Next
Meeting
10.30
for 11.00
Tuesday 24 September 2013
at
The
Institution of Structural Engineers, London
|
|
Discussion
|
(Top) |
- Research
Directions
Materials
relevant to the 21 September 2004 meeting:
- CIB W14 paper
on robustness of connections
Download (PDF
154kb)
- ODPM discussion
document on Creation of a Virtual Fire Research Academy
and National Fire and Rescue Strategy.
Download (PDF
125kb)
- Research
Priorities List - powerpoint presentation.
Please send additions or amendments to Ian Burgess
as soon as possible.
Download (PPT
31kb or PDF
90kb)
- Intumescent
temperature calculation
Hans van de
Weijgert's paper on the Eurocode method.
Download (PDF
521kb).
- 3D
Interpolation method for intumescents
Hans van de
Weijgert's graphical method for prediction of steel
temperatures with intumescent protection.
Download article
(PDF
547kb).
|
Asif
Usmani & Michael Rotter
Failure of Structures
Under Fire
To say
that the definition of failure of structures in fire is ‘complex’
is a huge understatement. It is much more than that, beginning
right from the most elementary issue of ‘what kind of failure’
is it that one is trying to define. As the fire safety of
a structure is of interest not only to the architect and structural
engineer but also to fire safety engineers and regulators/building
control officers (not to mention the owner/client). It is
the highly varying perspectives of this group of people that
confuses the issue and makes it very difficult for a consensus
on the definition of failure to emerge, if it were indeed
possible. For a fire safety engineer, failure may be said
to have occurred if a breach of compartmentation and uncontrolled
spread of fire occurs (with or without undesirable consequences)
irrespective of whether there had been ‘structural failure’.
For the owner, failure may be defined in terms of the economic
losses accrued from the fire, in terms of the cost of repair,
loss of business and loss of productivity etc. without
regard to structural failure. Structural engineers however
are concerned with structural failure, which is the purpose
of this document. In fire situations even this is far from
straightforward and hence the need for discussion.
In general, to structural
engineers, failure invariably means the inability of a structure
to continue to sustain a given loading. This may occur due
to:
- The magnitude of
the load being in excess of the capacity of the structure.
- Degradation of the
load carrying capacity of the structure (caused by age or
other factors) so that it is unable to sustain the loads
normally imposed
- Design faults, where
one or more failure mechanisms were not foreseen
- Construction faults,
where poor materials or quality of construction caused the
structure to be have a reduced capacity than that assumed
in design
When design
loads are applied, the structure normally responds by changing
its geometry (displacement) and reverts to its original geometry
after the load is removed and its capacity to carry loads
is undiminished (through the property of elasticity). However,
if the magnitude of the load is excessive the change in geometry
required is greater than the structure can sustain elastically.
The large deformations lead to permanent changes in the capacity
of the structure to withstand loads. In the limit a very large
load can cause the structure to ‘collapse’, which is certainly
‘failure’. In practice however, a structure that may not have
collapsed may still be said to have failed, if it is unfit
for any further use. On the other hand, as for instance in
the field of earthquake engineering, a structure can be designed
to sustain very large changes of geometry without collapse,
and in this case even if the structure is unusable after an
earthquake it cannot be said to have failed. Therefore ‘failure’
may be more accurately defined as the inability of the
structure to ‘perform’ as designed, which leads to a situation
where no absolute criteria for failure can be defined in isolation
from the requirements of a ‘performance based design’. There
are however large classes of structures similar enough in
construction and design to have a large overlap in the performance
requirements, for which it may be worthwhile to define some
general ‘failure’ criteria, if only for the purpose of opening
an informed debate on this complex question.
The traditional
criteria of structural failure at ambient temperature relied
on the following ideas (Fig. 1):
- attainment of a peak
strength under increasing load, followed by a reducing load
carrying capacity;
- in structures whose
strength does not reach a peak, the attainment of a deflection
deemed to be so large that it is unacceptable even for an
ultimate limit state.
The second
criterion works well when the load-displacement curve is relatively
flat at large displacements, but it is more difficult to apply
when continually increasing strength is seen.

Fig.
1 Possible forms of load-deflection curve at ambient temperature
When these
criteria are transferred to a fire scenario, the load is no
longer changing, but generally remains fixed during the fire.
Thus, the attainment of a peak strength is not so easily identified.
A rapid increase in deflections with a small rise in temperature,
commonly called ‘runaway’ has therefore been used as an analogy
for the second criterion defined above. The main problem with
such a description is that it has been based upon testing
simply-supported beams in furnaces subjected to ‘standard’
fires. It is widely accepted that a beam in a furnace is has
little or no relevance to a large frame structure in fire.
However in the absence of clear and simple alternatives it
continues to be the only picture that most professionals involved
in fire safety engineering associate with failure in fire.
Figure 2 illustrates the huge difference in the performance
of two beams (one simply-supported and one with end translations
restrained) subjected to fire. Runway is delayed considerably
in the beam with ends restrained against translation. Figure
2 shows clearly that for temperatures below 300 °C, the deflections
for the restrained beam are much larger than that for the
simply supported beam, however they have nothing to do with
‘runaway’. These deflections are caused entirely by the increased
length of the beam through thermal expansion and are not a
sign of loss of ‘strength’ or ‘stiffness’ in the beam until
much later. In fact approximately 90% of the defelection at
500°C and 75% at 600°C is explained by thermal expansion alone.
