peripheral portion of the flame front may enter
the annular passage 45 and reach the element means.
5. A flame arrester according to any of the preceding claims, wherein:
the element means comprises a stack of expanded metal sheets 31, each such sheet having
a multiplicity of generally diamond-shaped openings 32 having long and short widths,
the sheets 31 being alternately juxtapositioned so that a sheet 32 has its opening
long dimension rotated at about 90o relative to the next adjacent sheet.
6. A flame arrester for arresting the advance of a flame front through a pipe line,
comprising:
a generally tubular housing, said housing being adapted to be connected with the pipe
line, whereby the housing forms an integral component thereof, said housing forming
an inlet for a flame front advancing through the pipe line and an outlet, said housing
thus forming an open-ended chamber;
element means, positioned in the chamber at its outlet end and extending transversely
across the chamber, for quenching the flame attempting to pass therethrough; and
a generally cup-shaped member, positioned in the chamber in line with and adjacent
to but spaced from the inlet, said cup-shaped member being positioned between the
inlet and the element means said member having a solid end wall extending transversely
across the inlet and a side wall, said side wall being spaced inwardly from the longitudinally
extending wall of the housing, to form an annular passage therewith, said cup-shaped
member having its mouth directed towards the inlet, said cup-shaped member being operative
to receive the central portion of a detonation wave entering the chamber and to reflect
part of it back into the pipe line.
7. A flame arrestor including any integer disclosed in Claims 1,2 or 3 in combination
with any integer disclosed in Claims 4 or 5 and/or in combination with any integer
disclosed in Claim 6.