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Fire tests on protected steel columns with different cross-sections

Stanzak, W. W.; Lie, T. T.

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NATIONAL RESEARCH COUNCIL O F CANADA DIVISION O F BUILDING RESEARCH

F I R E TESTS ON P R O T E C T E D S T E E L COLUMNS WITH D I F F E R E N T (;ROSS -SECTIONS

by W. W. STANZAK and T. T. L I E F i r e Study No. 30 of the Division of Building R e s e a r c h OTTAWA F e b r u a r y 1973

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FIRE TESTS ON PROTECTED STEEL COLUMNS WITH DIFFERENT CROSS -SECTIONS

by

W. W. STANZAK* and T. T. LIE**

SUMMARY

Seven f i r e t e s t s were conducted to provide experimental data showing how column f i r e endurance varies with the size and shape of the s t e e l cross-section. All columns were protected with the s a m e thickness of insulating material. The results a r e plotted to show how generalized f i r e endurance ratings can be developed f o r a particular protective material.

*,

**

Steel Industries Fellow and Research Officer, respectively, F i r e Research Section, Division of Building Research, National Research Council of Canada.

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FIRE TESTS ON PROTECTED S T E E L COLUMNS WITH DIFFERENT CROSS -SECTIONS

by

W. W. STANZAK and T. T. LIE

Seven f i r e t e s t s on identically protected s t e e l columns w e r e conducted a s p a r t of an extensive column r e s e a r c h program at the Division of Building Research. The specimens w e r e designed t o i l l u s t r a t e how column f i r e resistance v a r i e s with the s i z e and shape (geometry) of the s t e e l cross-section. As the methods and m a t e r i a l s employed in the construction of the t e s t specimens a r e currently used in Canada, the r e s u l t s of this study a r e directly applicable in design.

PROTECTION

All specimens w e r e protected by one-inch thick vermiculite boards cemented together and t o the s t e e l with an adhesive m o r t a r . Vicuclad boards a r e produced from specially selected vermiculite which, after pre-treatment, i s bonded with an inorganic binder to

produce a non-combustible board. William ~ e n ~ b n and Sons (Vicuclad) Ltd.

,

Cheshire, England, have provided the following technical data concerning their product:

T h e r m a l conductivity: k = 0. 53 Btu in. /ft% deg F at 100 deg

F

mean

Standard size: 2 ft by 2 ft and 3 ft by 2 ft

Standard thickness:

Nominal density:

(inches) 3/4, 1, 1 1/4, 1 1/2, i, and 2 1/8

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Weight

p e r

s q ft: Vicuclad contains: V e r m i c u l i t e contains: 1 i n a t h i c k 2 1/4 lb; 1 1 / ~ in. t h i c k 3 1 / ~ lb; 2 1/8 in. t h i c k 4 3 / 4 lb; 1 1 / 4 in. t h i c k 3 lb; 2 in. t h i c k 4 1/2 1b 65 p e r c e n t V e r m i c u l i t e (* 5 p e r cent) 35 p e r cent Sodium S i l i c a t e

(f

5 p e r cent)

40 p e r cent S i l i c a 1 L p e r cent Alumina

5 p e r c e n t F e r r i c Oxide 17 p e r c e n t Magnesium Oxide

11 p e r c e n t F r e e and Combined W a t e r T h e Sodium S i l i c a t e h a s a SiO; Na,O r a t i o of 3. 3:l

T h e a d h e s i v e when d r y i s a 10:7 m i x t u r e of Sodium S i l i c a t e and V e r m i c u l i t e . T h e d e n s i t y of Vicuclad is 27 l b

(f

1 5 p e r cent) lb p e r cubic foot.

T h e c o m p r e s s i v e s t r e n g t h of Vicuclad i s 135 l b

(f

15 p e r c e n t ) l b p e r s q u a r e inch.

DESCRIPTION O F TEST SPECLMENS

T h e s t e e l c r o s s - s e c t i o n s u n d e r t e s t a r e specified i n T a b l e I. T h e y w e r e supplied with welded end p l a t e s and i n s u l a t e d , a s required('). Insulating m a t e r i a l w a s applied i n t h e f o r m of box e n c a s e m e n t on a l l t y p e s of s e c t i o n (hollow, wide flange and solid).