Most of the rest is explained by increased strains due to
reduced modulus of elasticity. However the behaviour remains
stable until about 700°C when the first signs of runaway begin
to appear.
In the
simply-supported beam, by contrast, the rapid increase in
deflections results from a great loss of tangent stiffness,
which corresponds exactly to the case of structures at ambient
temperature subjected to increasing loads and degrading stiffness.
If a small increment in load produced a great increase in
deflection the intended meaning of the second failure criterion
would be met. This criteria makes sense in an ambient temperature
situation as the large deflections correspond to a large loss
of load carrying capacity. The recognition of this relationship
between an ambient temperature failure criterion and a fire
criterion is valuable in assisting the development of an understanding
of the basis of failure criteria for fire.
In highly
redundant structures, very large deflections can develop at
moderate temperatures (for instance the restrained beam in
Figure 2). It might therefore be thought that a state corresponding
to the second criterion of failure has been reached. However,
the sensitivity to a small increase in loading is very small,
so the second criterion has not been reached even when the
deflections themselves are very large.
Moreover,
it has now become evident that large deflections in a highly
redundant structure at high temperature actually assist the
structure to survive the fire with minimal damage, so a criterion
which limits deflection itself would encourage the designer
towards a poorer design (against an ultimate limit state of
collapse). The source of the additional robustness imparted
by large thermally induced deflections derives from the fact
that a displaced configuration amenable to the alternative
load carrying mechanism of tensile membrane action is achieved
without large and damaging mechanical strains in the structure
(as would be the case at ambient temperature). Figure 3 below
shows the restrained beam of Figure 2 loaded with factors
of a udl w that will cause a plastic hinge to occur
at the beam midspan at ambient. It is interesting to see that
up to approximately 600 C the load has very little practical
effect on the deflection and nearly all the deflection increase
(after loading) from ambient to 600 C is thermally induced.
Therefore it would be simplistic to assume that the structure
is in distress (or approaching failure) just by looking at
the total deflection.
(Figs
2 and 3 are not available)
For these
reasons, it is necessary that new criteria of failure should
be developed for real structures in fire.
3. Discussion
Since the
deflections of the structure due to thermal effects can be
very large at even moderate temperatures and when the structure
is still quite undamaged, it would be meaningless to use a
criterion based solely on the deflection divided by the span,
or some similar measure to indicate structural failure in
fire.
Furthermore,
to mobilise the alternative load carrying mechanism of tensile
membrane action, large deflections are a requirement. This
action has been shown to be much more reliably available at
high temperatures than at ambient temperatures. This is because
large deflections, and the corresponding change of geometry
of the structure, can be achieved predominantly from thermal
strains. As a result, large mechanical strains, which are
detrimental to the structure, are not required. Moreover,
the restraint to thermal expansion often causes beneficial
mechanical strains (compression), which allow much greater
bending strengths to be exploited.
Large deflections
are used as indicators of failure at ambient temperatures
chiefly because deflections are closely related to mechanical
strains, and large mechanical strains are associated with
severe damage to the materials of construction. Thus, large
deflections at ambient temperature are a sign of structural
distress. They signal that the structure has reached an ‘undesirable
state’ where further loading may cause excessive material
degradation and the loss of capacity of the structure to support
the applied loads. This is termed an ‘ultimate limit state’.
Failure
under fire can be approached using the same philosophy of
identifying signs of ‘distress’ in the structure. As absolute
deflections are no longer a good measure of damage to the
material of construction, the concept of failure must be developed
by considering what the signs of distress must now be. The
behaviour of a structure under fire is considerably more complex
than its behaviour under normal loading at ambient temperature,
so it may be appropriate to use more than one criterion to
signal a potentially catastrophic or ‘undesirable state’.
4. Proposed
criteria
A computer
analysis may provide clues about the levels of degradation
of material properties experienced by various components of
the structure. Coupling this with recently developed knowledge
of structural responses that have the greatest bearing upon
precipitating a collapse, it is possible to identify some
of the most critical signs of distress:
-
The
first criterion can be based upon the fact that deflections
caused by non-thermal effects (leading to mechanical strains)
are the ones that cause damage to the structure. So if
the magnitude of the deflections is predominantly (say
over 90%) accounted for by considering only the thermal
strains (thermal expansion and thermal curvature) imposed
upon the structure (taking into consideration the conditions
of compatibility and boundary restraints etc.) then it
can be deemed to be "safe". This can be further refined
to include the deflection caused by reduction in stiffness
(modulus) at higher temperatures.
By contrast,
if a significant portion of the deflection (say over 10%)
consists of non-recoverable strains (non-thermal and non-elastic),
then the structure may be deemed to have reached the "undesirable
state of irrecoverable deflection".
-
The
tensile membrane capacity of the slab is terminated by
rupture of the reinforcement, which in turn depends on
the mechanical strain demand placed on the reinforcement.
Thus the mechanical strain (not total strain) in the composite
deck slab reinforcement is an important indicator of potential
failure at large deflections. This criterion is especially
important when cold-formed meshes are used, because the
steel may have a low strain capacity before rupture. Therefore
if the tensile mechanical strains (after excluding the
thermal strains) in the concrete slab reinforcement exceed
a specified maximum value an "undesirable state of slab
tensile mechanical strain" may be deemed to exist.
-
A third
criterion that may be considered important is the horizontal
displacement of exterior columns, caused by thermal expansion
of internal structural members or the floor system. This
may be seen as an undesirable due to unacceptably high
additional eccentricities of load may occur in columns
in the lower storeys. Therefore a limit may be required
on the outward displacement of exterior columns. When
this limit is exceeded the "undesirable state of exterior
column displacement" may deemed to have been reached.
-
Finally,
large deflections in beams at or near the compartment
boundaries may lead to partition damage, leading to a
breach of the compartmentation. Therefore, should the
deflections of beams at the compartment boundaries exceed
a specified value, the "undesirable state of compartment
breach" may deemed to have been reached.
The above
criteria must be developed in a quantitative manner, but the
amount of information on which to determine limits for each
is currently rather small. The following provide some suggestions
for quantitative failure indicators:
-
Over
20% of the total deflection of a member derives from irrecoverable
(or plastic) strains along its length (therefore excluding
high local strains through rotation at supports) (???)
-
The
rate of deflection increase at the point of highest deflection
is greater than that explained by the rate of compartment
temperature increase and creep effects (???)
-
The
tensile strain in the mesh reinforcement is over 50% of
the rupture strain at the point of largest deflection
(???)
-
The
tensile strain in the mesh reinforcement is over 75% of
the rupture strain at the points of support (???)
-
Exterior
column displacements are under 30 mm at any storey (???)
(Top) |
Comments
on the above by Kees Both (TNO)
In the
article I miss the description of the origin of fire failure
criteria and the actual description of them. To understand
the current fire failure criteria one must realise how traditionally
fire tests were performed. The tradition is that tests are
performed on components, which in Europe are un-restrained
(i.e. no restraint against thermal expansion or thermal curvatures).
Even statically indeterminate composite structures mostly
show typical run-away failure (i.e. if bending is the failure
mode, and not e.g. shear). The statement you make that deflections
in those cases correspond to high mechanical strains is in
fact the most important one. Obviously mechanical strains
(actual level) and mechanical strain rates are in fact the
pure failure indicators in bending. The development of thermal
strains due to (partial restraint to) thermal elongation "mystifies"
the engineers feeling that large deflections must always correspond
to high unfavourable mechanical strains.
Two other
remarks concern the strains in the reinforcement meshes. It
is in fact not only the effect of cold-worked reinforcement
which may cause rapid increase of strains (due to its different
stress-strain relationship), but also the reinforcement ratio.
Low ratios cause (earlier and more) localisation of deformations
and strains and therefore "undesirable" states may be reached
sooner than expected. Furthermore, the (mechanical) tensile
strain in the mesh should also and to my opinion more importantly
by checked in regions were the composite slab is in hogging
(this need not be the region with largest deflections). This
because the (statically indeterminate fire exposed) composite
steel-concrete slab will reach hogging plastic moment capacity
sooner than sagging (and thus solicitates hogging moment capacity
sooner and longer; for which also the steel decking does not
play any role as opposed to sagging were the steel decking
in realistic fires significantly contributes to the load bearing
capacity).
(Top) |
Roger
Plank (1)
The following
notes set out my personal thoughts in relation to how ‘failure’
may be defined. In doing this I have tried to view the problem
from the standpoint of establishing criteria which may be
used in computer modelling of the structural behaviour. I
have not addressed in detail issues such as integrity (which
is a separate performance requirement).
Arbitrary
deflection limits alone are not appropriate (except for
tests where furnace etc. must be protected)
Rate
of increase of deflection could be used as a measure -
e.g. when deflection rate = 10 x average rate of increase
between 20° C and q ’ - where q ’ is the temperature at which
the deflection is equal to span/30, say?
However
this may not adequately allow for ‘localised’ failure
- i.e. rapid deflections in one member which ‘fails’ but is
subsequently supported by alternative actions, OR an
initially lightly loaded element which subsequently attracts
load from a ‘failing’ member.
The
total deflection history could examined retrospectively,
but this is a lot of work, and more importantly is subjective.
There is
no evidence that horizontal deformations of columns are critical.
Structural failure in this context is not concerned with limiting
behaviour to prevent irreversible changes (although insurers
may wish to do so).
At
ambient temperature, collapse of steel structures (in the
absence of buckling) is equivalent to the formation of a mechanism.
The same conditions can be considered for steel structures
in fire (for design) – using a modified plastic analysis.
This is essentially the moment capacity method when applied
to isolated beams. However it is not directly applicable to
the analysis of complete structures - unless collapse mechanisms
can be defined. Most computer simulations represent stress-strain-temperature
functions in such a way that complete ‘plastic hinges’ do
not develop, and more importantly the interaction between
slab and frame invalidates a simple definition of the ‘plastic’
collapse mechanism.
Yield
line analysis of the whole floor slab (ignoring the frame),
and collapse analysis of the frame (ignoring the membrane
action of slab) could be performed independently, and collapse
be conservatively based on whichever gave the higher failure
temperature.