T h e wide flange c o l u m n s w e r e fitted with nogging p i e c e s of 1-in.

t h i c k Vicuclad, fixed between t h e f l a n g e s and t o t h e web with a d h e s i v e m o r t a r . T h e noggings w e r e s p a c e d a t 2-ft c e n t r e s on e a c h s i d e of t h e column. T h e Vicuclad p a n e l s w e r e fixed t o t h e o u t e r f a c e s of t h e f l a n g e s with t h e s a m e a d h e s i v e m o r t a r . T o c o m p l e t e t h e e n c a s e m e n t , additional p a n e l s w e r e fixed t o t h e noggings and t o t h e Vicuclad p a n e l s a l r e a d y in place. T h e d e t a i l s of t h e column e n c a s e m e n t a r e shown in F i g u r e s 1, 2 and 3.

T E S T PROCEDURE

T h e t e s t s w e r e c a r r i e d out i n a c c o r d a n c e with CSA B54. 3-64(11. T h e c o l u m n w a s t e s t e d v e r t i c a l l y in a g a s - f i r e d f u r n a c e . T h e f u r n a c e

t e m p e r a t u r e w a s m e a s u r e d by nine t h e r m o c o u p l e s positioned s y r n m e t r i c a l l y about t h e c o l u m n a s shown i n F i g u r e 4.

T h e t h e r m o c o u p l e s w e r e enclosed in 1 / ~ - i n . b l a c k i r o n pipe with a c a r b o n s t e e l c a p a t t h e tip. T h e hot junction of the t h e r m o c o u p l e s was p l a c e d

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t e m p e r a t u r e s at the nine points and the average of the nine thermocouples w e r e recorded during the t e s t .

The fuel input t o the furnace was controlled to make the average t e m p e r a t u r e follow a s closely a s possible the t e m p e r a t u r e v e r s u s t i m e

c u r v e p r e s c r i b e d by

CSA

B54. 3-64.

The t e m p e r a t u r e of the s t e e l columns was m e a s u r e d by t h e r m o - couples peened into the steel at five levels. The location of t h e s e t h e r m o - couples i s shown in F i g u r e s 5 and 6.

OBSERVATIONS

The cladding remained intact throughout the t e s t s without exception. Towards the end of the longer t e s t s ( 3 to 4 h r s ) c r a c k s developed in the

v e r t i c a l joints of the Vicuclad panels. The s t r u c t u r a l strength of the encasement was noticeably affected by the t e s t and in s e v e r a l instances pieces of the Vicuclad panels I'ell away from the column a s it was being removed f r o m the furnace.

F i g u r e s 7 and 8 show a column before and after the f i r e t e s t . The deterioration at t h e joints, evident in F i g u r e

9,

i s typical of the longer t e s t s . RESULTS

F i r e endurance t i m e s derived by the t e s t s a r e shown in Table I. T h e furnace t e m p e r a t u r e and the t e m p e r a t u r e of the l e v e l at which f a i l u r e o c c u r r e d a r e plotted against t i m e in F i g u r e s 1 0 t o 16.

It

was d e s i r a b l e to generalize t h i s f i r e t e s t data t o develop what might be called "universal f i r e r e s i s t a n c e ratings" for columns of any geometry with protective m a t e r i a l of various thicknesses. This i s now possible by utilizing knowledge a l r e a d y gained f r o m the DBR/NRC column

r e s e a r c h p r o g r a m .

The authors found that f o r relatively s t a b l e low density m a t e r i a l s the f i r e endurance t i m e of any rotected s t e e l column can be calculated by

R,

the s e m i - e m p i r i c a l expression

.

where: T = calculated f i r e endurance time, h r C

W = weight of s t e e l section p e r unit length, lb/ft

D = heated p e r i m e t e r , in. (development of inside s u r f a c e of protective m a t e r i a l )

A

=

thickness of protection, in.

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T h e 0. 5 t e r m r e p r e s e n t s a c o n s t a n t t h a t w a s found t o be a good a v e r a g e f o r popular ( c h e m i c a l l y s t a b l e ) f i r e p r o t e c t i v e m a t e r i a l s and t h e t e r m W / D r e f l e c t s t h e g e o m e t r y of t h e p r o t e c t e d column and i s c a l l e d t h e " s i z e and

shape" f a c t o r . F i r e t e s t d a t a developed i n t h i s t e s t s e r i e s and one unpublished t e s t point f r o m another l a b o r a t o r y f o r a m a t e r i a l t h i c k n e s s of 1 1/2 i c . a r e shown in F i g u r e 17 and a r e c o m p a r e d with t h e f i r e r e s i s t a n c e s c a l c u l a t e d by Equation 1 (a). As i s s e e n , t h e calculated f i r e r e s i s t a n c e t i m e s a r e q u i t e c o n s e r v a t i v e .