A more
sophisticated approach is to consider the combined behaviour
of slab and frame.
It
may be possible to establish limits on the behaviour of beam
and slab cross-sections and substitute real hinges/yield lines
when these limits are reached - at present most material properties
allow infinite deformation. However there remains the problem
of defining limits – for example over what length should ‘failure
strain’ be considered? Such an approach is suitable for elastic
behaviour (where the yield point or some proof limit can be
used), but how applicable is it when considering plastic behaviour
and rupture?
I am conscious
that in outlining these thoughts I have posed more questions
than suggested answers, but hopefully they will provoke some
thought and discussion.
(Top) |
Roger
Plank (2)
Behaviour of Whole
Structures
Background
Traditional
approaches to the design and analysis of structures in fire
are based on the behaviour of isolated elements – beams, slabs
and columns with idealised support conditions. This is convenient
for 'proof testing' and is consistent with the approaches
traditionally used for normal design at ambient temperature.
However, when exposed to fire, whole structures can behave
quite differently from the way individual members might respond
to the same conditions. This may be for a number of reasons,
but especially
-
structural
'continuity' (through connections considered as nominally
'simply supported' or 'pinned')
-
'free'
thermal expansion which can cause deformations and additional
(second order) stresses
-
restraint
to free expansion, which can lead to induced forces (axial
and bending)
The effects
of continuity are generally beneficial, whilst those of expansion
(free and restrained) are generally detrimental. They can
be very significant and it may be necessary to consider whole
building behaviour in relation to not only structural performance
but also the integrity of other building components (eg non
loadbearing walls).
Steel
framed structures
In steel
framed buildings the principal sources of continuity are the
connections, and, in the case of composite buildings, the
interaction between the slab and frame. For non-composite
buildings and in-situ concrete floors, the slab may still
provide some significant continuity which may be beneficial,
but this has not been adequately studied.
Evidence
supporting the difference between complete steel-framed buildings
and individual steel members comes from:
- Tests: Cardington,
King William St, Melbourne
- Analysis: Cardington,
parametric studies
- Case history of real
fires: Broadgate
The potential
influence of the connections is to reduce the effects of fire
on beams (reduced deflections and bending stresses), extending
survival times.
Connections
In steel
framed structures the connections between beams and columns
will almost always provide some continuity. The effect of
connection rigidity is to induce bending moments at the beam
ends, relieving those at midspan, and also reducing vertical
deflections. A significant research effort has been devoted
to establishing the moment-rotation characteristics of different
connections, and methods have been developed allowing designers
to account for the ‘semi-rigidity’ of the connections. However
these are not widely used, and it is usual for ambient temperature
design to be based on the assumption of simply supported beams.
In fire
conditions the connections may have a greater influence than
at ambient temperature because
- larger rotations,
associated with larger deflections, can develop
- the connections
generally remain somewhat cooler than the midspan of the
beam, so strength and stiffness degrade more slowly.
Unfortunately
there is little data available concerning the rotational stiffness
of connections in fire, represented by moment-rotation-temperature
relationships, but simplified calculation methods have been
proposed ( ).
The effect
of connection rigidity and strength on the performance of
frames in fire has been demonstrated by experiment (Dave Latham),
but this provided insufficient data to establish general conclusions.
However, parametric analysis has shown that, even with only
modest rotational stiffness, the beam behaviour is closer
to that of a fixed ended beams. (SCI design approach?)
In composite
construction the continuity of the slab at column supports
increases the rigidity of the connection, although cracking
of the concrete can make this unreliable.
In practice,
the continuity of the slab is a much greater influence than
connection rigidity for such structures, and the difference
between the behaviour of the frame assuming rigid joints is
very similar to the case of pinned joints.
Whilst
the connection rigidity reduces bending in the beam at mid-span,
the effect on the supporting columns can be to induce additional
bending, which could be detrimental to its performance. However,
analysis has shown that this is not significant.
Slab
continuity
In composite
construction the slab is generally continuous over the supports
even if it is normally designed as a series of isolated spans.
Evidence of real fires, tests and analysis (refs) indicates
that, as the steelwork softens and deforms, so the influence
of the slab increases. This reduces the beam deflections compared
with the equivalent bare steel skeleton, and can increase
survival temperatures and times significantly.
The precise
mechanisms are not fully understood at present, but appear
to involve tensile membrane action of the slab at large deflections.
The implications of this have yet to be fully explored but
a simplified design guide has been prepared (Cardington Design
Guide). Research is continuing to establish how much further
advantage can be taken of this, and what must be done to the
supporting structure to enable the membrane action to develop.
The principles
are not necessarily applicable to slab forms other than conventional
composite decking. Floor systems such as precast planks clearly
do not provide significant continuity and would be unable
to generate tensile membrane action. Even systems like Slimdek
may have insufficient continuity to mobilise the structural
actions evident with composite decks, and traditional solid
slabs acting compositely with the steel frame may spall, exposing
reinforcement and weakening the membrane action.
Compartmentation
Although
not strictly a structural performance requirement, it is an
important design criterion that any fire is contained within
its compartment of origin. This means that the enclosure,
including the ‘roof’, of a compartment does not allow the
transmission of flames. In this context two issues may be
important:
- the integrity of
severely deflected slabs
- the deflection
of the compartment ‘roof’ and its effect on (non-loadbearing)
compartment walls below.
The evidence
of experiments and real fires in buildings is that composite
deck floors generally maintain sufficient integrity, although
some large cracks were evident in some of the full scale tests
at Cardington. However, spalling of slabs with an exposed
concrete soffit may compromise their performance. This is
an issue even in conventional approaches to fire protection.
The effect
of a severely deflecting slab on compartment walls below should
be considered by the designer to ensure that lateral spread
of fire is contained. Two approaches are possible:
-
design
the compartment walls to carry the loads transferred by
the slab;
-
detail
the slab-wall junction to allow for the expected movement
(which can be considerable) without transfer of load or
breach of the compartment boundary.
Reinforced
concrete structures
RC structures
are rarely analysed for fire conditions, but continuity in
complete buildings is similar to steel frames. Thus the sources
of continuity are the connections, and the interaction between
slabs ands frame.
Connections
In a reinforced
concrete frame, the connections are generally close to rigid
This is often accounted for in ambient temperature design
so there is potentially less benefit in fire. Experience of
steel structures would suggest that joints should be treated
as rigid, unless detailed deliberately to minimise moment
transfer.
Slabs
For in
situ construction it is likely that the slab continuity will
demonstrate the same characteristics as for steel framed construction,
improving survival times. However, it is possible that cracking
of the concrete may prevent the large deflections associated
with tensile membrane action from developing, and spalling
may expose reinforcement, reducing membrane strength. At present
there is no data available for this.
Compartmentation
The issues
of maintaining the integrity of the compartment boundary are
the same as for steel framed structures. However, it is more
likely that the slab soffit will be bare concrete, increasing
the threat from spalled concrete. However, the mass of material
associated with reinforced concrete construction generally
results in a much slower rate of temperature increase of the
structure. This reduces deflections, and thus lessens the
risk of large deflections damaging walls below.
Masonry
structures
Very little
information is available in relation to the performance of
masonry structures in fire. In multi-storey buildings, masonry
is typically used as a non-loadbearing cladding material,
supported by the main frame. In order to avoid collapse of
the masonry it is necessary to limit both horizontal and vertical
deflections. Some guidance is given in ref () which is largely
derived from the tests undertaken on the steel framed building
at Cardington. These generally indicated that the floor plate
effectively restrained outward expansion of the frame. The
maximum movement observed was ???, which recovered to ???
after cooling. There was no apparent damage to the external
masonry wall, which comprised continuous, full height blockwork
on the end elevations, and a ??? high parapet wall (with windows
over) on the sides.
In addition
to the (minor) effects of the expanding steelwork, masonry
heated on one side is subject to thermal bowing. At Cardington,
where the maximum temperature difference across the wall was
about ??? the horizontal deflection at mid-storey reached
about ???, but this returned to almost zero on cooling.
(Top) |
On
4 October Tony O'Meagher wrote ...
There are
many failure conditions, but one of the key ones for composite
floors in fire would appear to be local structural failure
of a slab, which also happens to be breach of compartmentation
- perhaps the more important condition as far as fire safety
is concerned.
Slab failure
would not result in more significant structural collapse unless
it completely separated an area of the floor from the cores
that are providing lateral stability. Then more significant
structural collapse would only occur if the column framing
were unable to provide stability to the separated area of
the floor.
w.r.t.
a further test at Cardington: Verifying the mode of failure
of a slab panel certainly has merit in terms of providing
confidence in the Level 1 Design Guidance and any extension
of it; also it would assist the development of the more detailed
computer based analysis methods. The edge beams would need
to be protected (as required by the Level 1 Guidance) and
the fire compartment would extend over at least a couple of
bays so that the assumptions on panels acting in isolation
could be confirmed (i.e. slab acts as if it was not continuous
after initial heating) and also so that it could be confirmed
that there is satisfactory performance at the edges of the
panels (i.e. no loss of compartmentation etc.). In terms of
loading - increased applied load and/or increased fuel load
would probably bring about the failure condition. Protecting
the edge beams on the panels means that the test would not
endanger the overall stability of the Cardington frame.
w.r.t.
the comments regarding floor deformations disrupting evacuation
and safe refuges: Designs that call for phased evacuation
almost always evacuate the fire floor and one or two floors
above on first alarm or shortly thereafter. This evacuation
would occur long before any significant deformation of the
floor immediately above the fire occurs. Refuges for disabled
etc. are typically within core areas and hence would not be
directly exposed to fire from below. As far as brigade intervention
is concerned the overall stability of the frame needs to be
maintained, but they have always had to contend with local
failures in slabs and/or significant local deformations.
(Top) |
On
5 October Mick
Green wrote ...
Continuing
the debate ...
I still
think it is worth considering controlling deflection for a
variety of building scenarios. It is true that means of escape
takes place very early on compared to when structural deflections
begin for a large majority of buildings. However the following
conditions should be considered further.
Disabled
people don't like the current solution of refuges in cores
(it is not an inclusive solution so it doesn't go down very
well) and there are moves being made to create alternatives
either in adjacent compartments, in suitably designed corridor
areas etc.