A s s i x s e t s of f i r e t e s t d a t a a r e on hand h e r e , it i s p o s s i b l e t o develop

a b e t t e r f o r m of Equation 1 ( a ) by s u m m i n g t h e f i r e r e s i s t a n c e t i m e s and solving f o r a m o r e a p p r o p r i a t e value of t h e constant:

W

T = (LO

-

+

0. 68)

R

C D P

w h e r e t h e t e r m s h a v e t h e s a m e m e a n i n g a s before. F i g u r e 18 again shows t h e a v a i l a b l e f i r e t e s t d a t a a s well a s t h e f i r e r e s i s t a n c e s c a l c u i a t e d by Equation 1 (b), T h e a g r e e m e n t between t e s t d a t a and c a l c u l a t e d r e s u l t s

is good, and t h e c a l c u l a t e d v a l u e s a r e m o s t l y c o n s e r v a t i v e . Accordingly, Equation 1 (b) and t h e c o r r e s p o n d i n g l i n e s in F i g u r e 18, m a y b e talcen a s

" u n i v e r s a l f i r e r e s i s t a n c e r a t i n g s " f o r t h i s p r o t e c t i v e m a t e r i a l . 'l:

ACKNOWLEDGEMENT

T h i s w o r k w a s c a r r i e d out u n d e r a c o o p e r a t i v e p r o g r a m between DBR/NRC and t h e Canadian S t e e l I n d u s t r i e s C o n s t r u c t i o n Council, known a s t h e S t e e l I n d u s t r i e s F e l l o w s h i p A g r e e m e n t .

T h e a u t h o r s w i s h t o t h a n k M e s s r s . J. E. B e r n d t and E. 0. P o r t e o u s , who c a r r i e d out t h e f i r e t e s t s and a s s i s t e d i n a n a l y s i s of t h e d a t a developed. R E F E R E N C E

1. Methods of F i r e T e s t s of Walls, P a r t i t i o n s , F l o o r s , Roofs, C e i l i n g s , Columns, B e a m s and G i r d e r s . CSA S t a n d a r d B54. 3-1964, C a n a d i a n S t a n d a r d s A s s o c i a t i o n , Ottawa, Ontario, Canada.

2. Lie, T. T. and Stanzak, W. W. F i r e R e s i s t a n c e of P r o t e c t e d S t e e l Columns. ( In p r e p a r a t i o n )

>:< No f i r e r e s i s t a n c e exceeding 4 h r should be c a l c u l a t e d b y Equation 1 (b), a s t h i s w a s t h e m a x i m u m t i m e t h e m a t e r i a l w a s shown, by t e s t , t o r e m a i n r e l a t i v e l y i n t a c t .

(8)

TABLE I

F I R E RESISTANCE O F VARIOUS IDENTICALLY PROTECTED COLUMN SECTIONS

NO. Section W D W/D ~ ( m i n ) T (min) ~ ~ ( h r )

c E FRC 1 14W 136 59 2.30 143 153 2.55 2 2 10W 49 40 1.22 9 5 96 1. 60 1 1/2 3 l o x 6 HSS 36.8 32 1.15 9 2 9 8 1. 63 1 1/2 4 10x1 0 HSS 39.7 40 0.99 8 4 7 9 1. 32 1 5 12x12 HSS 57 48 1. 19 9 4 100 1. 67 1 1/2 6 12W 190 54 3.52 197 196 3. 27 3 7 lOxlOSOLID* 342 40 8.55 42 1

-

-

*

4+

D = heated p e r i m e t e r (in.), i. e. development of i n s i d e s u r f a c e of p r o t e c t i v e m a t e r i a l

W = weight of s t e e l s e c t i o n p e r unit height, lb/ft T = f i r e endurance t i m e calculated b y equation 1 (b)

C

T = e x p e r i m e n t a l f i r e endurance t i m e derived by t e s t E

FRC = F i r e R e s i s t a n c e Classification, h r

*

T h e f i r e t e s t on t h i s s p e c i m e n was t e r m i n a t e d a t 4 h r . F a i l u r e had not taken p l a c e by t h a t t i m e .