What is
said about phased evacuation is true but there is the
case of progressive evacuation into an adjacent compartment.
The objective is to create more time but equally there may
be no requirement to evacuate the second compartment if the
compartmentation performs to an adequate standard
If a
floor is truly a compartment floor the performance requirement
depends on how important it is to maintain the operation of
the upper compartment in the event of a fire in the compartment
below. Reasons could be to address item 2 or for business
continuity.
In
cases where some of the floor beams are protected then
we need to know that the fire protection will perform at large
deflections. At the moment this is limited by the capability
of the current test rigs. Therefore the assumption at the
moment must be that we have to use the current maximum deflection
limits until we know that the fire protection will still perform
when the deflections are higher
In
high rise buildings it can take along time to complete
the vertical evacuation and a badly affected floor may have
deflected significantly during this time. As we know cores
are not always on the edge of a building and there is a need
to traverse a series of floor slabs to get to the final exit
Major deflections in this scenario would not be very good.
Similarly search and rescue can take place at an advanced
time in large buildings so some consideration needs to be
given. We may decide there is no problem particularly if sprinklers
are provided to control this serviceability condition.
I think
the main point is that as we go away from traditional prescriptive
solutions to performance-based designs then we have to give
greater depth of consideration to a whole range of potential
failure scenarios. There will no doubt be some simple things
that we can recommend once we have examined the non-standard
conditions and become more confident by carrying out this
wider debate.
If we keep
this up we should have a good paper by the next meeting ...
(Top) |
August
2001
Prior to the 13 September
2001 meeting further contributions were received ...
E-mails from :
|
| On
16 August 2001 Barbara
Lane wrote ...
From a structural engineering
point of view failure did not occur at Cardington. In terms
of the standard fire resistance test is did as there were
breaches in the slab. In terms of the life safety requirements
of the Building regulations, failure did occur, only because
BS 476 recommendations were not met.
Question is does it
matter? Do we need to push frames to a total failure, what
ever that is, in order to truly define fire resistance/real
fire behavior?
The Cardington tests,
amongst other real fires, have shown us current fire resistance
requirements are protecting structures well in fire. But we
still cannot quantify by how much.
Current models, as a
result of Cardington, address global behavior only, but there
may be a local failure in a compartment wall/floor and therefore
in terms of current requirements, failure has occurred.
Can we predict such
local effects now? Will failure tests help this to be achieved
to a more accurate degree? Or are these failure tests to be
more of a "global" nature?
I am worried about this
new "failure" theme and how it relates to how people design
now. But more importantly how it relates to fire resistance
tests and application of such data.
If this failure work
is carried out and failure turns out to be say 10 hours longer
than the furnace test what does that mean? What happens if
it¹s just after current predictions? How will all this be
translated into the way things are protected now?
Local failure of slabs
means the main ingredient of fire resistance has failed. And
whether we like it or not every single product on the market
is tested using a fire resistance test, and it is not something
we can delete over night. So how do we progress from here
and how can failure tests help us achieve this?
How useful is overall
failure prediction in terms of life safety and/or property
protection?
Can we not use something
like probability of occurrence factors and more importantly
consequence of failure factors to address overall concerns
on the gap between current ratings and total failure.
At Cardington windows
had to be forcibly broken to get a flashover in the first
place. In other words what can be done to make "failure" happen
quadruple the fire duration? And if this works and causes
a global failure of the frame, what have we achieved?
Finally if we do have
a local failure of a single compartment e.g. beam/column collapse,
gap in slab, and structurally it does not affect adjacent
structure, is this failure?
As a fire engineer I
have to say if the people get out and the fire brigade can
do their job safely, no failure has occurred. As a structural
engineer is this relevant?
(Top) |
Reply
by Ian Burgess
Personally I'm reasonably
relaxed about this subject, because I think we sometimes get
obsessed with semantics, and the word "f*****e" is not doing
us any favours.
I think we should see
ourselves as moving towards a situation where:
The performance of
a building (not just structurally but functionally) should
stay within acceptable limits under a range of conditions,
and that these limits should be set largely on the basis
of the severity of the perceived outcomes - as indeed they
generally are. In fire these limits may include (perm any
number as appropriate from a much longer list):
- All the life safety
& escape issues ...
- Environmental
risks outside the building
- Insulation
- Integrity
- Resistance to collapse
- Damage to specialised
contents
- Repairability after
local or widespread events
- Safety and efficiency
of firefighting
A true limit state
philosophy should be applied, so that partial safety factors
are applied to the loadings and fire conditions (fire load
etc..) on the basis of the occurrence statistics and the
uncertainty of prediction.
These should be combined
with a "natural fire" prediction so that we can get rid
of most of the witchcraft (the ISO834 Standard Fire, time-equivalence,
fire resistance times ...) that currently muddies the waters.
Structurally the main
reason for continuing to do research is that we still don't
have good simplified guidance to give engineers about local
loss of integrity. On collapse things are getting a little
better, but this isn't a major problem in reality.
(Top)
|
Paper
tabled by Brian
Kirby in September 2001
Mechanisms
of Fire Spread
Conduction
The solid boundaries
of a fire enclosure will have one surface exposed to fire
conditions whilst the other non-exposed surface will face
into the adjacent enclosure/space. An excessive flow of heat
from the exposed to the non-exposed surfaces of the boundary
elements may lead to transmission of fire to adjacent spaces.
Traditionally, fire spread by this mechanism has been referred
to as "insulation" failure of the enclosure. Heat may be transmitted
from the enclosure by way of direct conduction to the non-exposed
side of boundary elements or by indirect conduction through
building components which are continuous to outside the enclosure,
eg pipes, ducts, beams, columns. Whether the heat conducted
to the non-exposed surface causes transmission of fire will
depend on the effect such heat may have on adjacent spaces.
The heat conducted to the non-exposed surface from the fire
enclosure may precipitate fire spread as follows;
- Ignition of the non-exposed
surface
- Conduction of heat
from non-exposed surface to combustibles with which it has
direct contact
- Convection of heat
from non-exposed surface to adjacent combustibles
- Radiation of heat
from non-exposed surface to adjacent combustibles
It is possible to inhibit
this fire spread mechanism through prevention of the above
scenarios. However, the conductive heating of the non-exposed
surface might need to be considered separately in terms of
its potential effect on building occupants.
Convection
The excessive flow of
hot gases or flames through openings in the enclosure may
cause ignition of combustible items in adjacent spaces. The
flow of hot gases from the enclosure may be by way of the
fixed openings from the enclosure or openings which have occurred
as a result of fire. Traditionally, fire spread by this mechanism
is termed integrity failure of the enclosure. In addition
collapse of the boundary element, eg due to its failure to
remain sufficiently load-bearing under fire conditions, may
also permit transmission of fire through excessive convection.
Heat flow through openings is one of the most difficult parameters
to quantify, particularly in the stage between initial integrity
failure and total collapse.
Radiation
The transmission of
heat from openings in the enclosure may cause ignition of
adjacent combustible items. Heat may be radiated from fixed
openings (e.g. doors, windows) or openings which have occurred
as a result of fire.
Mass transfer
It is possible that
burning fuel items within the fire enclosure may be transferred
from the enclosure through fixed or fire created openings.
Examples include the projection of flying brands and the flowing
of liquid pool fires under doors having no bund protection.
Direct pyrolysis
and reaction to fire
Where boundary elements
are combustible and continuous outside the fire enclosure,
it is possible that pyrolysis may extend beyond the enclosure.
Examples include lateral fire spread within the thickness
of combustible walls or roofs. Successful fire stopping of
such pyrolysis routes will be influenced by the reaction to
fire characteristics of the materials present as well as the
mechanical stability of the overall system. For example, continuous
members extending beyond the enclosure of fire origin may
permit fire spread by pyrolysis via some continuous combustible
component. Fire stopping may be impaired by local collapse
or deformation of the non-combustible part of the system.
The collapse of enclosure boundaries may also permit fire
to spread by direct pyrolysis.
Download
presentation slides
Download
illustrations of failure mechanisms and flowchart from BS7974
PD3
(Top) |
Paper
tabled by Ulf Wickström
in January 2004
Comments
on calculation of temperature in fire exposed bare steel structures
in prEN 1993-1-2
Eurocode 3 – Design of steel structures
– Part 1-2: General rules – Structural fire design
The Final Draft of
prEN 1993-1-2, December 2003 for calculation of the fire resistance
of fire exposed steel structures is out for Final Vote (Januari
2004). I have some specific comments which I would like to
draw your attention to. It relates to a procedure which has
been modified in comparison to the corresponding ENV on how
to calculate temperature in fire exposed bare (uninsulated)
steel sections. This procedure or formula is from a commercially
as well as from a safety point of view a very important, the
single most important in the above standard, as it is in many
cases decisive whether a steel structure need to be fire insulated
or not.
The formula for calculating
temperature in bare steel structures is given in Chapter 4.2.5
in the above standard. It is a simple and well established
formula as written in the ENV version of the standard,. However,
in the new standard the formula has been changed in two ways.
First the theoretical concept of “shadow effects” has been
introduced without any references or proofs of test results,
and secondly an unnamed factor of 0.9 has been introduced
which has no physical explanation what so ever.
In comparison with the
preliminary ENV standard this means that if all other parameters
remain the same, the required steel section factor may be
increased by up to 40% and still calculated steel temperatures
would be the same. The higher value refers to common open
I-sections. (An increase of the section factor corresponds
to proportionally the same decrease in the steel thickness.)
Thus the formula in the new standard yields a considerably
lower safety level for bare steel structures.
As the calculation procedure
most likely predicts considerably lower temperature and thereby
longer fire resistance times than standard furnace tests,
the classification system of these type of structures becomes
evidently inconsistent.
The favourable heat
transfer theory mentioned above is only introduced in Eurocode
3. If correct, it should of course have been introduced in
Eurocode 1 so that it could have been available for other
construction materials as well.
In
summary:
In the new draft Eurocode
3 standard for calculating fire resistance of steel structures
a very favourable heat transfer formula has been introduced
for bare steel sections. Thus
- A new concept ‘shadow
effects’ has been introduced which yields considerably lower
calculated steel temperatures. The introduced formula is
not tried out and verified in practical tests.