(9)

MOR

(10)

N E L S O F V I C U C L A D

M O R T A R

FIGURE 2

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1'

->.--

(12)

TOTAL OF 9 THERMOCOUPLES R A L TC SIDE 0

C

3 / 4 " B L A C K IRON PlPE UNINSULATED 3 " B L A C K IRON COLUMN

u

P l P E I N S U L A T E D FIGURE 4 L O C A T I O N OF FURNACE THERMOCOUPLES I N RELATION TO COLUMN I R 4 7 9 ~

-

z

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L E V E L 2 L E V E L 3 . - . L E V E L 4 L E V E L 5 F I G U R E 5 D I S T A N C E F R O M THE B O T T O M L E V E L 1

-

6 ' L E V E L 2

-

5

'

L E V E L 3

-

4 ' L E V E L 4

-

3 ' L E V E L 5 - 2 ' T H E R M O C O U P L E L O C A T I O N O F T H E R M O C O U P L E S O N W I D E - F L A N G E C O L U M N S . ma? 477u - 3

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LEVEL LEVEL LEVEL LEVEL LEVEL F I G U R E 6 D I S T A N C E F R O M THE B O T T O M LEVEL 1

-

6 ' LEVEL 2

-

5 ' LEVEL 3

-

4

'

LEVEL 4

-

3 ' LEVEL 5

-

2 ' T H E R M O C O U P L E L O C A T I O N O F T H E R M O C O U P L E S O N R E C T A N G U L A R C O L U M N S S R + 7 7 8 - Y

(15)
(16)

.

-

----

I

(17)
(18)

TIME, HOURS RESCRIBED FURNACE TEMPERATURE AVERAGE FURNACE TEMPERATURE

TIME OF FAILURE

AVERAGE TEMPERATURE LEVEL 4

(19)

PRESCRIBED FURNACE TEMPERATURE AVERAGE FURNACE TEMPERATURE

ERAGE TEMPERATURE LEVEL 4

TIME, MINUTES

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i 1 - 1 i I I

IY

-

-

PRESCRIBED FURNACE TEMPERATURE TIME OF FAILURE

-

AVERAGE FURNACE TEMPERATURE

-

-

-

-

AVERAGE TEMPERATURE LEVEL 4

-

L 1 I I 1 I t I I I 1

T I M E , M I N U T E S

FIGURE 1 2 C O L U M N TEST N O . 3 pr Y 7 7 8 -7 ( 1 0 x 6 HSS)

(21)

f 1 2 0 0 L

8

TIME OF FAILURE

TIME, MINUTES

FIGURE 13 COLUMN T E S T N O . 4 ( l o x 10 HSS)

(22)

-

-

-

PRESCRIBED FURNACE TEMPERATURE

TIME OF FAILURE

-

-

-

I

-

-

AVERAGE TEMPERATURE LEVEL 3

-

T I M E , M I N U T E S

F I G U R E 1 4 C O L U M N TEST N O . 5

(23)

-

-

-

AVERAGE FURNACE Tf MPERATURE TIME OF FAlLURE

-

-

1 2 3

TIME, HOURS

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1 I I 1 1 I I I I I I I I

-

-

PRESCRIBED FURNACE TEMPERATURE

HAVERAGE FURNACE TEMPERATURE -

-

-

-

-

AVERAGE TEMPERATURE LEVEL 4

-

1 1 1 1 1 I 1 I I I 1 I 1 I I I

1 2

T I M E , HOURS

FIGURE 16 C O L U M N TEST N O ( l o x 10 S O L I D )

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Ib/ft

"

S I Z E A N D SHAPE

"

F A C T O R W/D

-

in. F I G U R E 17 G E N E R A L I Z E D P L O T O F C O L U M N FIRE R E S I S T A N C E

,

f = 2 7 1b/ft3 B I S O 8 L

-

L

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Ib/ft " S I Z E A N D S H A P E " F A C T O R W/D,

-

I n . F I G U R E 18 G E N E R A L I Z E D P L O T OF FIRE R E S I S T A N C E F O R

"

V I C U C L A D

"

S

= 27 1b/ft3

Figure

FIGURE  1  DETAILS  OF  COLUMN  ENCASEMENT  r ~ 4 7 7 # - 1
Figure  8  -  Column  after  fire test
Figure  9  -  Close-up  of  joint  after  fire test
FIGURE  10  COLUMN  T E S T   N O .   1  ( 1 4 W )   P f l r 7 - r s - 5
+6

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