- In addition a new
unnamed and unexplained factor equal 0.9 has been introduced
which further reduces calculated steel temperatures. 06
January 2004
- Required steel thicknesses
based on calculations may be reduced by up to 40 % for open
steel sections.
- The formula yields
lower theoretical steel temperatures than would be obtained
in standard fire tests and thereby longer fire resistance
times.
- The formula is exclusive
to steel structures.
(Top) |
Reply
by Jean-Marc Franssen
Liège, le 20 janvier
2004
This document is a tentative
answer to the document "Comments on calculation of temperature
in fire exposed bare steel structures in prEN 1993-1-2" dated
06 January 2004 made by Ulf Wickström and contained in the
file "UWickstrom_2004.pdf".
Although the author
of this answer was one of the member of the draft team of
prEN 1993-1-2, this answer by no means represent the opinion
of the draft team; it is the sole opinion of the author at
the time.
What we think U. Wickström
failed to notice is that the boundary conditions for bare
steel sections have changed in the prEN's compared to the
preliminary ENV's. The emissivity, either called relative
emissivity or surface emissivity, has been changed
- from 0.50, see 4.2.5.1
(2) in ENV,
- to 0.70, see 2.2
(2) in prEN.
The energy introduced
in a bare steel section is proportional to :

with ksh = 1,0
in the ENV
For an I-section heated
of 4 sides, the radiative part of the energy, which is dominant
compared to the convective part, is thus proportional to
for the ENV
for the prEN
The following table
gives the value of this factor, noted k in the table, for
several I-sections of different sizes and shapes. This table
shows that the difference in term of radiative flux is by
far smaller than 40% and, also, that the modification is not
a systematic decrease. The change from ENV to prEN, for the
considered sections, is from -7% to +12%. If one considers
that the modification in calculated temperature is by an order
of magnitude smaller than the modification in the flux (because
the re-emitted flux depends on the temperature of the section
and this dampens the effect), it may be seen that the difference
will finally be marginal. Hence, because we agree with U.
Wickström that the formula was "… simple and well established
… in the ENV version…", we may assume that the safety level
is still appropriate in the prEN version.
This example is only
one case in the domain of temperature calculations when simple,
well established, engineering solutions that had proved to
work for years in the ENV versions have had to be modified,
usually in the sense of complexity, in order to finally reach
very similar results. In this case, it has been argued that
the emissivity of steel cannot physically be equal to 0.50
as was supposed in the ENV, and another equally "physical
" factor has had to be taken into account in order not to
change the final results, namely the fact that the amount
of radiative energy that crosses the box contour of a section
cannot be increased when it reaches the perimeter contour
of the section.
We have had personally
the opportunity to give our opinion on other similar cases
for other materials where we also disagreed with the draft
team but believe that, at that stage, i.e. so close to the
final vote, it is better to stick to the agreement/solution/compromise
that has been found on that matter.
Evaluation of the
radiative flux on unprotected steel sections This flux
is proportional to the factor k calculated hereafter:
|
|
ENV
|
EN
|
EN/ENV
|
|
[Am/V] |
k |
[Am/V]b |
k |
| IPE
A 80 |
389
|
195
|
317
|
200
|
1.03
|
| IPE
80 |
330 |
165 |
270 |
170 |
1.03 |
| IPE
A 300 |
192 |
96 |
160 |
101 |
1.05 |
| IPE
300 |
167
|
84
|
139 |
88
|
1.05
|
| IPE
O 300 |
145
|
73
|
121 |
76
|
1.05
|
| IPE
A 600 |
119
|
60
|
103
|
65
|
1.09
|
| IPE
600 |
105
|
53
|
91
|
57
|
1.09
|
| IPE
O 600 |
85
|
43
|
73
|
46
|
1.08
|
| IPN
80 |
322
|
161
|
266
|
168
|
1.04
|
| IPN
300 |
123 |
62
|
105
|
66
|
1.08
|
| IPN
550 |
71 |
36
|
61
|
38
|
1.08
|
| HE
100 AA |
245
|
123
|
181
|
114
|
0.93
|
| HE
100 A |
185
|
93 |
137
|
86
|
0.93
|
| HE
100 B |
154
|
77 |
115
|
72
|
0.94
|
| HE
100 M |
85
|
43
|
65
|
41
|
0.96
|
| HE
300 AA |
131
|
66
|
97
|
61
|
0.93
|
| HE
300 AA |
104
|
52
|
78
|
49
|
0.95
|
| HE
300 B |
80
|
40
|
60
|
38
|
0.95
|
| HE
300 M |
43
|
22
|
33
|
21
|
0.97
|
| HE
600 AA |
106
|
53
|
88
|
55
|
1.05
|
| HE
600 A |
79
|
40
|
65
|
41
|
1.04
|
| HE
600 B |
67
|
34
|
56
|
35
|
1.05
|
| HE
600 M |
51
|
26
|
42
|
26
|
1.04
|
| HE
1000 AA |
90
|
45
|
70
|
44
|
0.98
|
| HE
1000 A |
74
|
37
|
66
|
42
|
1.12
|
| HE
1000 B |
65 |
33 |
58 |
37 |
1.12 |
(Top) |
|